Annular bearing support dampers, gas turbine engines including the same, and methods for the manufacture thereof

• US 9,046,001 B2
• Filed: 08/29/2011
• Issued: 06/02/2015
• Est. Priority Date: 08/29/2011
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Hindle, Timothy, Barber, Tim Daniel, Buchele, Paul
• Primary Examiner(s): White, Dwayne J
• Assistant Examiner(s): ELLIS, RYAN H
• Application Number:
  US13/220,081
• Publication Number:
  US 20130051982A1
• Time in Patent Office: 1,373 Days
• Field of Search: 415/104, 415/107, 415/119, 384/199, 384/535, 384/536, 384/581, 384/582, 248/636
• US Class Current: 1/1
• CPC Class Codes: F01D 25/164 Flexible supports; Vibration damping means associated with the bearing
• CPC Class Codes: F02C 7/06 Arrangements of bearings bearings F16C; Lubricating of turbo machines F01D25/18; of machines or engines in general F01M
• CPC Class Codes: F16C 2360/23 Gas turbine engines in general F02C
• CPC Class Codes: F16C 27/04 Ball or roller bearings, e.g. with resilient rolling bodies
• CPC Class Codes: F16F 15/023 using fluid means
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

Embodiments of a gas turbine engine are provided, as are embodiments of an annular bearing support damper and embodiments of a method for manufacturing an annular bearing support damper. In one embodiment, the gas turbine engine includes engine housing and a rotor assembly disposed within the engine housing. A rotor bearing supports the rotor assembly within the engine housing, and an annular bearing support damper is positioned between the rotor bearing and the engine housing. The support damper includes an annular housing assembly having a damping fluid annulus. An array of circumferentially-spaced damper pistons is movably coupled to the annular housing assembly and fluidly communicates with the damping fluid annulus. The damper pistons are fixedly coupled to the rotor bearing and moves in conjunction therewith to force the flow of damping fluid around the annulus during engine operation to reduce the transmissions of vibrations to the engine housing.

Claims

1. A gas turbine engine, comprising:

an engine housing;

a rotor assembly disposed within the engine housing;

a rotor bearing supporting the rotor assembly within the engine housing; and

an annular bearing support damper positioned between the rotor bearing and the engine housing, the annular bearing support damper comprising;

an annular housing assembly fixedly coupled to the engine housing;

a damping fluid annulus formed within the annular housing assembly and fillable with a damping fluid; and

an array of circumferentially-spaced damper pistons comprising a plurality of piston caps and bellows, the piston caps sealingly coupled to the annular housing assembly by the bellows and in fluid communication with the damping fluid annulus, the piston caps further fixedly coupled to the rotor bearing and moving in conjunction therewith to force the flow of damping fluid around the damping fluid annulus during operation of the gas turbine engine to reduce the transmissions of vibrations to the engine housing;

wherein the annular housing assembly comprises;

a circumferential wall bounding the damping fluid annulus; and

a plurality of radial openings formed in the circumferential wall and accommodating the array of circumferentially-spaced damper pistons.

2. A gas turbine engine according to claim 1 wherein the annular bearing support damper circumscribes the rotor bearing.

3. A gas turbine engine according to claim 1 wherein the annular bearing support damper further comprises a centering spring having a fixed end portion coupled to the engine housing and having a floating end portion fixedly coupled to the array of circumferentially-spaced damper pistons and to the rotor bearing.

4. A gas turbine engine according to claim 3 wherein the rotor assembly comprises a spool extending through the centering spring and through the annular bearing support damper.

5. A gas turbine engine according to claim 3 wherein the floating end portion is disposed between the annular bearing support damper and the rotor bearing.

6. A gas turbine engine according to claim 5 wherein the annular housing assembly is separated from the floating end portion by a radial gap to permit relative radial movement between the annular housing assembly and the floating end portion.

7. A gas turbine engine according to claim 3 wherein the annular bearing support damper is a three parameter device.

8. A gas turbine engine according to claim 1 wherein the array of circumferentially-spaced pistons is at least partially contained within the annular housing assembly.

9. A gas turbine engine according to claim 1 wherein the plurality of piston caps normally reside within the plurality of radial openings, and wherein the outer circumferential edge of each piston cap is separated from the inner circumferential edge of its corresponding radial opening by a circumferential clearance to accommodate lateral movement.

10. A gas turbine engine according to claim 1 wherein the plurality of pistons caps are substantially flush with the circumferential wall bounding the damping fluid annulus when the annular bearing support damper resides in a centered position.

11. A gas turbine engine according to claim 1 further comprising a centering spring having a fixed end portion coupled to the engine housing and having a floating end portion fixedly coupled to the array of circumferentially-spaced damper pistons and to the rotor bearing;

wherein the array of circumferentially-spaced damper pistons further comprises a plurality of piston shafts each having a first end fixedly coupled to one of the plurality of piston caps and a second end fixedly coupled to the floating end portion of the centering spring.

12. A gas turbine engine according to claim 1 wherein the plurality of bellows are externally pressurized.

13. A gas turbine engine according to claim 1 wherein the array of circumferentially-spaced damper pistons comprises four damper pistons positioned around the circumference of the annular housing assembly at substantially 90 degree intervals.

14. An annular bearing support damper, comprising:

an annular housing assembly having a damping fluid annulus fillable with a damping fluid;

a centering spring around which the annular housing assembly extends; and

an array of circumferentially-spaced damper pistons, each comprising;

a piston cap in fluid communication with the damping fluid annulus;

a bellows sealingly coupled between the piston cap and the annular housing assembly such that the bellows deflects as the piston cap moves with respect to the annular housing assembly to force the flow of damping fluid around the damping fluid annulus and dampen vibrations during usage of the annular bearing support damper; and

a piston shaft extending through the bellows to fixedly couple the piston cap to the centering spring.

15. An annular bearing support damper according to claim 14 wherein the annular housing assembly comprises a ring portion circumferentially bounding the damping fluid annulus, and wherein each piston cap comprises a working surface that is substantially flush with the ring portion when the annular bearing support damper resides in a centered position with respect to the centering spring.

16. An annular bearing support damper according to claim 14 wherein each piston cap comprises a working surface having a sloped outer geometry.