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CANTED CO-AXIAL ROTOR FOR ROTOR CRAFT

机译:斜交斜交转子

摘要

To provide a system and method of using a rotor craft with canted rotors for increased yaw control.SOLUTION: A rotor craft has a frame and a plurality of rotors connected to the frame. The frame has a roll axis and a pitch axis. Each of the rotors includes a rotor shaft. The rotor shaft of each of the rotors is canted with respect to at least one of the roll axis and the pitch axis. The rotor shaft of each of the rotors may be canted between 3 and 15 degrees. Each of the rotors may be a co-axial co-rotating rotor. The rotors may be oriented in opposing pairs across the frame. Both rotors in each opposing pair rotate in the same direction. The rotor craft may include at least two additional rotors, each having a forward cant. Each of the additional rotors may be a co-axial contra-rotating rotor.SELECTED DRAWING: Figure 1
机译:提供一种使用带有倾斜转子的旋翼飞行器以增强偏航控制的系统和方法。解决方案:旋翼飞行器具有框架和连接到框架的多个转子。框架具有侧倾轴线和俯仰轴线。每个转子包括转子轴。每个转子的转子轴相对于侧倾轴线和俯仰轴线中的至少一个倾斜。每个转子的转子轴可以倾斜在3度和15度之间。每个转子可以是同轴同向旋转的转子。转子可以跨框架成对地定向。每对相对的两个转子都沿相同的方向旋转。旋翼飞行器可以包括至少两个附加的旋翼,每个旋翼具有向前的倾斜角。每个附加转子可以是同轴对转转子。图1

著录项

  • 公开/公告号JP2020033000A

    专利类型

  • 公开/公告日2020-03-05

    原文格式PDF

  • 申请/专利权人 BOEING CO;

    申请/专利号JP20190130792

  • 申请日2019-07-16

  • 分类号B64C27/08;

  • 国家 JP

  • 入库时间 2022-08-21 11:35:30

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