Shape memory alloy reinforced casing

Patent metadata

Field	Value
Publication number	US-2022098999-A1
Application number	US-202117387002-A
Country	US
Kind code	A1
Filing date	Jul 28, 2021
Priority date	Aug 8, 2019
Publication date	Mar 31, 2022
Grant date	—

Abstract

A casing for a bearing of a gas turbine engine includes a shaft extending along an axial direction. The casing includes an attachment feature at a radially outermost portion of the casing. The attachment feature is configured to be coupled to a static frame of the gas turbine engine. The casing further includes a plurality of support arms extend from the attachment feature to a radially innermost portion of the casing. At least one support arm of the plurality of support arms defines an internal cavity. Further, the radially innermost portion of the casing is configured to be coupled to an outer race of the bearing. The casing additionally includes a reinforcing member housed at least partially within the internal cavity of at least one support arm. Moreover, the reinforcing member includes a shape memory alloy material.

First claim

What is claimed is:

1 . A casing for a bearing of a gas turbine engine including a shaft extending along an axial direction, the casing comprising:
an attachment feature at a radially outermost portion of the casing, the attachment feature configured to be coupled to a static structure of the gas turbine engine; a plurality of support arms extending from the attachment feature to a radially innermost portion of the casing; a bumper at a radially inner surface of the casing, the bumper configured to define a radial gap between the bumper and the bearing; and a deflection limiter coupled to the bumper of the casing, the deflection limiter comprising a shape memory alloy material.

2 . The casing of claim 1 , wherein the radially inner surface of the casing is a radially inner surface of the radially innermost portion of the casing.

3 . The casing of claim 1 , wherein the plurality of support arms define an internal cavity, and wherein the bumper is positioned within the internal cavity.

4 . The casing of claim 1 , wherein the bumper is a part of or coupled to the attachment feature.

5 . The casing of claim 1 , wherein the deflection limiter is configured to deform after the radial gap has been closed.

6 . The casing of claim 1 , wherein the deflection limiter comprises at least one of a ring, a segmented ring, a leaf springs, a hairpin spring, or a corrugated spring.

7 . A casing for a bearing of a gas turbine engine including a shaft extending along an axial direction, the casing comprising:
an attachment feature at a radially outermost portion of the casing, the attachment feature configured to be coupled to a static structure of the gas turbine engine; a plurality of support arms extending from the attachment feature to a radially innermost portion of the casing; and a shape memory alloy material.

8 . A casing for a bearing of a turbomachine including a shaft extending along an axial direction, the casing comprising:
an attachment feature at a radially outermost portion of the casing, the attachment feature configured to be coupled to a static structure of the turbomachine; a plurality of support arms extending from the attachment feature to a radially innermost portion of the casing; and a shape memory alloy material.

9 . The casing of claim 8 , wherein at least one support arm of the plurality of support arms defines an internal cavity, and wherein the shape memory alloy material comprises a reinforcing member housed at least partially within the internal cavity of at least one support arm of the plurality of support arms.

10 . The casing of claim 9 , wherein the plurality of support arms includes at least one axially forward support arm extending from an axially forward face of the attachment feature and at least one axially aft support arm extending from an axially aft face of the attachment feature, each of the axially forward and axially aft support arms including axial rib portions axially aligned.

11 . The casing of claim 10 , wherein the internal cavity is defined through at least a portion of the axial rib portion of at least one of the axially forward support arm or axially aft support arm.

12 . The casing of claim 10 , wherein the internal cavity is defined through the axial rib portion of the axially forward support arm, the attachment feature, and the axial rib portion of the axially aft support arm.

13 . The casing of claim 9 , wherein the reinforcing member is prestressed.

14 . The casing of claim 8 , further comprising:
a bumper at a radially inner surface the casing, the bumper configured to define a radial gap between the bumper and the bearing, and wherein the shape memory alloy material comprises a deflection limiter coupled to the bumper of the casing.

15 . The casing of claim 14 , wherein the radially inner surface of the casing is a radially inner surface of the radially innermost portion of the casing.

16 . The casing of claim 14 , wherein the plurality of support arms define an internal cavity, and wherein the bumper is positioned within the internal cavity.

17 . The casing of claim 14 , wherein the bumper is a part of or coupled to the attachment feature.

18 . The casing of claim 14 , wherein the deflection limiter is configured to deform after the radial gap has been closed.

19 . The casing of claim 14 , wherein the deflection limiter comprises at least one of a ring, a segmented ring, a leaf springs, a hairpin spring, or a corrugated spring.

20 . The casing of claim 14 , wherein the deflection limiter is prestressed.

Assignees

• Gen Electric

Inventors

• Ganiger Ravindra Shankar
• Sharma Praveen
• Mittal Shivam
• Mahadeo Bhujabal Prashant
• Kang Weize
• Schmidt Richard

Classifications

• F03G7/0614 Primary

  using shape memory elements · CPC title

• F01D25/164 Primary

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

• F05D2260/79

  Bearing, support or actuation arrangements therefor · CPC title

• F16C2202/28

  Shape memory material · CPC title

• F02C7/36

  Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user ({F02C3/107 - F02C3/13 and} F02C7/32 take precedence; couplings for transmitting rotation F16D; gearing in general F16H) · CPC title