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Aircraft fuel line couplings in compliance with survivable crash and lightning strike requirements

机译:飞机油管接头符合可幸存的碰撞和雷击要求

摘要

Fuel line coupling components couple together coaxially aligned fuel lines (e.g., single wall metal aircraft fuel lines) and allow for relative longitudinal movements therebetween. The fuel line coupling component may include an outer tubular housing member, an inner tubular coupling member, a tubular collar member and a coupler. The inner tubular coupling member is adapted to being attached to a terminal end of one of the fuel lines and is received within an interior space of the outer tubular housing member for slidable movements therewithin to allow the fuel line attached thereto to be telescopically extended and retracted relative to the outer tubular housing. The tubular collar member is coaxially aligned with the outer tubular member and is adapted to being attached to a terminal end of the second fuel line in coaxial opposition to the first fuel line.
机译:燃料管线联接部件将同轴对准的燃料管线(例如,单壁金属飞机燃料管线)联接在一起,并允许它们之间的相对纵向运动。燃料管线联接部件可包括外部管状壳体构件,内部管状联接构件,管状套环构件和联接器。内管状联接构件适于附接到燃料管线之一的终端,并且被容纳在外管状壳体构件的内部空间中以在其中进行滑动运动,以允许附接到其上的燃料管线可伸缩地伸缩。相对于外部管状壳体。管状套环构件与外部管状构件同轴对准,并且适于以与第一燃料管线同轴相对的方式附接到第二燃料管线的终端。

著录项

  • 公开/公告号US9933093B2

    专利类型

  • 公开/公告日2018-04-03

    原文格式PDF

  • 申请/专利权人 EMBRAER S.A.;

    申请/专利号US201414556010

  • 申请日2014-11-28

  • 分类号F16L27/12;F16L23/08;F16L25/01;B64D37/00;F16L23/06;

  • 国家 US

  • 入库时间 2022-08-21 12:55:40

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