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INTEGRATED HEATING AIRSPEED TUBE AND UNMANNED AERIAL VEHICLE INCLUDING SAME

机译:集成加热空速管和无人驾驶飞行器,包括相同

摘要

An integrated heating airspeed tube and an unmanned aerial vehicle where the integrated heating airspeed tube has a tube body and a heating component. The tube body is provided with a heating cavity, the heating component is located inside the heating cavity, and the heating component and the tube body are integrally formed. The unmanned aerial vehicle includes the integrated heating airspeed tube as described above. The integrated heating airspeed tube and the unmanned aerial vehicle are heated in the tube body through the heating component, so that the heating removes liquid, effectively preventing liquid from blocking the integrated heating airspeed tube, and meeting the using requirements in severe weather. At the same time, the integrated heating structure design is higher in reliability and is not easy to cause operation failure, and saves the assembly cost.
机译:集成的加热空速管和无人驾驶飞行器,其中集成的加热空速管具有管体和加热部件。管主体设有加热腔,加热部件位于加热腔内,并且加热部件和管体一体地形成。无人驾驶飞行器包括如上所述的集成加热空速管。集成的加热空速管和无人驾驶航空公司通过加热部件在管体中加热,使得加热除去液体,有效地防止液体阻挡集成的加热空速管,并在恶劣天气下满足使用的要求。同时,集成的加热结构设计的可靠性较高,并且不易引起操作失效,并节省了组装成本。

著录项

  • 公开/公告号US2021107678A1

    专利类型

  • 公开/公告日2021-04-15

    原文格式PDF

  • 申请/专利权人 SHANGHAI AUTOFLIGHT CO. LTD.;

    申请/专利号US202017067686

  • 发明设计人 YU TIAN;

    申请日2020-10-10

  • 分类号B64D43/02;G01P5/165;B64D15/12;

  • 国家 US

  • 入库时间 2024-06-14 21:25:50

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