The invention relates to the field of aircrafts, in particular to a magnetic suspension delta wing aircraft, a controller is arranged in the aircraft, the aircraft is triangular, a mounting hole is formed in the center of the aircraft, a first pneumatic flight assembly is connected to the interior of the mounting hole through magnetic suspension, and a flap is hinged to the rear end of the aircraft; the single-rotor aircraft has the advantages that a single-rotor structure is adopted, a magnetic suspension structure system is used for replacing a traditional roller bearing, non-contact supporting of a rotating shaft is achieved, and the single-rotor aircraft has the advantages of being small in frictional resistance, not limited by the rotating speed, wide in working temperature range, long in service life, high in reliability and the like. And steady noise of the aircraft is reduced.
本发明涉及飞行器领域,具体涉及磁悬浮三角翼飞行器,飞行器内置有控制器,所述飞行器呈三角状,所述飞行器中心开设有安装孔,所述安装孔内部通过磁悬浮连接有第一气动飞行组件,所述飞行器后端铰接有襟翼,所述飞行器后端还设置有第二气动飞行组件,本发明的有益效果是:采用单旋翼结构,并利用磁悬浮结构系统代替传统的滚子轴承,实现转轴的无接触支撑,具有摩擦阻力小、不受转速限制、工作温度范围宽、使用寿命长,以及降低了飞行器定常噪声等优点。
Magnetic suspension delta wing aircraft
磁悬浮三角翼飞行器
2024-07-09
Patent
Electronic Resource
Chinese