PROBLEM TO BE SOLVED: To provide a vertical takeoff-and-landing flying object with a simple constitution, which can accelerate a flying speed without enlarging a size of a drive source, and can stably fly according to a flying status.SOLUTION: A vertical takeoff-and-landing flying object 1 comprises: an airframe 10; a plurality of linearly-extending arm parts 15 which intersect with each other with a center axis as a center when viewed from an axial direction of the center axis C which passes the center of gravity of the airframe 10; a plurality of propellers 17 which are arranged at both ends of a plurality of the arm parts 15, and arranged on a prescribed circumference around the center axis C when viewed from the axial direction of the center axis C; a turning mechanism which changes a distance along circumferences of the propeller 17 which is arranged at the turning arm part 15A and the propeller 17 which is adjacent thereto by making at least one arm part 15A out of the plurality of arm parts 15 turn around the center axis C; and a control unit which controls an operation of the turning mechanism.SELECTED DRAWING: Figure 1
【課題】簡易な構成を有し、駆動源のサイズを大きくすることなしに飛行速度を増加できるとともに、飛行状況に応じて安定して飛行することができる、垂直離着陸飛行体を提供する。【解決手段】垂直離着陸飛行体1は、機体10と、直線状に延在するとともに、機体10の重心を通る中心軸Cの軸方向から見た場合に中心軸を中心として互いに交差する複数のアーム部15と、複数のアーム部15の両端部に設けられ、中心軸Cの軸方向から見た場合に、中心軸Cまわりの所定の円周上に配置される複数のプロペラ17と、複数のアーム部15のうち少なくとも1つのアーム部15Aを中心軸Cまわり回動させることにより、回動するアーム部15Aに設けられたプロペラ17とこれに隣り合うプロペラ17との円周に沿った距離を変更する回動機構と、回動機構の動作を制御する制御部とを、備える。【選択図】図1
VERTICAL TAKEOFF-AND-LANDING FLYING OBJECT
垂直離着陸飛行体
2017-01-26
Patent
Electronic Resource
Japanese
IPC: | B64C AEROPLANES , Flugzeuge |
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