首页> 外国专利> Horizontal and vertical take-off and landing combination aircraft used as a rotary wing and fixed-wing aircraft comprises a rotor lift used as a telescopic device for a rotary wing drive lowered into and lifted out of the fuselage

Horizontal and vertical take-off and landing combination aircraft used as a rotary wing and fixed-wing aircraft comprises a rotor lift used as a telescopic device for a rotary wing drive lowered into and lifted out of the fuselage

机译:用作旋转机翼和固定翼飞机的水平和垂直起飞和着陆组合飞机,包括用作升降机的旋翼升降机,用于旋转机翼驱动器下降并从机身升起

摘要

Horizontal and vertical take-off and landing combination aircraft comprises a rotor lift (1) used as a telescopic device for a rotary wing drive (3). The rotary wing drive is lowered into and lifted out of the fuselage (6). A slat (2) arranged below the front wings (7) allows stabilization of the aircraft during the raising/lowering process of the rotary wing drive and during the transition from fixed-wing to rotary wing operation. Preferred Features: The rear wing (8) can be adjusted relative to the fuselage to increase agility and roll speed.
机译:水平和垂直起飞和着陆组合飞行器包括旋翼升降机(1),用作旋翼驱动器(3)的伸缩装置。旋转翼驱动器下降到机身(6)中并从中提出。布置在前机翼(7)下方的板条(2)可以在旋转翼驱动装置的升/降过程以及从固定翼向旋转翼操作的过渡过程中稳定飞机。首选功能:后翼(8)可以相对于机身进行调节,以提高敏捷性和侧翻速度。

著录项

  • 公开/公告号DE10241732A1

    专利类型

  • 公开/公告日2004-03-25

    原文格式PDF

  • 申请/专利权人 HINUEBER EDGAR V.;

    申请/专利号DE2002141732

  • 发明设计人 HIMBOT JUERGEN;

    申请日2002-09-06

  • 分类号B64C29/00;

  • 国家 DE

  • 入库时间 2022-08-21 22:43:57

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