Aircraft fuel system with clutched augmentor pump

Patent metadata

Field	Value
Publication number	US-11971040-B2
Application number	US-202117509996-A
Country	US
Kind code	B2
Filing date	Oct 25, 2021
Priority date	Oct 25, 2021
Publication date	Apr 30, 2024
Grant date	Apr 30, 2024

Abstract

A fuel system is disclosed for a gas turbine engine, which includes an augmentor pump having an inlet communicating with a fuel supply source and a discharge communicating with an augmentation stage of the engine, wherein the augmentor pump is connected to an accessory drive gearbox mounted to the engine, and a high speed clutch for selectively engaging and disengaging the augmentor pump and the accessory drive gearbox.

First claim

What is claimed is:

1. A fuel system for a gas turbine engine comprising:
a) an augmentor pump having an inlet communicating with a fuel supply source and a discharge communicating with an augmentation stage of the engine, wherein the augmentor pump is connected to an accessory drive gearbox mounted to the engine along a common drive shaft, wherein the augmentor pump, the drive gearbox and the engine are all mounted on the common drive shaft; and
b) a high speed clutch for selectively engaging and disengaging the augmentor pump and the accessory drive gearbox, wherein the high speed clutch is positioned between the augmentor pump and the drive gearbox along the common drive shaft.

2. The fuel system of claim 1 , wherein the augmentor pump is a centrifugal pump.

3. The fuel system of claim 1 , wherein the fuel supply source is a boost stage pump drawing fuel from a fuel storage tank.

4. The fuel system of claim 1 , wherein the fuel supply source is an inducer drawing fuel from a fuel storage tank.

5. The fuel system of claim 1 , wherein a duplex ball bearing arrangement is operatively associated with the common drive shaft of the augmentor pump.

6. The fuel system of claim 1 , wherein a journal bearing arrangement is operatively associated with the common drive shaft of the augmentor pump.

7. The fuel system of claim 5 , wherein a fluid seal is positioned between the duplex ball bearing arrangement and the augmentor pump.

8. The fuel system of claim 6 , wherein a fluid seal is positioned between the high speed clutch and the journal bearing arrangement.

9. The fuel system of claim 1 , wherein a check valve is operatively associated with the discharge of the augmentor pump.

10. The fuel system of claim 1 , wherein the high speed clutch is electro-magnetically actuated or hydraulically actuated.

11. A fuel system for a gas turbine engine comprising:
a) an augmentor pump having an inlet communicating with a boost pump drawing fuel from a fuel storage tank and a discharge communicating with an augmentation stage of the engine, wherein the augmentor pump is connected to an accessory drive gearbox mounted to the engine along a common drive shaft, wherein the augmentor pump, the drive gearbox and the engine are all mounted on the common drive shaft; and
b) a high speed clutch for selectively engaging and disengaging the augmentor pump and the accessory drive gearbox, wherein the high speed clutch is positioned between the augmentor pump and the drive gearbox along the common drive shaft.

12. The fuel system of claim 11 , wherein the augmentor pump is a centrifugal pump.

13. The fuel system of claim 11 , wherein a duplex ball bearing arrangement is operatively associated with the common drive shaft of the augmentor pump and a fluid seal is positioned between the duplex ball bearing arrangement and the augmentor pump.

14. The fuel system of claim 11 , wherein a journal bearing arrangement is operatively associated with the common drive shaft of the augmentor pump and a fluid seal is positioned between the high speed clutch and the journal bearing arrangement.

15. The fuel system of claim 11 , wherein a check valve is operatively associated with the discharge of the augmentor pump.

16. A fuel system for a gas turbine engine comprising:
a) an augmentor pump having an inlet communicating with an inducer drawing fuel from a fuel storage tank and a discharge communicating with an augmentation stage of the engine, wherein the augmentor pump is connected to an accessory drive gearbox mounted to the engine along a common drive shaft, wherein the augmentor pump, the drive gearbox and the engine are all mounted on the common drive shaft; and
b) a high speed clutch for selectively engaging and disengaging the augmentor pump and the accessory drive gearbox, wherein the high speed clutch is positioned between the augmentor pump and the drive gearbox along the common drive shaft.

17. The fuel system of claim 16 , wherein the augmentor pump is a centrifugal pump.

18. The fuel system of claim 16 , wherein a duplex ball bearing arrangement is operatively associated with the augmentor pump and a fluid seal is positioned between the duplex ball bearing arrangement and the augmentor pump.

19. The fuel system of claim 16 , wherein a journal bearing arrangement is operatively associated with the augmentor pump and a fluid seal is positioned between the high speed clutch and the journal bearing arrangement.

20. The fuel system of claim 16 , wherein a check valve is operatively associated with the discharge of the augmentor pump.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Goy Edward W
• Blewett Michael R

Classifications

• F04D13/14 Primary

  the pumps being all of centrifugal type {(deviation valves F04D15/0016)} · CPC title

• F04D13/021

  containing a coupling · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F05D2240/515

  Electromagnetic · CPC title

• F05D2240/55

  Seals · CPC title