首页> 外国专利> METHOD OF THE LIFT (moving) FORCE AIRCRAFT, METHOD OF SPATIAL MANOEUVRING orbiting spacecraft, propulsion devices for their implementation (optional), the vehicle (optional)

METHOD OF THE LIFT (moving) FORCE AIRCRAFT, METHOD OF SPATIAL MANOEUVRING orbiting spacecraft, propulsion devices for their implementation (optional), the vehicle (optional)

机译:提升(移动)力飞机的方法,空间飞行航天器的方法,用于其实施的推进装置(可选),飞行器(可选)

摘要

1. A method for producing a lifting (driving) force the body of the aircraft by rotation about its own axis using a motor, characterized in that the lift (driving) force created by accelerating the liquid in the body radially arranged ducts, fluid movement can bend in planes which belongs body axis of rotation in a direction opposite to the direction of lift generated (driving) force, thus providing resistance to movement of the liquid working fluid due to the velocity head vstrechnog a liquid stream using water seal or by setting the valves in nozzles radial kanalov.2. Method spatial maneuvering orbiting spacecraft, characterized in that the change in the spatial position of the orbital vehicle without changing its mass, by decreasing (increasing) the weight of the parts or decrease (increase) the weight of the aircraft, when the propulsion creating lift (driving) force due to acceleration of the fluid in the body radially arranged ducts, fluid movement can bend in planes which belongs Referring rotation of the body in a direction opposite to the direction of lift generated (driving) sily.3. The propulsion device comprising a housing within which is mounted a rotor driven by a motor, characterized in that the housing has a hydraulic and air channels in the inner cavity of a vertically disposed hollow rotor mounted fan, a rotor body made windows and radial channels for the passage of the liquid working medium, EMPTY
机译:1。一种通过使用电动机绕其自身轴线旋转来产生飞行器主体的提升(驱动)力的方法,其特征在于,所述提升(驱动)力是通过使径向布置的管道中的液体加速,流体运动而产生的。可以在属于人体旋转轴的平面内沿与产生的升力方向(驱动力)相反的方向弯曲,从而通过使用水封或通过设置速度来防止液体工作流体因速度头而产生阻力。喷嘴径向卡纳洛夫中的阀2。一种空间机动轨道飞行器的方法,其特征在于,当推进力产生升力时,通过减小(增加)零件的重量或减小(增加)飞机的重量,在不改变其质量的情况下改变轨道飞行器的空间位置。由于流体在径向布置的管道中的加速而产生的(驱动)力,流体的运动会在属于该平面的平面中弯曲。沿与生成(驱动)淤泥的升力方向相反的方向旋转。该推进装置包括壳体,该壳体中安装有由电动机驱动的转子,其特征在于,该壳体在垂直设置的中空转子安装风扇的内腔中具有液压通道和空气通道,转子主体制成的窗口和用于径向的径向通道。液体工作介质通过,空

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