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FIGHTER PLANE COCKPIT TRANSPARENT MEMBER FASTENING STRUCTURE AND FASTENING METHOD THEREFOR

机译:战斗机驾驶舱透明成员的发卡结构及其发卡方法

摘要

A fastening structure for a transparent member of a fighter plane cockpit and a fastening method therefor. The fastening structure comprises an aircraft body (1) and a cockpit transparent member (2) installed thereupon; the periphery of the cockpit transparent member (2) is fitted with an edge frame (3), said edge frame (3) comprising a compression component (31) and a fastening component (32). The combined pressure on the fastening component (32) of the compression component (31) matched to the cockpit transparent member (2) creates a prestressing force which serves to fasten the cockpit transparent member (2). The present fastening structure is very strong, and has a wide range of application.
机译:用于战斗机驾驶舱的透明构件的紧固结构及其紧固方法。该紧固结构包括:飞机主体(1)和安装在其上的驾驶舱透明构件(2);驾驶舱透明构件(2)的外围装有边缘框架(3),所述边缘框架(3)包括压缩部件(31)和紧固部件(32)。压缩部件(31)的紧固部件(32)上与驾驶舱透明部件(2)相匹配的组合压力产生预应力,该预应力用于紧固驾驶舱透明部件(2)。本紧固结构非常坚固,具有广泛的应用范围。

著录项

  • 公开/公告号WO2014183612A1

    专利类型

  • 公开/公告日2014-11-20

    原文格式PDF

  • 申请/专利权人 XIE XIAOBIN;

    申请/专利号WO2014CN77241

  • 发明设计人 LI ZHEN;XIE JUANYONG;

    申请日2014-05-12

  • 分类号E06B3/58;

  • 国家 WO

  • 入库时间 2022-08-21 15:10:13

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