首页> 外国专利> Supporting structure for force transmission member, aircraft reaction link, flight control surface driving unit, method of mounting force transmission member, and method of manufacturing aircraft reaction link

Supporting structure for force transmission member, aircraft reaction link, flight control surface driving unit, method of mounting force transmission member, and method of manufacturing aircraft reaction link

机译:力传递构件的支撑结构,飞机反作用连杆,飞行控制面驱动单元,力传递构件的安装方法以及飞机反作用连杆的制造方法

摘要

One object is to provide a supporting structure for a force transmission member, an aircraft reaction link, a flight control surface driving unit, a method of mounting a force transmission member, and a method of manufacturing aircraft reaction link that enable weight reduction while ensuring necessary strength. In accordance with one aspect, the reaction link includes a bush and a link body formed of a fiber-reinforced plastic and supporting the bush. The link body includes a supporting portion supporting the bush, and the fibers included in the supporting portion are continuous.
机译:一个目的是提供一种用于力传递构件的支撑结构,飞机反作用连杆,飞行控制面驱动单元,安装力传递构件的方法以及制造飞机反作用连杆的方法,其能够在确保必要的同时减轻重量。强度。根据一个方面,所述反作用链节包括衬套和由纤维增强塑料形成并支撑所述衬套的链节主体。链节体包括支撑衬套的支撑部分,并且包含在支撑部分中的纤维是连续的。

著录项

  • 公开/公告号US10493703B2

    专利类型

  • 公开/公告日2019-12-03

    原文格式PDF

  • 申请/专利权人 NABTESCO CORPORATION;

    申请/专利号US201615334965

  • 发明设计人 TSUTOMU YASUI;

    申请日2016-10-26

  • 分类号B29C70/30;B64C13/30;B29C70/86;B64C9/02;F16C7/02;B29K307/04;B29L31/30;B29L31/06;

  • 国家 US

  • 入库时间 2022-08-21 11:26:06

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