Patent Document

This application is a divisional of U.S. application Ser. No. 11/789,860, filed Apr. 6, 2007, which claims the benefit of U.S. Provisional Application No. 60/809,582, filed May 30, 2006, entitled “Co-Extrusion Method of Fabricating Electrode Structures in Honeycomb Substrates and Ultracapacitor Formed Thereby.” 
    
    
     FIELD OF THE INVENTION 
     This invention generally relates to ultracapacitor energy storage devices, and is particularly concerned with a method for forming electrode structures within the channels of a honeycomb substrate, and the ultracapacitor formed thereby. 
     BACKGROUND OF THE INVENTION 
     Electric double layered capacitors (EDLC), commonly known as ultracapacitors, are known in the prior art. Such devices are capable of storing larger amounts of electrical energy per unit volume than the traditional capacitors, generating much higher power in a short instant than many types of chemical batteries, and may be charged and discharged a large number of times with virtually no energy losses due to chemical reaction. Ultracapacitors having capacitances of thousands of Farads are already commercially available, and are being used as energy storage devices for providing back-up currents for microcomputers, clock radios, and other consumer electronics, as well as actuators or primary power sources capable of providing sufficient current for automobile engine cranking, as well as power sources for hybrid and electrical vehicles. 
     Such devices achieve their relatively high capacitances by virtue of a high-area electrode microstructure. In conventional capacitors, the electrodes are typically metallic plates separated by a dielectric material. As capacitance is dependent upon the area of the electrode, such plate-type electrode structures must be made very large to obtain capacitances in excess of one F. Ultracapacitors circumvent this limitation by means of electrodes formed from very fine, particulate materials, such as activated carbon, having surface area to mass ratios on the order of 1,000 to 3,000 m 2 /gm. The resulting high surface area per unit volume that such electrode structures provide allow much higher capacitances to be stored in the resulting ultracapacitor than could possibly be stored in a capacitor using conventional, plate type electrodes. 
     In the simplest design of an ultracapacitor, two high-area electrodes are separated a short distance from one another via a dielectric material. Current collectors (which may be in the form of either wires or plates) are centrally provided within each of the particulate carbon electrode structures. The electrodes and the dielectric separating them are soaked in an electrolyte, which is preferably non-aqueous in order to avoid limitations on the charging voltage that are inherent with aqueous-type electrolytes. A charging voltage is then applied across the current collectors of the two opposing electrodes, which in turn allows a relatively large amount of positive and negative charges to migrate from the current collectors to the surfaces of the mutually contacting carbon particles forming the electrode structures. The charging process is complete when the capacitor is saturated. Electrical power may then be tapped from the current collectors as needed. 
     Unfortunately, such a simplistic, two-electrode carbon-based design does not yield efficient electrical power. While the power output may be increased by shortening the distance between the current collectors and the particulate carbon, the resulting lower volume of electrodes would of course reduce the available electrode area and hence the capacitance. 
     To overcome these limitations, ultracapacitors having multiple electrodes connected in parallel have been constructed. In one such design, an extruded honeycomb substrate formed from a conductive carbon-based material forms the first set of electrodes of the ultracapacitor, while monolithic carbon rods disposed in the hollow channels of the honeycomb structure form the other set of electrodes. To prevent short circuiting between the two sets of electrodes, the interior walls of the channels of the honeycomb structure are coated with a dielectric polymer film prior to the insertion or manufacture of the rod-like electrode structures within the honeycomb channels. 
     Because honeycomb substrate having relatively high channel densities of between 400 and 2,000 channels per square inch may be manufactured with existing extrusion technology, an ultracapacitor having hundreds or even thousands of electrodes are possible with this approach. The relatively small cross section where the cross sectional area of the resulting electrodes provides short distances between the centrally disposed current collectors, and the surrounding matrix of particulate carbon, allowing electrical charges to migrate to the surfaces of the particulate carbon with relatively small internal resistance, thereby resulting in an ultracapacitor that is chargeable within a matter of a few seconds, and which has a highly usable discharge energy. 
     Unfortunately, such honeycomb-type ultracapacitors have not yet realized their full potential in providing a low-cost, high energy storage device. It has been proven very difficult to install the rod-like, carbon electrode structures within the channels of the ceramic substrate. No practical and time-efficient method has yet been found to produce such rod-like electrode structures and to insert the hundreds or thousands required into the small, individual openings of the honeycomb channels. While extrusion techniques have been attempted, the small cross-sections of the channels and their close distances together has made it difficult to reliably and rapidly form electrode structures with current collectors within the channels without the formation of void spaces which compromises the performance and capacity of the resulting ultracapacitor. It has also proven difficult and time consuming to uniformly and reliably apply a coat of dielectric, insulating polymer over the interior walls of the hundreds or thousands of small channels within such honeycomb structures. Finally, the carbon based honeycomb substrates tend to be brittle and fragile, and thus prone to cracking or breakage during the installation of the rod-like electrode structures. The resulting cracks or other discontinuities create electrical leakages in the final ultracapacitor, which in turn degrade its performance. 
     Clearly, what is needed is an ultracapacitor capable of exploiting all the advantages of extruded honeycomb substrates without the accompaniment of any of the aforementioned disadvantages. In particular, a technique for manufacturing a honeycomb based ultracapacitor is needed wherein electrode structures are quickly and easily formed within each of the channels of the substrate without potentially wall-breaking forces and without the formation of performance compromising voids that reduce both energy and power performance. Ideally, the design of the honeycomb based ultracapacitor would obviate the need for coating the interior walls of the channels with a dielectric polymer. Finally, it would be desirable if the honeycomb substrate could be formed from a material stronger and more robust than carbon-based conductive compounds, and hence less apt to form internal cracks or other discontinuities that would compromise the performance of the final device. 
     SUMMARY OF THE INVENTION 
     Generally speaking, the invention is a method of fabricating electrode structures within the channels of honeycomb substrates that overcomes or at least ameliorates all of the aforementioned shortcomings associated with the prior art. To this end, the method comprises the steps of providing a honeycomb substrate having a plurality of channels, and then simultaneously feeding a current collector along a central portion of at least one of the channels while injecting a paste containing an electrode material such that the interior of the channel becomes completely filled with electrode paste at substantially the same rate that the current collector is fed into the channel. The electrode paste is preferably extrudable, and the current collector and electrode paste may be simultaneously fed into the channel of the substrate by the nozzle of a co-extrusion device by inserting the nozzle to the far end of the channel, and commencing the simultaneous feeding of the current collector and extrudable electrode paste from the nozzle while withdrawing the nozzle from the channel at a same rate that the current collector and extrudable electrode paste are fed. 
     The current collector may be, for example, a wire or strand formed from an electrically conductive metal or polymer. The electrode paste may include, for example, particulate carbon having a relatively high surface area per weight, e.g. 1,000-3,000 m 2 /gm. Preferably, the dielectric honeycomb substrate may be of a form used in diesel particulate filters, wherein each of the elongated channels has a plugged end, and an open end, and wherein the plugging pattern on both ends of the substrate is a checkerboard pattern. Such a checkerboard plugging pattern not only provides an optimal distribution of three-dimensional interleaving electrode structures for ultracapacitator purposes, but further facilitates the simultaneous fabrication of an electrode structure in a plurality of channels that are all plugged at the same ends by allowing a wider spacing apart of the nozzles of a co-extrusion device than would otherwise occur if simultaneous co-extrusion were attempted within a plurality of mutually contiguous channels. 
     In a preferred embodiment of the method, two opposing arrays of co-extrusion nozzles are simultaneously inserted in all of the open ends of the channels on either end of the honeycomb substrate until the nozzles are adjacent to the plugged ends of the channels. All of the nozzles are then simultaneously actuated, and the two arrays of nozzles of the co-extrusion device are withdrawn as the current collectors and electrode paste are simultaneously extruded at such a rate that the channels become completely filled with electrode paste as the current collectors are fed along the central axis of the elongated channels. Extrusion of the electrode past ceases when the nozzles are withdrawn from the open ends of the channels. However, the feeding of the current collectors continues to provide a terminal portion of the current collector that extends out of each of the elongated channels of the substrate. The distal ends of the terminal portions are then cut, and all the terminal portions on either side of the honeycomb substrate are interconnected by means of collector plates. 
     The method is particularly adapted to forming an ultracapacitor having a high energy storage capacity per unit volume and a relatively low weight. The high processing speeds made possible by the inventive method and the use of low-cost materials advantageously result in a low-cost energy storage device. When the honeycomb substrate is formed from a dielectric ceramic material, the resulting structure is more robust than ultracapacitors utilizing a carbonaceous honeycomb substrate, and hence is less prone to breakage or manufacturing faults that can lead to power leakage during use. The co-extruded current collectors and electrode paste deposited within the channels of the dielectric ceramic substrate provides an electrode structure without the need for the deposition or coating of insulating films over the channel walls, and the terminal portions of the current collectors formed outside of the channels provides a convenient and robust means for interconnecting all of the electrodes on each side of the substrate via a conductive collector plate. Finally, the ability to manufacture channels in such ceramic honeycomb substrate having small cross sections (i.e., having a density of between 200 and 2,000 channels per square inch) provides an ultracapacitor which may be quickly charged, and which discharges at voltages comparable to those commonly associated with chemical batteries (i.e., between two and four volts). 
    
    
     
       BRIEF DESCRIPTION OF THE DRAWINGS 
         FIG. 1A  is a perspective view of a dielectric ceramic honeycomb substrate that the method of the invention is preferably applied to; 
         FIG. 1B  is an enlargement of the circled portion of the top surface of the honeycomb substrate of  FIG. 1A ; 
         FIG. 1C  is a partial, cross-sectional view of the honeycomb substrate illustrated in  FIG. 1A  along the line  1 C- 1 C; 
         FIG. 2A  is a partial cross-sectional view of a honeycomb substrate having electrode structures formed in its hollow channels via the method of the invention; 
         FIG. 2B  is an enlargement of the circled portion of the partial cross-sectional view of the substrate in  FIG. 2A ; 
         FIG. 2C  is a partial end view of a honeycomb substrate having electrode structures formed in accordance with the method of the invention; 
         FIGS. 3A ,  3 B and  3 C illustrate the formation of an electrode structure within a single channel of a ceramic honeycomb by a way of a co-extrusion nozzle in accordance with a method of the invention; and 
         FIG. 4  is a schematic diagram of a co-extrusion device for implementing the preferred method of the invention. 
     
    
    
     DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT 
     With reference to  FIGS. 1A-1C , the invention is preferably applied to ceramic honeycomb substrates  1  of the type used as diesel particulate filters. Such substrates  1  include a network  3  of web walls  5  which define a plurality of elongated channels  7 . While the channels  7  are illustrated as having a square cross-section in  FIG. 1B , they may just as easily be hexagonal or some other polygonal shape. The web walls  5  forming the channels  7  are typically between 2.0 and 5.0 mils thick, and the density of the channels  7  may be between 300 and 2,000 channels per square inch. The ceramic substrate  1  further includes an outer skin  9  which is typically cylindrical in shape, and having a thickness of approximately three times that of the web walls  5 . The network  3  of web walls  5  is integrally connected to the inner surface  11  of the outer skin  9 . The honeycomb substrate  1  has generally planar opposing ends  13   a ,  13   b  as shown. 
     With particular reference to  FIGS. 1B and 1C , the honeycomb substrate  1  that the method of the invention is preferably applied to is of the same structure as those presently used as diesel particulate filters. In such substrates  1 , the open ends of the elongated channels  7  are plugged in a checkerboard pattern with integrally formed, plugs  15  such that each channel  7  has a plugged end, and an open end  16 . The plugs  15  are preferably made from a non-conductive material, for example, glass, glass-ceramic, cement, or ceramic. Preferably the plug material will have CTE (coefficient of thermal expansion) similar to that of the honeycomb structure. The checkerboard plugging pattern creates two sets  17   a ,  17   b  of three-dimensionally, interleaved channels  7  which in turn may advantageously be used to form two sets of three-dimensionally interleaving electrode structures, as will be described hereinafter. While the method of the invention is applicable to honeycomb structures formed from carbonaceous or other conductive materials, it is more preferably applied to honeycomb structures formed from a dielectric ceramic material such as cordierite, mullite, silicon carbide, aluminum titanate, alumina and silicone alumina. As will be more appreciated hereinafter, the use of a ceramic dielectric material to form the honeycomb substrate  1  obviates the need for coating the inner walls of the channels  7  with insulating materials, and further facilitates the method of the invention by allowing the co-extrusion nozzles necessary to form the electrode substrates in situ within the elongated channels  7  to be spaced farther apart when the method is used to simultaneously form a plurality of electrode structures. 
       FIGS. 2A ,  2 B, AND  2 C illustrate the structure of an ultracapacitor  20  after the method of the invention has been used to fabricate electrode structures within the channels  7  of the honeycomb substrate  1  illustrated in  FIG. 1A . The resulting ultracapacitor  20  has two opposing sets  22   a ,  22   b  of electrode structures  24  disposed within the two opposing sets  17   a ,  17   b  of three-dimensionally, interleaving channels  7 . Each electrode structure  24  includes a wire-like current collector  26  disposed along the longitudinal axis of its respective channel  7 . The current collector  26  is completely surrounded by an electrode paste  28  that contains a particulate conductor  30  having a relatively high surface area per unit weight. An example of such a particulate conductor  30  is activated carbon having a surface area on the order of 2,000 m 2 /gm. The particulate carbon is mixed with an inert, plastic polymer, such as polyvinylidene chloride, polyethylene tetrafluoride, and binder such as methylcel, etc., to render the carbon particles into a form which may be readily extruded, and which will form a solid structure within the channels  7  which will mechanically secure the current collectors  26 . 
     As is shown in  FIGS. 2A and 2B , each of the current collectors  26  of the electrode structures  24  ends in a terminal portion  32 . The terminal portions  32  of each of the opposing sets  22   a ,  22   b  of electrode structures  24  are electrically connected by means of collector plates  34   a ,  34   b  so that all of the electrode structures  24  within each of the opposing sets  22   a ,  22   b  may be simultaneously charged and discharged. In the preferred embodiment of the ultracapacitor  20  of the invention, an electrode structure  24  is fabricated in all of the channels  7  of the honeycomb structure  1  with the exception of the partial channels formed at the interface between the web walls  5  and the inner surface  11  of the outer skin  9 . After the two opposing sets  22   a ,  22   b  of electrode structures  24  are so formed, the resulting structure is soaked in a non-aqueous electrolyte such as tetraethyl ammonium tetrafluoraborate or lithium salts dissolved within a solvent such as acetonitrile and/or propylene carbonate. The structure  1  is appropriately packaged to prevent the electrolyte from evaporating. The use of a non-aqueous electrolyte advantageously increases both the charging and discharging voltage of the resulting ultracapacitor  20 . It should be noted that the dielectric ceramic material that preferably forms with honeycomb substrate  1  is porous to allow absorption of the non-aqueous electrolyte within the web walls  5  forming the elongated channels  7 . To this end, the porosity quotient of the dielectric ceramic material may be between about 20 and 60 percent. 
       FIGS. 3A ,  3 B, and  3 C illustrate the implementation of the method of the invention within the honeycomb substrate  1  to form the electrode structures  24  in the resulting ultracapacitor  20 . In the first step of the method, a co-extrusion nozzle  40  is inserted through the open end  16  of the channel  7  all the way to a point closely adjacent to the (preferably ceramic) plug  15  at the opposite end of the channel  7 . The co-extrusion nozzle  40  is formed from a tubular sleeve  42  that is substantially narrower than the cross section of width of the channel  7  so as to be easily inserted therein. The sleeve  42  terminates in a beveled or rounded tip  44  having a central opening  46  for guiding wire-like stock  48  that forms the previously described current collectors  26 . Preferably, the wire-like stock  48  is made of a highly conductive and flexible metal material, such as copper wire that has been gold plated in order to render it corrosion resistant. However, other metals such as aluminum, nickel, titanium, tin, silver, platinum, and alloys thereof may also be used, as well as non-metallic, conductive plastic materials. The cross-sectional diameter of the wire-like stock  48  may range between 0.1 to 0.3 mm, depending upon the cross-sectional dimensions of the elongated channel  7 . The interior  50  of the tubular sleeve  42  is hollow in order to conduct the previously discussed, extrudable electrode paste  52  from the screw feeder of a co-extrusion device through extrusion orifices  54   a - 54   d  located at the tip  44  of the co-extrusion nozzle  40 . 
     After the co-extrusion nozzle  40  has been positioned toward the closed end of the channel  7  as illustrated in  FIG. 3A , the co-extrusion device to which the co-extrusion nozzle  40  is connected is actuated in order to commence the extrusion of electrode paste  52  through the orifices  54   a  through  54   d . This fills the closed end of the channel  7  with electrode paste  52 , as is illustrated in  FIG. 3B . Almost instantaneously, as is illustrated in  FIG. 3C , the co-extrusion nozzle  40  begins to withdraw, and to feed the wire-like stock  48  that forms the current collector at a same rate that the extruded electrode paste  52  fills the interior of the channel  7 . In other words, for every length “X” that the electrode paste  52  fills within the channel  7 , a length “X” of wire-like current collector stock is fed through the central opening  46  of the tip  44  of nozzle  40 . The feed rate of the extrudable electropaste  52  and wire-like stock  48  is maintained in this manner as co-extrusion nozzle  40  is withdrawn from the channel  7  until the tip  44  of the nozzle  40  reaches the open end  16 , whereupon the feeding of the extrudable electrode paste  52  is stopped. However, the wire-like stock  48  continues to be fed in order to form the previously described terminal portion  32  of the resulting current collector  26 , whereupon the feeding of the wire-like stock  48  stops. The stock  48  is then cut in order to complete the formation of an electrode structure  24  within the elongated channel  7 . While the method has been described in terms that imply that the co-extrusion nozzle  40  is withdrawn through the open end  16  of the channel  7  while the substrate  1  remains stationary, the method may just as easily be implemented by maintaining the co-extrusion nozzle stationary  40  while withdrawing the honeycomb substrate away from it. All such forms of relative motion are encompassed within the method of the invention. 
       FIG. 4  illustrates a co-extrusion device  60  that may be used in implementing a preferred embodiment of the method of the invention. Device  60  includes a pair of opposing co-extrusion assemblies  62   a ,  62   b . Each of these assemblies includes a nozzle array  64  formed from co-extrusion nozzles  40  which are arranged, via a supporting guide plate  66 , into a pattern which registers with the “checkerboard” pattern of channel open ends  16  of one of the opposing sets  17   a ,  17   b  of the three-dimensionally, interleaved channels  7  described with respect to  FIGS. 1B and 1C . The base ends  67  of each of the co-extrusion nozzles  40  are mounted in the manifold  68 . The manifold  68  is in turn connected to a screw feeder  70  for feeding electrode paste  52  through the hollow interiors  50  of the co-extrusion nozzles  40  at a selected rate. The manifold  68  is further connected to a wire feed mechanism  72  which, like the screw feeder  70 , is capable of feeding the current-collector forming stock  48  at a selected rate through the central openings  46  of the tips  44  of each of the co-extrusion nozzles  40 . Each of the co-extrusion assemblies  62   a, b  is slidably mounted on a support frame  74  so that their respective nozzle arrays  64  may be reciprocably inserted into the checkerboard patterns of channel open ends  16  of the honeycomb substrate  1 , and Original therefrom. Each of the co-extrusion assemblies  62   a ,  62   b  is connected to a drive mechanism  76  having lead screws  77   a, b , each having a length L, for inserting and withdrawing the nozzle array  64  of each of the assemblies  62 A,  62 B at a selected, steady rate. Finally, the co-extrusion device  60  includes a control mechanism in the form of digital processor  78  which is connected to screw feeder control wires  80   a ,  80   b ; wire feeder control wires  82   a ,  82   b  and drive motor control wire  84 . 
     In operation, a honeycomb substrate  1  is placed between the opposing nozzle arrays  60  of the two co-extrusion assemblies  62   a, b  as shown in  FIG. 4  such that the tips  44  are aligned with the checkerboard pattern of open ends  16  of the channel  7  present on the ends  13   a ,  13   b  of the substrate  1 . Following such alignment, the digital processor  78  actuates the motor of the drive mechanism  76  to insert the nozzle array  64  of each of the two opposing co-extrusion assemblies  62   a, b  so that the tips  44  of the nozzles  40  are adjacent to the ceramic plugs  15  disposed at the ends of each of the two sets  17   a ,  17   b  of channels  7 . The digital processor  78  then actuates the screw feeders  80  and the wire feeders  82  of each of the co-extrusion assemblies  62   a, b  as well as the drive mechanism  76 . The digital processor  78  coordinates the rate of feed of the screw feeder  80 , the wire feeder  82 , and the withdrawal rate of the nozzle array  64  of the co-extrusion assemblies  62   a, b  to simultaneously implement the electrode structure forming process for each channel  7  in accordance with the description given with respect to  FIGS. 3A-3C .

Technology Category: 5