发明名称 Landing gear for an aircraft
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.
申请公布号 GB201209419(D0) 申请公布日期 2012.07.11
申请号 GB20120009419 申请日期 2012.05.28
申请人 AIRBUS OPERATIONS LTD 发明人
分类号 主分类号
代理机构 代理人
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