Three-wheel air turbocompressor for PEM fuel cell systems

• US 6,607,854 B1
• Filed: 11/13/2000
• Issued: 08/19/2003
• Est. Priority Date: 11/13/2000
• Status: Expired due to Fees

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Gee, Mark, Ferrall, Joe, Sokolov, Pavel, Emerson, Terence P., Rehg, Tim
• Primary Examiner(s): Chaney, Carol
• Assistant Examiner(s): TSANG FOSTER, SUSY N
• Application Number:
  US09/712,621
• Time in Patent Office: 1,009 Days
• Field of Search: 429/12, 429/13, 429/17, 429/19, 429/20, 429/26
• US Class Current: 429/413
• CPC Class Codes: H01M 2300/0082 Organic polymers
• CPC Class Codes: H01M 8/04022 Heating by combustion
• CPC Class Codes: H01M 8/04029 Heat exchange using liquids
• CPC Class Codes: H01M 8/04089 of gaseous reactants
• CPC Class Codes: H01M 8/04119 with simultaneous supply or evacuation of electrolyte; Humidifying or dehumidifying
• CPC Class Codes: H01M 8/04156 with product water removal
• CPC Class Codes: H01M 8/0612 from carbon-containing material
• CPC Class Codes: Y02E 60/50 Fuel cells

Abstract

A fuel cell system comprises a compressor and a fuel processor downstream of the compressor. A fuel cell stack is in communication with the fuel processor and compressor. A combustor is downstream of the fuel cell stack. First and second turbines are downstream of the fuel processor and in parallel flow communication with one another. A distribution valve is in communication with the first and second turbines. The first and second turbines are mechanically engaged to the compressor. A bypass valve is intermediate the compressor and the second turbine, with the bypass valve enabling a compressed gas from the compressor to bypass the fuel processor.

Claims

1. A fuel cell system, comprising:

a compressor;

a fuel processor downstream of said compressor;

a fuel cell stack in communication with said fuel processor and compressor;

a first turbine downstream of said fuel processor; and

a second turbine downstream of said fuel processor, said second turbine being mechanically engaged to said compressor and first turbine.

2. The system of claim 1, further comprising a bypass valve intermediate said compressor and second turbine, said bypass valve enabling a compressed gas from said compressor to bypass said fuel processor.

3. The system of claim 1, further comprising a distribution valve in communication with said first and second turbines.

4. The system of claim 1, further comprising a combustor downstream of said fuel cell stack.

5. The system of claim 1, further comprising a heater/humidifier intermediate said compressor and fuel cell stack.

6. The system of claim 1, further comprising a condenser/separator downstream of said first and second turbines.

7. The system of claim 6, further comprising a heater/humidifier intermediate said condenser/separator and said first and second turbines.

8. The system of claim 1, further comprising members that split a flow of said compressed gas from said compressor and direct said compressed gas to both of said fuel processor and fuel cell stack.

9. The system of claim 1, wherein said first and second turbines are in parallel flow communication with one another.

10. The system of claim 1, wherein said fuel processor exchanges heat to an oxidant gas that flows in parallel to said first and second turbines.

11. The system of claim 1, further comprising members that combine exhaust from said first turbine with exhaust from said second turbine to produce a combined turbine exhaust.

12. A fuel cell system, comprising:

a compressor;

a fuel processor downstream of said compressor;

a fuel cell stack in communication with said fuel processor and compressor;

a first turbine downstream of said fuel processor;

a second turbine downstream of said fuel processor and in parallel flow communication with said first turbine, said second turbine being mechanically engaged to said compressor and first turbine; and

a distribution valve in communication with said first and second turbines.

13. The system of claim 12, further comprising a bypass valve intermediate said compressor and second turbine, said bypass valve enabling a compressed gas from said compressor to bypass said fuel processor.

14. The system of claim 12, further comprising a combustor that is intermediate said fuel cell stack and first turbine.

15. The system of claim 12, wherein said combustor is intermediate said fuel cell stack and fuel processor.

16. A fuel cell system, comprising:

a compressor;

a fuel processor downstream of said compressor;

a fuel cell in communication with said fuel processor;

a heater/humidifier intermediate said compressor and fuel cell;

a first turbine downstream of said fuel processor; and

a second turbine downstream of said fuel processor and in parallel flow communication with said first turbine, said second turbine being mechanically engaged to said compressor and first turbine.

17. The system of claim 16, further comprising a distribution valve in communication with said first and second turbines.

18. The system of claim 16, wherein said heater/humidifier is downstream of said first and second turbines.

19. The system of claim 18, further comprising a condenser/separator downstream of said heater/humidifier.

20. The system of claim 16, further comprising a condenser/separator downstream of said second turbine.

21. A fuel cell system, comprising:

a compressor;

a fuel processor downstream of said compressor;

a fuel cell stack in communication with said fuel processor;

a first turbine downstream of said fuel processor;

a second turbine downstream of said fuel processor and in parallel flow communication with said first turbine, said second turbine being mechanically engaged to said compressor and first turbine; and

a condenser/separator downstream of said second turbine.

22. The system of claim 21, further comprising a heater/humidifier intermediate said second turbine and condenser/separator.

23. The system of claim 21, further comprising a heater/humidifier downstream of said condenser/separator.

24. A method of processing an oxidant gas and a fuel gas for a fuel cell system, comprising:

compressing said oxidant gas in a compressor to produce a compressed oxidant gas;

flowing a first portion of said compressed oxidant gas to a fuel cell stack;

flowing a second portion of said compressed oxidant gas to a fuel processor;

flowing said fuel gas to said fuel processor to produce a hydrogen-rich gas;

flowing said hydrogen-rich gas to said fuel cell stack;

producing a heated oxidant gas from said fuel processor;

splitting said heated oxidant gas into a first portion and a second portion of heated oxidant gas such that said first and second portions of heated oxidant gas flow parallel to one another;

expanding said first portion of said heated oxidant gas in a first turbine to produce a first turbine exhaust;

expanding said second portion of said heated oxidant gas in a second turbine to produce a second turbine exhaust; and

rotatingly engage said compressor, first turbine and second turbine to one another.

25. The method of claim 24, wherein said compressed oxidant gas is split to produce said first and second portions of compressed oxidant gas.

26. The method of claim 24, further comprising humidifying said first portion of compressed oxidant gas flowing to said fuel cell stack.

27. The method of claim 24, further comprising combusting an anode exhaust gas with a cathode exhaust gas, both of which are from said fuel cell stack, to produce a combustor exhaust.

28. The method of claim 27, further comprising expanding said combustor exhaust in said first turbine.

29. The method of claim 27, further comprising flowing said combustor exhaust to said fuel processor.

30. The method of claim 24, further comprising condensing water vapor from a humidified oxidant flow downstream of said second turbine.

31. A fuel cell system, comprising:

a compressor that provides a flow of compressed oxidant gas;

a splitter member in communication with said compressed oxidant gas flow from said compressor that splits said compressed gas flow into a first portion flow and a second portion flow;

a fuel cell stack that is downstream of said compressor and is in communication with said compressor and receives said first portion flow and that is in communication with said fuel processor;

a fuel processor that is downstream of said compressor and is in communication with and receives said second portion flow;

a first turbine downstream of said fuel processor;

a second turbine downstream of said fuel processor, said second turbine being mechanically engaged to said compressor and first turbine; and

a distribution valve in communication with said fuel processor and with said first and second turbines that distributes gas that flows from said fuel processor to said first and second turbines.

32. The system of claim 31, further comprising a bypass valve intermediate said compressor and second turbine, said bypass valve enabling a compressed gas from said compressor to bypass said fuel processor.

33. The system of claim 31, further comprising a combustor downstream of said fuel cell stack.

34. The system of claim 31, further comprising a heater/humidifier intermediate said compressor and fuel cell stack.

35. The system of claim 31, further comprising a condenser/separator downstream of said first and second turbines.

36. The system of claim 35, further comprising a heater/humidifier intermediate said condenser/separator and said first and second turbines.

37. The system of claim 31, wherein said first and second turbines are in parallel flow communication with one another.

38. The system of claim 31, wherein said fuel processor exchanges heat to an oxidant gas that flows in parallel to said first and second turbines.

39. The system of claim 31, further comprising members that combine exhaust from said first turbine with exhaust from said second turbine to produce a combined turbine exhaust.

40. A method of processing an oxidant gas for a fuel cell system, comprising:

compressing said oxidant gas in a compressor to produce a compressed oxidant gas;

flowing a first portion of said compressed oxidant gas to a fuel cell stack and a second portion to a fuel processor;

exhausting a heated oxidant gas from said fuel cell stack;

flowing a first portion of said heated oxidant gas to a first turbine wherein said first compressed oxidant gas portion expands and wherefrom expanded gas is exhausted to produce a first turbine exhaust;

flowing a second portion of said heated oxidant gas to a second turbine wherein said second compressed oxidant gas portion expands and wherefrom expanded gas is exhausted to produce a second turbine exhaust; and

engaging said compressor, first turbine and second turbine with one another.

41. The method of claim 40, further comprising a distribution valve in communication with said first and second turbines.

42. The method of claim 40, further comprising disposing said first and second portions of said heated oxidant gas in parallel to one another.

43. The method of claim 40, wherein said first and second turbines are disposed in parallel to one another.

44. The method of claim 43, further comprising combining said first and second turbine exhausts to produce a combined turbine exhaust.

45. The method of claim 44, further comprising flowing said combined turbine exhaust through a heater/humidifier intermediate said compressor and said fuel cell stack.

46. The method of claim 44, further comprising flowing said combined turbine exhaust through a condenser/separator.

47. The method of claim 40, further comprising humidifying said first compressed oxidant air portion.

48. The method of claim 40, further comprising flowing a cathode exhaust gas from said fuel cell stack to a combustor.

49. The method of claim 48, wherein said combustor is intermediate said fuel cell stack and first turbine.

50. The method of claim 40, wherein said combustor is intermediate said fuel cell stack and fuel processor.

51. The method of claim 40, wherein a heated oxidant gas is exhausted from said fuel processor.

52. The method of claim 51, further comprising combining said heated oxidant gas from said fuel processor with said heated oxidant gas exhausted from said fuel cell stack.

53. A method of processing an oxidant gas and a fuel gas for a fuel cell system, comprising:

compressing said oxidant gas in a compressor to produce a compressed oxidant gas;

splitting said compressed oxidant gas to produce first and second portions of compressed oxidant gas;

flowing said first compressed oxidant gas portion to a fuel cell stack;

flowing said second compressed oxidant gas portion to a fuel processor;

flowing said fuel gas to said fuel processor to produce a hydrogen-rich gas;

flowing said hydrogen-rich gas to said fuel cell stack;

producing a heated oxidant gas from said fuel processor;

splitting said heated oxidant gas into a first portion and a second portion of heated oxidant gas such that said first and second portions of heated oxidant gas flow parallel to one another;

flowing said first portion of said heated oxidant gas to a first turbine wherein said first compressed oxidant gas portion expands and wherefrom expanded gas is exhausted to produce a first turbine exhaust;

flowing said second portion of said heated oxidant gas to a second turbine wherein said second compressed oxidant gas portion expands and wherefrom expanded gas is exhausted to produce a second turbine exhaust; and

rotatingly engaging said compressor, first turbine and second turbine one with another.

54. The method of claim 53, further comprising humidifying said first portion of compressed oxidant gas prior to the step of flowing said first portion of said compressed oxidant gas to said fuel cell stack.

55. The method of claim 53, further comprising combusting an anode exhaust gas with a cathode exhaust gas, both of which are from said fuel cell stack, to produce a combustor exhaust.

56. The method of claim 55 further comprising expanding said combustor exhaust in said first turbine.

57. The method of claim 56, further comprising flowing said combustor exhaust to said fuel processor.

58. The method of claim 54, further comprising condensing water vapor from a humidified oxidant flow downstream of said second turbine.