发明名称 |
VERTICAL TAKEOFF AND LANDING (VTOL) UNMANNED AERIAL VEHICLE (UAV) |
摘要 |
One example embodiment includes a vertical takeoff and landing (VTOL) unmanned aerial vehicle (UAV). The VTOL UAV includes a flight control system configured to provide avionic control of the VTOL UAV in a hover mode and in a level-flight mode. The VTOL UAV also includes a body encapsulating an engine and the flight control system. The VTOL UAV further includes a propeller disk coupled to the engine and configured to provide vertical thrust in the hover mode and to provide horizontal thrust for flight during the level-flight mode. |
申请公布号 |
EP3140188(A2) |
申请公布日期 |
2017.03.15 |
申请号 |
EP20150784502 |
申请日期 |
2015.04.24 |
申请人 |
Northrop Grumman Systems Corporation |
发明人 |
CREASMAN, Son F. |
分类号 |
B64C3/56;B64C3/54;B64C25/04;B64C29/00;B64C29/02 |
主分类号 |
B64C3/56 |
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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