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Dual-aircraft system

机译:双机系统

摘要

One example includes a dual-aircraft system. The system includes a glider aircraft configured to perform at least one mission objective in a gliding-flight mode during a mission objective stage. The system also includes an unmanned singlecopter configured to couple to the glider aircraft via a mechanical linkage to provide propulsion for the glider aircraft during a takeoff and delivery stage. The unmanned singlecopter can be further configured to decouple from the glider aircraft during a detach stage in response to achieving at least one of a predetermined altitude and a predetermined geographic location to provide the gliding-flight mode associated with the glider aircraft, such that the glider aircraft subsequently enters the mission objective stage.
机译:一个例子包括双飞机系统。该系统包括滑翔机,该滑翔机被配置为在任务目标阶段期间以滑行飞行模式执行至少一个任务目标。该系统还包括无人单直升机,其配置为通过机械联动装置耦合到滑翔机,以在起飞和交付阶段为滑翔机提供推进力。无人单直升机还可被配置为响应于实现预定高度和预定地理位置中的至少一个而在分离阶段期间与滑翔机解耦,以提供与滑翔机相关联的滑行飞行模式,使得滑翔机飞机随后进入任务目标阶段。

著录项

  • 公开/公告号US10293934B2

    专利类型

  • 公开/公告日2019-05-21

    原文格式PDF

  • 申请/专利权人 NICHOLAS K. CHRISTENSEN;

    申请/专利号US201615066460

  • 发明设计人 NICHOLAS K. CHRISTENSEN;

    申请日2016-03-10

  • 分类号B64C31/02;B64C39/02;B64D5;

  • 国家 US

  • 入库时间 2022-08-21 12:15:12

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