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Takeoff and landing assist apparatus for flight vehicle, and flight device

机译:用于飞行车辆的起飞和着陆辅助设备和飞行装置

摘要

A takeoff and landing assist apparatus for a flight vehicle with rotor blades causes the flight vehicle to take off from or be landed on a target point. The takeoff and landing assist apparatus includes a plurality of guide rods in parallel to each other, the plurality of guide rods being provided to one of the flight vehicle and the target point; and a plurality of guide rings into which the plurality of guide rods are insertable, the plurality of guide rings being provided to the other of the flight vehicle and the target point. A center-to-center distance between the plurality of guide rods and a center-to-center distance between the plurality of guide rings are set to be same.
机译:具有转子叶片的飞行车辆的起飞和着陆辅助装置使飞行车辆从目标点起飞或落在目标点上。起飞和着陆辅助装置包括彼此平行的多个导杆,多个导杆被提供给飞行车辆和目标点之一;和多个引导杆可插入的多个引导环,多个引导环设置在飞行车辆和目标点中的另一个引导环上。多个引导杆和多个引导环之间的中心到中心距离之间的中心到中心距离被设定为相同。

著录项

  • 公开/公告号US11046456B2

    专利类型

  • 公开/公告日2021-06-29

    原文格式PDF

  • 申请/专利权人 MITSUBISHI HEAVY INDUSTRIES LTD.;

    申请/专利号US201616063923

  • 发明设计人 JUN FUJITA;

    申请日2016-12-02

  • 分类号B64F1/02;B64C27/08;B64F1/12;B64D45/04;B64F1;B64C39/02;

  • 国家 US

  • 入库时间 2022-08-24 19:39:23

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