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1. 发明授权

US07731124B2 Landing gear 有权
标题翻译：起落架
公开(公告)号：US07731124B2
公开(公告)日：2010-06-08
申请号：US11460152
申请日：2006-07-26
申请人： John William Griffin
发明人： John William Griffin
IPC分类号： B64C25/10 , B64C25/14
CPC分类号： B64C25/34
摘要： In an aircraft having an aircraft landing gear, the aircraft landing gear includes an arm, a leg and a bogie at the lower end of the leg. The bogie is moveable in a direction along the length of the leg and pivotable between a trimmed deployed position and a stowable position. The arm is mounted on the landing gear and is rotatable between a first position in which the bogie is positioned in the trimmed deployed position, and a second position in which the bogie is positioned in the stowable position. Movement of the arm can be effected by a positioning rotary actuator, which is not located in the primary or secondary load paths.
摘要翻译：在具有飞机起落架的飞行器中，飞机起落架包括在腿的下端的一个臂，一个腿和一个转向架。转向架可沿着腿的长度方向移动，并可在修剪后的展开位置和收起位置之间枢转。臂安装在起落架上，并可在其中转向架位于修剪展开位置的第一位置和第二位置之间转动，转向架位于可收起位置的第二位置。臂的移动可以通过定位旋转致动器来实现，定位旋转致动器不位于主负载路径中。

2. 发明申请

US20100116930A1 LANDING GEAR 有权
标题翻译：起落架
公开(公告)号：US20100116930A1
公开(公告)日：2010-05-13
申请号：US11460152
申请日：2006-07-26
申请人： John William GRIFFIN
发明人： John William GRIFFIN
IPC分类号： B64C25/10 , B64C25/18
CPC分类号： B64C25/34
摘要： In an aircraft having an aircraft landing gear, the aircraft landing gear includes an arm, a leg and a bogie at the lower end of the leg. The bogie is moveable in a direction along the length of the leg and pivotable between a trimmed deployed position and a stowable position. The arm is mounted on the landing gear and is rotatable between a first position in which the bogie is positioned in the trimmed deployed position, and a second position in which the bogie is positioned in the stowable position. Movement of the arm can be effected by a positioning rotary actuator, which is not located in the primary or secondary load paths.
摘要翻译：在具有飞机起落架的飞行器中，飞机起落架包括在腿的下端的一个臂，一个腿和一个转向架。转向架可沿着腿的长度方向移动，并可在修剪后的展开位置和收起位置之间枢转。臂安装在起落架上，并可在其中转向架位于修剪展开位置的第一位置和第二位置之间转动，转向架位于可收起位置的第二位置。臂的移动可以通过定位旋转致动器来实现，定位旋转致动器不位于主负载路径中。

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