The invention relates to a tail section flow guide type rotor module and a rotor type aircraft, the tail section flow guide type rotor module comprises a fan cover, a motor part, a gravity heat pipe fitting, an air paddle and a flow guide empennage, one end of the fan cover is provided with an air inlet, the gravity heat pipe fitting is arranged at the end, close to the air inlet, of the fan cover, and the motor part is arranged on the side, away from the air inlet, of the gravity heat pipe fitting; the gravity heat pipe fitting can dissipate heat of a stator of the motor part, a rotor of the motor part can drive the air paddle to rotate, and a flow guide channel extending in the axial direction of the air paddle is arranged between the air paddle and the rotor of the motor part. One end of the flow guide tail fin is communicated with the fan cover, the other end of the flow guide tail fin is provided with an air outlet, and airflow sequentially penetrates through the air inlet, the gravity heat pipe fitting, the flow guide channel, the flow guide tail fin and the air outlet. According to the tail section diversion type rotor wing module and the rotor wing type aircraft, the problem that the rotor wing type aircraft is difficult to consider the heat dissipation efficiency of the motor and the flight stability of the rotor wing type aircraft at the same time is solved.
本申请涉及一种尾段导流式旋翼模块及旋翼式飞行器,尾段导流式旋翼模块包括风罩、电机件、重力热管件、空气桨和导流尾翼,风罩的一端设有进风口,重力热管件设置于风罩靠近进风口的一端,电机件设置于重力热管件远离进风口的一侧,重力热管件能够对电机件的定子进行散热,电机件的转子能够带动空气桨转动,空气桨和电机件的转子之间设有沿着空气桨轴向延伸的导流通道;导流尾翼设置于风罩远离进风口的一端,导流尾翼的一端连通风罩,另一端设有出风口,气流依次穿过进风口、重力热管件、导流通道、导流尾翼和出风口。本申请提供的尾段导流式旋翼模块及旋翼式飞行器,解决了旋翼式飞行器难以兼顾电机的散热效率和旋翼式飞行器的飞行稳定性问题。
Tail section flow guide type rotor wing module and rotor wing type aircraft
尾段导流式旋翼模块及旋翼式飞行器
25.04.2025
Patent
Elektronische Ressource
Chinesisch
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