Power system of unmanned helicopter

The invention relates to the technical field of unmanned helicopters, and discloses a power system of an unmanned helicopter. Comprising an engine mounting structure; the engine body is arranged on the inner side of the engine mounting structure, and the engine body is fixedly connected with the eng...

Full description

Saved in:
Bibliographic Details
Main Author SUN ZHIWU
Format Patent
LanguageChinese
English
Published 02.05.2023
Subjects
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
Online AccessGet full text

Cover

More Information
Summary:The invention relates to the technical field of unmanned helicopters, and discloses a power system of an unmanned helicopter. Comprising an engine mounting structure; the engine body is arranged on the inner side of the engine mounting structure, and the engine body is fixedly connected with the engine mounting structure; the accelerator steering engine is arranged at the top end of the engine body, and the accelerator steering engine is connected with the engine body; the engine exhaust pipe is arranged at the bottom end of the side face of the engine body, and the engine exhaust pipe communicates with the engine body; the oxygen sensor is arranged on the side face of the engine exhaust pipe, an oxygen sensor detection head is arranged in the engine exhaust pipe, and the oxygen sensor is connected with the engine body. The overall gravity center of the engine body can be balanced through the arranged front heat dissipation water tank structure, so that the torque of the engine body is balanced, and then the
Bibliography:Application Number: CN202310165690