Rotor aircraft with tilting mechanism driven by flexible steel wires to rotate

The rotorcraft comprises a tail rotor, a fuselage, wings, rotors, a tilting tower and tilting rotor wing mechanisms, the tail rotor is installed at the tail of the fuselage, the two wings are symmetrically installed on the two sides of the fuselage, the tilting rotor wing mechanisms and the tilting...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: BAI RUQING, LIU MINGQUE, PU HUAYAN, LUO JUN, LI ZHENTAN, SONG DAIPING, HOU LEI, SUN ZHI
Format: Patent
Sprache:chi ; eng
Schlagworte:
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Beschreibung
Zusammenfassung:The rotorcraft comprises a tail rotor, a fuselage, wings, rotors, a tilting tower and tilting rotor wing mechanisms, the tail rotor is installed at the tail of the fuselage, the two wings are symmetrically installed on the two sides of the fuselage, the tilting rotor wing mechanisms and the tilting tower are installed at the ends of the outer sides of the wings, and the tilting rotor wing mechanisms and the tilting tower are installed at the ends of the outer sides of the wings. The tilting rotor mechanism comprises an electric push rod assembly, a flexible steel wire and a pulley, a cylinder base of the electric push rod assembly is fixed to the fuselage, one end of the flexible steel wire is connected with the telescopic end of the electric push rod assembly, and the other end of the flexible steel wire is connected with a mounting base of the tilting tower after bypassing the pulley; the tilting rotor mechanism is used for driving the tilting tower to perform angle adjustment relative to the horizontal lin