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Rotor lifted and propelled aircraft - has separate lifting and propulsion rotors with vertical and horizontal ducts

机译:旋翼升降飞机-具有垂直和水平管道的单独的升降螺旋桨

摘要

The rotor driven aircraft has at least one pair of counter-rotating lifting rotors, and at least one separate propulsion rotor. All rotors and their air supply ducts are held in a common housing in the roof of a cabin. All the rotors are driven by a common drive unit. The lifting and propulsion rotors have separate air supply ducts. The first group of air supply ducts (11, 12) for the lifting rotors (9, 10) pass through the housing (2) vertically. The second air supply ducts (17, 18, 19, 20) for the propulsion rotors (14, 16) pass the housing in longitudinal direction. These ducts are formed as hollow aerofoil profiles with vertical profiles chord. The outlets of the first air supply ducts are arranged on the underside of the roof projecting beyond the cabin(1).
机译:旋翼驱动的飞机具有至少一对反向旋转的起升旋翼,以及至少一个单独的推进旋翼。所有转子及其供气管道均固定在机舱顶部的公共外壳中。所有转子均由一个公共驱动单元驱动。提升和推进转子具有单独的空气供应管道。用于提升转子(9、10)的第一组空气供应管道(11、12)垂直穿过壳体(2)。用于推进转子(14、16)的第二空气供应管道(17、18、19、20)在纵向上穿过壳体。这些导管形成为具有垂直轮廓弦的空心翼型轮廓。第一空气供应管道的出口布置在屋顶的下侧上,突出超过机舱(1)。

著录项

  • 公开/公告号DE2634837B1

    专利类型

  • 公开/公告日1978-01-19

    原文格式PDF

  • 申请/专利权人 HIEMER WILLIBALD;

    申请/专利号DE19762634837

  • 发明设计人 HIEMER WILLIBALD;

    申请日1976-08-03

  • 分类号B64C27/08;

  • 国家 DE

  • 入库时间 2022-08-22 22:01:21

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