PROBLEM TO BE SOLVED: To secure a stable posture during a period of transiting from a horizontal flight state to a hovering or descending state, or from a vertical takeoff or hovering state to horizontal flight.SOLUTION: A vertical takeoff and landing flying body is constituted of: a first main wing 200 composed of a left wing and a right wing and attached to a front upper part of an airframe 100; a second main wing 500 composed of a left wing and a right wing and attached to a rear upper part of the airframe; engines 300, 310, 320, 330 each arranged at an approximately longitudinal center position of the respective left and right wings of the first main wing and the second main wing; flaps 211, 221, 231, 241 each provided in the rear of each engine and for controlling ascending/descending of the airframe by its action; and rudders 210, 220, 230, 240 each provided in the rear of each engine and for controlling a traveling direction of the airframe by its action. The first main wing and the second main wing are configured to be pivotally moved vertically or horizontally in an integral manner with the engines, flaps and rudders.SELECTED DRAWING: Figure 6

    【課題】水平飛行状態からホバリング状態または下降状態、あるいは、垂直離陸上昇またはホバリング状態から水平飛行に移行するまでの間において安定的な姿勢を確保する。【解決手段】機体100の前部であってこの機体の上部に取り付けられた左翼および右翼からなる第一の主翼200と、機体の後部であってこの機体の上部に取り付けられた左翼および右翼からなる第二の主翼500と、第一の主翼および第二の主翼のそれぞれの左翼および右翼の長さ方向に対して略中心位置に配置されるエンジン300,310と、エンジンの後方にそれぞれ設けられその作用により機体の上昇・下降を制御するフラップ211,221と、エンジンの後方にそれぞれ設けられその作用により機体の進行方向を制御する方向舵210,220と、から構成し、第一の主翼と第二の主翼とエンジンとフラップおよび方向舵とともに一体的に垂直方向又は水平方向に枢動させる構成とした。【選択図】図6


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    Title :

    VERTICAL TAKEOFF AND LANDING FLYING BODY


    Additional title:

    垂直離着陸飛行体


    Contributors:

    Publication date :

    2016-09-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B60F VEHICLES FOR USE BOTH ON RAIL AND ON ROAD , Fahrzeuge für den Verkehr sowohl auf Schienen als auch auf Straßen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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