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Rotary wing VTOL with fixed wing forward flight mode

机译:旋翼VTOL固定翼前飞模式

摘要

An aircraft's two wings and joined thruster propellers or turbines serve as rotary wings in helicopter mode and as fixed wings in airplane mode. The thrusters along the wingspans or at the wing tips drive both rotary wing rotation and airplane flight. Large-angle controlled feathering about the pitch change axes of the left and right wings and thrusters allows them to rotate, relative to each other, between facing and thrusting forward in the same direction for airplane flight or facing and thrusting oppositely for helicopter flight. Optional controls include: helicopter cyclic and collective pitch; airplane roll by differential wing pitch; yaw by differential prop thrust; fuselage pitch by wing pitch change and prop thrust change interacting with an underslung craft e.g.; and fuselage yaw control independent of rotor rotation via a powered rotary mast coupling or a tail responsive to rotor downwash. A teetering rotor hub is a further option.
机译:飞机的两个机翼和相连的推进器螺旋桨或涡轮在直升机模式下用作旋转机翼,在飞机模式下用作固定机翼。沿着翼展或翼尖的推进器既驱动机翼旋转又驱动飞机飞行。围绕左右机翼和推进器的俯仰变化轴进行大角度控制的羽化,可以使它们在面向飞机的方向相同的方向和向前推动之间相对旋转,而对于直升机飞行的方向则相反。可选的控件包括:直升机的周期性和集体俯仰;飞机以不同的机翼倾角滚动;通过差动支撑推力偏航;通过机翼俯仰角变化和螺旋桨推力变化而引起的机身俯仰角与下悬式飞行器相互作用,例如;以及通过动力旋转的桅杆联轴器或响应于转子向下冲洗的尾部而独立于转子旋转的机身偏航控制。摇摇欲坠的转子轮毂是另一种选择。

著录项

  • 公开/公告号AU2015374294B2

    专利类型

  • 公开/公告日2020-03-12

    原文格式PDF

  • 申请/专利权人 JOSEPH SEALE;WALKER SLOAN;

    申请/专利号AU20150374294

  • 发明设计人 SEALE JOSEPH B.;SLOAN WALKER M.;

    申请日2015-12-28

  • 分类号B64C27/24;

  • 国家 AU

  • 入库时间 2022-08-21 11:13:09

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