IP Library Granted Patent US 10,830,179
Granted Patent B2
US 10,830,179 · App. 15/907,363 · Granted Nov 10, 2020

Variable bleed valve door assembly and system for gas turbine engines

Inventor: Ami Hatim (Karnataka, IN)
Assignee: GENERAL ELECTRIC COMPANY
F02K3/075F01D17/105F02C9/18F02C6/08F05D2270/62F05D2270/64F05D2270/65F16K1/2007F16K1/2021
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Quick Facts
Patent No.
US 10,830,179
App. No.
15/907,363
Granted
Nov 10, 2020
Kind
B2
Abstract

A variable bleed valve system for use in a turbofan engine includes a plurality of circumferentially spaced variable bleed valve assemblies. Each variable bleed valve assembly includes a plurality of circumferentially spaced variable bleed valve assemblies. Each variable bleed valve assembly includes a variable bleed valve door that is selectively adjustable through a range of intermediate positions between a closed position and an open position. The variable bleed valve door is configured to maintain any of the intermediate positions. Each variable bleed valve assembly also includes an actuator operatively coupled to the variable bleed valve door. The actuator is configured to selectively adjust a position of the variable bleed valve door through the range of intermediate positions between the closed position and the open position.

Claims (43)

1. A variable bleed valve system for use in a turbofan engine, said variable bleed valve system comprising:

a plurality of circumferentially spaced variable bleed valve assemblies, each variable bleed valve assembly of said plurality of variable bleed valve assemblies comprising:

a variable bleed valve door selectively adjustable through a range of intermediate positions between a closed position and an open position, said variable bleed valve door configured to maintain any of the intermediate positions; and

an actuator operatively coupled to said variable bleed valve door, said actuator configured to selectively adjust a position of said variable bleed valve door through the range of intermediate positions between the closed position and the open position, the position of said variable bleed valve door independently adjustable with respect to positions of each other variable bleed valve door of said plurality of variable bleed valve assemblies.

2. The variable bleed valve system of claim 1 , wherein each variable bleed valve assembly of said plurality of variable bleed valve assemblies further comprises:

a support member;

a translating member comprising a first end, a second end, and a body extending therebetween, said first end slidably coupled on said support member; and

a coupling member pivotally coupled between said second end of said translating member and said variable bleed valve door.

3. The variable bleed valve system of claim 2 , wherein said actuator is configured to translate said translating member on said support member.

4. The variable bleed valve system of claim 2 , wherein said coupling member is coupled to said translating member by a first joint and to said variable bleed valve door by a second joint.

5. The variable bleed valve system of claim 4 , wherein said first joint and said second joint are revolute joints.

6. The variable bleed valve system of claim 1 , wherein said actuator drives a single variable bleed valve door of said plurality of variable bleed valve assemblies.

7. The variable bleed valve system of claim 1 , wherein a position of one of said plurality of variable bleed valve assemblies is adjustable to compensate for an off normal position of one or more variable bleed valve assemblies.

8. A turbofan engine comprising:

a core engine case defining a compressor flow duct;

a high pressure compressor disposed within the compressor flow duct;

a low pressure compressor disposed axially upstream of said high pressure compressor;

a transition duct extending between said high pressure compressor and said low pressure compressor;

a plurality of circumferentially spaced variable bleed valve assemblies extending circumferentially about said transition duct, each variable bleed valve assembly of said plurality of variable bleed valve assemblies comprising:

a variable bleed valve door selectively adjustable through a range of intermediate positions between a closed position and an open position, said variable bleed valve door configured to maintain any of the intermediate positions; and

an actuator operatively coupled to said variable bleed valve door, said actuator configured to selectively adjust a position of said variable bleed valve door through the range of intermediate positions between the closed position and the open position, the position of said variable bleed valve door independently adjustable with respect to positions of each other variable bleed valve door of said plurality of variable bleed valve assemblies.

9. The turbofan engine of claim 8 , wherein said core engine case further comprises:

a compressor flow duct surface and a bypass air duct surface disposed radially outward of said compressor flow duct surface, and wherein a bleed duct is defined between said compressor flow duct surface and said bypass air duct surface.

10. The turbofan engine of claim 9 , wherein each variable bleed valve assembly is disposed within the bleed duct.

11. The turbofan engine of claim 8 , wherein each variable bleed valve assembly of said plurality of variable bleed valve assemblies further comprises:

a support member;

a translating member comprising a first end, a second end, and a body extending therebetween, said first end slidably coupled on said support member; and

a coupling member pivotally coupled between said second end of said translating member and said variable bleed valve door.

12. The turbofan engine of claim 11 , wherein said actuator is configured to translate said translating member on said support member.

13. The turbofan engine of claim 11 , wherein said coupling member is coupled to said translating member by a first joint and to said variable bleed valve door by a second joint.

14. The turbofan engine of claim 8 , wherein said actuator drives a single variable bleed valve door of said plurality of variable bleed valve assemblies.

15. The turbofan engine of claim 8 , wherein one of said plurality of variable bleed valve assemblies is adjustable to compensate for an off normal position of one or more variable bleed valve assemblies.

16. A variable bleed valve variable bleed valve assembly for use in a turbofan engine, the variable bleed valve assembly comprising:

a variable bleed valve door selectively adjustable through a range of intermediate positions between a closed position and an open position, said variable bleed valve door configured to maintain any of the intermediate positions; and

an actuator operatively coupled to said variable bleed valve door, said actuator configured to selectively adjust a position of said variable bleed valve door through the range of intermediate positions between the closed position and the open position, the position of said variable bleed valve door independently adjustable with respect to positions of each other variable bleed valve door.

17. The variable bleed valve assembly of claim 16 , wherein said variable bleed valve assembly further comprises:

a support member;

a translating member comprising a first end, a second end, and a body extending therebetween, said first end slidably coupled on said support member; and

a coupling member pivotally coupled between said second end of said translating member and said variable bleed valve door.

18. The variable bleed valve assembly of claim 17 , wherein said actuator is configured to translate said translating member on said support member.

19. The variable bleed valve assembly of claim 17 , wherein said coupling member is coupled to said translating member by a first joint and to said variable bleed valve door by a second joint.

20. The variable bleed valve assembly of claim 16 , wherein said actuator drives a single variable bleed valve door of a plurality of variable bleed valve assemblies.

21. The variable bleed valve assembly of claim 17 , wherein said variable bleed valve door is configured to open at least one of radially inward or radially outward.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 28, 2018
From: HATIM, AMI
To: GENERAL ELECTRIC COMPANY
Reel/Frame 045058/0927 →
Priority Claims (1)
IN 201741007280 · Mar 1, 2017 · national
Continuity (1)
Related Publication 20180252184A1 · Sep 6, 2018
Cited By (13)
US 12,320,259 US 12,366,202 US 12,416,261 US 12,618,368 US 12,631,143 US 12,655,804 US 12,663,016 US 12,669,131 US 12,674,467 US 12,674,468 US 12,680,552 US 12,692,874 US 12,704,092