Power unit fuel pressurization system

• US 5,184,458 A
• Filed: 11/21/1989
• Issued: 02/09/1993
• Est. Priority Date: 11/21/1989
• Status: Expired due to Fees

• Current Assignee: Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Lampe, Steven W., McArthur, Malcolm J.
• Primary Examiner(s): Bertsch, Richard A.
• Assistant Examiner(s): KOCHAROV, MICHAEL
• Application Number:
  US07/439,684
• Time in Patent Office: 1,176 Days
• Field of Search: 60/39.141, 60/39.142, 60/39.21, 60/39.27, 60/246, 60/727, 60/728, 60/39.163, 60/39.15, 60/39.33
• US Class Current: 60/787
• CPC Class Codes: B64D 41/00 Power installations for auxiliary purposes
• CPC Class Codes: F02C 7/272 generated by cartridges
• CPC Class Codes: F02C 7/277 the starter being a separate turbine
• CPC Class Codes: F02C 7/32 Arrangement, mounting, or driving, of auxiliaries
• CPC Class Codes: F05D 2220/50 for auxiliary power units (APU's)
• CPC Class Codes: F05D 2260/4023 through a friction clutch
• CPC Class Codes: Y02T 50/40 Weight reduction
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A power generating unit in accordance with the present invention comprises a pressurized gas source (44) providing pressurized gas containing oxygen to be used in combustion of a fuel; a combustor (42) for providing pressurized gas produced by combustion of a mixture of the pressurized gas provided to the combustor by the pressurized gas source and fuel provided to the combustor by a fuel supply (48); a first turbine (68) driven by pressurized gas produced by the combustor; a gear box (70) driven by the turbine having an output shaft (72); a fuel pump (46) disposed within the fuel supply having a pair of input shafts (64 and 76) for providing pressurized fuel to the combustor in response to rotation of either of the input shafts; a motor (58) coupled to the pressurized gas source having a drive shaft (60) which rotates in response to the pressurized gas applied from the gas source; and a coupling mechanism (62 and 74), coupled to the shafts, for applying driving torque to the fuel pump during rotation of the pressurized gas to the combustor from the input shaft which is rotating at a higher velocity.

Claims

1. A power generating unit for use in an airframe for supplying at least emergency power to a load comprising:

a pressurized gas source storing pressurized gas containing oxygen to be used in combusting a fuel;

a combustor for providing pressurized gas produced by combustion of a mixture of the pressurized gas provided to the combustor by the pressurized gas source and fuel provided to the combustor by a fuel supply;

a first turbine driven by pressurized gas produced by the combustor;

a gear box driven by the turbine having an output shaft;

a pair of input shafts directly connected to a fuel pump comprising the load disposed within the fuel supply for providing pressurized fuel to the combustor in response to rotation of either of the input shafts;

a motor coupled to the pressurized gas source having a drive shaft which rotates in response to pressurized gas applied from the gas source; and

means, coupled to the output and drive shafts, for applying driving torque to the fuel pump during application of pressurized gas to the combustor from the output or drive shaft, whichever is rotating at a higher velocity.

2. A power generating unit in accordance with claim 1 wherein the means for applying torque comprises:

a first overrunning clutch coupled to the output shaft and one of the input shafts; and

a second overrunning clutch coupled to the drive shaft and another of the input shafts.

3. A power generating unit in accordance with claim 1 wherein:

the motor has a rated operating rotational speed in driving the fuel pump in response to the stored pressurized gas which is less than the rotational velocity at which the output shaft drives the fuel pump when the first turbine is producing full output power.

4. A power generating unit in accordance with claim 2 wherein:

the motor has a rated operating rotational speed in driving the fuel pump in response to the stored pressurized gas which is less than the rotational velocity at which the output shaft drives the fuel pump when the first turbine is producing full output power.

5. A power generating unit in accordance with claim 1, wherein:

the first turbine is part of an emergency power unit.

6. A power generating unit in accordance with claim 2 wherein:

the first turbine is part of an emergency unit.

7. A power generating unit in accordance with claim 3 wherein:

the first turbine is part of an emergency power unit.

8. A power generating unit in accordance with claim 4, wherein:

the first turbine is part of an emergency power unit.

9. A power generating unit in accordance with claim 1, wherein:

the first turbine is part of an emergency power unit; and

further comprising

an auxiliary power unit coupled to the gear box containing a combustor driving a second turbine, the fuel pump being driven through the gear box by the second turbine to provide pressurized fuel to the second turbine during operation of the auxiliary power unit.

10. A power generating unit in accordance with claim 2 wherein:

the first turbine is part of an emergency power unit; and

further comprising

an auxiliary power unit coupled to the gear box containing a combustor driving a second turbine, the fuel pump being driven through the gear box by the second turbine to provide pressurized fuel to the second turbine during operation of the auxiliary power unit.

11. A power generating unit in accordance with claim 3 wherein:

the first turbine is part of an emergency power unit; and

further comprising

an auxiliary power unit coupled to the gear box containing a combustor driving a second turbine, the fuel pump being driven through the gear box by the second turbine to provide pressurized fuel to the second turbine during operation of the auxiliary power unit.

12. A power generating unit in accordance with claim 4 wherein:

the first turbine is part of an emergency power unit; and

further comprising

an auxiliary power unit coupled to the gear box containing a combustor driving a second turbine, the fuel pump being driven through the gear box by the second turbine to provide pressurized fuel to the second turbine during operation of the auxiliary power unit.

13. A power generating unit in accordance with claim 1 wherein the load further comprises:

an electrical generator, driven from the input shaft which is rotating at a higher velocity by the means for applying driving torque, for providing electrical power for use in starting the turbine.

14. A power generating unit in accordance with claim 2 wherein the load further comprises:

a self-excited electrical generator, driven from the input shaft which is rotating at a higher velocity by the means for applying driving torque, for providing electrical power for use in starting the turbine.

15. A power generating unit in accordance with claim 3 the load further comprises:

a self-excited electrical generator, driven from the input shaft which is rotating at a higher velocity by the means for applying driving torque, for providing electrical power for use in starting the turbine.

16. A power generating unit in accordance with claim 4 the load further comprises:

a self-excited electrical generator, driven from the input shaft which is rotating at a higher velocity by the means for applying driving torque, for providing electrical power for use in starting the turbine.

17. A power generating unit in accordance with claim 5 wherein:

the gear box is coupled to a power generator.

18. A power generating unit in accordance with claim 17, wherein:

the power generator generates electrical power.

19. A power generating unit in accordance with claim 17, wherein:

the power generator generates hydraulic power.

20. A power generating unit in accordance with claim 17, wherein:

the power generator generates electrical and hydraulic power.

21. A power generating unit for use in an airframe for supplying at least emergency power to a load comprising:

a pressurized gas source storing pressurized gas containing oxygen to be used in combusting a fuel;

a combustor for providing pressurized gas produced by combustion of a mixture of the pressurized gas provided to the combustor by the pressurized gas source and fuel provided to the combustor by a fuel supply;

a first turbine driven by pressurized gas produced by the combustor;

a gear box driven by the turbine having an output shaft;

a pair of input shafts directly connected to a fuel pump and a self-excited electrical generator comprising the load for providing an output utilized in operation of the turbine in response to rotation of either of the input shafts;

a motor coupled to the pressurized gas source having a drive shaft which rotates in response to pressurized gas applied from the gas source; and

means, coupled to the output and drive shafts, for applying driving torque to the driven element during application of pressurized gas to the combustor from the output or drive shaft, whichever is rotating at a higher velocity.

22. A power generating unit in accordance with claim 21 wherein the means for applying torque comprises:

a first overrunning clutch coupled to the output shaft and one of the input shafts; and

a second overrunning clutch coupled to the drive shaft and another of the input shafts.

23. A power generating unit in accordance with claim 21 wherein:

the motor has a rated operating rotational speed in driving the driven element in response to the stored pressurized gas which is less than the rotational velocity at which the output shaft drives the driven element when the first turbine is producing full output power.

24. A power generating unit in accordance with claim 22 wherein:

the motor has a rated operating rotational speed in driving the driven element in response to the stored pressurized gas which is less than the rotational velocity at which the output shaft drives the driven element when the first turbine is producing full output power.

25. A power generating unit for use in an airframe for supplying at least emergency power to a load comprising:

a pressurized gas source storing pressurized gas containing oxygen to be used in combusting a fuel;

a combustor for providing pressurized gas produced by combustion of a mixture of the pressurized gas provided to the combustor by the pressurized gas source and fuel provided to the combustor by a fuel supply;

a first turbine driven by pressurized gas produced by the combustor;

a gear box driven by the turbine having an output shaft;

a pair of input shafts directly connected to a self-excited electrical generator comprising the load for providing electrical power in response to rotation of either of the input shafts for use in starting the turbine;

a motor coupled to the pressurized gas source having a drive shaft which rotates in response to pressurized gas applied from the gas source; and

means, coupled to the output and drive shafts, for applying driving torque to the generator during application of pressurized gas to the combustor from the output or drive shaft, whichever is rotating at a higher velocity.

26. A power generating unit in accordance with claim 25 wherein the means for applying torque comprises:

a first overrunning clutch coupled to the output shaft and one of the input shafts; and

a second overrunning clutch coupled to the drive shaft and another of the input shafts; and

wherein

the electrical power generator is a permanent magnet generator.

27. A power generating unit in accordance with claim 25 wherein:

the motor has a rated operating rotational speed in driving the electrical generator in response to the stored pressurized gas which is less than the rotational velocity at which the output shaft drives the electrical generator when the first turbine is producing full output power.

28. A power generating unit in accordance with claim 26 wherein:

the motor has a rated operating rotational speed in driving the electrical generator in response to the stored pressurized gas which is less than the rotational velocity at which the output shaft drives the electrical generator when the first turbine is producing full output power.

29. A power generating unit for use in an airframe for supplying at least emergency power to a load comprising:

a pressurized gas source storing pressurized gas containing oxygen to be used in combusting a fuel;

a combustor for providing pressurized gas produced by combustion of a mixture of the pressurized gas provided to the combustor by the pressurized gas source and fuel provided to the combustor by a fuel supply;

a first turbine driven by pressurized gas produced by the combustor;

a gear box driven by the turbine having an output shaft;

a pair of input shafts directly connected to a driven element comprising the load for providing an output utilized in operating the turbine in response to rotation of either of the input shafts;

a motor which is activated during pressurized gas being supplied from the gas source to the combustor to rotate a drive shaft; and

means, coupled to the output and drive shafts, for applying driving torque to the driven element during application of pressurized gas to the combustor from the output or drive shaft, whichever is rotating at a higher velocity.

30. A power generating unit in accordance with claim 29 wherein the means for applying torque comprises:

a first overrunning clutch coupled to the output shaft and one of the input shafts; and

a second overrunning clutch coupled to the drive shaft and another of the input shafts.

31. A power generating unit in accordance with claim 29 wherein:

the motor has a rated operating rotational speed in driving the fuel pump in response to the stored pressurized gas prior to the combustion not producing full output power which is less than the rotational velocity at which the output shaft drives the fuel pump when the first turbine is producing full output power.

32. A power generating unit in accordance with claim 30 wherein:

the motor has a rated operating rotational speed in driving the fuel pump in response to the stored pressurized gas which is less than the rotational velocity at which the output shaft drives the fuel pump when the first turbine is producing full output power.