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    • 3. 发明公开
    • AIRCRAFT INTERIOR BRACKET
    • FLUGZEUGINNENRAUMKLAMMER
    • EP3141766A1
    • 2017-03-15
    • EP16189539.6
    • 2014-11-13
    • C&D Zodiac, Inc.
    • TANDJUNG, DarmoSMITHSON, Tyler
    • F16B5/06F16B11/00
    • F16B5/0614F16B11/006Y10T29/49895Y10T29/49966
    • 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.
    • 组件组件包括包括要接合的表面和端面的第一部件(100)和具有限定在待接合表面中的第一形状的托架开口(30),以及至少一个支架,其包括主体 主体部分(12)具有在其间形成第一角度的第一部分(14)和第二部分(16)。 第一部分包括通过其定义的紧固件开口(18)。 第二部分包括插入件(20),并且第二部分包括至少一个通过其定义的第一粘合剂开口(22)。 所述插入部件延伸到所述支架开口中,并且所述第二部分的下表面与所述第一部件的要被接合的表面接触,其中,粘合剂将所述插入部件固定在所述托架开口内,并且其中所述第一粘合剂开口处于连通状态 支架开口。