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1. 发明申请

WO2012018382A3 FLYING VEHICLE RETRACTABLE WING HINGE AND TRUSS 审中-公开
标题翻译：飞行车辆可撤回的WING HINGE和TRUSS
公开(公告)号：WO2012018382A3
公开(公告)日：2012-06-14
申请号：PCT/US2011001355
申请日：2011-08-02
申请人： SAMSON AIP INC , BOUSFIELD SAMUEL HALL , ROBERTS ROBERT N , BROWN MATTHEW A , ANEMAAT WILLEM A J
发明人： BOUSFIELD SAMUEL HALL , ROBERTS ROBERT N , BROWN MATTHEW A , ANEMAAT WILLEM A J
IPC分类号： B64C3/56 , B64C3/18
CPC分类号： B64C37/00 , B64C3/56
摘要： A truss for a flying vehicle supports a pair of wings in a manner which facilitates pivoting of the wings between a deployed configuration and a retracted configuration. The truss includes parallel top and bottom plates with the gap therebetween. The wings have wing brackets affixed thereto with the wing brackets pivotably supported by hinge assemblies to the top plate and bottom plate of the truss. Latch assemblies can be selectively actuated to secure the wing brackets and associated wings to the truss in either the deployed configuration or the retracted configuration, so that loads between the wings and the truss are primarily carried through the latch assemblies rather than through the hinge assemblies. A hinge position on the truss and on the wing brackets is selected to maximize wing length tip to tip while minimizing an outline required for the vehicle when the wings are fully retracted.
摘要翻译：用于飞行车辆的桁架以便于在展开配置和缩回配置之间枢转翼的方式支撑一对翼。桁架包括平行的顶板和底板之间的间隙。机翼具有固定于其上的翼架，翼架可枢转地由铰链组件支撑到桁架的顶板和底板。可以选择性地致动闩锁组件，以将翼支架和相关联的翼片以展开的构型或缩回构型固定到桁架上，使得翼和桁架之间的载荷主要通过闩锁组件而不是通过铰链组件承载。选择桁架和翼支架上的铰链位置，以最大限度地提高机翼长度的顶端到顶端，同时最小化当机翼完全缩回时车辆所需的轮廓。

2. 发明申请

WO2012018382A2 FLYING VEHICLE RETRACTABLE WING HINGE AND TRUSS 审中-公开
标题翻译：飞行的车辆可伸缩的门铰链和桁架
公开(公告)号：WO2012018382A2
公开(公告)日：2012-02-09
申请号：PCT/US2011/001355
申请日：2011-08-02
申请人： SAMSON AIP, INC. , BOUSFIELD, Samuel, Hall , ROBERTS, Robert, N. , BROWN, Matthew, A. , ANEMAAT, Willem, A.J.
发明人： BOUSFIELD, Samuel, Hall , ROBERTS, Robert, N. , BROWN, Matthew, A. , ANEMAAT, Willem, A.J.
IPC分类号： B64C3/56 , B64C3/18
CPC分类号： B64C37/00 , B64C3/56
摘要： A truss for a flying vehicle supports a pair of wings in a manner which facilitates pivoting of the wings between a deployed configuration and a retracted configuration. The truss includes parallel top and bottom plates with the gap therebetween. The wings have wing brackets affixed thereto with the wing brackets pivotably supported by hinge assemblies to the top plate and bottom plate of the truss. Latch assemblies can be selectively actuated to secure the wing brackets and associated wings to the truss in either the deployed configuration or the retracted configuration, so that loads between the wings and the truss are primarily carried through the latch assemblies rather than through the hinge assemblies. A hinge position on the truss and on the wing brackets is selected to maximize wing length tip to tip while minimizing an outline required for the vehicle when the wings are fully retracted.
摘要翻译：用于飞行器的桁架以便于在展开构造和缩回构造之间枢转翼的方式支撑一对翼。桁架包括平行的顶板和底板，其间具有间隙。翼具有固定在其上的翼托架，翼托架由铰接组件枢转地支撑到桁架的顶板和底板。闩锁组件可以被选择性地致动以将翼托架和相关联的翼部以展开构型或缩回构型固定到桁架，使得翼部和桁架之间的负荷主要通过闩锁组件而不是通过铰链组件而传递。选择桁架和翼托架上的铰链位置以最大化机翼长度的尖端至尖端，同时最小化机翼在完全缩回时所需的轮廓。

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