Aircraft and coaxial dual-rotor assembly

The invention provides an aircraft. The aircraft comprises a fuselage, a wing assembly, a tilt rotor assembly and a coaxial double-rotor assembly, and the wing assembly is connected to the fuselage; the tilting rotor assembly is connected to the wing assembly in a tilting manner; and the coaxial dou...

Full description

Saved in:
Bibliographic Details
Main Authors WANG TAN, CAO XUEYU, LIANG YICHENG, SHI YICHEN, LOU JINYUAN, WANG WEIMIN
Format Patent
LanguageChinese
English
Published 07.12.2021
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
Online AccessGet full text

Cover

More Information
Summary:The invention provides an aircraft. The aircraft comprises a fuselage, a wing assembly, a tilt rotor assembly and a coaxial double-rotor assembly, and the wing assembly is connected to the fuselage; the tilting rotor assembly is connected to the wing assembly in a tilting manner; and the coaxial double-rotor assembly comprises a mounting shaft, a first blade and a second blade, the mounting shaft is connected to the fuselage, the first blade and the second blade are rotatably connected to the two opposite ends of the mounting shaft respectively, and the rotating direction of the first blade is opposite to the rotating direction of the second blade. According to the aircraft provided by the invention, the coaxial dual-rotor assembly is arranged, and the rotation direction of the first blade of the coaxial dual-rotor assembly is opposite to the rotation direction of the second blade, so that reaction torque generated by the aircraft can be counteracted, the stability of the course of the aircraft is improved, a
Bibliography:Application Number: CN202111183897