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)(12). The VTOL UAV (12) includes a flight control system configured to provide avionic control of the VTOL UAV (12) in a hover mode and in a level-flight mode. The VTOL UAV (12) also includes a body (18) encapsulating an engine and the flight control system. The VTOL UAV (12) further includes a propeller disk (14) 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 WO2016003530(A3) 申请公布日期 2016.03.10
申请号 WO2015US27565 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
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