首页> 外国专利> VERTICAL TAKEOFF AND LANDING FLYING VEHICLE WITH AERODYNAMIC LIFTING TRACTOR-TYPE PROPELLER

VERTICAL TAKEOFF AND LANDING FLYING VEHICLE WITH AERODYNAMIC LIFTING TRACTOR-TYPE PROPELLER

机译:气动起升牵引式螺旋桨的垂直起降飞行器

摘要

FIELD: aeronautical engineering.;SUBSTANCE: proposed flying vehicle has fuselage 10 with tail 11, aerodynamic lifting tractor-type propeller mounted at side of tail 11, tail rotor 12 whose rotation shaft 13 is mounted horizontally and is turnable in horizontal plane through angle of 90°; it is also movable in vertical plane. Propeller axle 1 is shifted relative to horizontal plane of symmetry of fuselage 10 to side opposite to tail rotor 12 and is inclined from vertical through angle lesser than 10°. Tail rotor 12 may be made as two-stage version at opposite rotation of stages.;EFFECT: extended range of capabilities.;2 cl, 3 dwg
机译:领域:拟议的飞行器具有带尾部11的机身10,在尾部11的侧面安装有气动提升拖拉机式螺旋桨,其尾桨12的转轴13水平安装并且可在水平面内旋转角度为90°;它也可以在垂直平面上移动。螺旋桨轴1相对于机身10的对称水平面向与尾旋翼12相反的一侧移动,并且从竖直方向倾斜小于10°的角度。尾旋翼12可以制成两级版本,每级反向旋转;效果:功能范围扩大; 2 cl,3 dwg

著录项

  • 公开/公告号RU2260546C1

    专利类型

  • 公开/公告日2005-09-20

    原文格式PDF

  • 申请/专利权人

    申请/专利号RU20040115483

  • 发明设计人 AKARO A.I.;MEDVEDEV M.M.;ZELINSKIJ A.M.;

    申请日2004-05-24

  • 分类号B64C27/82;

  • 国家 RU

  • 入库时间 2022-08-21 22:01:56

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