首页> 外国专利> FASTENER WITH LUBRICATING RING FOR INTERFERENCE FITTING, AND ASSEMBLY METHOD USING SUCH A FASTENER

FASTENER WITH LUBRICATING RING FOR INTERFERENCE FITTING, AND ASSEMBLY METHOD USING SUCH A FASTENER

机译:带润滑环的紧固件,用于干涉配合,以及使用这种紧固件的组装方法

摘要

The invention relates to a fastener for assembling at least two structural elements, comprising a aperture, the fastener comprising an enlarged head (12) and a shank (14) exhibiting, prior to fitting, an outside diameter (D1) greater than an inside diameter (DS) of the aperture, and a locking portion comprising a screw thread or annular grooves. The fastener further comprises a lubricating sacrificial ring (40) on the exterior surface of the fastener, extending at least between a distal end of the shank and a proximal end of the locking portion, said ring having, before the fastener is fitted into the structure, an outside diameter greater than a diameter of the aperture. The sacrificial ring comprises a polymer resin forming a matrix encapsulating dispersant molecules and oil molecules.;The invention applies to the assembly of aircraft structures.
机译:本发明涉及一种用于组装至少两个结构元件的紧固件,该结构元件包括孔,该紧固件包括扩大的头部( 12 )和柄部( 14 ),该紧固件具有先有技术。为了配合,孔的外径(D 1 )大于孔的内径(D S ),并且锁定部分包括螺纹或环形槽。紧固件还包括在紧固件的外表面上的润滑牺牲环( 40 ),该润滑牺牲环至少在柄的远端与锁定部分的近端之间延伸,所述环在之前具有紧固件装配到结构中,其外径大于孔的直径。牺牲环包括形成包封分散剂分子和油分子的基质的聚合物树脂。本发明适用于飞机结构的组装。

著录项

  • 公开/公告号US2019195268A1

    专利类型

  • 公开/公告日2019-06-27

    原文格式PDF

  • 申请/专利权人 LISI AEROSPACE;

    申请/专利号US201916273558

  • 申请日2019-02-12

  • 分类号F16B33/06;F16B19/05;

  • 国家 US

  • 入库时间 2022-08-21 12:08:23

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