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公开(公告)号：US20120168561A1
公开(公告)日：2012-07-05
申请号：US12722848
申请日：2010-03-12
CPC分类号： B64C25/12 , B64C25/18 , B64C25/26 , B64C2025/125
摘要： A landing gear for an aircraft. The landing gear may have a wheel/truck assembly, an oleo strut/support frame for supporting the wheel/truck assembly, and a retraction assembly attached to the oleo strut/support frame, the retraction assembly for moving the landing gear between a deployed position and a retracted position. The retraction assembly may have a pivoting trunnion brace attached to the oleo strut/support frame and to a fuselage of the aircraft for positioning the wheel/truck assembly, the oleo strut/support frame and the retraction assembly at least substantially fully within the fuselage of the aircraft in the retracted position.
摘要翻译： 飞机起落架。 起落架可以具有轮/卡车组件，用于支撑车轮/卡车组件的油支架/支撑框架和连接到油支架/支撑框架的缩回组件，该缩回组件用于将起落架移动在展开位置 和缩回位置。 缩回组件可以具有连接到油支架/支撑框架和机身的机身的枢转耳轴支架，用于将车轮/卡车组件，油支架/支撑框架和缩回组件至少基本上完全地设置在机身内 飞机处于缩回位置。
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公开(公告)号：US08523107B2
公开(公告)日：2013-09-03
申请号：US12722848
申请日：2010-03-12
IPC分类号： B64C25/10
CPC分类号： B64C25/12 , B64C25/18 , B64C25/26 , B64C2025/125
摘要： A landing gear for an aircraft. The landing gear may have a wheel/truck assembly, an oleo strut/support frame for supporting the wheel/truck assembly, and a retraction assembly attached to the oleo strut/support frame, the retraction assembly for moving the landing gear between a deployed position and a retracted position. The retraction assembly may have a pivoting trunnion brace attached to the oleo strut/support frame and to a fuselage of the aircraft for positioning the wheel/truck assembly, the oleo strut/support frame and the retraction assembly at least substantially fully within the fuselage of the aircraft in the retracted position.
摘要翻译： 飞机起落架。 起落架可以具有轮/卡车组件，用于支撑车轮/卡车组件的油支架/支撑框架和连接到油支架/支撑框架的缩回组件，该缩回组件用于将起落架移动在展开位置 和缩回位置。 缩回组件可以具有连接到油支架/支撑框架和机身的机身的枢转耳轴支架，用于将车轮/卡车组件，油支架/支撑框架和缩回组件至少基本上完全地设置在机身内 飞机处于缩回位置。
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