首页> 外国专利> MULTIROTOR TYPE DRONE COMPRISING A ROTATION SPEED MANAGEMENT UNIT OF EACH ROTOR AND METHOD OF CONTROLLING SUCH A DRONE

MULTIROTOR TYPE DRONE COMPRISING A ROTATION SPEED MANAGEMENT UNIT OF EACH ROTOR AND METHOD OF CONTROLLING SUCH A DRONE

机译:包括每个转子的旋转速度管理单元的多转子型无人机及其控制方法

摘要

The present invention relates to a drone (1) of multirotor type comprising a carrier frame (2), at least three independent electric motors (4), at least three rotors (5) for propulsion and / or lift independently movable in rotation with each other. others with respect to said carrier frame (2) and respectively rotated by one of said at least three electric motors (4), at least one source of electrical energy (6) for supplying electrical power to said at least three electric motors (4), and a management unit (7) for generating a rotational speed reference of each of said at least three electric motors (4). According to the invention, such a drone (1) makes it possible to provide a solution for reducing the intensity of the acoustic pulses over a given frequency range while guaranteeing the maintenance of its flight performance.
机译:多旋翼无人机技术领域本发明涉及一种多旋翼无人机(1),其包括承载架(2),至少三个独立的电动机(4),至少三个用于推进和/或提升的转子(5),它们各自独立地旋转运动。其他。另一个相对于所述承载架(2)并且分别由所述至少三个电动机(4)之一旋转,至少一个电能来源(6)用于向所述至少三个电动机(4)供应电力以及管理单元(7),用于产生所述至少三个电动机(4)中的每一个的转速参考。根据本发明,这种无人驾驶飞机(1)可以提供一种解决方案,用于在给定频率范围内减小声脉冲的强度,同时保证其飞行性能的维持。

著录项

  • 公开/公告号FR3071816A1

    专利类型

  • 公开/公告日2019-04-05

    原文格式PDF

  • 申请/专利权人 AIRBUS HELICOPTERS;

    申请/专利号FR20170071032

  • 发明设计人 LIONEL THOMASSEY;

    申请日2017-09-29

  • 分类号B64C27/57;B64C27/72;B64C39/02;

  • 国家 FR

  • 入库时间 2022-08-21 11:43:49

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