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Enhanced rig check and leak detection of aircraft doors

机译:增强钻机检查和飞机门的泄漏检测

摘要

Systems and methods for leak detection of aircraft doors. One embodiment is an apparatus for leak testing a seal between an aircraft door and a fuselage of an aircraft. The apparatus includes a structural frame that includes a suction cup configured to suction an outer surface of the aircraft door. The structural frame further includes legs to extend in length to push the structural frame away from the fuselage and cause the suction cup to pull the aircraft door toward an outside of the aircraft to tighten the seal between the aircraft door and the fuselage of the aircraft.
机译:用于防漏飞机门的系统和方法。一个实施例是用于在飞机门和飞机的机身之间进行泄漏测试的装置。该装置包括结构框架,该结构框架包括构造成吸入飞机门的外表面的抽吸杯。结构框架进一步包括腿部长度延伸以将结构框架推远离机身,并使吸盘将飞机门拉向飞机外部,以拧紧飞机门和飞机的机身之间的密封。

著录项

  • 公开/公告号US11067468B2

    专利类型

  • 公开/公告日2021-07-20

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号US201816019946

  • 发明设计人 TYLER EMERSON BERKEY;EMNET T. GEMECHU;

    申请日2018-06-27

  • 分类号B64C1/14;G01M3/26;F16J15/10;G01M3/16;

  • 国家 US

  • 入库时间 2022-08-24 20:01:21

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