Load reduction assemblies for a gas turbine engine
US-2018112554-A1 · Apr 26, 2018 · US
US10823228B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10823228-B2 |
| Application number | US-201916394180-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 25, 2019 |
| Priority date | Oct 21, 2016 |
| Publication date | Nov 3, 2020 |
| Grant date | Nov 3, 2020 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A hybrid bearing support system includes a shaft extension fixedly coupled to a rotatable member at a radial inner end of the shaft extension, a radial outer end of the shaft extension fixedly coupled to a rotatable race of a bearing supporting the rotatable member, and a recoupler device formed of a shape memory alloy (SMA) material coupled in parallel with at least a portion of the shaft extension between the radial inner end and the radial outer end.
Opening claim text (preview).
What is claimed is: 1. A shape memory alloy recoupler device comprising: a radial inner flange comprising a circular cross-section; a radial outer flange comprising a circular cross-section; and a web member comprising an axial portion extending axially between said radial inner flange and said radial outer flange, said web member formed of a shape memory alloy (SMA) material. 2. The recoupler device of claim 1 , wherein at least one of said radial inner flange and said radial outer flange is formed of an SMA material. 3. The recoupler device of claim 1 , wherein said web member is unitarily formed. 4. The recoupler device of claim 1 , wherein said web member comprises a single skirt extending circumferentially approximately 360°. 5. The recoupler device of claim 1 , wherein said web member comprises a plurality of spokes, each spoke of the plurality of spokes extending for a predetermined arc of a circumference of the recoupler device. 6. The recoupler device of claim 1 , wherein said radial inner flange and said radial outer flange are axisymmetric. 7. The recoupler device of claim 1 , wherein said web member comprises a crystal structure that responds to stress above a predetermined threshold by changing phase from a first phase to a second phase. 8. The recoupler device of claim 1 , wherein said recoupler device comprises a first crystalline structure having a first stiffness when subjected to a first stress, and said recoupler device comprises a second crystalline structure having a second stiffness when subjected to a second stress. 9. The recoupler device of claim 1 , wherein said web member comprises a plurality of spokes, and wherein all of the plurality of spokes extend between said radial inner flange and said radial outer flange.
Products made by additive manufacturing · CPC title
Resilience, elasticity, super-elasticity · CPC title
using mechanical means · CPC title
with a single row or balls · CPC title
special arrangements in stators or in rotors dealing with breaking-off of part of rotor · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.