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1. 发明公开

EP2669193A2 Landing gear for an aircraft 审中-公开
标题翻译： Fahrwerkfürein Luftfahrzeug
公开(公告)号：EP2669193A2
公开(公告)日：2013-12-04
申请号：EP13169017.4
申请日：2013-05-23
申请人： AIRBUS OPERATIONS LIMITED
发明人： Chow, Leung Choi , Wood, Christopher Neil , Campbell, Phillip Ian
IPC分类号： B64C25/12 , B64C25/20
CPC分类号： B64C23/00 , B64C25/001 , B64C25/12 , B64C25/20 , B64C25/26 , B64C2025/003
摘要： The invention provides a landing gear 120 for an aircraft 110, the landing gear comprising a main strut 121 having a first upper end arranged to be moveably mounted to a structure of the aircraft, a landing gear wheel assembly 131, 132 connected to a second lower end of the main strut, the landing gear wheel assembly comprising at least one landing gear wheel arranged to roll in a fore-aft direction with respect to the main strut, and a stay 122 having a first upper end arranged to be connected to a structure of the aircraft, and a second lower end pivotally mounted to a mounting element 140 on the main strut, wherein the mounting element on the main strut is positioned substantially in line with the main strut in the fore-aft direction. The invention also provides a main strut, an aircraft and a kit of parts.
摘要翻译：本发明提供了一种用于飞行器110的起落架120，起落架包括主支柱121，主支柱121具有布置成可移动地安装到飞行器结构的第一上端，连接到第二下部的起落架齿轮组件131,132 主支柱的端部，起落架轮组件包括布置成相对于主支柱在前后方向上滚动的至少一个起落架，以及具有布置成连接到主支柱的结构的第一上端的撑杆122 以及可枢转地安装到主支柱上的安装元件140的第二下端，其中主支柱上的安装元件基本上与主支柱沿前后方向一致地定位。本发明还提供主支柱，飞机和一套零件。

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