Four-rotor aircraft capable of tilt rotating in multi-direction

Four-rotor aircraft capable of tilt rotating in multi-direction

The invention relates to a four-rotor aircraft capable of tilt rotating in multi-direction. The four-rotor aircraft comprises a control module, a battery module, a rack, a first rotor mechanism, a second rotor mechanism, a third rotor mechanism and a fourth rotor mechanism, wherein the first rotor m...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: QU HUA, WANG ZHENG, LI WENSHEN, DAI CHAOFAN, SHI MENGCHENG, NIU HUITONG
Format: Patent
Sprache:chi ; eng
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:The invention relates to a four-rotor aircraft capable of tilt rotating in multi-direction. The four-rotor aircraft comprises a control module, a battery module, a rack, a first rotor mechanism, a second rotor mechanism, a third rotor mechanism and a fourth rotor mechanism, wherein the first rotor mechanism, the second rotor mechanism, the third rotor mechanism and the fourth rotor mechanism are symmetrically arranged at four corners of the rack, wherein the four rotor mechanisms all can rotate, the first rotor mechanism and the second rotor mechanism, and the third rotor mechanism and the fourth rotor mechanism are respectively connected through rotor connecting rods respectively, a rotatable direction control rod is arranged in the middle of the rack, the direction control rod is connected with the two rotor connecting rods through transmission connecting rods respectively, a driving motor module is further installed on the rack, the driving motor module is connected with the direction control rod through a