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公开(公告)号：US20170233070A1
公开(公告)日：2017-08-17
申请号：US15256140
申请日：2016-09-02
CPC分类号： B64C29/02 , B64C3/56 , B64C9/00 , B64C27/57 , B64C39/024 , B64C2201/088 , B64C2201/102 , B64C2201/108 , B64C2201/141 , B64C2201/146 , G05D1/0011 , G05D1/0088 , G05D1/0858
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 rotor disk coupled to the engine and configured to provide vertical thrust and cyclic pitch control in the hover mode and to provide horizontal thrust for flight during the level-flight mode.
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公开(公告)号：US5458041A
公开(公告)日：1995-10-17
申请号：US284875
申请日：1994-08-02
CPC分类号： F41G7/226 , F41G7/00 , F41G7/007 , F41G7/008 , F41G7/22 , F41G7/2206 , F41G7/2226 , F41G7/2233 , F41G7/224 , F41G7/2286 , F41G7/2293 , F41G7/308
摘要： An air defense missile weapon system in which a plurality of unmanned missiles penetrate, survey, identify, attack and destroy target areas that include air defense sites and sites of military interest. Each of the missiles has an airframe, sensors, data links, propulsion means, and a plurality of control surfaces. The missiles are launched from a carrier aircraft towards the target sites from a stand-off range. The missiles preferably operate in cooperative teams of hunter and killer missiles, and are interoperable with a plurality of military aircraft and other existing weapon systems.
摘要翻译： 一种防空导弹武器系统，其中多枚无人导弹穿透，勘察，识别，攻击和销毁包括防空地点和军事地带的目标地区。 每个导弹都有机身，传感器，数据链接，推进装置和多个控制面。 导弹从承运人飞机向远离目标地点发射。 导弹最好在猎人和杀戮导弹的合作团队中工作，并可与多架军用飞机和其他现有的武器系统互操作。
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公开(公告)号：US10287013B2
公开(公告)日：2019-05-14
申请号：US15256140
申请日：2016-09-02
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 rotor disk coupled to the engine and configured to provide vertical thrust and cyclic pitch control in the hover mode and to provide horizontal thrust for flight during the level-flight mode.
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