发明名称 ENERGY ABSORBING LINK
摘要 An apparatus and method for a composite structural aircraft transmission support link having an integral energy-absorbing feature is disclosed. The link is a two-force member that can carry structural loads up an ultimate load. When loaded beyond ultimate load the design allows sections of the link to fail in a controlled and progressive manner, so that energy is absorbed over a defined stroking distance.
申请公布号 US2016265613(A1) 申请公布日期 2016.09.15
申请号 US201514641586 申请日期 2015.03.09
申请人 The Boeing Company 发明人 Ludin Douglas R.;Stauffer Matthew S.;Bolukbasi Akif O.;Birchette Terrence S.
分类号 F16F7/12 主分类号 F16F7/12
代理机构 代理人
主权项 1. A two-force member energy-absorbing link structure comprising: an elongated structural member having first and second opposing ends and a lengthwise extending central axis, wherein at least the first and second opposing ends of the elongated structural member are constructed of a primary material having a strength characteristic sufficient to link together two structures; a thru-hole extending substantially orthogonally with respect to the central axis and through the first opposing end; and a section of the elongated structural member constructed of secondary material having a lesser strength characteristic than the strength characteristic of the primary material, said section extending a lengthwise distance substantially along a direction that the lengthwise extending central axis extends, and said section extending from a location proximate and adjacent the thru-hole.
地址 Chicago IL US