首页> 外国专利> Aircraft leg deployment device and aircraft leg deployment method

Aircraft leg deployment device and aircraft leg deployment method

机译:飞机腿部部署设备和飞机腿部部署方法

摘要

PROBLEM TO BE SOLVED: To provide a landing gear deploying device for an aircraft, which can perform deploying and shock-absorbing of a landing gear of the aircraft with a simpler configuration.;SOLUTION: A landing gear deploying device 1 for an aircraft has an expansion and contraction mechanism 3 and a motor 4. The expansion and contraction mechanism is connected to a landing gear 2A of the aircraft to deploy and store the landing gear and absorb a shock on the landing gear. The motor expands and contracts the expansion and contraction mechanism. In a method of deploying a landing gear of an aircraft, deployment and storage of the landing gear and shock-absorbing of the landing gear are performed using the landing gear deploying device for the aircraft. A control circuit 5 can exert control for mitigating a roll in wing low landing under the situation of a cross wind.;SELECTED DRAWING: Figure 1;COPYRIGHT: (C)2018,JPO&INPIT
机译:要解决的问题:提供一种用于飞机的着陆齿轮展开装置,其可以以更简单的配置进行飞机的着陆齿轮的展开和减震。;解决方案:飞机的着陆齿轮部署装置1有一个膨胀和收缩机构3和电动机4.膨胀和收缩机构连接到飞机的着陆齿轮2a,以展开和存储着陆齿轮并吸收着陆齿轮的冲击。电机扩展并收缩扩展和收缩机制。在展开飞机的着陆齿轮的方法中,使用用于飞机的着陆齿轮展开装置进行着陆齿轮的展开和吸收着陆齿轮的吸收。控制电路5可以在交叉风的情况下施加用于减轻翼低陆的辊的控制。;选定的绘图:图1;版权:(c)2018,JPO和INPIT

著录项

  • 公开/公告号JP6871000B2

    专利类型

  • 公开/公告日2021-05-12

    原文格式PDF

  • 申请/专利权人 株式会社SUBARU;

    申请/专利号JP20170015390

  • 发明设计人 人見 敦;

    申请日2017-01-31

  • 分类号B64C25/12;B64C25/24;B64C25/26;

  • 国家 JP

  • 入库时间 2022-08-24 18:38:34

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号