- 专利标题: Load controlling bolted flange deformable spacers
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申请号: US16174643申请日: 2018-10-30
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公开(公告)号: US10955022B2公开(公告)日: 2021-03-23
- 发明人: Adrian Stanescu
- 申请人: The Boeing Company
- 申请人地址: US IL Chicago
- 专利权人: The Boeing Company
- 当前专利权人: The Boeing Company
- 当前专利权人地址: US IL Chicago
- 代理机构: Miller, Matthias & Hull LLP
- 主分类号: F16F7/12
- IPC分类号: F16F7/12 ; F16B31/02 ; F16B5/02 ; B64D29/06 ; F16B43/02
摘要:
Deformable spacers and spacer assemblies absorb energy when flange bolts are subjected to compressive axial loads by plastically deforming, failing in shear, rupturing or in a combination of failure modes so the flange bolts and the flanges connected thereby are not damaged. One deformable spacer may have a hollow cylindrical body with a plurality of elongated slots there through. Another deformable spacer may have an annular stiffener extending inwardly from an inner surface of a hollow cylindrical body. A spacer assembly may include an inner cylindrical body, and outer cylindrical body, and an annular shoulder extending from one of the bodies and engaged by the other body shears when a shear failure load is applied to the flange bolt. Another spacer assembly may include an annular belt around a cylindrical body so that the belt will rupture before the cylindrical body plastically deforms.
公开/授权文献
- US20190128358A1 Load Controlling Bolted Flange Deformable Spacers 公开/授权日:2019-05-02
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