发明名称 Aircraft comprising a link rod one part of which is made of composite
摘要 The link for an aircraft comprises at least two portions respectively made of metal and of composite material together forming a common section of a middle segment of the link in a plane perpendicular to a longitudinal direction of the link.
申请公布号 US9638241(B2) 申请公布日期 2017.05.02
申请号 US201113811802 申请日期 2011.07.18
申请人 Airbus Operations (S.A.S.) 发明人 Gallant Guillaume;Guillemaut Julien
分类号 F16C7/00;F16C7/02;G01D21/00 主分类号 F16C7/00
代理机构 Nixon & Vanderhye P.C. 代理人 Nixon & Vanderhye P.C.
主权项 1. A link for an aircraft, the link comprising: at least two portions respectively made of metal and of composite material together forming a middle segment of the link with both being present in any section of the middle segment in a plane perpendicular to a longitudinal direction of the link, and end parts located at opposite ends of the middle segment, the middle segment extending between the end parts, wherein the at least two portions are spaced apart from each other in the middle segment by spacer elements engaging the end parts, whereby the two portions have no region of mutual contact, wherein each of the end parts includes a connector configured to be connected to a structure or other part of the aircraft, at least one of the connectors including an inclined face arranged to urge a corresponding ring in abutment with a corresponding one of the spacer elements, which is prevented from sliding relative to the composite portion in either of two opposite longitudinal directions, and wherein the at least two portions are arranged to face each other in the middle segment with no material whatsoever between them in the middle segment.
地址 Toulouse FR