Wing tilting structure and aircraft

The utility model relates to a wing tilting structure and an aircraft. The wing tilting structure comprises a central wing rib, a tilting mechanism and a flight power assembly, one end of the central wing rib is used for being connected with an aircraft body of the aircraft, the tilting mechanism co...

Full description

Saved in:
Bibliographic Details
Main Authors ZHANG RUI, WANG TAN, LI ZHIDE, LIANG YICHENG, JIANG HUAQIANG, SHI YICHEN, LOU JINYUAN, CHEN ZHOUXIAN
Format Patent
LanguageChinese
English
Published 22.11.2022
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
Online AccessGet full text

Cover

More Information
Summary:The utility model relates to a wing tilting structure and an aircraft. The wing tilting structure comprises a central wing rib, a tilting mechanism and a flight power assembly, one end of the central wing rib is used for being connected with an aircraft body of the aircraft, the tilting mechanism comprises a connecting beam and a driving part, one end of the connecting beam is connected to the side, away from the aircraft body, of the central wing rib, and the driving part is arranged at the other end of the connecting beam; the flight power assembly is connected to the driving part, and the driving part drives the flight power assembly to rotate relative to the central wing rib so as to change the airflow thrust direction of the flight power assembly. According to the technical scheme, by driving the flight power assembly to rotate relative to the central wing rib and changing the airflow thrust direction of the flight power assembly, the aircraft can take off and land vertically or take off and land in a sl
Bibliography:Application Number: CN202221876400U