- 专利标题： Link for aircraft component mounting
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申请号： US14842907申请日： 2015-09-02
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公开(公告)号： US11066178B2公开(公告)日： 2021-07-20
- 发明人: Jason Husband
- 申请人： United Technologies Corporation
- 申请人地址： US CT Hartford
- 专利权人： United Technologies Corporation
- 当前专利权人： United Technologies Corporation
- 当前专利权人地址： US CT Hartford
- 代理机构： Carlson, Gaskey & Olds, P.C.
- 主分类号： B64D27/26
- IPC分类号： B64D27/26 ; B64D27/12 ; B64D27/14
摘要：
A gas turbine engine mount for an aircraft wing including a link body having a first joint, a second joint and a linking structure connecting the first joint to the second joint. The linking structure includes at least a flexing portion and an elastic portion. The flexing portion is configured to flex during a load outside of an expected load window.
公开/授权文献
- US20170057651A1 LINK FOR AIRCRAFT COMPONENT MOUNTING 公开/授权日：2017-03-02
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