Support system having shape memory alloys

US10968775B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10968775-B2
Application numberUS-201715823631-A
CountryUS
Kind codeB2
Filing dateNov 28, 2017
Priority dateNov 28, 2017
Publication dateApr 6, 2021
Grant dateApr 6, 2021

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  1. Title

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  2. Abstract

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  4. Key dates

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  5. First independent claim

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Abstract

Official abstract text for this publication.

A support system for a gas turbine engine is provided. The support system includes a load-bearing unit that includes a first flange, a support element supporting the load-bearing unit and having a second flange, a fastener connecting the first flange and the second flange, a first super-elastic shape memory alloy component in contact with the first flange, and a second super-elastic shape memory alloy component in contact with the second flange. The first and the second super-elastic shape memory alloy components are configured to deform when a load exerted by the fastener exceeds a threshold load value of the fastener.

First claim

Opening claim text (preview).

The invention claimed is: 1. A support system for a gas turbine engine, the support system comprising: a load-bearing unit comprising a first flange; a support element supporting the load-bearing unit, the support element comprising a second flange; a fastener connecting the first flange and the second flange; a first super-elastic shape memory alloy component in contact with a first side of the first flange, the first side of the first flange being opposite a second side of the first flange, the second side of the first flange adjacent a first side of the second flange; and a second super-elastic shape memory alloy component in contact with a second side of the second flange, the first side of the second flange being opposite the second side of the second flange, wherein the first and the second super-elastic shape memory alloy components are configured to deform when a load exerted by the fastener exceeds a threshold load value of the fastener. 2. The support system of claim 1 , wherein the first flange is a bearing housing flange of a rotor support system. 3. The support system of claim 1 , wherein the second flange is a forward mounting flange of a bearing cone. 4. The support system of claim 1 , wherein the first super-elastic shape memory alloy component is in the form of a gusset, a flange, a bolt, a bolt sleeve, a gasket seal, a washer, or combinations thereof. 5. The support system of claim 1 , wherein the second super-elastic shape memory alloy component is in the form of a gusset, a bolt, a bolt sleeve, a gasket seal, a washer, or combinations thereof. 6. The support system of claim 1 , wherein both the first and the second super-elastic shape memory alloy components are in the form of gussets. 7. The support system of claim 1 , wherein the first super-elastic shape memory alloy component is in the form of a gusset, a flange, a washer, or combinations thereof, and the second super-elastic shape memory alloy component is in the form of a gasket seal, a gusset, a washer, or combinations thereof. 8. The support system of claim 1 , wherein the fastener is an axial bolt. 9. The support system of claim 1 , wherein the fastener comprises a super-elastic shape memory alloy. 10. The support system of claim 1 , wherein a radial gap exists between at least a portion of the fastener and at least one of the first flange or the second flange. 11. The support system of claim 1 , wherein at least one of the first flange or the second flange comprises a super-elastic shape memory alloy. 12. The support system of claim 1 , further comprising a super-elastic shape memory alloy sleeve to the fastener. 13. The support system of claim 1 , wherein the fastener is a radial bolt. 14. A bearing support system for a gas turbine engine, the bearing support system comprising: a load-bearing unit comprising a first flange; a frame supporting the load-bearing unit, the frame comprising a second flange; an axial bolt connecting the first flange and the second flange; a first super-elastic shape memory alloy component in contact with a first side of the first flange, the first side of the first flange being opposite a second side of the first flange, the second side of the first flange adjacent a first side of the second flange; and a second super-elastic shape memory alloy component in contact with a second side of the second flange, the first side of the second flange being opposite the second side of the second flange, wherein the first super-elastic shape memory alloy component is in the form of a gusset, a flange, or a combination thereof, and the second super-elastic shape memory alloy component is in the form of a gasket seal, a gusset, a washer, or combinations thereof, and wherein the first and the second super-elastic shape memory alloy components are configured to deform when a load exerted by the axial bolt exceeds a threshold load value of the axial bolt. 15. The bearing support system of claim 14 , wherein the first flange is a bearing housing flange of a rotor support system. 16. The bearing support system of claim 14 , wherein the second super-elastic shape memory alloy component is a gasket seal. 17. The bearing support system of claim 14 , wherein the axial bolt comprises a super-elastic shape memory alloy. 18. A bearing support system for a gas turbine engine, the bearing support system comprising: a load-bearing unit comprising a first flange; a frame supporting the load-bearing unit, the frame comprising a second flange; an axial bolt connecting the first flange and the second flange, wherein the axial bolt comprises a super-elastic shape memory alloy; a first super-elastic shape memory alloy component in contact with a first side of the first flange, the first side of the first flange being opposite a second side of the first flange, the second side of the first flange adjacent a first side of the second flange; and a second super-elastic shape memory alloy component in contact with a second side of the second flange, the first side of the second flange being opposite the second side of the second flange, wherein the first super-elastic shape memory alloy component is in the form of a gusset, a flange, or a combination thereof, and the second super-elastic shape memory alloy component is in the form of a gusset, a flange, or a combination thereof, and wherein the first and the second super-elastic shape memory alloy components, and the axial bolt are configured to deform when a load exerted by the axial bolt exceeds a threshold load value of the axial bolt. 19. The bearing support system of claim 18 , further comprising a L-shaped super-elastic shape memory alloy sleeve to the axial bolt. 20. The bearing support system of claim 18 , further comprising a super-elastic shape memory alloy sleeve to the axial bolt.

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What does patent US10968775B2 cover?
A support system for a gas turbine engine is provided. The support system includes a load-bearing unit that includes a first flange, a support element supporting the load-bearing unit and having a second flange, a fastener connecting the first flange and the second flange, a first super-elastic shape memory alloy component in contact with the first flange, and a second super-elastic shape memor…
Who is the assignee on this patent?
Gen Electric
What technology area does this patent fall under?
Primary CPC classification F01D25/164. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Apr 06 2021 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 4 related publications on this page (citations in our corpus or others sharing the same primary CPC).