Gas turbine lubrication systems

Patent metadata

Field	Value
Publication number	US-10082077-B2
Application number	US-201415024506-A
Country	US
Kind code	B2
Filing date	Oct 1, 2014
Priority date	Oct 24, 2013
Publication date	Sep 25, 2018
Grant date	Sep 25, 2018

Abstract

A lubrication circuit for a gas turbine engine includes a bearing compartment, an air inlet connected to the bearing compartment, a lubricant inlet, and a lubricant outlet. The air inlet fluidly connects the bearing compartment to an environment external to the compartment. The lubricant inlet and outlet are connected to the bearing compartment. A scavenge valve is operatively connected between the lubricant outlet and a scavenge pump that is responsive to bearing compartment pressure for controlling pressure drop across the air inlet.

First claim

What is claimed is:

1. A lubrication circuit for a gas turbine engine, comprising:
a bearing compartment;
an air inlet connected to the bearing compartment;
a lubricant inlet and a lubricant outlet connected to the bearing compartment;
a scavenge pump connected to the lubricant outlet; and
a scavenge valve operatively connected between the lubricant outlet and the scavenge pump responsive to bearing compartment pressure for controlling pressure drop across the air inlet.

2. A lubrication circuit as recited in claim 1 , wherein the scavenge valve includes a movable valve member for reducing fluid flow through the scavenge valve.

3. A lubrication circuit as recited in claim 1 , wherein the scavenge valve includes a valve member movable between restricted and unrestricted positions in response to differential pressure between the bearing compartment and the bearing compartment external environment.

4. A lubrication circuit as recited in claim 2 , wherein the scavenge valve is a continuously variable scavenge valve having a valve member configured and adapted to restrict fluid flow through the scavenge valve in response to differential pressure between the bearing compartment interior and the environment external to the bearing compartment.

5. A lubrication circuit as recited in claim 4 , wherein the valve member is movable between first and second restricted positions, flow restriction being greater at the first restricted position than the second restricted position.

6. A lubrication circuit as recited in claim 4 , further including a pressure sensor connected between the bearing compartment and the scavenge valve.

7. A lubrication circuit as recited in claim 6 , further including a mechanical regulator operatively connected to the scavenge valve for controlling restriction in response to differential pressure between the bearing compartment interior and the bearing compartment external environment.

8. A lubrication circuit as recited in claim 6 , further including a control module connected to the pressure sensor and the scavenge valve and configured and adapted to vary scavenge valve restriction based on sensed pressure.

9. A lubrication circuit as recited in claim 8 , wherein the control module is tuned over a range of shaft speed to adjust restriction based on sensed pressure.

10. A lubrication circuit as recited in claim 1 , wherein the air inlet is a shaft seal bounding the bearing compartment and separating the bearing compartment interior from the environment external to the bearing compartment.

11. A lubrication circuit as recited in claim 10 , further including a spool rotatably supported by a bearing body disposed within the bearing compartment and having a rotatable portion sealably engaged by the shaft seal.

12. A lubrication circuit as recited in claim 11 , wherein the spool is mechanically connected to the scavenge pump for driving the scavenge pump.

13. A lubrication circuit as recited in claim 11 , wherein air flow through the air inlet is a function of rotational speed of the spool.

14. A lubrication system for a gas turbine engine, comprising:
a bearing compartment;
an air inlet connected to the bearing compartment;
a lubricant inlet and a lubricant outlet connected to the bearing compartment;
a scavenge pump connected to the lubricant outlet; and
a scavenge valve operatively connected between the lubricant outlet and the scavenge pump responsive to bearing compartment pressure for controlling pressure drop across the air inlet, wherein the air inlet is a contacting shaft seal bounding the bearing compartment and separating the bearing compartment interior from the environment external to the bearing compartment; and
a spool rotatably supported by a bearing body disposed within the bearing compartment and having a rotatable portion sealably engaged by the shaft seal, wherein the spool is mechanically connected to the scavenge pump for driving the scavenge pump such that air flow through the air inlet is a function of rotational speed of the spool.

15. A lubrication system as recited in claim 14 , wherein the scavenge valve is a continuously variable scavenge valve having a valve member configured and adapted to restrict fluid flow through the scavenge valve in response to differential pressure between the bearing compartment interior and the environment external to the bearing compartment.

16. A lubrication system as recited in claim 15 , wherein the valve member is movable between first and second restricted positions, flow restriction being greater at the first restricted position than the second restricted position.

17. A lubrication system as recited in claim 15 , further including a pressure sensor connected between the bearing compartment and the scavenge valve.

18. A lubrication system as recited in claim 17 , further including a mechanical regulator operatively connected to the scavenge valve for controlling restriction in response to differential pressure between the bearing compartment interior and the bearing compartment external environment.

19. A lubrication system as recited in claim 17 , further including a control module connected to the pressure sensor and the scavenge valve and configured and adapted to vary scavenge valve restriction based on sensed pressure.

Assignees

• United Technologies Corp

Inventors

• Denman James H
• Henion Julie

Classifications

• F02C7/06 Primary

  Arrangements of bearings (bearings F16C); Lubricating ({of turbo machines F01D25/18; of machines or} engines in general F01M) · CPC title

• F01D25/183

  Sealing means · CPC title

• F01M1/16

  Controlling lubricant pressure or quantity (rendering machines or engines inoperative or idling on lubricant pressure failure F01M1/22) · CPC title

• F05D2270/20

  to optimize the performance of a machine · CPC title

• F05D2260/98

  Lubrication · CPC title