发明名称 VERTICAL TAKEOFF AND LANDING MACHINE
摘要 PROBLEM TO BE SOLVED: To provide a vertical takeoff and landing machine capable of generating thrust for moving toward a desired direction without increasing a weight of an airframe.SOLUTION: A vertical takeoff and landing machine comprises: plural rotor units 20; a rotor deflection servo motor 20b for adjusting a direction of thrust Fn which is generated by each of the plural rotor units; and a control part for controlling magnitude and a direction of the thrust Fn. The plural rotor units are formed of plural rotor unit pairs which are arranged in a point symmetric state about a main body. The rotor deflection servo motor swings the direction of thrust Fn of each of the rotor units forming each rotor unit pair around a single swing shaft, and makes a shaft direction of the swing shaft of each of the plural rotor unit pairs different from each other. The control part performs control so that magnitude and direction of the thrust Fn generated by each of the rotor units forming each rotor unit pair become identical.SELECTED DRAWING: Figure 3
申请公布号 JP2016032971(A) 申请公布日期 2016.03.10
申请号 JP20140156367 申请日期 2014.07.31
申请人 MITSUBISHI HEAVY IND LTD 发明人 KONO NAOKI
分类号 B64C27/08;B64C13/18;B64C39/02;B64D27/24 主分类号 B64C27/08
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