发明授权
- 专利标题: Aircraft control system component with improved ballistic tolerance
- 专利标题(中): 飞机控制系统组件具有改进的防弹性
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申请号: US848953申请日: 1977-11-07
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公开(公告)号: US4161125A公开(公告)日: 1979-07-17
- 发明人: William G. Degnan
- 申请人: William G. Degnan
- 申请人地址: 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: CT Hartford
- 主分类号: B64C13/24
- IPC分类号: B64C13/24 ; G05G1/04 ; F41H5/04 ; G05G7/00
摘要:
An aircraft control system component, such as a bellcrank, having sideplate members of three-ply laminates bonded together with an elastomer-modified epoxy, with the thickness of the central ply twice the thickness of the end plies, and with the outboard end ply being of selected thickness and yield strength so that when petalling occurs therein due to the passage of a projectile therethrough, the petals are deformable under control loads when they come in contact thereafter with associated parts to thereby permit the control system to continue to perform its function due to the improved ballistic tolerance of the component.
公开/授权文献
- US5846055A Structured surfaces for turbo-machine parts 公开/授权日:1998-12-08
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