Molded part
US-9739175-B2 · Aug 22, 2017 · US
US10968775B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10968775-B2 |
| Application number | US-201715823631-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 28, 2017 |
| Priority date | Nov 28, 2017 |
| Publication date | Apr 6, 2021 |
| Grant date | Apr 6, 2021 |
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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.
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.
Flexible supports; Vibration damping means associated with the bearing · CPC title
Elasticity · CPC title
Shape memory behaviour · CPC title
Restoring position · CPC title
in gas turbines · CPC title
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