The invention discloses a turbojet manned aircraft based on vector control, and belongs to the field of aircrafts. The problems that an existing manned aircraft is complex in attitude adjustment and large in resolving amount are solved. The two vector power units are arranged in the x-axis direction and symmetrically installed on the left side and the right side of a fuselage, and thrust is provided for navigation and attitude adjustment of the aircraft. The man-machine fixing unit and the fuel tank are arranged in the y-axis direction and installed on the front side and the rear side of the aircraft body respectively, and the man-machine fixing unit is fixed to the body of an operator so that the aircraft can be fixed to the operator. The fuel tank is connected with the two vector power units and provides endurance fuel for the two vector power units. The main control unit is installed on the aircraft body 1 and electrically connected with the two vector power units respectively, control over the thrust vector of each vector power unit is achieved, and then control over the thrust vector of the aircraft is achieved. The method is mainly used for traffic trip of people.
一种基于矢量控制的涡喷载人飞行器,属于飞行器领域。为了解决现有的载人飞行器姿态调节复杂,解算量大的问题。本发明中的两个所述的矢量动力单元沿着x轴方向进行布置,且对称安装在机身的左右两侧,并为飞行器的航行和姿态调整提供推力;所述的人机固定单元和燃料箱沿着y轴方向进行布置,且分别安装在机身的前后两侧,所述的人机固定单元固定在操纵者身体上,以实现飞行器与操纵者的固定;所述的燃料箱分别与两个矢量动力单元连接,并为两个矢量动力单元提供续航燃料;所述的主控单元安装于机身1上,并分别与两个矢量动力单元电连接,实现每个矢量动力单元推力矢量的控制,进而实现飞行器推力矢量的控制。本发明主要用于人员的交通出行。
Turbojet manned aircraft based on vector control
一种基于矢量控制的涡喷载人飞行器
2024-08-16
Patent
Electronic Resource
Chinese
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