To provide a vertically taking-off/landing flight vehicle that can change a wing attachment angle without needing to change a direction of propulsion power during transition from vertically taking-off to horizontal flight and transition from horizontal flight to vertically landing.SOLUTION: A vertically taking-off/landing flight vehicle 1 is equipped with: a fuselage 10; main wings 20 for horizontal flight mounted on left and right sides with respect to the fuselage 10; three or more propulsion parts 40 whose propulsion power can be controlled individually; and arms 50 with which the propulsion parts 40 are mounted on the fuselage 10 so that propulsion power is applied to an upper side in an axial direction of the fuselage 10 when the fuselage 10 is turned to be nearly vertical to the ground, with a positional relation in which remaining one or more propulsion parts 40 are not included in a plane which is parallel to a shaft of the fuselage 10 including arbitrary two propulsion parts 40, of the three or more propulsion parts 40.SELECTED DRAWING: Figure 1
【課題】垂直離陸から水平飛行への移行時及び水平飛行から垂直着陸への移行時に推進力の向きを変化させる必要がなく移行可能であり、主翼取付角度を変更することができる垂直離着陸飛行体を提供する。【解決手段】胴体10と、胴体10軸に対して左右に取り付けられた水平飛行用の主翼20と、推進力を個別に制御することができる3以上の推進部40と、3以上の推進部40のうち、任意の2つの推進部40を含む胴体10軸と平行な平面内に、残りの1以上の推進部40が含まれないような位置関係で、胴体10を地面に対してほぼ垂直にした際に、胴体10の軸方向上方に推進力を与える向きになるように推進部40を胴体10に取り付けるアーム50と、を備えることを特徴とする垂直離着陸飛行体1。【選択図】図1
VERTICALLY TAKING-OFF/LANDING FLIGHT VEHICLE
垂直離着陸飛行体
2024-02-16
Patent
Electronic Resource
Japanese
IPC: | B64C AEROPLANES , Flugzeuge |
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