The present invention proposes a window mounting structure (24) to improve the mounting and maintenance of an aircraft window (18), the window mounting structure (24) having a mounting bearing joint (38) mounted on a fuselage (12). The window glass assembly (26) is inserted into the window opening (34) and presses the mounting frame (46) against the mounting support engagement portion (38). The mounting frame (46) may be locked in position with a locking member (59).
本发明提出一种窗安装结构(24),以改进对飞行器窗(18)的安装和维护,该窗安装结构(24)具有安装在机身(12)上的安装支承接合部(38)。窗玻璃组件(26)插入窗开口(34)中,并且将安装框架(46)按压在安装支承接合部(38)上。安装框架(46)可以利用锁定构件(59)锁定就位。
Window mounting structure for snap-fitting and snap-fitting window assembly of aircraft
用于卡扣和卡合安装飞行器的窗组件的窗安装结构
2024-02-23
Patent
Electronic Resource
Chinese
A WINDOW MOUNTING STRUCTURE FOR SNAP AND CLICK MOUNTING OF A WINDOW ASSEMBLY OF AN AIRCRAFT
European Patent Office | 2024
|WINDOW MOUNTING STRUCTURE FOR SNAP AND CLICK MOUNTING OF A WINDOW ASSEMBLY OF AN AIRCRAFT
European Patent Office | 2024
|A WINDOW MOUNTING STRUCTURE FOR SNAP AND CLICK MOUNTING OF A WINDOW ASSEMBLY OF AN AIRCRAFT
European Patent Office | 2024
|