Self-righting frame and aeronautical vehicle |
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| 申请号 | EP12165691.2 | 申请日 | 2012-04-26 | 公开(公告)号 | EP2517767A3 | 公开(公告)日 | 2013-03-27 |
| 申请人 | Dees, James; Yan, Gaofei; | 发明人 | Dees, James; Yan, Gaofei; | ||||
| 摘要 | An aeronautical vehicle that rights itself from an inverted state to an upright state has a self-righting frame assembly has a protrusion extending upwardly from a central vertical axis. The protrusion provides an initial instability to begin a self-righting process when the aeronautical vehicle is inverted on a surface. A propulsion system, such as rotor driven by a motor can be mounted in a central void of the self-righting frame assembly and oriented to provide a lifting force. A power supply is mounted in the central void of the self-righting frame assembly and operationally connected to the at least one rotor for rotatably powering the rotor. An electronics assembly is also mounted in the central void of the self-righting frame for receiving remote control commands and is communicatively interconnected to the power supply for remotely controlling the aeronautical vehicle to take off, to fly, and to land on a surface. | ||||||
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