发明名称 |
AERODYNAMICALLY EFFICIENT LIGHTWEIGHT VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH PIVOTING ROTORS AND STOWING ROTOR BLADES |
摘要 |
An aerial vehicle adapted for vertical takeoff and landing using a set of wing mounted thrust producing elements and a set of tail mounted rotors for takeoff and landing. An aerial vehicle which is adapted to vertical takeoff with the rotors in a rotated, take-off attitude then transitions to a horizontal flight path, with the rotors rotated to a typical horizontal configuration. The aerial vehicle uses different configurations of its wing mounted rotors and propellers to reduce drag in all flight modes. |
申请公布号 |
EP3119673(A2) |
申请公布日期 |
2017.01.25 |
申请号 |
EP20150765064 |
申请日期 |
2015.03.18 |
申请人 |
Joby Aviation, Inc. |
发明人 |
BEVIRT, JoeBen;STOLL, Alex |
分类号 |
B64C27/28 |
主分类号 |
B64C27/28 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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