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Helicopter with tandem rotors - has rotors angled so that front does not reduce lift of rear

机译:带有串联旋翼的直升机-旋翼成角度,因此前部不会降低后部的升力

摘要

The helicopter with rotors in tandem, has the front rotor turning in the opposite direction to the rear. The dia. of the front rotor is smaller than that of the rear. The downwards deflection of the front rotor does not interfere with the tips of the blades of the rear rotor. The axes of the two rotors slope at an acute angle from the vertical, and in opposite directions from each other. The front rotor has fewer blades than the rear and is in the ratio of their dias. The front rotor may have three blades, and the rear rotor has four. They may rotate at different speeds and in inverse ratio to the number of blades.
机译:旋翼串联的直升飞机的前旋翼向后旋转。直径前转子的直径小于后转子的直径。前转子的向下偏转不会干扰后转子叶片的尖端。两个转子的轴线与竖直方向成锐角,并且彼此相反。前转子的叶片比后转子的叶片少,且直径相等。前转子可具有三个叶片,后转子可具有四个叶片。它们可能以不同的速度旋转,并且与叶片数量成反比。

著录项

  • 公开/公告号FR2473465A1

    专利类型

  • 公开/公告日1981-07-17

    原文格式PDF

  • 申请/专利权人 WESTLAND AIRCRAFT LTD;

    申请/专利号FR19810000441

  • 发明设计人 ROBERT JOHN JUPE;

    申请日1981-01-13

  • 分类号B64C27/08;

  • 国家 FR

  • 入库时间 2022-08-22 15:02:12

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