Hybrid power rotorcraft

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 o...

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Bibliographic Details
Main Author LI FANGJUN
Format Patent
LanguageChinese
English
Published 26.03.2024
Subjects
AIRCRAFT
AVIATION
COSMONAUTICS
PERFORMING OPERATIONS
TRANSPORTING
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Summary: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 ver
Bibliography:Application Number: CN202322051255U