Fuselage integrated structure of unmanned helicopter

The utility model relates to the technical field of unmanned helicopter parts, in particular to a fuselage integrated structure of an unmanned helicopter, which comprises a fuselage body, and the fuselage body comprises a nose section at the front end and a tail section at the rear end; engine inspe...

Full description

Saved in:
Bibliographic Details
Main Author SUN ZHIWU
Format Patent
LanguageChinese
English
Published 04.11.2022
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
Online AccessGet full text

Cover

More Information
Summary:The utility model relates to the technical field of unmanned helicopter parts, in particular to a fuselage integrated structure of an unmanned helicopter, which comprises a fuselage body, and the fuselage body comprises a nose section at the front end and a tail section at the rear end; engine inspection windows are formed in the front face and the two sides of the machine head section, speed reducer inspection windows, coupler hatch cover inspection windows and cargo hold placement windows are further arranged on the two sides of the machine head section, and multiple sets of transmission shaft maintenance windows are arranged on the two sides of the machine tail section; the engine inspection window, the speed reducer inspection window, the coupler hatch cover inspection window, the cargo hold placement window and the transmission shaft maintenance window are all provided with hatch covers through bolts. And a vertical stabilizer is further arranged at the tail part of the tail section. The fuselage has goo
Bibliography:Application Number: CN202221931597U