Patent Publication Number: US-8529662-B2

Title: Removal of heavy hydrocarbons from gas mixtures containing heavy hydrocarbons and methane

Description:
This application claims the benefit of U.S. Provisional Application No. 60/930,993 filed May 18, 2007. 
    
    
     FIELD OF THE INVENTION 
     The present invention relates to a process for the separation of one or more heavy hydrocarbon gases from a gas mixture containing said heavy hydrocarbon gas(s) and methane. The process is conducted in swing adsorption apparatus containing adsorbent contactor having a plurality of flow channels and wherein 20 volume percent or less of the open pore volume of the contactors, excluding the flow channels, is in the mesopore and macropore range. 
     BACKGROUND OF THE INVENTION 
     Gas separation is important in various industries and can typically be accomplished by flowing a mixture of gases over an adsorbent that preferentially adsorbs a more readily adsorbed component relative to a less readily adsorbed component of the mixture. One of the more important gas separation techniques is pressure swing adsorption (PSA). PSA processes rely on the fact that under pressure gases tend to be adsorbed within the pore structure of the microporous adsorbent materials or within the free volume of a polymeric material. The higher the pressure, the more gas is adsorbed. When the pressure is reduced, the gas is released, or desorbed. PSA processes can be used to separate gases in a mixture because different gases tend to fill the micropore or free volume of the adsorbent to different extents. If a gas mixture, such as natural gas, for example, is passed under pressure through a vessel containing polymeric or microporous adsorbent that fills with more nitrogen than it does methane, part or all of the nitrogen will stay in the sorbent bed, and the gas coming out of the vessel will be enriched in methane. When the bed reaches the end of its capacity to adsorb nitrogen, it can be regenerated by reducing the pressure, thereby releasing the adsorbed nitrogen. It is then ready for another cycle. 
     Another important gas separation technique is temperature swing adsorption (TSA). TSA processes also rely on the fact that under pressure gases tend to be adsorbed within the pore structure of the microporous adsorbent materials or within the free volume of a polymeric material. When the temperature of the adsorbent is increased, the gas is released, or desorbed. By cyclically swinging the temperature of adsorbent beds, TSA processes can be used to separate gases in a mixture when used with an adsorbent that selectively picks up one or more of the components in the gas mixture. 
     Adsorbents for PSA systems are usually very porous materials chosen because of their large surface area. Typical adsorbents are activated carbons, silica gels, aluminas and zeolites. In some cases a polymeric material can be used as the adsorbent material. Though the gas adsorbed on the interior surfaces of microporous materials may consist of a layer only one, or at most a few molecules thick, surface areas of several hundred square meters per gram enable the adsorption of a significant portion of the adsorbent&#39;s weight in gas. 
     Different molecules can have different affinities for adsorption into the pore structure or open volume of the adsorbent. This provides one mechanism for the adsorbent to discriminate between different gasses. In addition to their affinity for different gases, zeolites and some types of activated carbons, called carbon molecular sieves, may utilize their molecular sieve characteristics to exclude or slow the diffusion of some gas molecules into their structure. This provides a mechanism for selective adsorption based on the size of the molecules and usually restricts the ability of the larger molecules to be adsorbed. Either of these mechanisms can be employed to selectively fill the micropore structure of an adsorbent with one or more species from a multi-component gas mixture. The molecular species that selectively fill the micropores or open volume of the adsorbent are usually referred to as the “heavy” components and the molecular species that do not selectively fill the micropores or open volume of the adsorbent are usually referred to as the “light” components. 
     An early teaching of a PSA process having a multi-bed system is found in U.S. Pat. No. 3,430,418 wherein a system having at least four beds is described. This &#39;418 patent describes a cyclic PSA processing sequence that includes in each bed: (1) higher pressure adsorption with release of product effluent from the product end of the bed; (2) co-current depressurization to intermediate pressure with release of void space gas from the product end thereof; (3) countercurrent depressurization to a lower pressure; (4) purge; and (5) repressurization. The void space gas released during the co-current depressurization step is commonly employed for pressure equalization purposes and to provide purge gas to a bed at its lower desorption pressure. Another conventional PSA processes using three sorbent beds is disclosed in U.S. Pat. No. 3,738,087. Conventional PSA processes are typically able to recover only one of the key components (i.e., light or heavy) at high purity and are unable to make a complete separation and separate both components with a high recovery. The light component usually has a low recovery factor. Recovery of the light component usually drops even lower when the feed gas is introduced at higher pressures (i.e., pressures above 500 psig). 
     For the recovery of a purified strongly adsorbed “heavy” component, an additional step is usually necessary, namely, rinsing of the bed with a heavy component to displace the light component from the bed prior to depressurization. The rinsing step is well known in the art. The problems associated with these processes are the following: (a) if the rinsing is complete and the light component is completely displaced from the bed, substantially pure heavy component can be obtained, but the adsorption front of the heavy component breaks through to the light component and the latter cannot be recovered at high purity; (b) if the displacement of the light component is incomplete, the typical concentration profile of the heavy component in the bed is not optimum and as such the bed is depressurized countercurrently to recover the heavy key component at the feed end, the light component still present in the bed reaches the feed end very rapidly and the purity of the heavy component drops. Therefore it is not practical in the prior art to obtain both key components at high purity in a single PSA unit. 
     The faster the beds perform steps to complete a cycle, the smaller the beds can be when used to process a given hourly feed gas flow. Several other approaches to reducing cycle time in PSA processes have emerged which use rotary valve technologies as disclosed in U.S. Pat. Nos. 4,801,308; 4,816,121; 4,968,329; 5,082,473; 5,256,172; 6,051,050; 6,056,80; 6,063,161; 6,406,523; 6,629,525; 6,651,658 and 6,691,702. A parallel channel (or parallel passage) contactor with a structured adsorbent is used to allow for efficient mass transfer in these rapid cycle pressure swing adsorption processes. Approaches to constructing parallel passage contactors with structured adsorbents have been disclosed in US20060169142 A1, US20060048648 A1, WO2006074343 A2, WO2006017940 A1, WO2005070518 A1, and WO2005032694 A1. 
     In a parallel channel contactor, the adsorbent lines the wall of the flow channel which can be formed from the space between parallel plates or the open path through a duct or tube. When parallel plates are used to form the parallel channel, a spacer may be present in the space of the parallel channel. An example of a spacer-less parallel passage contactor as provided in US20040197596 A1 and an example of a parallel passage contactor with a high density adsorbent structure is given in US20050129952A1. In all cases, the adsorbent used to line the parallel channel contains both mesopores and macropores. 
     Mesopores and macropores are known in the art to improve the mass transfer characteristics of adsorbents used in either a parallel channel contactor or conventional packed bed contactors. Improvements in mass transfer characteristics from the presence of mesopores and macropores in conventional packed bed contactors have been widely discussed. See for example U.S. Pat. Nos. 6,436,171 and 6,284,021. Improvements in mass transfer characteristics from the presence of mesopores and macropores in parallel channel contactors are discussed in EP1413348 A1. As such, the prior art teaches that a large number of mesopores and macropores are needed in an adsorbent particle or layer of adsorbent in order to have mass transfer characteristics good enough to operate a pressure swing adsorption cycle. The inventors hereof have unexpected found that adequate mass transfer characteristics can be attained without a significant amount of mesopores and/or macropores providing easy access to the micropore structure in the adsorbent where selective separation occurs. 
     While there are various teachings in the art with respect to new adsorbent materials, new and improved parallel channel contactors, and improved rapid cycle PSA equipment, none of these to date present a viable solution to the problem of producing good recovery of the light component and purity when the feed gas is at very high-pressure. This is a critical issue since natural gas is often produced at high pressures (500-7000 psi) and methane acts as a light component in the adsorption process. Many gas fields also contain significant levels of H 2 O, H 2 S, CO 2 , N 2 , mercaptans and/or heavy hydrocarbons that have to be removed to various degrees before the gas can be transported to market. It is preferred that as much of the acid gases H 2 S and CO 2  be removed from natural gas as possible. In all natural gas separations, methane is a valuable component and acts as a light component in swing adsorption processes. Small increases in recovery of this light component can result in significant improvements in process economics and also serve to prevent unwanted resource loss. It is desirable to recover more than 80 vol. %, preferably more than 90 vol. % of the methane when detrimental impurities are removed. While various processes exist for removing CO 2 , H 2 S, and N 2  from natural gas there remains a need for processes and materials that will perform this recovery more efficiently, at lower costs, and at higher hydrocarbon yields, particularly at higher methane yields. 
     Similarly, for other gaseous feed streams, the prior art describes several ways to recover high amounts of the heavy components in a heavy component rich “reject” stream, but cannot achieve as high a recovery of the light components in the light component rich product stream. This difference in recoveries becomes greater as the feed pressure increases. 
     SUMMARY OF THE INVENTION 
     In accordance with the present invention there is provided a process for the removing heavy hydrocarbon components from a gas mixture containing both a heavy hydrocarbon components and methane, which process comprises: 
     a) conducting said gas mixture to a swing adsorption gas separation unit wherein the gas separation unit contains at least one adsorbent contactor comprising a gas inlet and a gas outlet, wherein the gas inlet and the gas outlet are in fluid connection by a plurality of open flow channels, wherein the surfaces of the open flow channels are comprised of an adsorbent material that has a selectivity for said heavy hydrocarbon components over said methane greater than 5, wherein the contactor has less than about 20% of its open pore volume in pores with diameters greater than about 20 angstroms and less than about 1 micron, and wherein at least a portion of said heavy hydrocarbon components is adsorbed into said adsorbent material, thereby resulting in a product stream depleted of said heavy hydrocarbon components; 
     b) collecting said the product stream; 
     c) desorbing the adsorbed gases from said adsorbent, thereby resulting in a waste gas stream rich in said heavy hydrocarbon components; and 
     d) collecting said waste gas stream, 
     wherein said heavy hydrocarbon components are defined as the total of the hydrocarbon compounds in the gas mixture which contain at least 2 carbon atoms, and the product stream has a wt % of methane greater than the wt % of methane of said gas mixture. 
     In a preferred embodiment of the present invention the adsorbent material is comprised of a material selected from the group consisting of polymers and structured microporous adsorbents. 
     In another preferred embodiment of the present invention the structured microporous adsorbent is comprised of a molecular sieve selected from the group consisting of carbon molecular sieves, aluminophosphate molecular sieves (ALPOs), and silicoaluminophosphate molecular sieves (SAPOs). 
     In still another preferred embodiment of the present invention the structured microporous adsorbent is comprised of a zeolite selected from the group consisting of MFI, faujasite, MCM-41 and Beta. 
     In a preferred embodiment, the adsorbent contactor is a parallel channel contactor comprising structured (engineered) adsorbents in which substantially parallel flow channels are incorporated into the adsorbent structure. 
     In still another embodiment the contactor has less than about 10% of its open pore volume in pores with diameters greater than about 20 angstroms and less than about 1 micron. 
     In another embodiment the adsorbent contains an effective amount of blocking agent occupying mesopores and macropores so that no more that about 20 vol. % of open pore volume of the adsorbent is in the mesopore or greater size range. 
    
    
     
       BRIEF DESCRIPTION OF THE FIGURES 
         FIG. 1  hereof is a representation of one embodiment of a parallel channel contactor of the present invention in the form of a monolith directly formed from the microporous adsorbent of the present invention and containing a plurality of parallel channels. 
         FIG. 2  hereof is a cross-sectional representation along the longitudinal axis of the monolith of  FIG. 1 . 
         FIG. 3  hereof is a representation of a magnified section of the cross-sectional view of the monolith of  FIG. 2  showing the detailed structure of the adsorbent layer along with a blocking agent occupying some of the mesopores and macropores. 
         FIG. 4  hereof is another representation of an embodiment of a parallel channel contactor of the present invention in the form of a coated monolith where the adsorbent layer is coated onto the channel wall. 
         FIG. 5  hereof is an electron micrograph of the surface of a DDR film that is suitable to act as the adsorbent layer of the contactors of the present invention with a volume fraction of open mesopores and micropores that is less than about 7%. 
         FIG. 6  is an electron micrograph of the surface of an MFI film that is also suitable to act as an adsorbent layer of the contactors of the present invention with a volume fraction of open mesopores and micropores that is less than about 7%. 
         FIG. 7  hereof represents another embodiment of the present invention in which the parallel channel contactor is in the form of a coated monolith for TSA applications where the adsorbent layer is coated onto the channel walls of a preformed monolith. 
         FIG. 8  hereof is a representation of a parallel channel contactor of the present invention in the form of an array of hollow fibers. 
         FIG. 9  hereof is yet another representation of a parallel channel contactor of the present invention but in the form of a hollow fiber contactor for TSA applications. 
         FIG. 10  hereof is another representation of a hollow fiber contactor for TSA as shown in  FIG. 9  but with the outer surfaces of the housing for the contactor rendered transparent. Dotted lines are used to indicate the edges of the outer surface. 
         FIG. 11  hereof is a representation of an embodiment of the present invention wherein the parallel contactor is constructed from parallel laminate sheets. 
         FIG. 12  hereof is a schematic diagram of a preferred five steps PSA/RCPSA process for treating a stream containing about 20 vol. % CO 2  and about 80 vol. % CH 4 . 
         FIG. 13  hereof is a schematic diagram of a preferred five steps PSA/RCPSA process for treating a stream containing about 2 vol. % N 2  and about 98 vol. % CH 4 . 
         FIG. 14  hereof is a schematic diagram of an integrated process utilizing a turboexpander and a PSA process of the present invention. 
         FIG. 15  hereof is a schematic representation of a preferred procedure for measuring the volume fraction of mesopores and macropores of adsorbent contactors of the present invention. 
     
    
    
     DETAILED DESCRIPTION OF THE INVENTION 
     The present invention is directed to adsorbent contactors for use in swing adsorption processes, which adsorbent contactors contain a plurality of flow channels and which contactors contain 20 vol. % or less, preferably 15 vol. % or less, more preferably 10 vol. % or less, and most preferably 5 vol. % or less of their open pore volume in pores in the mesopore and macropore size range. The term “adsorbent contactor” as utilized herein includes both structured and unstructured adsorbent contactors. The preferred contactors of the present invention are a type of structured adsorbent contactor entitled herein as “parallel channel contactors” The preferred contactors of the present invention are parallel channel contactors for use in thermal swing adsorption (TSA) and various types of pressure swing adsorption processes including conventional pressure swing adsorption (PSA), and partial pressure swing or displacement purge adsorption (PPSA) technologies. These swing adsorption processes can be conducted with rapid cycles, in which case they are referred to as rapid cycle thermal swing adsorption (RCTSA), rapid cycle pressure swing adsorption (RCPSA), and rapid cycle partial pressure swing or displacement purge adsorption (RCPPSA) technologies. The term swing adsorption processes shall be taken to include all of these processes (i.e. TSA, PSA, PPSA, RCTSA, RCPSA, and RCPPSA) including combinations of these processes. Such processes require efficient contact of a gas mixture with a solid adsorbent material. It should also be noted that unless otherwise noted herein or by reference to specific “geometric shapes” (in which case would apply only to structured adsorbent contactors), that all preferred embodiments as described in this application, such as, but limited to, contactor voidages, separation components and efficiencies, operating conditions, preferred materials, etc., apply to both structured and unstructured adsorbent contactors of the present invention as described herein. 
     The structure of parallel channel contactors, including fixed surfaces on which the adsorbent or other active material is held, provides significant benefits over previous conventional gas separation methods, such as vessels containing adsorbent beads or extruded adsorbent particles. “Parallel channel contactors” are defined herein as a subset of adsorbent contactors comprising structured (engineered) adsorbents in which substantially parallel flow channels are incorporated into the adsorbent structure. These flow channels may be formed by a variety of means, many of which are described herein and in addition to the adsorbent material, the adsorbent structure may contain items such as, but not limited to, support materials, heat sink materials, void reduction components, etc., which are described more fully herein. 
     Swing adsorption processes are all well known to those having ordinary skill in the art and they can be applied to remove a variety of target gases from a wide variety of gas mixtures. It is possible to significantly improve the recovery percentage of the light component of a gas mixture by use of the present invention. The “light component” as utilized herein is taken to be the species, or molecular component, or components that are not preferentially taken up by the adsorbent in the adsorption step of the process. Conversely, the “heavy component” as utilized herein is taken to be the species, or molecular component, or components that are preferentially taken up by the adsorbent in the adsorption step of the process. With the contactors of the present invention, it has been unexpectedly discovered that total recovery of the light component achieved in the swing adsorption process can be greater than about 80 vol. %, more preferably greater than about 85 vol. %, even more preferably greater than about 90 vol. %, and most preferably greater than about 95 vol. % of the content of the light component introduced into the process. Recovery of the light component is defined as the time averaged molar flow rate of the light component in the product stream divided by the time averaged molar flow rate of the light component in the feedstream. Similarly, recovery of the heavy component is defined as the the time averaged molar flow rate of the heavy component in the product stream divided by the time averaged molar flow rate of the heavy component in the feedstream. 
     The structured adsorbent contactors of the present invention contain a very low volume fraction of open mesopores and macropores. That is, the structured bed adsorbent contactors of the present invention contain less than about 20 vol. %, preferably less than about 15 vol. %, more preferably less than about 10 vol. %, and most preferably less than about 5 vol. % of their pore volume in open pores in the mesopore and macropore size range. Mesopores are defined by the IUPAC to be pores with sizes in the 20 to 500 angstrom size range. Macropores are defined herein to be pores with sizes greater than 500 angstroms and less than 1 micron. Because the flow channels are larger than 1 micron in size, they are not considered to be part of the macropore volume. By open pores we mean mesopores and macropores that are not occupied by a blocking agent and that are capable of being occupied, essentially non-selectively, by components of a gas mixture. Different test methods as described below are to be used to measure the volume fraction of open pores in a contactor depending on the structure of the contactor. 
     Open pore volume (in percent or volume percent) is defined herein as the volume of the pores in the adsorbent that are between 20 angstroms and 10,000 angstroms (1 micron) in diameter divided by the total volume of the contactor that is occupied by the adsorbent material including associated mesopores and macropores in the adsorbent structure. “Swept volumes” such as engineering flow channels as well as the volume occupied by any non-adsorbent material, such as but not limited to, support materials, blocking agents, thermal masses, etc., are not included in the amount of volume occupied by the adsorbent material. 
     The preferred test for determining the volume fraction of open mesopores and macropores of the contactor is defined as follows and involves an analysis of the isotherm of a condensable vapor adsorbed by the contactor. A liquid which has a vapor pressure greater than 0.1 torr at the temperature of the test is a suitable material that can be used to produce a condensable vapor. At 20° C., water, hexane, trimehtlybenzene, toluene, xylenes, and isooctane have sufficiently high vapor pressures that they can be used as condensable vapors. In the adsorption branch of the isotherm (obtained by increasing the pressure of the condensable vapor), capillary condensation fills empty micropore, mesopore, and much of the empty macropore volume with liquid. In the desorption branch micropores, mesopores, and macropores pores filled with liquid are emptied. It is well known that there is a hysteresis between the adsorption and desorption branches of the isotherm. Detailed analysis of the adsorption isotherm relies in part on the Kelvin equation which is well known to those skilled in the art. The detailed analysis provides a measurement of the volume fraction of the mesopores and macropores in the structured adsorbent. The preferred measurement technique described in the following paragraphs derives from these principles. 
     If a liquid blocking agent is not used in the contactor the procedure outlined in this paragraph is used to measure the volume of open mesopores and macropores of the subject contactor. This measurement is performed on either the entire contactor or a representative portion of the contactor. A representative portion of the contactor contains a least an entire cross section of the contactor and has a mass that is between 10% and 100% of the mass of the contactor. Additionally, the mass of the contactor used in this measurement should be more than 50 grams. A preferred procedure is represented in  FIG. 15  hereof wherein the initial steps of the procedure involve placing the contactor  1101  or a representative portion of the contactor, into a sealable vacuum tight container  1103  and evacuating the container. Chamber  1103  is designed so that the volume defined by the exterior surface of the contactor  1101  is at least 50% of the interior volume of the chamber. The vacuum tight container is equipped with a pressure transducer  1173  and a cable  1171  to power the transducer and transmit the signal generated. The transducer is chosen so that it can measure pressures with an accuracy of 0.01 torr. A suitable transducer for such a measurement is a capacitance manometer. 
     The vacuum tight vessel  1103  and all of the equipment used to evacuate the vessel and fill the vessel with known quantities of the condensable vapor are located in an isothermal chamber  1191 . The isothermal chamber  1191  is kept at a temperature of 30.00 (+/−0.01)° C. To make sure that the vacuum tight container  1103  and vessels  1125  and  1141  are at a constant temperature before and after each step used to dose hexane into the contactor their temperature is monitored with thermocouples  1195 ,  1197  and  1199  that can be read with a resolution of 0.01° C. The thermocouple readings may differ by a small amount because the accuracy of thermocouple readings is generally 0.2° C. The important issue is that before and after each hexane dosing step the readings of thermocouples  1195 ,  1197  and  1199  remain constant to within +/−0.01° C. Initially all valves ( 1113 ,  1127 ,  1149 ,  1151 ,  1153  and  1165 ) in the system are closed. It is preferred that the valves be air actuated (instead of solenoid activated) so that do not heat the gas or piping when they are opened. Before the measurement begins the equipment used to fill hexane vapor (chosen as an example of a condensable vapor at 30° C.) into vessel  1103  must be leak checked. This is done by opening valves  1127 ,  1151 , and  1153 , allowing line  1119  that is attached to a vacuum pump to evacuate vessels  1125  and  1141 . 
     Pressure in these vessels is measured with transducers  1163  and  1143  which have cables  1161  and  1145 , respectively to power them and transmit the signals generated. The transducer is chosen so that they can measure pressures with an accuracy of 0.01 torr and suitable transducers are capacitance manometers. The vessel  1125  and  1141  are evacuated so that transducers  1163  and  1143  read a pressure of less than 0.03 torr. Valve  1127  is then closed and the system is considered leak tight if the pressure recorded by transducers  1163  and  1143  does not rise by more than 0.02 torr over a three hour period. At this point valves  1153  and  1151  are closed and the evacuated vessel  1141  is filled with hexane through line  1147  by opening valve  1149 . Line  1147  was originally filled with liquid hexane. To stop the filling of reservoir  1141 , valve  1149  is shut. 
     A procedure is then instituted to remove any impurity gases that may have been carried into vessel  1141  during the hexane filling step. Gases are removed by opening valve  1127  and then opening valve  1151  for a period of 2 minutes dropping the pressure in vessel  1141  thus allowing the hexane to boil. This degassing procedure is repeated five times before the hexane in vessel  1141  can be used. At this point valve  1153  is closed and valve  1127  is open, thus evacuating line  1129 . Valve  1153  is then opened pulling a vacuum on vessel  1125 . Adsorbed molecules in the contactor or a representative piece of the contactor  1101  in chamber  1103  are then removed by opening valve  1113 . This allows line  1115  that is attached to a vacuum pump to evacuate chamber  1103 . The evacuation procedure continues until the pressure in the vessel  1103  falls below 0.03 torr. At this point valve  1113  is closed and the pressure in the chamber is monitored for an hour. If the pressure in the chamber rises by more than 0.02 torr during this time period then the evacuation procedure is repeated. If the evacuation procedure has to be repeated more than ten times then alternative means of removing molecules from the contactor  1101  should be employed (such as heating the contactor). After adsorbed molecules have been successfully removed from the contactor, valves  1127  and  1153  are closed. 
     Valve  1151  is then opened allowing line  1129  to fill with hexane vapor. Under the conditions of the test this will be approximately 187 torr of hexane vapor. Valve  1151  is then closed and valve  1153  is opened allowing the vapor in the line to expand into vessel  1125 . Because of the difference in volume between line  1129  and vessel  1125  the pressure measured by transducer  1163  will be less than 5 torr. Valve  1153  is then closed and this filling procedure is repeated until the pressure in vessel  1125  is approximately 5 torr. At this point valve  1165  is opened to dose the contactor  1101  with hexane vapor. The pressure in vessel  1125  drops because of gas expansion into chamber  1103  and possible adsorption of molecules of hexane into micropores of the contactor. After the pressure in vessel  1125  stops dropping and stabilizes, the pressure is recorded and the number of moles of hexane transferred into chamber  1103  is computed from the ideal gas law. This requires knowledge (previous measurement) of the interior volume of vessel  1125  and its associated piping. 
     The moles of gas transferred into vessel  1103  that would be needed to fill the gas space inside it are computed using the ideal gas law with the pressure measured by transducer  1173 . Again, knowledge of the available gas space in chamber  1103  is required for the calculation. The interior volume of chamber  1103  is known (previous measurement) and the available gas volume is computed by subtracting from the interior volume of vessel  1103  the exterior volume of the contactor and adding back the volume of the flow channels in the contactor. Errors in knowledge of the exterior volume of the contactor or the volume of the flow channels will not significantly affect the measurement of the total open mesopore and macropore volumes. The quantity which is the difference between the exterior volume of the contactor and the volume of the flow channels only has to be known to an accuracy of 20%. 
     The moles of gas adsorbed by the contactor is then the difference between the moles of gas transferred and the moles of gas required to fill the available gas space in vessel  1103  and its associated piping. After completing this dosing step and the evaluation of the moles of gas adsorbed in the contactor  1101  valve  1165  is closed and pressure in vessel  1125  is increased 5 more torr by repeating the procedure originally used to fill it with hexane vapor. The dosing step to adsorb more molecules into the contactor is then repeated. The filling and dosing steps continue to be repeated until the pressure in vessel  1125  at the end of a dosing step is within +/−2.5 torr of 15% of the reading of pressure transducer  1143 . This range is expected to be between 25.5 and 30.5 torr. From this point onward in the procedure the additional moles of hexane that are adsorbed in the contactor are considered to fill the mesopores and macropores. The filling and dosing steps are continued until the pressure in chamber  1103  housing the contactor exceeds 95% of the pressure read by transducer  1143 . 
     Filling and dosing steps are continued in a manner such that the pressure in vessel  1125  is only increased by  1  torr in each filling step. When the pressure read by transducer  1173  at the end of a dosing step exceeds 98.5% of the pressure read by transducer  1143  the pressure increase in vessel  1125  during a filling step is decreased to 0.5 torr. When the pressure read by transducer  1173  at the end of a dosing step exceeds 99.25% of the pressure read by transducer  1143  the pressure increase in vessel  1125  during a filling step is decreased to 0.05 torr. The filling and dosing steps are then continued until the pressure read by the transducer  1173  at the end of a dosing step exceeds 99.6% of the pressure read by transducer  1143 . The pressure at which the experiment is ended is expected to be approximately 186.4 torr. The total number of moles adsorbed by the contactor from the point at which at the end of a dosing step transducer  1161  was in a range between within +/−2.5 torr of 15% of the reading of pressure transducer  1143  and the point at which the pressure read by the transducer  1173  at the end of a dosing step exceeded 99.6% of the pressure read by transducer  1143  is the total number of moles of hexane adsorbed in the mesopore and macropore volume of the contactor. The volume of the open mesopores and macropores in the contactor is then determined by multiplying this number of moles by the molar volume of hexane. The open pore volume as expressed in a volume fraction as used herein is then obtained by dividing the volume of open mesopores and macropores determined by this test by the total volume of the contactor that is occupied by the adsorbent material as defined prior. Although the open pore volume for the contactor is determined by the test procedure described above, scanning electron microscopy may be used to further confirm the relative volume of mesopores and macropores in the sample. When scanning electron microscopy is used the surface as well as a cross section of the contactor should be imaged. 
     If a liquid material is used as a blocking agent in the formulation of the contactor, and the contactor is operated under conditions where the pores remain substantially fully filled with liquid no assay as described above is required to determine the open pore volume of the contactor. In this contactor configuration, the mesopores and macropores of the contactor will remain filled with liquid as long as the liquid remains condensable at the operating temperature of the contactor and the feed flowing into the contactor is fully saturated with the vapor of the liquid at the inlet temperature and pressure. In this case, there is no open mesopore or macropore volume in the contactor because it has all been filled-in by the condensable vapor. If under operating conditions (i.e., inlet temperature and pressure) the feed flowing into the contactor is only partially saturated with the vapor of the liquid then some fraction of the mesopore or macropore volume will remain open. The degree of saturation is characterized by a liquid activity (a liquid ) that is the ratio of the partial pressure of the vapor of the liquid in the flowing gas stream to the saturated vapor pressure of the liquid at the temperature of the contactor (i.e. P i /P sat ). The amount of open mesopore and macropore volume increases as the partial pressure of the condensable liquid in the feed decreases. To determine the volume of mesopores and macropores under operating conditions the liquid material used in the formulation of the contactor is removed from the mesopores and macropores of the contactor by drying. Liquid can be dried-out of the mesopores and macropores of the contactor by heating it in a sealed container while drawing a vacuum or by heating it while passing a substantially pure purge gas, such as He, over the contactor. Once liquid has been removed from the mesopores and macropores of the contactor, the assay method previously described can be conducted. In this assay the amount of gas adsorbed by the contactor is plotted against the hexane activity (a hexane ) which is the hexane pressure at the end of an adsorption step divided by the saturated hexane vapor pressure. The amount of open mesopores and macropores that would be expected in operation is then determined from the cumulative number of moles of hexane adsorbed between the point at which the hexane activity exceeds a liquid  and the point at which the experiment is terminated (i.e., when the pressure read by the transducer  1173  at the end of a dosing step exceeds 99.6% of the pressure read by transducer  1143 ). Again the molar volume of hexane is used to compute the actual open mesopore and macropore volume. The open pore volume as expressed in a volume fraction as used herein is then obtained by dividing the volume of open mesopores and macropores determined by this test by the total volume of the contactor that is occupied by the adsorbent material as defined prior. 
     In equilibrium controlled swing adsorption processes most of the selectivity is imparted by the equilibrium adsorption properties of the adsorbent, and the competitive adsorption isotherm of the light product in the micropores or free volume of the adsorbent is not favored. In a kinetically controlled swing adsorption processes most of the selectivity is imparted by the diffusional properties of the adsorbent and the transport diffusion coefficient in the micropores and free volume of the adsorbent of the light species is less than that of the heavier species. Also, in kinetically controlled swing adsorption processes with microporous adsorbents the diffusional selectivity can arise from diffusion differences in the micropores of the adsorbent or from a selective diffusional surface resistance in the crystals or particles that make-up the adsorbent. 
     It will be understood that the term PSA, unless preceded by the term “conventional” or “rapid cycle” refers collectively to all pressure swing adsorption processes including conventional PSA, RCPSA and PPSA. In PSA processes, a gaseous mixture is conducted under pressure for a period of time over a first bed of a solid sorbent that is selective, or relatively selective, for one or more components, usually regarded as a contaminant, that is to be removed from the gaseous mixture. The components that are selectively adsorbed are referred to as the heavy component and the weakly adsorbed components that pass through the bed are referred to as the light components. It is possible to remove two or more contaminants simultaneously but for convenience, the component or components, that are to be removed by selective adsorption will be referred to in the singular and referred to as a contaminant or heavy component. 
     Unless otherwise noted, the term “selectivity” as used herein is based on binary (pairwise) comparison of the molar concentration of components in the feed stream and the total number of moles of these components adsorbed by the particular adsorbent during the adsorption step of the process cycle under the specific system operating conditions and feedstream composition. For a feed containing component A, component B, as well as additional components, an adsorbent that has a greater “selectivity” for component A than component B will have at the end of the adsorption step of the swing adsorption process cycle a ratio:
 
 U   A =(total moles of  A  in the adsorbent)/(molar concentration of  A  in the feed) that is greater than the ratio:
 
 U   B =(total moles of  B  in the adsorbent)/(molar concentration of  B  in the feed)
 
     Where U A  is the “Adsorption Uptake of component A” and U B  is the “Adsorption Uptake of component B”. 
     Therefore for an adsorbent having a selectivity for component A over component B that is greater than one:
 
Selectivity= U   A   /U   B  (where  U   A   &gt;U   B ).
 
     Amongst a comparison of different components in the feed, the component with the smallest ratio of the total moles picked up in the adsorbent to its molar concentration in the feed is the lightest component in the swing adsorption process. This means that the molar concentration of the lightest component in the stream coming out during the adsorption step is greater than the molar concentration of that lightest component in the feed. The adsorbent contactors of the present invention have a selectivity for a first component (e.g., component A) over a second component (e.g., component B) of at least 5, more preferably a selectivity for a first component over a second component of at least 10, and most preferably a selectivity for a first component over a second component of at least 25. 
     Examples of components are molecules such as molecular nitrogen, N 2 , or compounds, such as carbon dioxide, CO 2 , and methane, CH 4 . In a preferred embodiment of the present invention, the adsorbent contactor has a selectivity for CO 2  over CH 4  of at least 5, more preferably a selectivity for CO 2  over CH 4  of at least 10, and most preferably a selectivity for CO 2  over CH 4  of at least 25. In another preferred embodiment of the present invention, the adsorbent contactor has a selectivity for N 2  over CH 4  of at least 5, more preferably a selectivity for N 2  over CH 4  of at least 10, and most preferably a selectivity for N 2  over CH 4  of at least 25. In yet another preferred embodiment of the present invention, the adsorbent contactor has a selectivity for H 2 S over CH 4  of at least 5, more preferably a selectivity for H 2 S over CH 4  of at least 10, and most preferably a selectivity for H 2 S over CH 4  of at least 25. 
     In a preferred embodiment of the present invention, the adsorbent has a “kinetic selectivity” for two or more gas components. As used herein, the term “kinetic selectivity” is defined as the ratio of single component diffusion coefficients, D (in m 2 /sec), for two different species. These single component diffusion coefficients are also known as the Stefan-Maxwell transport diffusion coefficients that are measured for a given adsorbent for a given pure gas component. Therefore, for example, the kinetic selectivity for a particular adsorbent for component A with respect to component B would be equal to D A /D B . The single component diffusion coefficients for a material can be determined by tests well known in the adsorptive materials art. The preferred way to measure the kinetic diffusion coefficient is with a frequency response technique described by Reyes et al. in “Frequency Modulation Methods for Diffusion and Adsorption Measurements in Porous Solids”, J. Phys. Chem. B. 101, pages 614-622, 1997. In a kinetically controlled separation it is preferred that kinetic selectivity (i.e., D A /D B ) of the selected adsorbent for the first component (e.g., Component A) with respect to the second component (e.g., Component B) be greater than 5, more preferably greater than 20, even more preferably greater than 50. 
     In another preferred embodiment of the present invention, the adsorbent has an “equilibrium selectivity” for two or more gas components. As used herein, the term “equilibrium selectivity” is defined in terms of the slope of the single component uptake into the adsorbent (in μmole/g) vs. pressure (in torr) in the linear portion, or “Henry&#39;s regime”, of the uptake isotherm for a given adsorbent for a given pure component. The slope of this line is called herein the Henrys constant or “equilibrium uptake slope”, or “H”. The “equilibrium selectivity” is defined in terms of a binary (or pairwise) comparison of the Henrys constants of different components in the feed for a particular adsorbent. Therefore, for example, the equilibrium selectivity for a particular adsorbent for component A with respect to component B would be H A /H B . It is preferred that in an equilibrium controlled separation the equilibrium selectivity (i.e., H A /H B ) of the selected adsorbent for the first component (e.g., Component A) with respect to the second component (e.g., Component B) be greater than 5, more preferably greater than 20, even more preferably greater than 50. 
     In the PSA process, the gaseous mixture is passed over a first adsorption bed in a first vessel and a light component enriched product stream emerges from the bed depleted in the contaminant, or heavy component, which remains sorbed in the bed. After a predetermined time or, alternatively when a break-through of the contaminant or heavy component is observed, the flow of the gaseous mixture is switched to a second adsorption bed in a second vessel for the purification to continue. While the second bed is in adsorption service, the sorbed contaminant, or heavy component is removed from the first adsorption bed by a reduction in pressure. In some embodiments, the reduction in pressure is accompanied by a reverse flow of gas to assist in desorbing the heavy component. As the pressure in the vessels is reduced, the heavy component previously adsorbed in the bed is progressively desorbed to a heavy component enriched product stream. When desorption is complete, the sorbent bed may be purged with an inert gas stream, e.g., nitrogen or a purified stream of process gas. Purging may also be facilitated by the use of a higher temperature purge gas stream. 
     After the first bed has been regenerated so that it is again ready for adsorption service, the flow of the gaseous mixture is switched from the second bed to the first bed, and the second bed is regenerated. The total cycle time is the length of time from when the gaseous mixture is first conducted to the first bed in a first cycle to the time when the gaseous mixture is first conducted to the first bed in the immediately succeeding cycle, i.e., after a single regeneration of the first bed. The use of third, fourth, fifth, etc. vessels in addition to the second vessel can serve to increase cycle time when the adsorption cycle time for the bed is shorter than the cycle times for the desorption &amp; purging cycles for the bed. 
     Conventional PSA processes suffer from several inherent disadvantages. For example, conventional PSA units are typically more costly to build and operate and are significantly larger in size for the same amount of target gas that needs to be recovered from a target-gas containing gas stream, such as natural gas, as compared to RCPSA. Also, a conventional PSA unit will generally have cycle times in excess of one minute, typically in excess of 2 to 4 minutes due to time limitations required to allow diffusion of the components through the larger beds utilized in conventional PSA and the equipment configuration involved. In contrast, RCPSA generally has a total cycle times of less than one minute. The total cycle times of RCPSA may be less than 30 seconds, preferably less than 15 seconds, more preferably less than 10 seconds, even more preferably less than 5 seconds, and even more preferably less than 1 second. Further, the rapid cycle pressure swing adsorption units can make use of substantially different sorbents, such as, but not limited to, structured materials such as monoliths, laminates, and hollow fibers. 
     RCPSA can enable a significant increase in process intensification (e.g., higher operating frequencies and gas flow velocities) when compared to conventional PSA. RCPSA typically utilizes a rotary valving system to conduct the gas flow through a rotary adsorber module that contains a number of separate adsorbent bed compartments or “tubes”, each of which is successively cycled through the sorption and desorption steps as the rotary module completes the cycle of operations. The rotary sorber module is normally comprised of multiple tubes held between two seal plates on either end of the rotary sorber module wherein the seal plates are in contact with a stator comprised of separate manifolds wherein the inlet gas is conducted to the RCPSA tubes and the processed purified product gas and the tail gas exiting the RCPSA tubes are conducted away from the rotary sorber module. By suitable arrangement of the seal plates and manifolds, a number of individual compartments or tubes may pass through the characteristic steps of the complete cycle at any given time. In contrast, with conventional PSA, the flow and pressure variations, required for the RCPSA sorption/desorption cycle, changes in a number of separate increments on the order of seconds per cycle, which smoothes out the pressure and flow rate pulsations encountered by the compression and valving machinery. In this form, the RCPSA module includes valving elements angularly spaced around the circular path taken by the rotating sorption module so that each compartment is successively passed to a gas flow path in the appropriate direction and pressure to achieve one of the incremental pressure/flow direction steps in the complete RCPSA cycle. One key advantage of the RCPSA technology is a significantly more efficient use of the adsorbent material. The quantity of adsorbent required with RCPSA technology can be only a fraction of that required for conventional PSA technology to achieve the same separation quantities and qualities. As a result, the footprint, investment, and the amount of active adsorbent required for RCPSA is typically significantly lower than that for a conventional PSA unit processing an equivalent amount of gas. 
     The present invention may be used in PPSA, RCPSA or hybrid PPSA or RCPPSA processes where a gas or liquid is purged through the bed to help desorb molecules. In a PPSA process, desorption of the adsorbed species is accomplished by passing a gas or liquid through the contactor to desorb molecules taken up during an adsorption step. An example of a gas that may be used is steam. In hybrid PPSA processes, the desorption of molecules from the contactor is accomplished by use of a thermal or pressure swing and part of the desorption is accomplished with a purge. 
     Improvements in the recovery of the light component are especially important for processes used to remove impurities from natural gas streams, particularly high pressure natural gas streams. It is desirable to recover the impurities, also referred to as the “heavy component(s)”, and the methane-rich product, also referred to as the “light component”, at as high a pressure as practical for operability in natural gas processing. As previously mentioned, the present invention can be used to obtain methane recovery of greater than about 80 vol. %, more preferably greater than about 85 vol. %, even more preferably greater than about 90 vol. %, and most preferably greater than about 95 vol. %, even when the natural gas is fed at high inlet pressures, such as at inlet pressures greater than about 50 psig, preferably at inlet pressures greater than about 150 psig, more preferably at inlet pressures greater than about 450 psig, even more preferably at inlet pressures greater than about 600 psig and most preferably at inlet pressures greater than about 1200 psig. The present invention can be used even when the gas stream is at an exceptionally high inlet pressure of up to about 7000 psig. The composition of natural gas streams directly from an underground field (raw natural gas) will vary from field to field. Non-limiting examples of components that comprise a raw natural gas stream include water, condensates (higher molecular weight organics), methane, ethane, propane, butane, CO 2 , N 2 , He, H 2 S, Hg, and mercaptans. Water and condensates are typically removed and the condensates sent to a petroleum refinery. In order to produce a gas that can be introduced into a pipeline for sale to residential and commercial fuel markets contaminants, such as N 2 , Hg, mercaptans, and the acid gases CO 2  and H 2 S must to removed to acceptable levels. The levels and impurity types vary from gas field to gas field and in some cases can comprise the majority of molecules in the produced gas. For example, it is not uncommon for some natural gas fields to contain from about 0 to 90 vol. % CO 2 , more typically from about 10 vol. % to about 70 vol. % CO 2 . 
     The present invention also provides a method to increase recovery of the light component by conditioning the temperature and pressure of gas fed to the contactor. This method can be used with or without a contactor having a low volume fraction of mesopores and macropores. During the adsorptive step of well designed kinetically controlled swing adsorption processes, the amount of heavy component in the micropores or free volume can be approximately computed from the adsorption isotherm of the heavy component in equilibrium with its local gas phase concentration in the contactor. In well designed equilibrium controlled swing adsorption processes the amount of heavy component in the micropores or free volume can be approximately computed from the competitive adsorption isotherm of the heavy and light components in equilibrium with their local gas phase concentration in the contactor. These approximations are possible because in well designed swing adsorption processes, the contactor provides good mass transfer characteristics between the gas phase and the adsorbed phase in the micropores or free volume of the contactor. The maximum attainable loading of the heavy component in the macropores or free volume of the contactor is called q s  (units for q s  are milli-mole/m 3 of the microporous or polymeric material). At low pressures the adsorption isotherm for the heavy component usually obeys Henry&#39;s Law and the amount of heavy component adsorbed, q Heavy , in the microporous or polymeric material is:
 
 q   heavy   =K   Heavy   P   Heavy   q   s (in milli-mole/m 3 )
 
where K Heavy  is the Henry&#39;s constant and P Heavy  is the partial pressure of the heavy component. The Henry&#39;s constant, K Heavy  depends on temperature and usually varies according to the equation:
 
               K   Heavy     =       K   0     ⁢     ⅇ       Δ   ⁢           ⁢   H     RT       ⁢           ⁢     (     in   ⁢           ⁢     Pascals     -   1         )             
where K 0  is a pre-exponential factor and AH is the heat of adsorption (in joule/mole).
 
     To improve selectivity and recovery for either a kinetically or equilibrium controlled swing adsorption processes the inlet temperature and pressure should be chosen such that at the end of the adsorption step the loading of the heavy component in the micropores or free volume near the point at which feed is introduced to the contactor should be greater than 0.15 q s  and preferably greater than 0.3 q s  and even more preferably greater than 0.6 q s . This requirement places a lower bound on the inlet pressure and a maximum bound on the inlet temperature. With increasing loading of the heavy component in the micropores or free volume of the adsorbent the amount of material that is selectively adsorbed in the contactor is increased and the amount of material that can be selectively released in the desorption step is increased. These increases reduce the loss of the light component that is non-selectively adsorbed into the mesopores and macropores. Increasing the loading significantly beyond this range reduces the recovery of the light component because the slope of the adsorption isotherm tends to decrease with increasing pressure. To maximize the recovery of the light component it is also preferred that near the point at which feed is introduced to the contactor the slope of the adsorption isotherm for the heavy component be large enough so that: 
                 ∂     q   Heavy         ∂     P   Heavy         &gt;     α   ⁢           ⁢     K   Heavy     ⁢     q   s             
where α= 1/50, more preferably α= 1/25, and even more preferably α=⅛. This inequality places a maximum bound on the inlet pressure and a minimum bound on the inlet temperature. As such these requirements define a window (i.e., maxima and minima) for feed pressure and temperature in which the recovery of the light component is optimized. Usually it is preferred to operate the swing adsorption process at the lowest pressure within the operating window as is practical. As the feed pressure decreases, the concentration of molecules in the mesopores and macropores of the contactor decreases. Lower concentrations of molecules nonselectively adsorbed in the mesopores and macropores leads to lower losses of the light component in the swing adsorption process.
 
     This window is especially important in natural gas separations because natural gas is usually produced at pressures ranging from 1,500 to 7,000 psi. These feed pressures are usually too high to fall within the optimum recovery window for methane which acts as a light component in swing adsorption separation. It is possible to reduce the feed pressure with a simple expansion nozzle, however this technique wastes energy. It is also possible to access the optimum light component recovery window for separations of most heavy components (such as CO 2 , N 2 , H 2 S, H 2 O, heavy hydrocarbons, and mercaptans) by preconditioning the natural gas with a turboexpander that recovers the energy from the gas expansion. Energy recovered from gas expansion can then be used for power generation or to help recompress separated acid gas components (such as CO 2  or H 2 S) so that they can be disposed of in underground formations. Underground formations that are suitable for disposal/sequestration of CO 2  and H 2 S include aquifers that have a top seal that prevents significant loss of injected acid gas components, oil reservoirs, gas reservoirs, depleted oil reservoirs and depleted gas reservoirs. Typically the separated CO 2  and H 2 S has to be recompressed to pressures greater than 2,000 psi and often to pressures greater than 5,000 psi to be injected into these types of underground formations. Thus, it is important to be able to reuse energy recovered from a turboexpander for recompression. The cost of a turboexpander is also less than a gas fired turbine producing the same amount of power. As such, it is economically advantageous to use a turboexpander to capture energy from gas expansion used to condition natural gas for the optimum methane recovery window. When a turboexpander is used, the energy can either be recovered with a shaft coupled electric generator or with a shaft coupled compressor. It can be advantageous to pass the gas coming out of the turboexpander through a heat exchanger before introducing it into the swing adsorption process in order to access the operating window that maximizes methane recovery. Gas coming out of a turboexpander can be too cold to be in the optimum recovery window because the work is recovered in an isentropic expansion. Typically a heat exchanger will be run so that the gas temperature is increased before entering a swing adsorption process. These considerations are especially important when the swing adsorption is a PSA or RCPSA process. 
     In applications where CO 2  is removed from natural gas in swing adsorption processes it is preferred to formulate the adsorbent with a specific class of 8-ring zeolite materials that has a kinetic selectivity. The kinetic selectivity of this class of 8-ring zeolite materials allows CO 2  to be rapidly transmitted into zeolite crystals while hindering the transport of methane so that it is possible to selectively separate CO 2  from a mixture of CO 2  and methane. For the removal of CO 2  from natural gas, this specific class of 8-ring zeolite materials has a Si/Al ratio from about 1:1 to about 1000:1, preferably from about 10:1 to about 500:1, and more from about 50:1 to about 300:1. It should be noted that as used herein, the term Si/Al is defined as the molar ratio of silica to alumina of the zeolitic structure. This preferred class of 8-ring zeolites that are suitable for use herein allow CO 2  to access the internal pore structure through 8-ring windows in a manner such that the ratio of single component diffusion coefficients of CO 2  and methane (i.e., D CO2 /D CH4 ) is greater than 10, preferably greater than about 50, and more preferably greater than about 100 and even more preferably greater than 200. Single component diffusion coefficients are taken to be transport diffusion coefficients measured for a pure gas in the Henry&#39;s law regime of the adsorption isotherm. The loading of molecules in the zeolite is low in the Henry&#39;s law regime and in this regime the Fickian and Stephan Maxwell diffusion coefficients are nearly equal. The diffusivity of a porous crystalline material for a particular sorbate is conveniently measured in terms of its diffusion time constant, D/r 2 , wherein D is the Fickian diffusion coefficient (m 2 /sec) and the value “r” is the radius of the crystallites (m) characterizing the diffusion distance. In situations where the crystals are not of uniform size and geometry, r represents a mean radius representative of their corresponding distributions. One way to measure the time constant and diffusion coefficient is from analysis of standard adsorption kinetics (i.e., gravimetric uptake) using methods described by J. Crank in “The Mathematics of Diffusion”, 2nd Ed., Oxford University Press, Great Britain, 1975. Another way to measure the time constant and diffusion coefficient is from analysis of zero length chromatography data using methods described by D. M. Ruthven in “Principles of Adsorption and Adsorption Processes”, John Wiley, N.Y. (1984) and by J. Kärger and D. M. Ruthven in “Diffusion in Zeolites and Other Microporous Solids”, John Wiley, N.Y. (1992). A preferred way to measure the time constant and diffusion coefficient is with a frequency response technique described by Reyes et al. in “Frequency Modulation Methods for Diffusion and Adsorption Measurements in Porous Solids”, J. Phys. Chem. B. 101, pages 614-622, 1997. An example of a 8-ring zeolite in this class of materials that is preferred for use in swing adsorption processes to remove CO 2  from natural gas is zeolite DDR. Additional preferred 8-ring zeolites are Sigma-1 and ZSM-58 which are zeolites that are isotypic framework structures of DDR. At temperatures below 100° C. the single component diffusion coefficient of CO 2  is found to be more than a hundred times greater than that of methane. From the measured activation energies of the diffusion coefficients, at temperatures up to about 300° C., the diffusion coefficient of CO 2  is computed to be more than five fold times greater than that of methane. Resistance to fouling in swing adsorption processes that remove CO 2  from natural gas is another advantage offered by this class of 8-ring zeolite materials. 
     In many instances, nitrogen also has to be removed from natural gas or gas associated with the production of oil. In some cases this is because of the high nitrogen levels (&gt;2 vol %) in the produced gas, and in other cases nitrogen removal is needed in order to liquefy natural gas. It may also be advantageous to separate nitrogen from flash gas that occurs in LNG production so that the methane and hydrocarbon products can be used as fuel. Another application is the purification of gas from LNG boil-off so that the methane and hydrocarbon products can be recovered or used as fuel. When recovered, it may be advantageous to re-liquefy the methane and hydrocarbon and returned them back to the LNG cargo. In all of these applications it is desirable to selectively adsorb the nitrogen to obtain high recovery of a purified methane product from nitrogen containing gas. There have been very few molecular sieve sorbents with significant equilibrium or kinetic selectivity for nitrogen separation from methane. For N 2  separation from natural gas it is also preferred to formulate the adsorbent with a class of 8-ring zeolite materials that has a kinetic selectivity. The kinetic selectivity of this class of 8-ring materials allows N 2  to be rapidly transmitted into zeolite crystals while hindering the transport of methane so that it is possible to selectively separate N 2  from a mixture of N 2  and methane. For the removal of N 2 , from natural gas, this specific class of 8-ring zeolite materials also has a Si/Al ratio from about 1:1 to about 1000:1, preferably from about 10:1 to about 500:1, and more from about 50:1 to about 300:1. This preferred class of 8-ring zeolites that are suitable for use herein allow N 2  to access the internal pore structure through 8-ring windows in a manner such that the ratio of single component diffusion coefficients of N 2  and methane (i.e., D N2 /D CH4 ) is greater than 5, preferably greater than about 20, and more preferably greater than about 50 and even more preferably greater than 100. Resistance to fouling in swing adsorption processes during the remove N 2  from natural gas is another advantage offered by this class of 8-ring zeolite materials. 
     In other instances, it is also desirable to remove H 2 S from natural gas which can contain from about 0.001 vol % H 2 S to about 70 vol % H 2 S. In this case, it can be advantageous to formulate the adsorbent with stannosilicates as well as the aforementioned class of 8-ring zeolites that has kinetic selectivity. The kinetic selectivity of this class of 8-ring materials allows H 2 S to be rapidly transmitted into zeolite crystals while hindering the transport of methane so that it is possible to selectively separate H 2 S from a mixture of H 2 S and methane. For the removal of H 2 S, from natural gas, this specific class of 8-ring zeolite materials has a Si/Al ratio from about 1:1 to about 1000:1, preferably from about 10:1 to about 500:1, and more from about 50:1 to about 300:1. This preferred class of 8-ring zeolites that are suitable for use herein allow H 2 S to access the internal pore structure through 8-ring windows in a manner such that the ratio of single component diffusion coefficients of H 2 S and methane (i.e., D H2S /D CH4 ) is greater than 5, preferably greater than about 20, and more preferably greater than about 50 and even more preferably greater than 100. DDR framework zeolites, such as Sigma-1 and ZSM-58, are also suitable for the removal of H 2 S from natural gas. In some applications the H 2 S has to be removed to the ppm or sub-ppm levels. To achieve such extensive removal of H 2 S it can be advantageous to use a PPSA or RCPPSA process. 
     It is sometimes necessary to remove heavy hydrocarbons from a gas mixture containing said heavy hydrocarbons and methane. The term “heavy hydrocarbon” as used in this application means hydrocarbons having 2 or more carbon atoms. The preferred gas mixture is natural gas or gas associated with the production of oil, more preferably natural gas. Heavy hydrocarbon removal may be necessary for dew point conditioning before the natural gas is shipped via pipeline or to condition natural gas before it is liquefied. In other instances it may be advantageous to recover heavy hydrocarbons from produced gas in enhanced oil recovery (EOR) floods that employ CO 2  and nitrogen. In still other instances it may be advantageous to recover heavy hydrocarbons from associated gas that is cycled back into an oil reservoir during some types of oil production. In many instances where it is desirable to recover heavy hydrocarbons, the gas can be at pressures in excess of 1,000 psi and in some instances the gas pressure can be in excess of 5,000 psig, even sometimes in excess of about 7,000 psig. It is advantageous in these applications to use an adsorbent formulated with a zeolite having a pore size between about 5 and about 20 angstroms. Non-limiting examples of zeolites having pores in this size range are MFI, faujasite, MCM-41 and Beta. It is preferred that the Si/Al ratio of zeolites utilized in an embodiment of a process of the present invention for heavy hydrocarbon removal be from about 20 to about 1000, preferably from about 200 to about 1000 in order to prevent excessive fouling of the adsorbent. 
     In some instances, natural gas is produced with mercaptans present and it is advantageous to use adsorption processes to aid in their separation. Streams containing mercaptans and components found in natural gas are present in several processes that have been developed to purify natural gas. It is possible to more selectively separate mercaptans from natural gas or natural gas components and increase the recovery of the valuable components (such as methane) using the contactors of the present invention. It is advantageous in these applications to also use an adsorbent formulated with a zeolite having a pore size between about 5 and about 20 angstroms. Non-limiting examples of zeolites having pores in this size range are MFI, faujasite, MCM-41 and Beta. In these applications the Si/Al ratio of the zeolite can be from about 1 to about 1000. 
     The low mesoporous and macroporous adsorbent is an integral component of the contactors of the present invention that can be used in both equilibrium and kinetically controlled swing adsorption processes to improve light component product recovery. Adsorbents contactors of the prior art contain significant levels of mesopores and macropores. At the end of the adsorption step, the mesopores and macropores, which are non-selective, will contain significant amounts of light components because transport into the mesopores and macropores is nonselective. This is an especially important problem in high pressure RCPSA, PSA, TSA and PPSA processes because at the end of the adsorption step the number of molecules in the mesopore and macropore spaces can be comparable to the number of molecules selectively adsorbed in the micropores of the adsorbent. In the desorption step most of the light components contained in the mesopores and macropores are undesirably lost to the heavy component product stream. As such, these light molecules are not recovered as desired with the light product. This can result in significant loss of valuable light product. The adsorbent contactors of the present invention can significantly improve this recovery of light products by reducing the volume fraction of the open mesopore and macropore spaces. 
     In one embodiment of the present invention, the walls of the open flow parallel channels are comprised of the adsorbent. The adsorbent is preferably a microporous adsorbent or polymer that selectively adsorbs the heavy components. Non-limiting examples of microporous adsorbents include zeolites, titanosilicates, ferrosilicates, stannosilicates, aluminophosphates (AlPOs), silicaaluminophosphates (SAPOs) and carbon molecular sieves. In other preferred embodiments, the adsorbent material is comprised of a microporous adsorbent selected from the group consisting of titanosilicates and stannosilicates. In yet other preferred embodiments, the adsorbent material is comprised of a microporous adsorbent selected from the group consisting of aluminophosphates (AlPOs), silicaaluminophosphates (SAPOs) and carbon molecular sieves. Preferred are zeolites for the removal of CO 2 , N 2 , and H 2 S with the stannosilicates being more preferred for the removal of H 2 S. In other preferred embodiments, the adsorbent material is comprised of a zeolite selected from the group consisting of MFI, faujasite, MCM-41, and Beta. Non-limiting examples of polymers that can be used as selective adsorbents include polyimides, polysulfones, and functionalized polymers such as amine functionalized polymers. 
     The adsorbent contactors of the present invention may optionally contain a thermal mass (heat transfer) material to help control heating and cooling of the adsorbent of the contactor during both the adsorption step and desorption step of a pressure swing adsorption process. Heating during adsorption is caused by the heat of adsorption of molecules entering the adsorbent. The optional thermal mass material also helps control cooling of the contactor during the desorption step. The thermal mass can be incorporated into the flow channels of the contactor, incorporated into the adsorbent itself, or incorporated as part of the wall of the flow channels. When it is incorporated into the adsorbent, it can be a solid material distributed throughout the adsorbent layer or it can be included as a layer within the adsorbent. When it is incorporated as part of the wall of the flow channel, the adsorbent is deposited or formed onto the wall. Any suitable material can be used as the thermal mass material in the practice of the present invention. Non-limiting examples of such materials include metals, ceramics, and polymers. Non-limiting examples of preferred metals include steel, copper, and aluminum alloys. Non-limiting examples of preferred ceramics include silica, alumina, and zirconia. An example of a preferred polymer that can be used in the practice of the present invention is polyimide. Depending upon the degree to which the temperature rise is to be limited during the adsorption step, the amount of thermal mass material used can range from about 0 to about 25 times the mass of the microporous adsorbent of the contactor. 
     A preferred range for the amount of thermal mass in the contactor is from about 0 to 5 times the mass of the microporous adsorbent of the contactor. A more preferred range for the amount of thermal mass material will be from about 0 to 2 times the mass of the microporous adsorbent material, most preferably from about 0 to 1 times the mass of the microporous material of the contactor. In a preferred embodiment, an effective amount of thermal mass is incorporated into the contactor. The effective amount of thermal mass is an amount sufficient to maintain the thermal rise of the adsorbent during the adsorption step to less than about 100° C. In a preferred embodiment, the amount of thermal mass incorporated into the contactor is an amount sufficient to maintain the thermal rise of the adsorbent during the adsorption step to less than about 50° C., and more preferably to less than about 10° C. 
     Open mesopore and macropore volume includes the volume fraction of all mesopores and macropores that are not filled with a blocking agent, and that are non-selective and thus are capable of being occupied essentially by all components of the gas mixture. Non-limiting examples of blocking agents that can be used in the practice of the present invention include polymers, microporous materials, solid hydrocarbons, and liquids that can fill the open mesopore and macropore space but still allow molecules to transport into the micropores in the selective adsorbent. When the blocking agent is a polymer or liquid, it is preferred that the molecular size of the blocking agent be large enough so that is does not significantly invade micropores of the adsorbent, but not so large that it does not fill the mesopores and macropores. When solid blocking agents are used the particle size of the solid is greater than any selective micropores in the adsorbent but smaller than the mesopores and macropores. As such the blocking agent can fit into the mesopores and macropores without significantly occluding or filling micropores which may be present in the adsorbent. 
     The blocking agent fills the open mesopores and macropores of the adsorbent to an extent that the volume fraction of the open mesopores and macropores of the adsorbent meets the aforementioned requirements. Non-limiting examples of polymers that can be used as blocking agents include polyimides, polysulfones, and silicone rubbers. Non-limiting examples of liquids that can be used as blocking agents include amines, aromatics such as 1,3,5 trimethylbenzene and branched saturated hydrocarbons such a heptamethylnonane as well as liquid hydrocarbons having carbon numbers in the about 5 to about 60 range. When a liquid blocking agent is used it is advantageous to saturate, or nearly saturate, the feed gas with the liquid blocking agent. Non-limiting examples of solid blocking agents include hydrocarbons such as waxes and those having carbon numbers in the 10-1000 range. Non-limiting examples of microporous materials that can be used in the practice of the present invention include microporous carbons and zeolites having pore sizes larger than those of the selective structured adsorbent of this invention. An example of an adsorbent formulated with a blocking agent is a silica or alumina bound zeolite layer having about 30% mesopore and macropore volume in the interstices between the zeolite particles that is filled in with a liquid so that substantially all voids are filled with liquid (i.e., the total resulting macroporosity and mesoporosity in the layer is less than about 20%). In some cases, the blocking agent forms a continuous network and the adsorbent is a composite structure with the microporous material embedded within the blocking agent. A non-limiting example of such a structure is a zeolite/polymer composite where the polymer is continuous and the composite has less than about 20 volume % in open mesopores or macropores. 
     It is also possible to formulate the adsorbent using a mesoporous material that fills the macropores to reduce the overall void, or open, volume. An example of such a structure would be an adsorbent having about 30 volume % of macropores that are filled in with a mesoporous sol gel so that the resulting mesopore and macropore volume is less than about 20%. 
     The channels, also sometimes referred to as “flow channels” or “gas flow channels” are paths in the contactor that allow gas flow through. Generally, flow channels provide for relatively low fluid resistance coupled with relatively high surface area. Flow channel length should be sufficient to provide the mass transfer zone which is at least, a function of the fluid velocity, and the surface area to channel volume ratio. The channels are preferably configured to minimize pressure drop in the channels. In many embodiments, a fluid flow fraction entering a channel at the first end of the contactor does not communicate with any other fluid fraction entering another channel at the first end until the fractions recombine after exiting at the second end. It is important that there be channel uniformity to ensure that substantially all of the channels are being fully utilized, and that the mass transfer zone is substantially equally contained. Both productivity and gas purity will suffer if there is excessive channel inconsistency. If one flow channel is larger than an adjacent flow channel, premature product break through may occur, which leads to a reduction in the purity of the product gas to unacceptable purity levels. Moreover, devices operating at cycle frequencies greater than about 50 cycles per minute (cpm) require greater flow channel uniformity and less pressure drop than those operating at lower cycles per minute. Further, if too much pressure drop occurs across the bed, then higher cycle frequencies, such as on the order of greater than 100 cpm, are not readily achieved. 
     The dimensions and geometric shapes of the parallel channel contactors of the present invention can be any dimension or geometric shape that is suitable for use in swing adsorption process equipment. Non-limiting examples of geometric shapes include various shaped monoliths having a plurality of substantially parallel channels extending from one end of the monolith to the other; a plurality of tubular members; stacked layers of adsorbent sheets with and without spacers between each sheet; multi-layered spiral rolls, bundles of hollow fibers, as well as bundles of substantially parallel solid fibers. The adsorbent can be coated onto these geometric shapes or the shapes can, in many instances, be formed directly from the adsorbent material plus suitable binder. An example of a geometric shape formed directly from the adsorbent/binder would be the extrusion of a zeolite/polymer composite into a monolith. Another example of a geometric shape formed directly from the adsorbent would be extruded or spun hollow fibers made from a zeolite/polymer composite. An example of a geometric shape that is coated with the adsorbent would be a thin flat steel sheet that is coated with a microporous, low mesopore, adsorbent film, such as a zeolite film. The directly formed or coated adsorbent layer can be itself structured into multiple layers or the same or different adsorbent materials. Multi-layered adsorbent sheet structures are taught in United States Patent Application Publication No. 2006/0169142, which is incorporated herein by reference. 
     The dimensions of the flow channels can be computed from considerations of pressure drop along the flow channel. It is preferred that the flow channels have a channel gap from about 5 to about 1,000 microns, preferably from about 50 to about 250 microns. As utilized herein, the “channel gap” of a flow channel is defined as the length of a line across the minimum dimension of the flow channel as viewed orthogonal to the flow path. For instance, if the flow channel is circular in cross-section, then the channel gap is the internal diameter of the circle. However, if the channel gap is rectangular in cross-section, the flow gap is the distance of a line perpendicular to and connecting the two longest sides of the rectangular (i.e., the length of the smallest side of the rectangle). It should also be noted that the flow channels can be of any cross-sectional configuration. Preferred embodiments are wherein the flow channel cross-sectional configuration is either circular, rectangular or square. However, any geometric cross-sectional configuration may be used, such as but not limited to, ellipses, ovals, triangles, or various polygonal shapes. In other preferred embodiments, the ratio of the adsorbent volume to flow channel volume in the adsorbent contactor is from about 0.5:1 to about 100:1, and more preferably from about 1:1 to about 50:1. 
     In some RCPSA applications, the flow channels are formed when adsorbent sheets are laminated together. Typically, adsorbent laminates for RCPSA applications have flow channel lengths from about 0.5 centimeter to about 10 meter, more typically flow channel lengths from about 10 cm to about 1 meter and a channel gap height of about 50 to about 250 microns. The channels may contain a spacer or mesh that acts as a spacer. For laminated adsorbents, spacers can be used which are structures or material, that define a separation between adsorbent laminates. Non-limiting examples of the type of spacers that can be used in the present invention are those comprised of dimensionally accurate: plastic, metal, glass, or carbon mesh; plastic film or metal foil; plastic, metal, glass, ceramic, or carbon fibers and threads; ceramic pillars; plastic, glass, ceramic, or metal spheres, or disks; or combinations thereof. Adsorbent laminates have been used in devices operating at PSA cycle frequencies up to at least about 150 cpm. The flow channel length may be correlated with cycle speed. At lower cycle speeds, such as from about 20 to about 40 cpm, the flow channel length can be as long as or longer than one meter, even up to about 10 meters. For cycle speeds greater than 40 cpm, the flow channel length typically is decreased, and may vary from about 10 cm to about 1 meter. Longer flow channel lengths can be used for slower cycle PSA processes. Rapid cycle TSA processes tend to be slower than rapid cycle PSA processes and as such longer flow channel lengths can also be used with TSA processes. 
     The overall adsorption rate of the swing adsorption processes is characterized by the mass transfer rate from the flow channel into the adsorbent. It is desirable to have the mass transfer rate of the species being removed (i.e., the heavy component) high enough so that most of the volume of the adsorbent is utilized in the process. Since the adsorbent selectively removes the heavy component from the gas stream, inefficient use of the adsorbent layer can lower recovery of the light component and/or decrease the purity of the light product stream. With use of the present invention, it is possible to formulate an adsorbent with a low volume fraction of mesoporous and macroporous such that most of the volume of the adsorbent, which will be in the microporous range, is efficiently used in the adsorption and desorption of the heavy component. One way of doing this is to have an adsorbent of substantially uniform thickness where the thickness of the adsorbent layer is set by the mass transfer coefficients of the heavy component and the time of the adsorption and desorption steps of the process. The thickness uniformity can be assessed from measurements of the thickness of the adsorbent or from the way in which it is fabricated. It is preferred that the uniformity of the adsorbent be such that the standard deviation of its thickness is less than about 25% of the average thickness. More preferably, the standard deviation of the thickness of the adsorbent is less than about 15% of the average thickness. It is even more preferred that the standard deviation of the adsorbent thickness be less than about 5% of the average thickness. 
     Calculation of these mass transfer rate constants is well known to those having ordinary skill in the art and may also be derived by those having ordinary skill in the art from standard testing data. D. M. Ruthven &amp; C. Thaeron, Performance of a Parallel Passage Absorbent Contactor, Separation and Purification Technology 12 (1997) 43-60, which is incorporated herein by reference, clarifies many aspects of how the mass transfer is affected by the thickness of the adsorbent, channel gap and the cycle time of the process. Also, U.S. Pat. No. 6,607,584 to Moreau et al., which is also incorporated by reference, describes the details for calculating these transfer rates and associated coefficients for a given adsorbent and the test standard compositions used for conventional PSA. 
     A figure of merit for the mass transfer through the adsorbent layer is a time constant, τ a , for transport of the heavy component computed at each point in the adsorbent. For a planar adsorbent sheet with thickness in the x direction, and the y and z directions being in the plane of the sheet, the time constant τ a  of the heavy component is
 
τ a   [x,y,z ]=Minimum[ L   path   2   /D   path ](in seconds)
 
where D path  is the average transport diffusion coefficient of the heavy component along a path from the feed channel to the point (x,y,z) and L path  is the distance along the path. There are many possible trajectories or paths from the feed channel to each point (x,y,z) in the adsorbent. The time constant is the minimum of the possible time constants (L path   2 /D path ) along all possible paths from the feed channel to the (x,y,z) point in the adsorbent. This includes paths through mesopores and macropores. If there is a solid material in the adsorbent (such as that which may be included for heat management) there will be no transport within it and (x,y,z) points within it are not included in the computation. The transport diffusion coefficient of each species is taken to be the single component Stefan-Maxwell diffusion coefficient for each species. The average transport diffusion coefficient along the path, D path , is the linearly averaged diffusion coefficient along the path. A linear averaging is sufficient to provide a diffusion coefficient characterizing the path. When the heavy component has many species the diffusion coefficient, D path , is also compositionally averaged. The diffusion coefficient depends on temperature and it may depend on pressure as well. To the extent that the diffusion coefficient changes, it must be averaged for the temperature and pressure changes occurring during a cycle. For an adsorbent to be efficient, the averaged thickness of the adsorbent layer preferably is chosen such that the time constant for at least half the points (or volume) in the adsorbent that is not a dense solid is less than the cycle time of the process. More preferably, the average thickness of the adsorbent layer is chosen such that the time constant for at least 75% of the points (or volume) in the adsorbent that is not a dense solid is less than the cycle time of the process. Even more preferably the average thickness of the adsorbent layer is chosen such that the time constant for at least 75% of the points (or volume) in the adsorbent that is not a dense solid is less than about 25% of the cycle time of the process.
 
     The present invention can be applied to improve the separation of molecular species from synthesis gas. Synthesis gas can be produced by a wide variety of methods, including steam reforming of hydrocarbons, thermal and catalytic partial oxidation of hydrocarbons, and many other processes and combinations known in the art. Synthesis gas is used in a large number of fuel and chemical applications, as well as power applications such as Integrated Gasification Combined Cycle (IGCC). All of these applications have a specification of the exact composition of the syngas required for the process. As produced, synthesis gas contains at least CO and H 2 . Other molecular components in the gas can be CH 4 , CO 2 , H 2 S, H 2 O, and N 2 . Minority (or trace) components in the gas can include hydrocarbons, NH 3  and NOx. In almost all applications most of the H 2 S has to be removed from the syngas before it can be used and in many applications it is desirable to remove much of the CO 2 . In applications where the syngas is used as a feedstock for a chemical synthesis process, it is generally desirable to adjust the H 2 /CO ratio to a value that is optimum for the process. In certain fuel applications, a water-gas shift reaction may be employed to shift the syngas almost entirely to H 2  and CO 2 , and in many such applications it is desirable to remove the CO 2 . 
     The present invention provides a method for increasing the recovery of the valuable molecular components from synthesis gas. In most applications valuable components are CO and H 2 . When multiple species are removed from the synthesis gas, individual contactors, each optimized for the removal of a particular component, can be used. Multiple contactors can be used because the invention provides a means of rapidly changing the pressure in the contactor allowing for rapid cycle operation and consequentially small equipment size. Alternatively several different adsorbents can be incorporated into a single contactor. This provides a means of selectively removing several species with a single contactor. 
     It can be desirable to recover separated acid gases, such as H 2 S and/or CO 2 , at higher pressure. The recovery of higher pressure acid gases can be desirable, for example, when CO 2  sequestration is planned. In these cases, adsorption by temperature swing (TSA) can be preferred over pressure swing. The invention provides a means to rapidly change the contactor temperature without experiencing large heat losses, long heat-up and cool-down times, or adsorbate dilution. Temperature swing adsorption can be executed with fixed parallel-channel contactors and associated valves, or by means of a rotary-based parallel-channel contactor following the approach of a Ljungstrom heat exchanger. 
     Rapid TSA cycle operation is facilitated with a parallel channel contactor where the adsorbent is on one surface of a compact heat exchange structure. Heating and cooling would take place in a channel isolated from the adsorbing and desorbing material. In this configuration, a thermal wave can be made to move through the contactor during the adsorption step allowing for better separation of adsorbed components. In some instance a chromatographic like separation can be achieved (with no dilution from a carrier gas). This type of parallel channel contactor arrangement can be extremely energy efficient. Thermal energy used in the swing adsorption process can be readily recovered and reused. Because of the energy efficiency a larger degree of thermal swing can be used. 
     The contactors of the present invention can better be understood with reference to the figures hereof.  FIG. 1  hereof is a representation of a parallel channel contactor of the present invention in the form of a monolith formed directly from a microporous adsorbent plus binder and containing a plurality of parallel flow channels. A wide variety of monolith shapes can be formed directly by extrusion processes. An example of a cylindrical monolith  1  is shown schematically in  FIG. 1  hereof The cylindrical monolith  1  contains a plurality of parallel flow channels  3 . These flow channels  3  can have diameters (channel gap) from about 5 to about 1,000 microns, preferably from about 50 to about 250 microns, as long as all channels of a given contactor have substantially the same size channel gap. The channels can be formed having a variety of shapes including, but not limited to, round, square, triangular, and hexagonal. The space between the channels is occupied by the adsorbent  5 . As shown the channels  3  occupy about 25% of the volume of the monolith and the adsorbent  5  occupies about 75% of the volume of the monolith. The adsorbent  5  can occupy from about 50% to about 98% of the volume of the monolith. The effective thickness of the adsorbent can be defined from the volume fractions occupied by the adsorbent  5  and channel structure as: 
     
       
         
           
             
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               Diameter 
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                   Volume 
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                   Fraction 
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                   Volume 
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     For the monolith of  FIG. 1  hereof the effective thickness of the adsorbent will be about 1.5 times the diameter of the feed channel. When the channel diameter is in a range from about 50 to about 250 microns it is preferred that the thickness of the adsorbent layer, in the case wherein the entire contactor is not comprised of the adsorbent, be in a range from about 25 to about 2,500 microns. For a 50 micron diameter channel, the preferred range of thickness for the adsorbent layer is from about 25 to about 300 microns, more preferred range from about 50 to about 250 microns.  FIG. 2  is a cross-sectional view along the longitudinal axis showing feed channels  3  extending through the length of the monolith with the walls of the flow channels formed entirely from adsorbent  5  plus binder. A schematic diagram enlarging a small cross section of the feed channels  3  and adsorbent layer  5  of  FIG. 2  is shown in  FIG. 3  hereof. The adsorbent layer is comprised of a microporous adsorbent, or polymeric, particles  7 ; solid particles (thermal mass)  9 ; that act as heat sinks, a blocking agent  13  and open mesopores and micropores  11 . As shown, the microporous adsorbent or polymeric particles  7  occupy about 60% of the volume of the adsorbent layer and the particles of thermal mass  9  occupy about 5% of the volume. With this composition, the voidage (flow channels) is about 55% of the volume occupied by the microporous adsorbent or polymeric particles. The volume of the microporous adsorbent  5  or polymeric particles  7  can range from about 25% of the volume of the adsorbent layer to about 98% of the volume of the adsorbent layer. In practice, the volume fraction of solid particles  9  used to control heat will range from about 0% to about 75%, preferably about 5% to about 75%, and more preferably from about 10% to about 60% of the volume of the adsorbent layer. A blocking agent  13  fills the desired amount of space or voids left between particles so that the volume fraction of open mesopores and macropores  11  in the adsorbent layer  5  is less than about 20%. 
     When the monolith is used in a gas separation process that relies on a kinetic separation (predominantly diffusion controlled) it is advantageous for the microporous adsorbent or polymeric particles  7  to be substantially the same size. It is preferred that the standard deviation of the volume of the individual microporous adsorbent or polymeric particles  7  be less than 100% of the average particle volume for kinetically controlled processes. In a more preferred embodiment the standard deviation of the volume of the individual microporous adsorbent or polymeric particles  7  is less than 50% of the average particle volume. The particle size distribution for zeolite adsorbents can be controlled by the method used to synthesize the particles. It is also possible to separate pre-synthesized microporous adsorbent particles by size using methods such as a gravitational settling column. It may also be advantageous to use uniformly sized microporous adsorbent or polymeric particles in equilibrium controlled separations. 
     There are several ways that monoliths can be formed directly from a structured microporous adsorbent. For example, when the microporous adsorbent is a zeolite, the monolith can be prepared by extruding an aqueous mixture containing effective amounts of a solid binder, zeolite and adsorbent, solid heat control particles, and polymer. The solid binder can be colloidal sized silica or alumina that is used to bind the zeolite and solid heat control particles together. The effective amount of solid binder will typically range from about 0.5 to about 50% of the volume of the zeolite and solid heat control particles used in the mixture. If desired, silica binder materials can be converted in a post processing step to zeolites using hydrothermal synthesis techniques and, as such, they are not always present in a finished monolith. A polymer is optionally added to the mixture for rheology control and to give green extrudate strength. The extruded monolith is cured by firing it in a kiln where the water evaporates and the polymer burns away, thereby resulting in a monolith of desired composition. After curing the monolith, the adsorbent layer  5  will have about 20 to about 40 vol. % mesopores and macropores. A predetermined amount of these pores can be filled with a blocking agent  13 , as previously discussed, in a subsequent step such as by vacuum impregnation. 
     Another method by which a monolith can be formed directly from a microporous adsorbent is by extruding a polymer and microporous adsorbent mixture. Preferred microporous adsorbents for use in extrusion process are carbon molecular sieves and zeolites. Non-limiting examples of polymers suitable for the extrusion process include epoxies, thermoplastics, and curable polymers such as silicone rubbers that can be extruded without an added solvent. When these polymers are used in the extrusion process, the resulting product will preferably have a low volume fraction of mesopores and macropores in the adsorbent layer. 
       FIG. 4  hereof is a representation of a parallel channel contactor  101  of the present invention in the form of a coated monolith where an adsorbent layer is coated onto the walls of the flow channels of a preformed monolith. For the parallel channel contactors of this Figure, an extrusion process is used to form a monolith from a suitable non-adsorbent solid material, preferably a metal such as steel, a ceramic such as cordierite, or a carbon material. By the term “non-adsorbent solid material” we mean a solid material that is not to be used as the selective adsorbent for the parallel channel contactor. An effective amount and thickness of a ceramic or metallic glaze, or sol gel coating,  119  is preferably applied to effectively seal the channel walls of the monolith. Such glazes can be applied by slurry coating the channel walls, by any suitable conventional means, followed by firing the monolith in a kiln. 
     Another approach is to apply a sol gel to the channel walls followed by firing under conditions that density the coating. It is also possible to use vacuum and pressure impregnation techniques to apply the glaze or sol gel to the channel walls. In such a case, the glaze or sol gel will penetrate into the pore structure of the monolith  117 . In all cases, the glaze seals the wall of the channel such that gas flowing thorough the channel is not readily transmitted into the body of the monolith. An adsorbent layer  105  is then uniformly applied onto the sealed walls of the channels. The adsorbent layer  105  reduces the opening, or bore, of the channels, thus the flow channel  103  used in swing adsorption processes is the open channel left inside of the coating. These flow channels  103  can have channel gaps as previously defined. The adsorbent layer  105  can be applied as a coating, or layer, on the walls of the flow channels by any suitable method. Non-limiting examples of such methods include fluid phase coating techniques, such as slurry coating, slip coating, hydrothermal film formation, hydrothermal coating conversion, and hydrothermal growth. When non-hydrothermal coating techniques are used, the coating solutions should include at least the microporous adsorbent or polymeric particles, a viscosifying agent such as polyvinyl alcohol, heat transfer (thermal mass) solids, and optionally a binder. The heat transfer solid may not be needed because the body of the monolith  101  can act to as its own heat transfer solid by storing and releasing heat in the different steps of the separation process cycle. In such a case, the heat diffuses through the adsorbent layer  105  and into the body of the monolith  101 . If a viscosifying agent, such as polyvinyl alcohol, is used it is usually burns away when the coating is cured in a kiln. It can be advantageous to employ a binder such as colloidal silica or alumina to increase the mechanical strength of the fired coating. Mesopores or macropores will typically occupy from about 20 to about 40% of the volume of the cured coating. An effective amount of blocking agent is applied to complete the adsorbent layer for use. By effective amount of blocking agent we mean that amount needed to occupy enough of the mesopores and macropores such that the resulting coating contains less than about 20% of its pore volume in open mesopores and macropores. 
     If a hydrothermal film formation method is employed, the coating techniques used can be very similar to the way in which zeolite membranes are prepared. An example of a method for growing a zeolite layer is taught in U.S. Pat. No. 7,049,259, which is incorporated herein by reference. Zeolite layers grown by hydrothermal synthesis on supports often have cracks and grain boundaries that are mesopore and macropore in size. The volume of these pores is often less than about 10 volume % of the film thickness and there is often a characteristic distance, or gap, between cracks. Thus, as-grown films can often be used directly as an adsorbent layer without the need for a blocking agent. Examples of crack and grain boundaries in as-grown zeolite films are shown in high resolution scanning electron micrographs  FIGS. 5 and 6  hereof. The zeolite film of  FIG. 5  is comprised of Sigma-1 zeolite which has a framework structure that is isotypic with DDR. The film is about 25 micrometers thick with cracks  151  that are about 100 to about 300 angstrom wide, which cracks are readily visible on the surface of the film. The zeolite film in  FIG. 6  is an MFI film that was produced by coating a first coating layer approximately 0.5 micrometers thick using colloidal ZSM-5 seeds onto a support and then placing the seed covered support in a hydrothermal synthesis solution. The colloidal ZSM-5 seeds nucleated the growth of a MFI film about 15 micrometers thick in the hydrothermal synthesis step. The Si/Al ratio of the deposited film was greater than about 100. Cracks of several hundred angstrom size  153  and gaps  155  between the MFI zeolite crystals are apparent in the micrograph. Besides the cracks and gaps there are grain boundaries between crystals. These grain boundaries can connect to the crack structure and aid in transport of molecules to the zeolite crystals that are deeper in the film. Many of the grain boundaries have dimensions in the micropore range and some have dimensions in the mesopore range. It is apparent from the micrographs of  FIGS. 5 and 6  that the open mesopores and macropores occupy a very small amount of the volume at the surface of the film. Cross sectional images of these films confirmed that the open mesopores and macropores in fact do occupy less than about 7% of the volume of the films. 
       FIG. 7  hereof is a representation of a parallel channel contactor of the present invention in the form of a coated monolith  201  for TSA applications where the adsorbent layer is coated onto the channel of a preformed monolith comprised of non-adsorbent material. When TSA or RCTSA processes are performed the contactor will preferably have paths, or separate channels, that can be used to heat and cool the adsorbent. For TSA or RCTSA processes, the parallel channel contactor can be configured in a configuration similar to a shell and tube heat exchanger with the adsorbent coated on the tube walls of the heat exchanger. In this Figure, an extrusion process is used to form a monolith from a suitable non-adsorbent material including a metal such as steel, or a ceramic such as cordierite, or a carbon. A ceramic or metallic glaze or sol gel coating  219  is applied to seal the channel walls of the monolith. As previously mentioned, such glazes can be applied by slurry coating the channel walls followed by curing by firing. A sol gel can also be applied to the channel walls and then fired under conditions that densify the coating. As previously mentioned, it is also possible to use vacuum and pressure impregnation techniques to apply the glaze or sol gel. In this case the glaze or sol gel will penetrate into the pore structure of the monolith  217 . In all cases the glaze seals the wall of the channel such that gas flowing thorough the channel is not readily transmitted into the body of the monolith. It may also be desirable to impregnate the pore structure of the monolith  217  with a solid material before the channel walls are sealed. Alternate rows of channels are sealed at their ends  215  in order to provide for TSA operation. At the opposite end of the monolith these same rows of channels are also sealed. Slots ( 223  and  225 ) are cut through the monolith at both ends to provide flow access to the sealed rows of channels  215 . Sealing surfaces  219  are provided at both ends of the monolith as well as in the middle of the monolith  221 . In operation, the monolith will be mounted in a module in a manner that seals the ends of the channels as well as the middle of the monolith. Any suitable technology can be used to seal the ends of the channels including metallic welds, gasketing with materials such as rubbers or carbons, and the use of adhesives such as inorganic cements and epoxies. The module is configured so that a heating or cooling fluid can be flowed through the channels sealed at the ends  215  by introducing it through the slots  223  and removing it through slots  225 . The heating and cooling fluid will undergo heat exchange with fluid flowing through the channels that are open at the end of the module. These modifications to the monolith convert it into a heat exchanger. It will be understood that there are various other ways in which heat exchangers can be produced or configured. Non-limiting examples of such other ways include shell and tube heat exchangers, fiber film heat exchangers and printed circuit heat exchangers, all of which are well known in the art. By coating an adsorbent layer with a low volume fraction of mesopores and macropores on one side of a heat exchanger it can be used in accordance with the present invention. As such, this example illustrates how heat exchangers can be converted into modules suitable for TSA with an adsorbent layer having a low volume fraction of mesopores and macropores. 
     Feed channels  203  can have channel gaps from about 5 to about 1,000 microns, preferably from about 50 to about 250 microns. When the feed channel diameter  203  is in a range from 50 to about 250 microns it is preferred that the thickness of the adsorbent layer  205  be in a range form about 25 to about 2,500 microns. For a 50 micron diameter feed channel  203  the preferred range of thickness for the adsorbent layer is from 25 to 300 microns and a more preferred range is from 50 to 250 microns. The techniques previously discussed above can be used to coat the adsorbent layer into the monolith. 
       FIG. 8  hereof is a schematic of a parallel channel contactor of the present invention in the form of a substantially parallel array of hollow fibers embedded in a matrix material  331 . A wide variety of hollow fibers can be formed directly using conventional spinning and extrusion processes. The contactor of  FIG. 8  is formed from an array of hollow fibers  301 . The bores  303  of the fibers are used as flow channels. These flow channels  303  can also have channel gaps from about 5 to about 1,000 microns, preferably from about 50 to about 250 microns as previously mentioned. Also as previously mentioned, the walls of the fibers contain an adsorbent layer  305 . When the channel gap  303  is in a range from 50 to about 250 microns it is preferred that the thickness of the adsorbent layer  305  be in a range from about 25 to 2,500 microns. 
     Various different methods known in the art can be used to produce the adsorbent layer  305  in the fiber. For example, the hollow polymer fibers with low mesoporosity can be extruded. Some spinning techniques can also be used to produce hollow fibers with mesopores and macropores that can be removed in post treatments such as thermal annealing, polymer coating, epoxy coating or filling with a blocking agent. Hollow fibers that are composites of polymers and adsorbents can be formed in both spinning and extrusion processes. These processes often form the fiber from a dope containing the polymer, adsorbent particles, and often a solvent. In some cases, the surface of the adsorbent particle is functionalized to promote adhesion between the polymer matrix and the adsorbent particle. When the volume fraction of mesopores and macropores is too high, it can be lowered by a post treatment using thermal annealing, or by filling an effective amount of mesopores and macropores with a blocking agent. 
     It is also possible to produce hollow fibers of zeolites by extrusion. In these processes the zeolite is mixed with a polymer or an oligomeric viscosifying agent, such as a lower molecular weight polyvinyl alcohol. Optionally, a solvent such as water, alcohol, or liquid hydrocarbon can be added to the dope. It is also optional to use a binder material, such as colloidal silica or colloidal alumina that can be added to this dope. Solid particles, such as alumina or aluminum can also be added to the dope. The dope is then extruded and from the green state the final ceramic body is produced. This fiber, in the green state, can then be placed into a kiln and fired to form the final fiber comprised of zeolite, and optionally binder and solid particles. Alternatively, the fiber in the green state can be placed in a hydrothermal synthesis reactor to produce a final fiber comprised of zeolite, and optionally binder and solid thermal mass particles. Another method to produce a zeolite fiber is by hydrothermally growing a zeolite coating on a solid polymer fiber that burns away during the calcinations step. In all cases, mesoporosity and macroporosity in the fiber can be reduced to within a target range by filling with a blocking agent in a subsequent step. 
     The fibers can be formed into a substantially parallel array to form a contactor of the present invention. One method to do this is with an embedding or potting process that surrounds the entire length of the fibers with a matrix material  325 . To visualize the array in  FIG. 8  the end of the matrix material  351  has been rendered transparent along with the face  321  of the embedded hollow fiber bundle. In many instances, it can be advantageous to coat the exterior of the fiber with a material that acts as a diffusion barrier  315 . Non-limiting examples of materials that can act as diffusion barriers include sputter deposited metal and ceramic films, evaporated metal and ceramic films, metal and ceramic films formed by chemical vapor deposition, coated composites of polymers and solids (such as clays) and coatings of polymers that have low diffusion coefficients. To act as a diffusion barrier, the effective diffusion coefficient of the coating should be less than about 1/10 the average diffusion coefficient in the adsorbent layer and preferably less than about 1/1000 the average diffusion coefficient in the adsorbent layer. When a diffusion barrier is used, the gas in the feed channel is effectively contained in the feed channel and adsorbent layer. This can eliminate the need for a supporting matrix around the fibers, thus lowering the mass of the contactor, and in some cases allowing for the cycle time in the process to be decreased (i.e., rapid cycle operation). 
     Another fabrication method suitable for use herein is to coat the adsorbent inside the prefabricated fiber such as a hollow glass fiber, hollow silica fiber or hollow polymer fiber. Coating methods previously described can be used to form an adsorbent layer inside of a prefabricated fiber. When the prefabricated fiber is made from glass, or silica, the final product has a built in diffusion barrier  315 . 
     When there is no diffusion barrier on the fiber it is advantageous for the matrix material to contain an adsorbent having a low volume fraction of mesopores and macropores. In this case, it is advantageous to space the fibers closely together with the distance between adjacent fibers less than about 5 fiber diameters, preferably less than about 1.5 fiber diameters. When there is a diffusion barrier on the outer surface of the fibers, it can be advantageous to embed only the ends  351  and  353  of the fiber bundle in the matrix material. In this case, the matrix material only has to support the fibers and not have substantial gas flow through the material. It can be composed of polymer, metal or ceramic or combinations thereof. It is preferred that the matrix be nonporous and requirements for having an adsorbent in the matrix material can be relaxed or eliminated. Requirements for spacing between fibers can be less critical than when the entire length of the fiber is potted or embedded. The matrix material can be applied selectively to the ends of the fiber bundles by any suitable method known in the art. Non-limiting examples of such methods include potting, embedding, casting, electroplating, or electroless plating processes. To avoid plugging the end of the fibers the end of the fibers can be filled with a material that can be readily removed after the matrix is applied. Non-limiting examples of materials that can be readily removed include polymers, metals, salts and inorganics that can be selectively dissolved or etched away after the matrix material has been applied. Grinding, machining and polishing methods can also be used to open the ends of the fibers. Other methods to pot or embed the ends of the fibers are similar to those used to form hollow fiber membrane modules. When the ends of the fiber bundle are potted with a matrix material it is advantageous to place the contactor into an operational PSA, RCPSA, RCPPSA or PPSA module in a manner such that most of the feed gas flows through the bore of the fiber. One way to ensure that the flow goes through the bore of the fiber is to place a fiberous packing, or inram, between the matrix material at the ends  351  and  353  and the interior of the PSA, RCPSA, RCPPSA or PPSA module. Another way is to bond the ends of the contactor to the interior of the pressure swing adsorption module. 
       FIGS. 9 and 10  hereof are representations of a parallel channel contactor of the present invention in the form of a hollow fiber contactor for a TSA process where the adsorbent layer  405  comprises part of the wall of the fiber with a center feed channel  403 . In  FIG. 10 , the outer surfaces of the housing for the contactor  401  are rendered transparent with only dotted lines indicating the edges of the outer surface. The hollow fibers used in this example have a diffusion barrier  415  on their exterior surface and can be manufactured using techniques described for  FIG. 4  hereof. The ends of the fiber bundle are potted or embedded in a matrix material  417 . This potted array is then sealed into a tubular housing  401 . Sealing surfaces  419  are provided at the ends of the tubular housing  401 . A sealing surface  421  is also provided in the middle of the housing. Slots  423  and  425  are cut through the wall near the ends of the tubular housing to allow for the flow of heating and cooling fluids. 
     In operation, the tubular housing is mounted in a TSA or RCTSA module in a manner that seals the ends of the channels as well as the middle of the monolith. Any suitable sealing technology can be used. Non-limiting examples of sealing technologies that can be used in the practice of the present invention include metallic welds, gasketing with materials such as rubbers or carbons, and the use of adhesives such as inorganic cements or epoxies. The module is configured so that a heating or cooling fluid can be flowed inside the hollow tubular housing  401  by introducing it through slots  423  and removing it through slots  425 . The heating and cooling fluid will undergo heat exchange with fluid flowing through the hollow fibers which are open at the end of the module. With these sealing arrangements, the tubular housing  401  containing the parallel array of hollow fibers becomes a heat exchanger suitable for use in TSA processes. The fibers have an adsorbent layer  405  with a low volume fraction of mesopores and macropores. 
       FIG. 11  hereof is a representation of a parallel channel contactor of the present invention in which the parallel channels are formed from laminated sheets containing adsorbent material. Laminates, laminates of sheets, or laminates of corrugated sheets can be used in PSA RCPSA, PPSA or RCPPSA processes. Laminates of sheets are known in the art and are disclosed in US Patent Applications US20060169142 A1 and U.S. Pat. No. 7,094,275 B2 which are incorporated herein by reference. When the adsorbent is coated onto a geometric structure or components of a geometric structure that are laminated together, the adsorbent can be applied using any suitable liquid phase coating techniques. Non-limiting examples of liquid phase coating techniques that can be used in the practice of the present invention include slurry coating, dip coating, slip coating, spin coating, hydrothermal film formation and hydrothermal growth. When the geometric structure is formed from a laminate, the laminate can be formed from any material to which the adsorbent of the present invention can be coated. The coating can be done before or after the material is laminated. In all these cases the adsorbent is coated onto a material that is used for the geometric shape of the contactor. Non-limiting examples of such materials include glass fibers, milled glass fiber, glass fiber cloth, fiber glass, fiber glass scrim, ceramic fibers, metallic woven wire mesh, expanded metal, embossed metal, surface-treated materials, including surface-treated metals, metal foil, metal mesh, carbon-fiber, cellulosic materials, polymeric materials, hollow fibers, metal foils, heat exchange surfaces, and combinations of these materials. Coated supports typically have two major opposing surfaces, and one or both of these surfaces can be coated with the adsorbent material. When the coated support is comprised of hollow fibers, the coating extends around the circumference of the fiber. Further support sheets may be individual, presized sheets, or they may be made of a continuous sheet of material. The thickness of the substrate, plus applied adsorbent or other materials (such as desiccant, catalyst, etc.), typically ranges from about 10 micrometers to about 2000 micrometers, more typically from about 150 micrometers to about 300 micrometers. 
     Metallic mesh supports can provide desirable thermal properties of high heat capacity and conductivity which “isothermalize” a PSA, RCPSA, PPSA or RCPPSA cycle to reduce temperature variations that degrade the process when conducted under more adiabatic conditions. Also, metal foils are manufactured with highly accurate thickness dimensional control. The metal foil may be composed of, without limitation, aluminum, steel, nickel, stainless steel or alloys thereof. Hence there is a need for a method to coat metal foils with a thin adsorbent layer of accurately controlled thickness, with necessary good adhesion. One method for doing this is by hydrothermal synthesis. Coating procedures used can be very similar to the way in which zeolite membranes are prepared as discussed above. Zeolite layers grown by hydrothermal synthesis on supports often have cracks which are mesopores and micropores. Examples of these cracks have been shown in  FIGS. 5 and 6  hereof. The volume of these pores is often less than about 10 volume % of the film thickness and there is often a characteristic distance between cracks. Another method of coating a metal foil is with thick film coating is slip casting, or doctor blading. An aqueous slurry of prefabricated zeolite particles, binder (for example colloidal silica or alumina), viscosifying agent such as a polymer like polyvinyl alcohol is cast for example onto a metal foil and fired to remove the polymer and cure the binder and zeolite. The product, after firing, is then a bound zeolite film on a metal foil typically containing about 30 to about 40 volume % voids. To make a suitable adsorbent layer, the voids are filled in a subsequent step by coating the bound zeolite film with a polymer or by introducing a liquid into the voids of the bound zeolite film. The final product, after filling the voids with a polymer or liquid, will be an adsorbent layer having the low mesoporosity and macroporosity requirements of the present invention. 
     Another method for coating metal foils with prefabricated zeolite crystals, or microporous particles, is electrophoretic deposition (EPD). EPD is a technique for applying high quality coatings of uniform thickness to metal substrates. The method can be used to apply organic and inorganic particulate coatings on electrically conductive substrates. Slurry compositions containing prefabricated zeolites, or microporous particles, may be electrophoretically applied to a rigid support material, such as by using the method described in Bowie Keefer et al.&#39;s prior Canadian patent application No. 2,306,311, entitled “Adsorbent Laminate Structure,” which is incorporated herein by reference. 
     Some contactor geometric shapes will require that the adsorbent be applied to the channel surface in a layer using a colloidal binder material or that an entire geometric shape be comprised of the adsorbent plus colloidal binder and containing a plurality of parallel channels. When a colloidal binder is used, the selection of the colloidal material depends on the particular adsorbent used. Colloidal materials capable of functioning as a binder and/or which form a gel are preferred. Such colloidal materials include, without limitation, colloidal silica-based binders, colloidal alumina, colloidal zirconia, and mixtures of colloidal materials. “Colloidal silica” refers to a stable dispersion of discrete amorphous silicon dioxide particles having a particle size ranging from about 1 to about 100 nanometers. Suitable colloidal silica materials also can be surface modified, such as by surface modification with alumina. Another type of colloidal binder suitable for use herein include clay materials, such as palygorskite (also known as attapulgite), which are hydrated magnesium aluminum silicates. Also, inorganic binders may be inert; however, certain inorganic binders, such as clays, used with zeolite adsorbents may be converted in-situ from kaolin binders to zeolite so that the zeolite is self-bound with minimal inert material. In these bound structures, the voids between the colloidal particles form mesopores and the voids between the adsorbent particles form mesopores and/or macropores. A blocking agent can be applied to fill the majority of the mesoporosity and macroporosity in these bound layers so that the adsorbent meets the open pore volume requirement of this invention. Organic binders used to bind activated carbon particulates in laminated structures may be pyrolyzed to form a useful carbonaceous adsorbent. 
       FIG. 11  hereof illustrates an exploded view of an embodiment of the present invention wherein a microporous adsorbent film  505 , preferably comprising DDR, is hydrothermally grown on each of both faces of flat metal foils  509 , which is preferably fabricated from a corrosion resistant metal such as stainless steel. The separate metal foils  509  with the adsorbent films  505  are fabricated to form a parallel channel contactor  501 . Spacers of appropriate size may placed between the metal foils during contactor fabrication so that the channel gap  503  is of a predetermined size. Preferably about half of the volume of the feed channels  503  are filled with a spacer that keeps the sheets substantially evenly spaced apart. 
     The heat capacity of the metal foils  509  limits the thermal excursions in the process. When CO 2  is adsorbed in the adsorbent, heat is released in the amount of the heat of adsorption. This warms the adsorbent films and as the film warms, its temperature rises above that of the metal foils and heat diffuses into the metal foil where it is stored. Desorption of CO 2  from the adsorbent is an endothermic process and heat must be supplied in an amount equal to the heat of adsorption. When CO 2  desorbs, the temperature of the films falls below that of the metal foils and heat stored in the metal foils flows into the films. The thermal excursion of the adsorbent film is less than +/−10° C. with the contactor dimensions and the process as described in Example 1. 
     The adsorbent film is composed of individual adsorbent crystals, mesopores (including grain boundaries) and macropores. In this example, the crystals in the film are substantially of the same size. Most of the open volume in the film is comprised of mesoporous cracks with characteristic widths of about 200 angstroms. These mesoporous cracks are substantially evenly distributed throughout the film. The total volume of the mesopores and macropores is about 5 vol. % of the total volume of the adsorbent film. 
     The present invention can better be understood with reference to the following examples that are presented for illustrative purposes and not to be taken as limiting the invention. 
     EXAMPLE 1 
     With a laminated sheet parallel channel contactor described for  FIG. 11  hereof, a PSA/RCPSA cycle with five steps is operated to produce a product stream containing about 20 vol. % CO 2  and about 80 vol. % CH 4 . Overall methane recovery for the PSA/RCPSA cycle is computed to be about 95 vol. %.  FIG. 12  hereof is a schematic diagram of five different steps in a preferred PSA/RCPSA cycle suitable for use in this invention. In the first step  611  a parallel channel contactor PSA/RCPSA cycle is pressurized with high pressure product gas  625 . This pressurization raises the pressure in the parallel channel contactor and fills the contactor with the purified product containing about 20 vol. % CO 2  and about 80 vol. % CH 4 . In a second step  621  a high pressure  51  atmosphere (atm) feed gas  671  is conducted through the parallel channel contactor. During this step  621  the DDR adsorbent layer adsorbs CO 2  from the flowing feed gas  671 . A purified product  625  flows out of the end of the contactor. The feed gas  671  is flowed at a rate such that as the product  625  emerges from the parallel channel contactor as a concentration front moves through the contactor. Ahead of the front the gas has a composition near that of the product  625 . Behind the front the gas has a composition near that of the feed  671 . The second step  621  is stopped before this front completely breaks-through the end of the contactor. The amount of feed which emerges from the contactor before this step is halted determines in part the product purity. 
     At this point, a third step of the cycle  631  is initiated which serves to purge the contactor of feed gas trapped in the contactor channels. The third step  631  also acts, in part, as a partial pressure displacement purge of the contactor. Valves are opened at the top and bottom of the contactor. A pressurized CO 2  rich stream  633  flows into the top of the module and gas originally contained in the flow channel  503  of the structured parallel channel contactor flows out  639 . The gas fed into the top of the module  633  is a CO 2 -rich gas produced in later steps  4  and  5  that has been compressed  675  to a pressure slightly greater than the feed pressure (51 atm.). The composition of the gas fed through the top of the contactor is substantially equal to that of the CO 2  reject stream  681 , containing 97.5 vol. % CO 2  and 2.5 vol. % CH 4 . The gas exiting out the bottom of the contactor has a composition nearer to that of the feed gas  671  (70 vol. % CO 2  and 30 vol. % CH 4 ). 
     As the gas stream entering the module  633  displaces the gas in the flow channels, a compositional front moves from top to bottom of the module. The third step  631  is stopped and a fourth step  641  is begun before, or shortly after, this front breaks through the bottom of the module. The fourth step  641  lets the pressure of the contactor down to an intermediate pressure and recovers some of the CO 2  for recompression. In the design discussed in this example, the intermediate pressure is about 22 atm. In the fourth step, a CO 2 -rich stream  649  exits the module at a pressure of about 22 atm. This stream is split into two streams  679  and  681 . Stream  679  is fed to compressor  675  and stream  681  is rejected from the process at a pressure of about 22 atm. Stream  633  that was used to rinse the contactor in the third step of the process  631 , is comprised of the gas stream  679  that emerges from compressor  675 . As the pressure in the contactor drops towards the outlet pressure of about 22 atm., the flow in streams  679  and  681  decreases. When the flow in these streams has fallen to approximately ¼ of the initial value step  4  is stopped and a step  5  is begun. In the fifth step of the process  651 , the module pressure is dropped to about 5 atm. and a CO 2 -rich stream is recovered  685 . This stream  685  can optionally be fed through a compressor  677  that raises the stream pressure to about 22 atm. The stream is then combined with stream  681  and a CO 2 -rich stream  683  is rejected from the process at a pressure of about 22 atmospheres. 
     To improve the operation of the process, as well as the pressure at which CO 2  is recovered, gas may be recovered in the fifth step  651  using a multi-step process in which the contactor pressure is decreased in a series of pressure equalization steps. Gas from these pressure equalization steps can be recovered as individual gas streams and recompressed. In an example with two pressure equalization steps, one portion of the CO 2 -rich gas is recovered at a pressure of about 12 atmospheres while the rest is recovered at about 5 atmospheres. 
     It is also possible to decrease the module pressure in step four  641  using a series of pressure equalization steps. Again, each pressure equalization step can be used to form a gas stream that can either be rejected from the process in stream  683  or recompressed to form stream  633 . If pressure equalization steps are employed, it is advantageous to design them to maximize the pressure at which the CO 2  reject streams are captured. 
     Modeling used to predict the performance of the parallel channel contactor uses isotherms for CO 2  and CH 4  that were measured with well known gravimetric uptake methods, PVT (pressure, volume, temperature) methods, and with analysis of single component gas transport data in DDR membranes. A statistical isotherm shape was found to best describe the single component isotherms for CO 2  and CH 4 . The best fits to the measured isotherms for CO 2  and CH 4  give saturation capacities of 6 and 5 molecules per cage, respectively, in the DDR zeolite framework. These values correspond to a maximum loading of 5 milli-moles/gram (of DDR) for CO 2  and 4.16 milli-moles/gram (of DDR) for CH 4 . These saturation capacities are consistent with the physical expectation that the maximum possible loading would correspond to CO 2  and CH 4  filling the pores at a liquid density. A single parameter K, that is analogous to the Henry&#39;s constant in a Langmuir isotherm, describes the shape of the statistical isotherm. The K values used for modeling are: 
               K     CO   2       =     1.93   ×     10     -   10       ⁢     ⅇ       25   ×     10   3     ⁢           ⁢     Joule   Mole       RT       ⁢           ⁢     (     in   ⁢           ⁢     pascals     -   1         )                     K     CH   4       =     4.25   ×     10     -   10       ⁢     ⅇ       17.8   ×     10   3     ⁢           ⁢     Joule   Mole       RT       ⁢           ⁢     (     in   ⁢           ⁢     pascals     -   1         )             
where R is the molar gas constant and T is the temperature in Kelvin.
 
     Over a wide range of conditions (less than about 50% of saturation capacity loading), the shape of the statistical and Langmuir isotherms are very similar. For simple modeling of the process given in this example, the statistical isotherm can be supplanted by an equivalent Langmuir isotherm. For modeling competitive adsorption effects, competitive adsorption isotherms can be derived from the single component statistical isotherms using well known techniques. 
     The single component Stefan-Maxwell transport diffusion coefficients for CO 2  and CH 4  used in the modeling hereof were: 
               D     CO   2       =     5.70   ×     10     -   10       ⁢     ⅇ     -       7.4   ×     10   3     ⁢           ⁢     Joule   Mole       RT         ⁢           ⁢     (     in   ⁢           ⁢     m   2     ⁢     /     ⁢   sec     )                     D     CH   4       =     0.48   ×     10     -   10       ⁢     ⅇ     -       13.4   ×     10   3     ⁢           ⁢     Joule   Mole       RT         ⁢           ⁢     (     in   ⁢           ⁢     m   2     ⁢     /     ⁢   sec     )             
where R is the molar gas constant and T is the temperature in Kelvin.
 
     It is seen that there is a large difference in the diffusion coefficients of CO 2  and CH 4  and a smaller difference in the isotherms when these transport parameters are evaluated at a given temperature. From a 50/50 molar mixture of CO 2  and CH 4  the isotherms slightly favor CO 2  adsorption and dramatically favor the diffusional transport of CO 2  into the DDR crystals. By controlling the time scale of the adsorption step  621  and the purge displacement step  631 , it is possible to take advantage of this difference in diffusion coefficients and improve the selectivity of the process. By controlling these time steps, a kinetic separation of CO 2  and CH 4  can be achieved that takes advantage of differences in diffusivity of these molecules. The class of 8-ring zeolites preferred for the removal of CO 2  from natural gas will have a large difference in CO 2  and CH 4  diffusion coefficients. This example illustrates a particular RCPSA cycle that can be tuned to achieve a kinetic separation of CO 2  and CH 4 , however, other swing adsorption cycles are possible. A parameter that can be used to evaluate the ability of a given material to produce a kinetic separation is the ratio of diffusion coefficients for the components that are to be separated and the diffusion coefficients are evaluated at the temperature and pressure of the intended process, 
     
       
         
           
             κ 
             = 
             
               
                 D 
                 
                   CO 
                   2 
                 
               
               
                 D 
                 
                   CH 
                   4 
                 
               
             
           
         
       
     
     It is preferred that the material be chosen to have a value of κ for CO 2  and methane separation greater than 10 at the operating temperature. More preferably the material is chosen to have a value of κ greater than 25 at the operating temperature. More preferably the material is chosen to have a value of κ greater than 50 at the operating temperature. 
     In order to take advantage of the intrinsic kinetic selectivity of the preferred class of 8-ring zeolite materials for removal of CO 2  from natural gas, the crystals forming the contactor must be of substantially the same size. If they have widely different sizes, some will substantially fill with CH 4  during the adsorption step  621 , resulting in increased methane loss during the desorption step  651 . It is therefore preferred that the standard deviation of the volume of the individual crystallites in the DDR film forming the adsorbent layer  505  (as seen in  FIG. 11 ) be less than 100% of the volume of an average crystallite in order to increase methane recovery in the process. In a more preferred embodiment, the standard deviation of the volume of the crystallites in the DDR film forming the adsorbent layer  505  is less than 50% of the volume of an average crystallite. In the most preferred embodiment, the standard deviation of the volume of the crystallites in the DDR film forming the adsorbent layer  505  is less than 10% of the volume of an average crystallite. The most preferred embodiment was chosen to model the PSA cycle described in this example. 
     With this type of adsorbent, the time for steps  621  and  631  is set by the average crystal size in the adsorbent. It is preferred that the time step be chosen so that adsorbed CO 2  in the DDR has time to equilibrate with gaseous CO 2  in the feed channel  503  but the methane does not have time to equilibrate. The time for CO 2  to achieve 90% approach to equilibrium (following a change in surface concentration) within a single DDR crystal that has rapid diffusion path to the gas in the contactor is;
 
τ 90 =0.183 r   2   /D   CO2  
 
where r is the average DDR crystal radius and D CO2  is the diffusion coefficient of CO 2  at the operating temperature. It is preferred that the time for steps  621  and  631  be in a range from 0.5τ 90  go to 10τ 90  and it is more preferred that the time for steps  621  and  631  be in a range from 1τ 90  go to 5τ 90 . For modeling, a time step of 1.5τ 90  was chosen for steps  621  and  631 . The numerical value of the time step is then set by the crystal size. It is preferred that the average DDR crystal size be in a range from about 0.005 μm to about 100 μm. It is more preferred that the average DDR crystal size be in a range from about 0.5 μm to about 50 μm and it is most preferred that the average DDR crystal size be in a range from about 1 μm to about 10 μm. For modeling an average DDR crystal size of 1 μm was used.
 
     Several different treatments of the molecular transport into and out of the adsorbent layer were developed and results of the different modeling approximations were compared. The most exact treatment solved the time dependent fundamental multi-component transport equations into and out of the DDR zeolite layer at all points along the feed channel for every time step in the process. For this model the DDR film was idealized as fins along the side of the channel with 200 angstrom gaps between the fins. The mesopores formed by these 200 angstrom gaps occupied 5% of the volume of the adsorbent layer. On a grid encompassing 500,000 points, the fundamental time dependent transport equations were solved for this geometry. Three pressure equalization steps were used in the blow-down step  651  for process modeling. Pressure equalizations at 15, 10 and 5 atmospheres were employed. It was determined that the thermal excursion in the adsorption step was 10° C. The methane recovery was computed as the ratio of the methane molar flow rate in purified product stream  625  to that in the feed stream  671  entering the process. The model using the most exact treatment of transport showed a 96% methane recovery. The average pressure at which molecules were recovered in streams  681  and  685  was found to be 12.5 atmospheres. 
     This modeling approach provides a much more exact solution than the linear driving force (LDF) models that are conventionally used to model PSA processes. Using knowledge of the most exact solution, a simpler model has been constructed that can readily be used by one skilled in the art to compute methane recoveries. In the adsorption step  621 , the simple model separately treats the equilibration of CO 2  and CH 4  in the feed channel within the DDR crystals forming the adsorbent layer. The amount of CO 2  adsorbed in the DDR crystals is taken to be 80% of the amount that might be expected if the CO 2  adsorbed in the DDR were fully equilibrated with the gaseous feed entering the process  671  at a temperature that is 10° C. higher than the feed temperature. The amount of CH 4  adsorbed in the DDR crystals is 1% of the amount that might be expected if the CH 4  adsorbed in the DDR has fully equilibrated with the gaseous feed entering the process  671  at a temperature that is 10° C. higher than the feed temperature. In the simple model gas filling the mesopores and macropores in the laminate at the end of the adsorption step  621  is not recovered. For the simple model, the CO 2  purge used in step  631  displaces all of the methane left in the feed channel into stream  639 . With these approximations, the methane recovery from the process is predicted to be 95%. This closely agrees with the exact model and the model provides a simple method for one skilled in the art to evaluate the effect of changing the mesopore and macropore volume of the adsorbent. 
     Optionally when the CO 2  reject stream  683  is sequestered it is preferred to capture the CO 2  at a pressure that is more than 1/10 of the partial CO 2  pressure in the feed. In a more preferred embodiment the pressure at which the CO 2  is captured is more than ¼ of the CO 2  partial pressure in the feed. 
     EXAMPLE 2 
     The process of Example 1 is repeated except the feed and product specifications are held constant and the volume fraction of mesopores and macropores in the adsorbent are increased from 5% to 10%. The predicted methane recovery is found to fall from 95% (in Example 1) to 92%. 
     EXAMPLE 3 
     The process of Example 1 is repeated except the feed and product specifications are held constant and the volume fraction of mesopores and macropores in the adsorbent are increased from 5% to 15%. The predicted methane recovery is found to fall from 95% (in Example 1) to 88%. 
     EXAMPLE 4 
     The process of Example 1 is repeated except the feed and product specifications are held constant and the volume fraction of mesopores and macropores in the adsorbent are increased from 5% to 20%. The predicted methane recovery is found to fall from 95% (in Example 1) to 85%. 
     EXAMPLE 5 
     The process of Example 1 is repeated except the feed and product specifications are held constant and the volume fraction of mesopores and macropores in the adsorbent are increased from 5% to 25%. The predicted methane recovery is found to fall from 95% (in Example 1) to 81%. 
     EXAMPLE 6 
     The process of Example 1 is repeated except the feed and product specifications are held constant and the volume fraction of mesopores and macropores in the adsorbent are increased from 5% to 30%. The predicted methane recovery is found to fall from 95% (in Example 1) to 77%. 
     EXAMPLE 7 
     The process of Example 1 is repeated except the feed and product specifications are held constant and the volume fraction of mesopores and macropores in the adsorbent are increased from 5% to 35%. The predicted methane recovery is found to fall from 95% (in Example 1) to 73%. 
     EXAMPLE 8 
     The process of Example 1 is repeated except the feed and product specifications are held constant and the volume fraction of mesopores and macropores in the adsorbent are decreased from 5% to 2.5%. The predicted methane recovery is found to increase from 95% (in Example 1) to 97%. 
     EXAMPLE 9 
     The process of Example 1 is repeated but the feed specification is held constant and purity of methane in the product stream  625  is increased from 80% CH 4 /20% CO 2  to 90% CH 4 /10% CO 2 . This is done by changing the feed flow rates and the degree to which compositional fronts are allowed to break-through before steps  621  and  631  are stopped. With a 5% volume fraction of mesopores and macropores in the adsorbent the predicted methane recovery is 94%. 
     EXAMPLE 10 
     The process of Example 1 is followed but the feed specification is held constant and purity of methane in the product stream  625  is increased from 80% CH 4 /20% CO 2  to 90% CH 4 /10% CO 2 . This is done by changing the feed flow rates and the degree to which compositional fronts are allowed to break-through through before steps  621  and  631  are stopped. With a 10% volume fraction of mesopores and macropores in the adsorbent the predicted methane recovery is 90%. 
     EXAMPLE 11 
     This example illustrates use of a parallel contactor of the present invention in a separation process that produces relatively high pressure products and high methane recoveries from N 2  containing natural gas stream. In processing natural gas, the amount of N 2  that has to be removed depends on the concentration in the field and the way in which the gas is transported to market (i.e., liquefied natural gas vs. pipeline). This example will consider a natural gas stream containing a small amount (&lt;5%) of impurities (for example H 2 O and mercury compounds) other than N 2 . These impurities are removed in initial processing steps using conventional separation techniques. The gas stream fed to the parallel contactor of the present invention has a composition of 70% CH 4  and 30% N 2 . The flowing gas stream is fed to the contactor at a pressure of 100 atmospheres and a temperature of 50° C. 
     The contactor is comprised of laminated flat sheets of the type described above and a schematic diagram of the type of sheet used in the present example is shown in  FIG. 11  hereof. Using the methods described above a 50 μm thick DDR film  505  with an Si/Al ratio greater than 100 is hydrothermally grown on each of both faces of a 100 μm thick flat metal foil  509  (for example stainless steel). The metal foils  509  with the DDR films  505  are laminated together  501  to form a parallel channel contactor. During lamination, spacers are placed between the metal foils so that the channel gap  503  is 50 μm across. Approximately half the volume of the feed channels  503  are filled with spacers that keep the sheets substantially evenly spaced 50 μm apart. 
     The heat capacity of the metal foil  509  limits the thermal excursions in the process. When N 2  is adsorbed in DDR it releases heat in the amount of the heat of adsorption. This warms the DDR film. The DDR film warms to a temperature above that of the metal foil and heat diffuses into the metal foil where it is stored. Desorption of N 2  from DDR is an endothermic process and heat must be supplied in the amount of the heat of the adsorption. When N 2  desorbs the temperature of the DDR film falls below that of the metal foil and heat stored in the foil flows into the DDR film. With the contactor dimensions and the process described in this example, the thermal excursion of the DDR film is expected to be less than +/−5° C. Due to the smaller heat of adsorption for N 2  (compared to CO 2 ) this temperature rise is less than that of the description for Example 1 above. 
     The DDR film is comprised of individual DDR crystals, mesopores (including grain boundaries) and macropores. In this example, the crystals in the DDR film are substantially of the same size. Most of the open volume in the film is comprised of mesoporous cracks with characteristic widths of 200 angstroms. These mesoporous cracks are substantially evenly distributed throughout the film. The total volume of the mesopores and macropores is 2.5% of the total volume of the in the DDR film. 
     Using this parallel channel contactor, a PSA/RCPSA cycle with five different steps is operated to produce product stream containing 2% N 2  and 98% CH 4 . Overall methane recovery for the PSA/RCPSA cycle is computed to be 91%.  FIG. 13  hereof shows a schematic diagram of the five different steps in the PSA/RCPSA cycle. In the first step  711  a parallel channel contactor PSA/RCPSA cycle is pressurized with high pressure product gas  787 . This pressurization raises the pressure in the parallel channel contactor and fills the contactor with the purified product containing 2% N 2  and 98% CH 4 . In a second step  721  a high pressure 100 atm feed gas  771  is flowed through the contactor. During this step  721  the DDR adsorbent layer removes N 2  from the flowing feed gas  771 . A purified product  725  flows out of the end of the contactor. The feed gas  771  is flowed at a rate such that as the product  725  emerges from the contactor a concentration front moves through the contactor. Ahead of the front the gas has a composition near that of the product  725 . Behind the front the gas has a composition near that of the feed  771 . Before this front completely breaks through the end of the contactor the second step  721  is stopped. The amount of feed which emerges from the contactor before this step is halted determines in part the product purity. 
     At this point, a third step of the cycle  731  is initiated which serves to purge the contactor of feed gas trapped in the contactor channels. The third step  731  also acts in part as a partial pressure displacement purge of the contactor. Valves are opened at the top and bottom of the contactor. A pressurized N 2  rich stream  733  flows into the top of the module and gas originally contained in the flow channel  503  (of  FIG. 11  hereof) of the structured parallel channel contactor flows out  739 . The gas fed into the top of the module  733  is a N 2  rich gas produced in later steps ( 4  and  5 ) that has been compressed  775  to a pressure slightly greater than the feed pressure (100 atm.). Composition of the gas fed in through the top of the contactor is nearly that of the N 2  reject stream  781 . The gas exiting out the bottom of the contactor has a composition nearer to that of the feed gas  771  (30% N 2  and 70% CH 4 ). 
     As the gas stream entering the module  733  displaces the gas in the feed channel a compositional front moves from top to bottom of the module. Before or shortly after this front breaks through the bottom of the module the third step  731  is stopped and a fourth step  741  is begun. The fourth step  741  lets the pressure of the contactor down to an intermediate pressure and recovers some of the N 2  for recompression. In the design discussed in this example the intermediate pressure is 30 atm. In the fourth step a N 2  rich stream  749  exits the module at a pressure of 30 atm. This stream is split into two streams  779  and  781 . Gas in stream  779  is fed to a compressor  775  and gas in stream  781  is rejected from the process at a pressure of 30 atm. In an optimization of this process a pressure in step  741  is chosen that minimizes the amount of gas flowing in stream  781 . Stream  733  that was used to rinse the contactor in the third step of the process  731  is comprised of the gas stream  779  that emerged from the compressor  775 . As the pressure in the contactor drops towards the outlet pressure of 30 atm, the flow in streams  779  and  781  decrease. When the flow in these streams has fallen to approximately ¼ of the initial value the fourth step is stopped and a fifth step is begun. In the fifth step of the process  751  the module pressure is dropped to 1.2 atm and a N 2  rich stream is recovered  785 . 
     To improve the operation of the process, as well as the pressure at which N 2  is recovered, gas may be recovered in the fifth step  751  using a multi-step process in which the contactor pressure is decreased in a series of pressure equalization steps. In an example with two pressure equalization steps, one portion of the N 2  rich gas is recovered at a pressure of 12 atmospheres while the rest is recovered at 1.2 atmospheres. 
     It is also possible to decrease the module pressure in step four  741  with a series of pressure equalization steps. Again each pressure equalization step can be used to form a gas stream that can either be rejected from the process in stream  783  or recompressed to form stream  733 . If pressure equalization steps are employed is it advantageous to design them to maximize the pressure at which the N 2  reject streams are captured. 
     The modeling used to predict the performance of the contactor used isotherms for N 2  and CH 4  that were measured with well known gravimetric uptake methods, PVT (pressure, volume, temperature) methods, and with analysis of single component transport data in DDR membranes. A statistical isotherm shape was found to best describe the single component isotherms for N 2  and CH 4 . The best fits to the measured isotherms for N 2  and CH 4  give saturation capacities of 5 molecules par cage in the DDR zeolite framework. These values correspond to a maximum loading of 4.17 milli-moles/gram (of DDR). These saturation capacities are consistent with the physical expectation that the maximum possible loading would correspond to N 2  and CH 4  filling the pores at a liquid density. A single parameter K, that is analogous to the Henry&#39;s constant in a Langmuir isotherm, describes the shape of the statistical isotherm. The K values used for modeling are: 
               K     N   2       =     3.79   ×     10     -   9       ⁢     ⅇ       9.6   ×     10   3     ⁢           ⁢     Joule   Mole       RT       ⁢           ⁢     (     in   ⁢           ⁢     pascals     -   1         )                     K     CH   4       =     4.25   ×     10     -   10       ⁢     ⅇ       17.8   ×     10   3     ⁢           ⁢     Joule   Mole       RT       ⁢           ⁢     (     in   ⁢           ⁢     pascals     -   1         )             
where R is the molar gas constant and T is the temperature in Kelvin.
 
     Over a wide range of conditions the shape of the statistical and Langmuir isotherms are very similar. For simple modeling of the process given in this example, the statistical isotherm can be supplanted by an equivalent Langmuir isotherm. For modeling competitive adsorption effects, competitive adsorption isotherms can be derived from the single component statistical isotherms using well known techniques. 
     The single component Stefan-Maxwell transport diffusion coefficients for N 2  and CH 4  used in the modeling were 
               D     N   2       =     0.48   ×     10     -   10       ⁢     ⅇ     -       1.5   ×     10   3     ⁢           ⁢     Joule   Mole       RT         ⁢           ⁢     (     in   ⁢           ⁢     m   2     ⁢     /     ⁢   sec     )                     D     CH   4       =     0.48   ×     10     -   10       ⁢     ⅇ     -       13.4   ×     10   3     ⁢           ⁢     Joule   Mole       RT         ⁢           ⁢     (     in   ⁢           ⁢     m   2     ⁢     /     ⁢   sec     )             
where R is the molar gas constant and T is the temperature in Kelvin.
 
     When these transport parameters are evaluated at a given temperature, it is seen that there is a large difference in the diffusion coefficients of N 2  and CH 4  and a smaller difference in the isotherms. From a 50/50 molar mixture of N 2  and CH 4 , the isotherms slightly favor CH 4  adsorption but dramatically favor the diffusional transport of N 2  into the DDR crystals. By controlling the time scale of the adsorption step  721  and the purge displacement step  731 , it is possible to take advantage of this difference in diffusion coefficients and improve the selectivity of the process. By controlling these time steps a kinetic separation of N 2  and CH 4  can be achieved that takes advantage of differences in diffusivity of these molecules. The preferred class of 8-ring zeolite materials for removal of N 2  from natural gas will have a large difference in N 2  and CH 4  diffusion coefficients. This example illustrates a particular RCPSA cycle that can be tuned to achieve a kinetic separation of N 2  and CH 4 ; however, other swing adsorption cycles are possible. A parameter that can be used to evaluate the ability of a given material to produce a kinetic separation is the ratio of the single component diffusion coefficients for the components. The ratio is evaluated at the temperature of the intended process, 
             κ   =       D     N   2         C     CH   4               
Values of κ for DDR for nitrogen and methane separation at several different temperatures are given in the table below:
 
     
       
         
           
               
               
               
             
               
                   
                   
               
               
                   
                 Temperature (C.) 
                 κ 
               
               
                   
                   
               
             
            
               
                   
               
            
           
           
               
               
               
            
               
                   
                 20 
                 130 
               
               
                   
                 40 
                 100 
               
               
                   
                 60 
                 75 
               
               
                   
                 80 
                 60 
               
               
                   
                 100 
                 50 
               
               
                   
                   
               
            
           
         
       
     
     For the preferred class of 8-ring zeolite materials for removal of N 2  from natural gas κ N2/CH4  is a function of temperature. It is preferred that the material be chosen to have a value of κ N2/CH4  greater than 5 at the operating temperature. More preferably the material is chosen to have a value of κ N2/CH4  greater than 20 at the operating temperature. Even more preferably the material is chosen to have a value of κ N2/CH4  greater than 50 at the operating temperature. 
     In order to take advantage of the intrinsic kinetic selectivity of the preferred class of 8-ring zeolite materials for removal of N 2  from natural gas, the crystals forming the contactor must have substantially the same size. If they have widely different sizes some will substantially fill with CH 4  during the adsorption step  721 , resulting in increased methane loss during the desorption step  751 . To increase methane recovery in the process it is then preferred that the standard deviation of the volume of the individual crystallites in the DDR film forming the adsorbent layer  505  be less than 100% of the volume of an average crystallite. In a more preferred embodiment the standard deviation of the volume of the crystallites in the DDR film forming the adsorbent layer  505  is less than 50% of the volume of an average crystallite. In the most preferred embodiment the standard deviation of the volume of the crystallites in the DDR film forming the adsorbent layer  505  is less than 10% of the volume of an average crystallite. The most preferred embodiment was chosen to model the PSA cycle described in this example. 
     With this type of adsorbent, the time for steps  721  and  731  is set by the average crystal size in the adsorbent. It is preferred that the time step be chosen so that adsorbed N 2  in the DDR has time to equilibrate with gaseous N 2  in the feed channel  503  but the CH 4  does not have time to equilibrate. The time for N 2  or CH 4  achieve 90% approach to equilibrium (following a change in surface concentration) within a single DDR crystal that has rapid diffusion path to the gas in the contactor is;
 
τ 90 =0.183 r   2   /D   N2  
 
and
 
τ 90 =0.183 r   2   /D   CH4  
 
where r is the average DDR crystal radius and D N2  and D CH4  are the diffusion coefficients of N 2  and CH 4  at the operating temperature. If there are no external mass transfer limitations, the equilibration times for different crystallite sizes are given in the table below:
 
     
       
         
           
               
               
               
             
               
                   
               
               
                 Crystallite Size (μm) 
                 Nitrogen τ 90  (seconds) 
                 Methane τ 90  (seconds) 
               
               
                   
               
             
            
               
                   
               
            
           
           
               
               
               
            
               
                 1.5 
                 0.01 
                 2 
               
               
                 5 
                 0.1 
                 22 
               
               
                 10 
                 0.45 
                 91 
               
               
                 25 
                 2.8 
                 570 
               
               
                 40 
                 7.3 
                 1460 
               
               
                   
               
            
           
         
       
     
     It is preferred that for N 2  the time for steps  721  and  731  be in a range from 0.5τ 90  to 10τ 90  and it is more preferred that the time for steps  721  and  731  be in a range from 1τ 90  to 5τ 90 . For modeling, a time step of 1.5τ 90  was chosen for steps  721  and  731 . The numerical value of the time step is then set by the crystal size. It is preferred that the average DDR crystal size be in a range from 0.005 μm to 100 μm. It is more preferred that the average DDR crystal size be in a range from 0.5 μm to 50 μm and it is most preferred that the average DDR crystal size be in a range from 1 μm to 10 μm. For modeling an average DDR crystal size of 5 μm was used. 
     A simplified modeling approach similar to that described above was used. In the adsorption step  721 , the simple model separately treats the equilibration of N 2  and CH 4  in the feed channel with the DDR crystals forming the adsorbent layer. The amount of N 2  adsorbed in the DDR crystals is taken to be 80% of the amount that might be expected if the N 2  adsorbed in the DDR has fully equilibrated with the gaseous feed entering the process  771  at a temperature that is 10° C. higher than the feed temperature. The amount of CH 4  adsorbed in the DDR crystals is 1% of the amount that might be expected if the CH 4  adsorbed in the DDR has fully equilibrated with the gaseous feed entering the process  771  at a temperature that is 10° C. higher than the feed temperature. In the simple model, gas filling the mesopores and macropores in the laminate at the end of the adsorption step  721  is not recovered. Also, for the simple model the N 2  purge used in step  731  displaces all of the methane left in the feed channel into stream  739 . With these approximations the methane recovery from the process is predicted to be 91%. This closely agrees with the exact model and the model provides a simple method for one skilled in the art to evaluate the effect of changing the mesopore and macropore volume of the adsorbent. 
     EXAMPLE 12 
     The process of Example 11 is followed but the feed and product specifications are held constant and the volume fraction of mesopores and macropores in the adsorbent are increased from 2.5% to 5%. The predicted methane recovery is found to fall from 91% (in Example 11) to 90%. 
     EXAMPLE 13 
     The process of Example 11 is followed but the feed and product specifications are held constant and the volume fraction of mesopores and macropores in the adsorbent are increased from 2.5% to 15%. The predicted methane recovery is found to fall from 91% (in Example 11) to 84%. 
     EXAMPLE 14 
     The process of Example 11 is followed but the feed and product specifications are held constant and the volume fraction of mesopores and macropores in the adsorbent are increased from 2.5% to 20%. The predicted methane recovery is found to fall from 91% (in Example 11) to 81%. 
     EXAMPLE 15 
     The process of Example 11 is followed but the feed and product specifications are held constant and the volume fraction of mesopores and macropores in the adsorbent are increased from 2.5% to 25%. The predicted methane recovery is found to fall from 91% (in Example 11) to 78%. 
     EXAMPLE 16 
     This example illustrates the use of a turboexpander to condition sour gas (i.e., natural gas-containing H 2 S and CO 2 ) so that PSA can operate in the window that optimizes methane recovery.  FIG. 14  hereof shows a process scheme in which a turboexpander is used to set the pressure and temperature of a sour gas that is separated in a PSA apparatus. A sour gas stream  811  with a temperature of 100° C. and a pressure of 1,500 psi is produced from a gas field and fed to the process. The CO 2  content of the stream is 66 mole % and the H 2 S concentration is 2 mole %. Water is present at its saturated vapor pressure, and the concentration of the heavy hydrocarbons is 2 mole %. The heavy hydrocarbons contain a small fraction of waxy species with carbon numbers as large as 36. For this stream  811 , CO 2  comprises the majority of the heavy component that will be removed by a kinetically controlled PSA process. If DDR zeolite is used as the adsorbent in the kinetically controlled PSA, the loading in the DDR zeolite from CO 2  partial pressure in stream  811  would be in excess of 0.6 q s  and the slope of the CO 2  isotherm would be: 
                 ∂     q     CO   2           ∂     P     CO   2           ≅     .02   ⁢           ⁢     K     CO   2       ⁢     q   s             
where K CO2  is the Henry&#39;s constant for CO 2 , and q s  is the saturated loading for CO 2  in DDR.
 
     To bring the stream into a more preferred window of operation the stream is passed through a turboexpander  821  that reduces the stream pressure to about 500 psi. In a preferred embodiment, the turboexpander  821  is designed to have a radial inflow. Radial inflow turbine designs suitable for use in this process can be found in Perry&#39;s Chemical Engineers&#39; Handbook (7th Edition. © 1997 McGraw-Hill edited by R. H. Perry and D. W. Green). During the approximately isentropic expansion, the gas temperature falls significantly and liquids may fall out of the gas stream due to a change in the dew point and reduction in temperature. Radial inflow turbine designs can be operated so that liquids falling out of the gas stream will not impede the operation of the turboexpander. In this example, the power generated by the turboexpander is coupled through a shaft  831  to and an electric generator  823 . In an alternative embodiment, the power from the turboexpander shaft is coupled to a compressor instead of an electric generator. 
     Before the stream is passed through turboexpander  821 , it may optionally be sent through a process  813  to remove any particles, or a portion of the wax, or optionally some of the heavy hydrocarbons, H 2 S and/or water. The absolute temperature of the stream  837  coming out of the turboexpander is approximately 30% less than feedstream  811 , and it contains a mixture of gas and liquid droplets. Stream  837  is then sent to a process block  839  that at least removes the liquid droplets from the stream. Liquid droplet removal can be accomplished through a variety of methods including coalescing filters, settling drums, static centrifugation, and electrostatic precipitation. The process block  839  also contains equipment to increase the temperature of stream  837 . Means of heating the stream within process block  839  include heat exchangers such as shell and tube heat exchangers as well as other types of heat exchangers including the many varieties discussed in Perry&#39;s Chemical Engineers&#39; Handbook (7th Edition. © 1997 McGraw-Hill edited by R. H. Perry and D. W. Green), including packed bed heat exchangers. Alternatively, stream  837  may be by mixing it with a separately formed hot gas stream  835 . When heat exchangers are used in process block  839 , it is preferred that they extract heat from stream  881 ,  891 ,  895 , or some combination thereof using a multi-pass heat exchanger. Optionally, the heat exchanger used in process block  839  can extract heat from an optional stream  835 . In one embodiment stream  835  is produced by combusting hydrocarbon and air or oxygen enriched air. In another embodiment, stream  835  is produced by heat exchanging a working fluid or gas with high temperature combustion products. Besides increasing the temperature of stream  837  and removing liquid droplets, process block  839  can optionally be configured to remove heavy hydrocarbons, water vapor, or H 2 S from the gas phase. In this example, process block  839  is configured to remove liquid droplets, and to heat stream  837  to a temperature of 90° C. 
     The physical composition of stream  871  coming from process block  839  is such that if DDR zeolite is used as the adsorbent in a kinetically controlled PSA, the loading in the DDR zeolite from CO 2  partial pressure in stream  871  would be in excess of 0.5 q s  and the slope of the CO 2  isotherm would be: 
                 ∂     q     CO   2           ∂     P     CO   2           ≅     .07   ⁢     K     CO   2       ⁢     q   s             
where K CO2  is the Henry&#39;s constant for CO 2  at 90° C. and q s  is the saturated loading for CO 2  in DDR.
 
     This operating condition is in a more desirable range for high methane recovery with a kinetically controlled PSA process than that for stream  811 . PSA unit  841  is used to separate most of the CO 2  and a fraction of the H 2 S out of stream  871 . In a preferred embodiment, PSA unit  841  contains a parallel channel contactor with an adsorbent having an open volume fraction of mesopores and macropores that is less than 10%. In a preferred embodiment, the microporous adsorbent in the contactor is an 8-ring zeolite and PSA unit  841  is a RCPSA unit that is operated in a kinetically controlled mode. In a preferred embodiment more than 90% of the methane and heavy hydrocarbon fed to PSA unit  841  is recovered in the methane enriched stream  815 . In a an even more preferred embodiment, more than 95% of the methane and heavy hydrocarbon fed to PSA unit  841  is recovered in the methane enriched stream  815 . In this example the molar ratio of methane to CO 2  in the methane enriched stream  815  is greater than 9:1. Depending upon final use, the methane enriched stream  815  may be further processed or purified in other processes. The CO 2  enriched stream  881  coming from the PSA  841  can be sent through an optional process block  851  to remove water vapor. 
     The optional process block  851  can also contain one side of a heat exchanger that is used to provide heat to the heat exchanger in process block  839 . The CO 2  in stream  881  is ultimately sent to a compressor  829 . The compressor  829  is preferably driven by the energy recovered from the turboexpander  821 . In this example energy produced by the electric generator  823  is sent through a power transmission line  825  to power a motor  827  that is shaft-coupled via  833  to the compressor  829 . As was previously mentioned in an alternative embodiment, the compressor  829  can be shaft-coupled to the turboexpander  821 . Because of the work of compression, the temperature of the stream  891  coming out of the compressor  829  is greater than that of stream  881 . It can be advantageous to cool this stream  891  before further compression to pressures required for CO 2  disposal/sequestration. Cooling can be accomplished with an optional process block  883  that contains one side of a heat exchanger that is used to provide heat to the heat exchanger in process block  839 . If needed, process block  883  can contain equipment such as a glycol dehydration unit to reduce the corrosivity of the gas mixture. To raise the pressure of the CO 2  rich gas stream  893  to the level needed for CO 2  disposal/sequestration, a final compressor  897  is provided. The compressed CO 2  rich gas stream  895  is injected into an underground formation for CO 2  disposal/sequestration, or for enhanced oil recovery.