A hybrid power rotorcraft comprises a rotorcraft body, rotors are arranged at the top of the rotorcraft body, propellers are arranged on the left side and the right side of the rotorcraft body respectively, a top driver, a left motor and a right motor are arranged in the rotorcraft body, the power output end of the top driver is connected with the rotors, and the power output ends of the left motor and the right motor are connected with the corresponding propellers respectively. A central distribution box and a power module are arranged in the machine body, a power supply loop is arranged on the power module and connected with the central distribution box, the top driver, the left motor and the right motor are connected with the central distribution box, a tilting mechanism connected with the propeller is arranged in the machine body, and the propeller is driven by the tilting mechanism to rotate in the circumferential direction. And in addition, propellers on the two sides of the aircraft body are in the vertical state in the take-off and descending processes of the aircraft body. The motor is adopted for driving, the propellers on the two sides are matched with the top rotor wings, and vertical take-off and landing and hovering can be achieved.
一种复合动力旋翼机,包括机体,机体顶部设有旋翼,机体的左右两侧分别设有螺旋桨,所述机体内设有顶部驱动器、左侧电机和右侧电机,顶部驱动器的动力输出端与旋翼连接,左侧电机和右侧电机的动力输出端分别与对应的螺旋桨连接,机体内设有中央分电箱和电源模组,电源模组上设有供电回路,该供电回路与中央分电箱连接,顶部驱动器、左侧电机和右侧电机分别与中央分电箱连接,机体内设有与螺旋桨连接的倾转机构,通倾转机构带动螺旋桨进行圆周方向转动,实现倾斜和垂直方向的调整,并且机体在起飞和下降过程中使机体两侧的螺旋桨均处于垂直状态。本发明采用电机驱动,两侧螺旋桨配合顶部旋翼,实现可垂直起降、可悬停。
Hybrid power rotorcraft
一种复合动力旋翼机
2023-10-20
Patent
Elektronische Ressource
Chinesisch
IPC: | B64U |
Hybrid Power Supply For Electric Multirotor Rotorcraft
Europäisches Patentamt | 2017
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