发明名称 AIRCRAFT INTERIOR BRACKET
摘要 A component assembly comprises a first component (100) that includes a surface to be joined and an end surface, and a bracket opening (30) having a first shape defined in the surface to be joined, and at least one bracket that includes a main body portion (12) having a first portion (14) and a second portion (16) that form a first angle therebetween. The first portion includes a fastener opening (18) defined therethrough. The second portion includes an insert feature (20), and the second portion includes at least a first adhesive opening (22) defined therethrough. The insert feature extends into the bracket opening and the lower surface of the second portion is in contact with the surface to be joined of the first component, wherein an adhesive secures the insert feature within the bracket opening and wherein the first adhesive opening is in communication with the bracket opening.
申请公布号 EP3141766(A1) 申请公布日期 2017.03.15
申请号 EP20160189539 申请日期 2014.11.13
申请人 C&D Zodiac, Inc. 发明人 TANDJUNG, Darmo;SMITHSON, Tyler
分类号 F16B5/06;F16B11/00 主分类号 F16B5/06
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