首页> 外国专利> Seal member for aircraft window and window structure of aircraft

Seal member for aircraft window and window structure of aircraft

机译:飞机窗口和窗户结构的密封件

摘要

Problem to be solved: to seal the gap between the window panel and the frame without requiring high accuracy in the dimensional shape and assembly of the window panel and frame, and to increase the size of the fixing member such as the clamp, or to reduce the workability of attaching the window panel to the frame.The sealing member 10 for the window of the aircraft is disposed between the seal surface 222 of the panel member 2 pressed against the pressed surface 322 of the frame 3 and the pressing surface 322, and seals between the seal surface 222 and the pressing surface 322.The seal member 10 includes a first portion 101 corresponding to an end portion 322a of the pressed surface 322, a second portion 102 corresponding to an end portion 222b of the seal surface 222, and a curved portion 100 curved in a non load state.The curved portion 100 extends between the first portion 101 and the second portion 102 in a cross section crossing the circumferential direction of the seal member 10, and is curved in a direction retracting from one of the seal surface 222 and the pressing surface 322.Diagram
机译:要解决的问题:密封窗板和框架之间的间隙,而不需要窗口面板和框架的尺寸形状和组装的高精度,并增加诸如夹具的固定构件的尺寸,或减少将窗口面板连接到框架的可加工性。用于飞机的窗口的密封构件10设置在面板构件2的密封表面222之间,按压靠在框架3和按压表面322的压制表面322上,并在密封表面222和按压表面322之间密封。密封构件10包括对应于压制表面322的端部322a的第一部分101,对应于密封表面222的端部222b的第二部分102,以及在非负载状态下弯曲的弯曲部分100。弯曲部分100在穿过密封构件10的圆周方向的横截面中延伸在第一部分101和第二部分102之间,并且在从密封表面222和按压表面322.dia122.diagram中缩回的方向上弯曲

著录项

  • 公开/公告号JP2021088200A

    专利类型

  • 公开/公告日2021-06-10

    原文格式PDF

  • 申请/专利权人 三菱航空機株式会社;

    申请/专利号JP20190217717

  • 发明设计人 中嶋 慶士;佐野 貴章;

    申请日2019-12-02

  • 分类号B64C1/14;F16J15/10;H05K9;

  • 国家 JP

  • 入库时间 2022-08-24 19:09:31

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