The present invention comprises: a fuselage body (1); a thrust generating unit (6) that has one or more thrust generating subunits (3); and a joint (5) that is provided so as to correspond to each ofthe thrust generating subunits and that connects the corresponding thrust generating subunit to the fuselage body so that the thrust generating subunit is turnable in the circumferential direction about a first turning axis (R), which intersects the direction of thrust generated by the thrust generating subunit. Each of the thrust generating subunits has a plurality of thrust generators (9), whichcan independently change the magnitude of thrust generated. In each of the thrust generating subunits, a first thrust generator group (G1) composed of one or more thrust generators from among the plurality of thrust generators is disposed so as to generate a torque (tao 1) such that the thrust generating subunit is urged toward one side in the circumferential direction about the first turning axis by the generated thrust. A second thrust generator group (G2) composed of one or more other thrust generators is disposed so as to generate a torque (tao 2) such that the thrust generating subunit is urged toward the other side in the circumferential direction about the first turning axis (R) by the generated thrust.

    具备机体主体(1);具有一个以上推力产生子单元(3)的推力产生单元(6);和对应各推力产生子单元地设置,将对应的推力产生子单元相对于机体主体在以与对应的推力产生子单元生成的推力方向相交的第一转动轴线(R)为中心的圆周方向上转动自如地连接的关节(5);各推力产生子单元具有多个推力产生部(9),多个推力产生部能互相独立地改变生成的推力大小,在各所述推力产生子单元中,多个推力产生部中一个以上的推力产生部构成的第一推力产生部组(G1)配设为通过生成的推力产生向以第一转动轴线为中心的圆周方向一侧对所述推力产生子单元施力的转矩(τ1);其它一个以上的推力产生部构成的第二推力产生部组(G2)配设为通过生成的推力产生向以第一转动轴线(R)为中心的圆周方向另一侧对所述推力产生子单元施力的转矩(τ2)。


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    Titel :

    AIRCRAFT AND METHOD FOR CONTROLLING AIRCRAFT


    Weitere Titelangaben:

    飞行体以及飞行体的控制方法


    Beteiligte:

    Erscheinungsdatum :

    2021-01-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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