Turbomachine bearing support structure

Patent metadata

Field	Value
Publication number	US-9695870-B2
Application number	US-201314427760-A
Country	US
Kind code	B2
Filing date	Jan 18, 2013
Priority date	Sep 25, 2012
Publication date	Jul 4, 2017
Grant date	Jul 4, 2017

Abstract

A centering spring assembly of a turbomachine according to an exemplary aspect of the present disclosure includes, among other things, a damper beam, a bearing support, and a spanner nut. At least a portion of the damper beam axially overlaps at least a portion of the spanner nut relative to a rotational axis of the turbomachine.

First claim

We claim:

1. A centering spring assembly of a turbomachine, comprising:
a damper beam;
a bearing support;
a connection flange connecting to the bearing support at a first interface and to the damper beam at a second interface;
a spanner nut having a main body portion; and
a spanner nut flange structure extending radially from the main body portion toward a rotational axis of the turbomachine to provide an axial boundary of a lubrication trough, the spanner nut flange structure axially overlapping with at least a portion of the connection flange, the spanner nut flange structure axially overlapping with at least a portion of the bearing support, wherein the spanner nut flange structure that provides the axial boundary is axially aligned with the first interface such that no portion of the spanner nut flange structure providing the axial boundary extends axially outside the first interface.

2. The centering spring assembly of claim 1 , wherein the spanner nut is configured to directly contact an axially facing surface of a bearing race.

3. The centering spring assembly of claim 1 , wherein at least a portion of the first interface is upstream from an axially forwardmost portion of the second interface relative to a direction of flow through the turbomachine such that the connection flange extends along a longitudinal axis having an axial component.

4. The centering spring assembly of claim 1 , including a plurality of the damper beam distributed circumferentially about a rotation axis of the turbomachine.

5. The centering spring assembly of claim 1 , wherein the connection flange extends along a longitudinal axis having an axial component such that the connection flange is angled relative to a radial direction.

6. A centering spring assembly of a turbomachine, comprising:
a damper beam;
a bearing support;
a radial flange having a first end connected to the bearing support at a first interface, and a second end connected to the damper beam at a second interface that is downstream from the first interface relative to a direction of flow through the turbomachine, the radial flange extending along a longitudinal axis having an axial component;
a spanner nut, wherein at least a portion of the damper beam axially overlaps at least a portion of the spanner nut relative to a rotational axis of the turbomachine; and
a flange structure extending radially from a main body portion of the spanner nut toward the axis to provide an axial boundary of a lubrication trough, wherein the flange structure providing the axial boundary is axially aligned with the first interface such that no portion of the flange structure providing the axial boundary extends axially outside the first interface.

7. The centering spring assembly of claim 6 , wherein the damper beam is radially outside the bearing support.

8. The centering spring assembly of claim 6 , wherein the radial flange is a first radial flange extending from a first end of the damper beam, and a second radial flange extends from a second end of the damper beam, the first end opposite the second end.

9. The centering spring assembly of claim 8 , wherein the first and second radial flange extend from the damper beam in opposite radial directions.

10. The centering spring assembly of claim 6 , wherein the bearing support and the damper beam are portions of a single continuous piece.

11. The centering spring assembly of claim 6 , including a bearing race that is radially supported by the bearing support, and axially supported by the spanner nut.

12. The centering spring assembly of claim 6 , including an outer race of a ball bearing assembly support, the outer race supported by the bearing support.

13. The centering spring assembly of claim 6 , wherein at least a portion of the radial flange axially overlaps at least a portion of the damper beam.

14. A method of supporting a centering spring, comprising:
damping a centering spring at a position that axially overlaps a bearing support;
rotatably supporting a turbine shaft with a bearing assembly;
supporting the bearing assembly with the bearing support, wherein a connection flange connects to a damping member providing the damping to the bearing support, and the position of the damping at least partially axially overlaps an interface between the connection flange and the bearing support; and
capturing lubricant from the bearing assembly or a bearing compartment using a trough that is defined at an axial end by a flange structure extending radially from a spanner nut toward the axis, wherein the flange structure defining the axial end is axially aligned with the interface such that no portion of the flange structure defining the axial end extends axially outside the interface between the connection flange and the bearing support.

15. The method of claim 14 , wherein the damping member providing the damping axially overlaps at least a portion of the spanner nut.

16. The method of claim 14 , wherein the connection flange extends along a longitudinal axis having an axial component such that the connection flange is transverse to a radial direction.

Assignees

• United Technologies Corp

Inventors

• Amador Armando
• Mccutchan Sean

Classifications

• F16C19/06

  with a single row or balls · CPC title

• F16C27/04

  Ball or roller bearings, e.g. with resilient rolling bodies · CPC title

• F16C27/045

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

• F01D25/164 Primary

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

• F16C2360/23

  Gas turbine engines · CPC title