发明名称 Joint between aircraft components
摘要 A joint between a pair of aircraft components comprising a first component; a second component bonded to the first component over a bonded area, the bonded area terminating at an edge; a non-bonded area located between the edge of the bonded area and an edge of the second component, the components not being bonded over the non-bonded area; and one or more fasteners passing through the non-bonded area and fastening the first component to the second component.
申请公布号 US9242715(B2) 申请公布日期 2016.01.26
申请号 US200912998048 申请日期 2009.10.15
申请人 Airbus Operations Limited 发明人 Cosentino Enzo
分类号 F16B11/00;B64C1/12 主分类号 F16B11/00
代理机构 Nixon & Vanderhye P.C. 代理人 Nixon & Vanderhye P.C.
主权项 1. A joint between a pair of aircraft components comprising: a first component; a second component bonded to the first component over a bonded area, the bonded area terminating at an edge; a non-bonded area between said first and second components located between the edge of the bonded area and an edge of the second component, the components not being bonded over the non-bonded area and said non-bonded area not transferring substantial shear forces between said components, wherein a shim layer confined to the non-bonded area is between the first and second components and has a coefficient of friction with respect to the first or second components which is less than a coefficient of friction between the first and second components in the bonded area; and one or more fasteners passing through the non-bonded area and fastening the first component to the second component, wherein each of the components is formed from a composite material, and the one or more fasteners passes through the first and second components.
地址 Bristol GB