Squeeze film damper for a gas turbine engine

Patent metadata

Field	Value
Publication number	US-10400630-B2
Application number	US-201816185184-A
Country	US
Kind code	B2
Filing date	Nov 9, 2018
Priority date	Aug 22, 2017
Publication date	Sep 3, 2019
Grant date	Sep 3, 2019

Abstract

Squeeze film damping systems and methods therefore are provided that include features for optimizing the damping response to vibrational loads experienced by a rotary component of a gas turbine engine. In one exemplary aspect, a damping system actively controls a dynamic sleeve to adjust the damping response. In particular, the dynamic sleeve is disposed within a chamber defined by a damper housing. The damping system controls the damper gap by translating the dynamic sleeve. When the dynamic sleeve is translated, a variable damper gap is varied, allowing for fluid to squeeze into or out of the damper gap, thereby adjusting the damping response to the vibration of the rotary component.

First claim

What is claimed is:

1. A damping system for damping vibrations of a rotary component operatively coupled thereto, the damping system comprising:
a damper housing having an inclined surface and defining a chamber;
a dynamic sleeve movable within the chamber, the dynamic sleeve having an inclined surface complementary to the inclined surface of the damper housing, the inclined surface of the dynamic sleeve and the inclined surface of the damper housing defining a damper gap therebetween, and
wherein when the sleeve is moved within the chamber, the damper gap is varied such that a damping response of the damping system is varied.

2. The damping system of claim 1 , wherein the dynamic sleeve extends between a first end and a second end along an axial direction and has a first end portion at the first end, and wherein the dynamic sleeve has a first wall extending between the first end and the second end, the inclined surface of the dynamic sleeve forms a portion of the first wall, and wherein the first wall along the first end portion is not inclined with respect to the axial direction.

3. The damping system of claim 2 , further comprising:
one or more seals operable to engage the first end portion of the dynamic sleeve throughout the movement of the dynamic sleeve within the chamber.

4. The damping system of claim 2 , wherein the dynamic sleeve has a second end portion at the second end, and wherein the first wall along the second end portion is not inclined with respect to the axial direction.

5. The damping system of claim 4 , further comprising:
one or more seals operable to engage the second end portion of the dynamic sleeve throughout the movement of the dynamic sleeve within the chamber.

6. The damping system of claim 1 , wherein the first damper gap is operable to receive an amount of fluid to form a first squeeze film, and wherein when the sleeve is moved within the chamber, the damper gap and a thickness of the first squeeze film vary such that the damping response of the damping system is varied.

7. The damping system of claim 1 , wherein the sleeve has a first wall and a second wall spaced from the first wall along a radial direction, and wherein the inclined surface of the dynamic sleeve forms a portion of the first wall and the second wall has an inclined surface.

8. The damping system of claim 1 , wherein the dynamic sleeve extends between a first end and a second end along an axial direction, and wherein the inclined surface of the first wall and the inclined surface of the second wall diverge toward one another along the radial direction at the second end.

9. A method for varying a damping response of a damping system for a rotary component coupled therewith, the damping system having a damper housing defining a chamber in which a dynamic sleeve is disposed, and wherein a variable damper gap is defined between the dynamic sleeve and the damper housing, the method comprising:
moving the dynamic sleeve within the chamber to vary the variable damper gap such that the damping response of the damping system is varied.

10. The method of claim 9 , further comprising:
receiving, by a controller of the damping system, a rotary speed input indicative of a rotary speed of the rotary component; and
determining, by the controller, whether the rotary component has reached a predetermined speed based at least in part on the rotary speed input.

11. The method of claim 10 , further comprising:
determining, by the controller, whether the rotary component is operating under a bowed rotor start condition if the rotary component has not reached the predetermined speed; and
causing, by the controller, the dynamic sleeve to move within the chamber based at least in part on whether the rotary component is operating under the bowed rotor start condition.

12. The method of claim 9 , further comprising:
receiving, by a controller of the damping system, an oil temperature input indicative of an oil temperature associated with the rotary component;
determining, by the controller, whether the oil temperature has reached a threshold temperature based at least in part on the oil temperature input, and
causing, by the controller, the dynamic sleeve to move within the chamber based at least in part on whether the oil temperature has reached the threshold temperature.

13. The method of claim 12 , wherein if the oil temperature has reached the threshold temperature, the controller causes the dynamic sleeve to move within the chamber such that the variable damper gap is decreased, and wherein if the oil temperature has not reached the threshold temperature, the controller causes the dynamic sleeve to move within the chamber such that the variable damper gap is increased.

14. The method of claim 9 , further comprising:
receiving, by a controller of the damping system, a vibration input indicative of a vibration of the rotary component;
determining, by the controller, whether the vibration of the rotary component has reached a vibration threshold based at least in part on the vibration input, and
causing, by the controller, the dynamic sleeve to move within the chamber based at least in part on whether the vibration of the rotary component has reached the vibration threshold.

15. The method of claim 9 , wherein the damper housing has an inclined surface and the dynamic sleeve has an inclined surface complementary to the inclined surface of the damper housing, and wherein the variable damper gap is defined between the inclined surface of the dynamic sleeve and the incline surface of the damper housing.

16. The method of claim 9 , wherein the sleeve is at least one of hydraulically, pneumatically, magnetically, electromagnetically, and mechanically moved within the chamber.

17. A turbomachine, comprising:
a rotary component rotatable about an axis of rotation;
a damping system, comprising:
a damper housing operatively coupled with the rotary component and defining a chamber;
a dynamic sleeve movable within the chamber, wherein a damper gap is defined between the dynamic sleeve and the damper housing and is operable to receive an amount of fluid, and
wherein when the sleeve is moved within the chamber, the damper gap is varied such that a damping response of the damping system is varied.

18. The turbomachine of claim 17 , wherein the turbomachine defines an axial direction and a radial direction, and wherein the damper housing has an inclined surface, and wherein the dynamic sleeve has a first wall and a second wall spaced from the first wall along the radial direction, and wherein the inclined surface of the damper housing and the first wall of the dynamic sleeve define the damper gap configured to receive the amount of fluid to form a first squeeze film.

19. The turbomachine of claim 18 , further comprising:
a bearing assembly operatively coupling the rotary component and the damper housing, the bearing assembly having a bearing interface, and
wherein the second wall of the dynamic sleeve and the bearing interface define a second damper gap configured to receive an amount of fluid to form a second squeeze film, and wherein the dynamic sleeve defines a radial throughhole that provides fluid communication between the first squeeze film and the second squeeze film.

20. The turbomachine of claim 18 , further comprising:
a bearing assembly operatively coupling the rotary component and the damper housing, the bearing assembly having a bearing interface, and
wherein the second wall of the dynamic sleeve has an inclined s

Assignees

• Gen Electric

Inventors

• Ganiger Ravindra Shankar
• Yadav Satish Kumar
• Ghosh Shuvajyoti

Classifications

• F16F15/0237

  involving squeeze-film damping · CPC title

• F01D25/06

  for preventing blade vibration (means on blade-carrying members or blades F01D5/00) · CPC title

• F16C27/045

  with a fluid film, e.g. squeeze film damping · CPC title

• F16C2360/23

  Gas turbine engines · CPC title

• F01D25/164 Primary

  Flexible supports; Vibration damping means associated with the bearing · CPC title