发明名称 Aircraft conduit harness retention system
摘要 A conduit harness retention system has a base, a first spacer, a second spacer and a cap which snap-fit together to retain P-clip harnesses in position spaced from an aircraft fuselage.
申请公布号 US9168997(B2) 申请公布日期 2015.10.27
申请号 US201414517198 申请日期 2014.10.17
申请人 AIRBUS OPERATIONS LIMITED 发明人 Blanchard Jack;Routledge David
分类号 F16L3/00;B64C1/40;F16L3/22;H02G3/32;F16L3/123;F16L3/127;F16L3/13;F16M13/02;F16L3/237;F16L3/227 主分类号 F16L3/00
代理机构 Hauptman Ham, LLP 代理人 Hauptman Ham, LLP
主权项 1. An aircraft conduit harness retention system comprising: a base having a flange attachment formation for attachment to an aircraft component at a first end and a first mating formation at a second end; a spacer having a second mating formation at a first end and a mating formation identical to the base first mating formation and a second end; a cap having a mating formation identical to the spacer first end; and a conduit harness separate from the base and the spacer, wherein said conduit harness includes a wire loom receiving portion and a flange connected to the wire loom receiving formation, the flange having a bore defined therethrough, wherein the bore of the flange is engaged by at least one of the first mating formation and second mating formation and the first mating formation and the second mating formation are engaged via a snap-fit to clamp the flange of the conduit harness between the base and spacer or cap such that the conduit harness is offset from the aircraft component.
地址 Bristol GB