WING STRUCTURE AND ATTACHMENT TO FRAME FOR UNMANNED AERIAL VEHICLES
Systems for wing structure and attachment to frame for Unmanned Autonomous Vehicle (UAV) are disclosed herein. In one embodiment, a UAV includes an H-frame having a wing spar (112) secured to two or more boom carriers (212). The wing spar includes two or more mounting locations, where each of the tw...
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Main Authors | , , |
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Format | Patent |
Language | Chinese English |
Published |
30.06.2020
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Subjects | |
Online Access | Get full text |
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Summary: | Systems for wing structure and attachment to frame for Unmanned Autonomous Vehicle (UAV) are disclosed herein. In one embodiment, a UAV includes an H-frame having a wing spar (112) secured to two or more boom carriers (212). The wing spar includes two or more mounting locations, where each of the two or more mounting locations of the wing spar secures a horizontal propulsion unit. The boom carriers include a plurality of mounting locations, each of the plurality of mounting locations of the boom carriers securing a vertical propulsion unit (242). The UAV also includes a pre-formed wing shell attached to the H-frame.
本文公开了用于无人驾驶自主运载工具(UAV)的机翼结构的系统和框架附接。在一个实施方式中,UAV包括具有固定到两个或更多个吊杆支架(212)的机翼翼梁的H框架。机翼翼梁包括两个或更多个安装位置,在该处机翼翼梁的所述两个或更多个安装位置中的每个固定水平推进单元。吊杆支架包括多个安装位置,吊杆支架的所述多个安装位置中的每个固定垂直推进单元(242)。UAV还包括附接到H框架的预形成的机翼壳体。 |
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Bibliography: | Application Number: CN201880075029 |