To solve the problem that any helicopter as a conventional vertical taking-off/landing machine blows a strong air flow downwardly from its machine body to lift the machine body through aerodynamic reaction, and has defects of, for example, "strong wind damage around takeoff and landing sites", "loud noise", "low efficiency of fuel consumption due to inferior efficiency in propulsion by a rotor, a propeller and a fan in a machine body moving direction", etc.SOLUTION: There is provided "a disk lift force type vertical taking-off/landing machine" as a vertical taking-off/landing machine that solves "defects" by horizontally rotating a rotor mounted on an upper part of a machine body and a lift disk mounted on the rotor by respective rotary drive devices to generate "disk lift force" on the top surface of the lift force disk, and then generating lift force of the machine according to the rotor including the lift force disk with the upward lift force thereof.SELECTED DRAWING: Figure 1
【課題】従来の垂直離着陸機としてのヘリコプター等はいずれも機体の下方に向けて強力な空気流を吹き付けてその空力的反作用として機体を上昇させていたものであり、「離着陸地点の周辺に強い風害を生じさせる」「騒音が酷い」「ローターやプロペラやファンによる機体進行方向に対する推進効率が劣るために燃費効率が悪い」等の欠点があった。【解決手段】「機体の上部に装着された回転翼および回転翼に装着された揚力円盤をそれぞれの回転駆動装置により水平回転させることによって揚力円盤の上面に『円盤揚力』を発生させこの上方向への揚力の作用により揚力円盤を含む回転翼したがってまた機体に上昇力を発生させる」ことにより「上記の欠点を解消した垂直離着陸機としての『円盤揚力型垂直離着陸機』」を提供する。【選択図】図1
DISC LIFT FORCE TYPE VERTICAL TAKING-OFF/LANDING MACHINE (DISC LIFT FORCE MACHINE, CIRCULAR LIFT MACHINE)
円盤揚力型垂直離着陸機(円盤揚力機・円揚機)
26.09.2022
Patent
Elektronische Ressource
Japanisch
IPC: | B64C AEROPLANES , Flugzeuge |
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