Patent Abstract:
An apparatus ( 10 ) is provided for determining the flow rate of a gas. The apparatus comprises a housing ( 12 ) forming a vaporization chamber ( 14 ) for converting a fluid into a gas vapor when subjected to heat ( 22 ). An oscillation flow meter is formed within the housing ( 12 ), thereby being integrated with the vaporization chamber, for receiving the gas vapor and providing a frequency signal ( 60 ) indicative of the rate of flow of the gas vapor.

Full Description:
FIELD OF THE INVENTION  
       [0001]     The present invention generally relates to an apparatus for measuring the amount of fluid flowing in a channel, and more particularly to a fluidic oscillation flow meter for determining the flow rate of a gas.  
       BACKGROUND OF THE INVENTION  
       [0002]     Fluidic oscillator flow meters are well known in the art. See for example, Horton et al., U.S. Pat. No. 3,185,166; Testerman et al., U.S. Pat. No. 3,273,377; Taplin, U.S. Pat. No. 3,373,600; Adams et al., U.S. Pat. No. 3,640,133; Villarroel et al., U.S. Pat. No. 3,756,068; Zupanick, U.S. Pat. No. 4,150,561; Bauer, U.S. Pat. No. 4,244,230; and Drzewiecki, U.S. Pat. No. 6,553,844. These conventional fluidic oscillators comprise a fluidic amplifier having two channels with the outputs fed back to the input to produce a free running oscillation wherein the fluid alternatively flows through one channel then the other by means of the fluid fed back being transversely applied to the input stream thereby forcing the input to the other channel.  
         [0003]     Most fluidic oscillator flow meters measure some characteristic, e.g., volumetric flow, density, quality, enthalpy, and bulk modulus of a fluid. In the case of measuring volumetric flow, this is typically accomplished by measuring the frequency of the fluid shifting from one channel to the other. The frequency is linearly related to the volumetric flow because the flow transit time is related to flow velocity. Since the amplifier nozzle area is known, the product of velocity and area yields volumetric flow. In most cases, the acoustic feedback time for most fluids can be designed to be only a few percent of the total flow transit time.  
         [0004]     In U.S. Pat. No. 6,076,392, the constituents of a gas mixture are determined by measuring both the flow of the fluid sample stream and the speed of sound in the fluid. A measure of the volumetric flow is required to determine the properties density and viscosity of the fluid sample, and a measure of the speed of sound is required to determine the property specific heat of the fluid.  
         [0005]     In “A Fluidic-Electronic Hybrid System for Measuring the Composition of Binary Mixtures”, Anderson et al., Ind. Eng. Chem. Fundam., Vol. 11, No. 3, 1972, it has been shown that the density of a gas may be determined by use of an oscillation flow meter for gasses with temperatures ranging from −20 to +120° C. The speed of a pressure pulse traveling through a gas (sonic velocity) is proportional to the square root of the gas density. However, the disclosed system requires a separate liquid vaporizer.  
         [0006]     Accordingly, it is desirable to provide a fluidic oscillation flow meter integrated within a fuel cell for measuring the volumetric flow rate of elevated temperature vapor. Furthermore, other desirable features and characteristics of the present invention will become apparent from the subsequent detailed description of the invention and the appended claims, taken in conjunction with the accompanying drawings and this background of the invention.  
       BRIEF SUMMARY OF THE INVENTION  
       [0007]     An integrated vaporizer and flow meter is provided for determining the flow rate of a gas. The apparatus comprises a housing forming a vaporization chamber for converting a fluid into a gas vapor when subjected to heat. An oscillation flow meter is formed within the housing, thereby being integrated with the vaporization chamber, for receiving the gas vapor and providing a frequency signal indicative of the rate of flow of the gas vapor. 
     
    
     BRIEF DESCRIPTION OF THE DRAWINGS  
       [0008]     The present invention will hereinafter be described in conjunction with the following drawing figures, wherein like numerals denote like elements, and  
         [0009]      FIG. 1  is a schematic diagram of a fluidic oscillation flow meter in accordance with an exemplary embodiment of the present invention; and  
         [0010]      FIG. 2  is a block diagram of a fuel cell system including the fluidic oscillation flow meter of  FIG. 1 .  
     
    
     DETAILED DESCRIPTION OF THE INVENTION  
       [0011]     The following detailed description of the invention is merely exemplary in nature and is not intended to limit the invention or the application and uses of the invention. Furthermore, there is no intention to be bound by any theory presented in the preceding background of the invention or the following detailed description of the invention.  
         [0012]     Referring to  FIG. 1 , a gas oscillation flow meter  10  in accordance with an exemplary embodiment of the present invention includes a vaporization chamber  14  and a flow meter  16  within a housing  12 . Ideally the device should be able to operate from a minimum of the boiling point temperature of the measured fluid to a maximum of the temperature of a secondary process. The housing  12  comprises a material able to withstand high temperatures, such as a metal, but would preferably comprise ceramic. The vaporization chamber  12  optionally includes a porous material  18  spaced throughout. The porous material  18  may comprise zirconia or alumina, for example. The porous material  18  improves the spreading of the fluid resulting in an improved uniform evaporation.  
         [0013]     The flow meter  16  comprises a flow meter inlet nozzle  26  and first and second diversion channels  28 ,  30 . Vents  32 ,  34 ,  36 , and  38  (output vias) are accessible through output channels  42 ,  44 ,  46 ,  48 . Piezo chamber  52  is spaced between the first diversion channel  28  and a first return channel  54 , and piezo chamber  56  is spaced between the second diversion channel  30  and a second return channel  58 . A piezo device  62  is positioned within piezo chamber  52  and a piezo device  64  is positioned within piezo chamber  56 . In some embodiments, e.g., a multi-layer ceramic embodiment, the various elements may reside on different levels. For simplicity, the various components are shown in  FIG. 1  as being on the same level.  
         [0014]     In operation, a liquid is provided into the chamber  14  at the inlet  20 . The liquid may comprise, for example, a methanol and water mixture (such as may be used in a fuel cell system to be described subsequently in more detail). The liquid will saturate a portion of the porous material  18 . Heat  22  is applied to the chamber  14 , either by actively heating the chamber or by reclaiming waste heat from a thermally coupled secondary process, resulting in a gas vapor exiting the chamber  14  at outlet  24 . The desired temperature of heat is above the maximum boiling temperature of the inlet fluid and below the thermal constraints of the construction materials.  
         [0015]     The gas vapor exiting the outlet  24  enters the flow meter inlet nozzle  26  having a certain velocity. As the gas vapor proceeds into the flow meter  16 , the majority of the gas vapor will enter either the first or second diversion channel. For example, the gas vapor might enter diversion channel  28 , and proceed around through piezo chamber  52  and first return channel  54 , passing through the first nozzle  66 . As the gas vapor passes through first nozzle  66 , it impacts the gas vapor entering at flow meter inlet nozzle  26 , deflecting the entering gas vapor and causing the majority of the entering gas vapor to now divert to the second diversion channel  30 . The gas vapor would then proceed around through piezo chamber  56  and second return channel  58 , passing through the second nozzle  68 . As the gas vapor passes through second nozzle  68 , it impacts the gas vapor entering at flow meter inlet nozzle  26 , deflecting the entering gas vapor and causing the majority of the entering gas vapor to again enter the first diversion channel  28 . This switching from one side of the flow meter  16  to the other will continue in a cyclic fashion having a certain frequency depending on the rate of flow of the gas as long as gas vapor enters the flow meter  16 .  
         [0016]     As gas vapor fills the flow meter  16  and the pressure builds, gas vapor will enter output channels  42 ,  44 ,  46 ,  48  and exit the flow meter  16  through vents  32 ,  34 ,  36 ,  38 . The vents  32 ,  34 ,  36 ,  38  may converge into a single outlet (not shown). Additionally, though four vents  32 ,  34 ,  36 ,  38  are shown, any number of vents may be used. Typically, an equal number of vents would be positioned on both sides.  
         [0017]     As the gas vapor passes through piezo chambers  52 ,  56 , the pressure pulse is sufficient to trigger piezo devices  62 ,  64  thus generating an ac electrical signal  60  indicative of the frequency of the oscillatory nature of the flow meter  16 . The frequency of the gas shifting from one channel  28 ,  30  to the other is approximately linearly related to the volumetric flow.  
         [0018]     The gas oscillation flow meter  10  may be used most effectively in any application that consumes liquid fuel and operates at temperatures above the boiling point of that fuel, e.g., internal combustion engine, microreactors, and more specifically fuel cells. Fuel cells are electrochemical cells in which a free energy change resulting from a fuel oxidation reaction is converted into electrical energy. Reformed Hydrogen Fuel Cells (RHFCs) utilize hydrogen fuel processed from liquid or gaseous hydrocarbon fuels, such as methanol, using a reactor, called a fuel reformer, for converting the fuel into hydrogen. Methanol is the preferred fuel for use in fuel reformers for portable applications because it is easier to reform into hydrogen gas at a relatively low temperature compared to other hydrocarbon fuels such as ethanol, gasoline, or butane. The reforming or converting of methanol into hydrogen usually takes place by one of three different types of reforming. These three types are steam reforming, partial oxidation reforming, and autothermal reforming. Of these types, stean reforming is the preferred process for methanol reforming because it is the easiest to control and produces a higher concentration of hydrogen output by the reformer, at a lower temperature, thus lending itself to favored use.  
         [0019]     Utilizing multilayer laminated ceramic technology, ceramic components and systems are now being developed for use in microfluidic chemical processing and energy management systems, e.g., fuel cells. Monolithic structures formed of these laminated ceramic components are inert and stable to chemical reactions and capable of tolerating high temperatures. These structures can also provide for miniaturized components, with a high degree of electrical and electronic circuitry or components embedded or integrated into the ceramic structure for system control and functionality. Additionally, the ceramic materials used to form ceramic components or devices, including microchanneled configurations, are considered to be excellent candidates for catalyst supports and so are extraordinarily compatible for use in microreactor devices for generating hydrogen used in conjunction with miniaturized fuel cells. An example of a fuel cell formed in a ceramic material is disclosed in U.S. Pat. No. 6,569,553.  
         [0020]     A simplified block diagram of a fuel cell system, including an exemplary embodiment of the fluidic oscillation flow meter  10 , is shown in  FIG. 2 . A mixture  70  of methanol and water is supplied by a fuel pump  72  via fuel line  71  to the fluidic oscillation flow meter  10 . The mixture  70  of methanol and water is converted to a gas vapor as previously explained. Heat  22  is supplied to the gas oscillation flow meter  10  by the waste heat of a fuel cell  92  (an electric heater, not shown, may provide heat for startup). A frequency signal  60  is generated, as previously discussed, as well as a vapor temperature signal  73 , and supplied to micro-controller  74 . The micro-controller  74  forwards a control signal  76  to the fuel pump  72  for controlling the amount of fuel pumped in response to the frequency signal  60 . Each frequency relates proportionally to a specific flow rate. The pump control circuitry  74  determines the flow rate based on the frequency signal  60  and the vapor temperature signal  73  and directs the fuel pump  72  via the control signal  76  to increase, decrease, or maintain the fuel flow rate.  
         [0021]     The gas vapor exits the fluidic oscillation flow meter  10  via line  81  and enters a reformer section  82  of a fuel processor  80 . A first air pump  84  pumps preferably air, though any oxidant could be used, to a mixer  86 , for mixing the air with fuel received from the fuel cell  92  via line  85 . The micro-controller  74  determines the speed of the flow rate of the first air pump  84  and controls the speed thereof with the combustor pump control signal  81 . The mixture of air and fuel is fed via line  87  to a combustor  88  for supplying heat to the reformer  82 . A heater control signal  79  from the micro-controller  74  to the combustor  88  controls the amount of heat generated by the combustor  88  for optimum operation of the reformer  82 . The reformer supplies hydrogen vapor via line  83  to the anode  72  of the fuel cell  92 .  
         [0022]     The fuel cell  92  comprises a fuel electrode, or anode  94 , and an oxidant electrode, or cathode  96 , separated by an ion-conducting electrolyte  98 . The electrodes  94 ,  96  are connected electrically to a load (such as an electronic circuit) by an external circuit conductor (not shown). In the circuit conductor, electric current is transported by the flow of electrons, whereas in the electrolyte  98 , it is transported by the flow of ions, such as the hydrogen ion (H + ) in acid electrolytes, or the hydroxyl ion (OH − ) in alkaline electrolytes. In theory, any substance capable of chemical oxidation that can be supplied continuously (as a gas or fluid) can be oxidized galvanically as the fuel at the anode of a fuel cell. Similarly, the oxidant, supplied via line  103  by second air pump  102 , can be any material that can be reduced at a sufficient rate. Gaseous hydrogen has become the fuel of choice for most applications, because of its high reactivity in the presence of suitable catalysts and because of its high power density. Similarly, at the fuel cell cathode  96 , the most common oxidant is gaseous oxygen, which is readily and economically available from air for fuel cells used in terrestrial applications. When gaseous hydrogen and oxygen are used as fuel and oxidant, the electrodes  94 ,  96  are porous to permit the gas-electrolyte junction area to be as great as possible. The electrodes  94 ,  96  must be electronic conductors, and possess the appropriate reactivity to give significant reaction rates. At the anode  94 , incoming hydrogen gas is oxidized to produce hydrogen ions (protons) and electrons. Since the electrolyte is a non-electronic conductor, the electrons flow away from the anode  94  via an external electrical circuit. At the cathode  96 , oxygen gas is reduced and reacts with the hydrogen ions migrating through the electrolyte  98  and the incoming electrons from the external circuit to produce water as a byproduct. The byproduct water is typically expelled as vapor at elevated temperatures via line  99 . The overall reaction that takes place in the fuel cell is the sum of the anode  94  and cathode  96  reactions, with part of the free energy of reaction released directly as electrical energy. The difference between this available free energy and the heat of reaction is produced as heat at the temperature of the fuel cell  92 . It can be seen that as long as hydrogen and oxygen are supplied to the fuel cell  92 , the flow of electric current will be sustained by electronic flow in the external circuit and ionic flow in the electrolyte.  
         [0023]     In practice, a number of these unit fuel cells  92  are normally stacked or ‘ganged’ together to form a fuel cell assembly. A number of individual cells are electrically connected in series by abutting the anode current collector of one cell with the cathode current collector of its nearest neighbor in the stack.  
         [0024]     The micro-controller  74  controls the overall operation of the system. For example, the operating point of the fuel cell  92  is controlled by a heater control signal  91  from the micro-controller  74  in response to a temperature signal  93  and a cell voltage signal  95  from the fuel cell  92 . The amount of oxidant supplied to the cathode  96  by the second air pump (or blower)  102  is controlled by the cathode blower signal  101  from the micro-controller. Exhaust from the fuel cell  92  via line  99  through dilution fan  106  is controlled by the micro-processor  74  via dilution fan signal  105 . A DC-DC converter  108  receives electrical current produced by the fuel cell  92  and provides power to the micro-controller  74 .  
         [0025]     While at least one exemplary embodiment has been presented in the foregoing detailed description of the invention, it should be appreciated that a vast number of variations exist. It should also be appreciated that the exemplary embodiment or exemplary embodiments are only examples, and are not intended to limit the scope, applicability, or configuration of the invention in any way. Rather, the foregoing detailed description will provide those skilled in the art with a convenient road map for implementing an exemplary embodiment of the invention, it being understood that various changes may be made in the function and arrangement of elements described in an exemplary embodiment without departing from the scope of the invention as set forth in the appended claims.

Technology Classification (CPC): 8