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Bushing assemblies, bushing assembly kits, apparatuses including bushing assembles, and associated methods

机译:衬套组件,衬套组件套件,包括衬套组件的设备以及相关方法

摘要

#$%^&*AU2013245500A120140529.pdf#####BUSHING ASSEMBLIES, BUSHING ASSEMBLY KITS, APPARATUSES INCLUDING BUSHING ASSEMBLES, AND ASSOCIATED METHODS ABSTRACT Bushing assemblies (16) include a first tubular end portion (50), a second tubular end portion (52), and a middle tubular portion (54). The middle tubular portion (54) has a longitudinal compressive strength that is less than that of the end portions (50, 52). In some embodiments, the middle tubular portion (54) is constructed of braided sleeving. Also disclosed are bushing assembly kits, apparatuses that include bushing assemblies (16), such as aircraft (24), and associated methods of utilizing bushing assemblies (16). (7938332 1):JAA10 2/4 40 34 14 18 42 16 'i 44 42 46 34 44 16 1 116 56 5 Fi.8
机译:#$%^&* AU2013245500A120140529.pdf #####衬套组件,衬套组件,设备包括衬套组件及相关方法抽象衬套组件(16)包括第一管状端部(50),第二管状端部(52)和中间管状部分(54)。中间管状部分(54)具有纵向其抗压强度小于端部部分(50、52)的抗压强度。在某些实施例中,中间管状部分(54)由编织套管构成。还公开了衬套组装套件,包括衬套组件(16)的设备,例如飞机(24),以及衬套组件(16)的相关方法。(7938332 1):JAA10 2/44034 1418岁4216'i 4442 4634 44161 11656 5Fi.8

著录项

  • 公开/公告号AU2013245500A1

    专利类型

  • 公开/公告日2014-05-29

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号AU2013245500A1

  • 发明设计人 ALVARADO JR. SANTIAGO;

    申请日2013-10-17

  • 分类号F16C33/04;F16C17/26;

  • 国家 AU

  • 入库时间 2022-08-21 15:52:35

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