MULTICOPTER

MULTICOPTER

To provide a multicopter capable of enhancing turning performance.SOLUTION: In a multicopter 10, multiple rotors 12FL, 12FR, 12RL, 12RR respectively comprising propellers 14FL, 14FR, 14RL, 14RR and motors 16FL, 16FR, 16RL, 16RR for driving the propellers are attached to a frame 20 of an airframe 18....

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser: KUSUMOTO MAKOTO
Format: Patent
Sprache:eng ; jpn
Schlagworte:
AEROPLANES
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
HELICOPTERS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:To provide a multicopter capable of enhancing turning performance.SOLUTION: In a multicopter 10, multiple rotors 12FL, 12FR, 12RL, 12RR respectively comprising propellers 14FL, 14FR, 14RL, 14RR and motors 16FL, 16FR, 16RL, 16RR for driving the propellers are attached to a frame 20 of an airframe 18. This frame is provided with frame coupling mechanisms 34 (rotor inclination mechanisms) including elastic elements and attenuation elements. The frame coupling mechanism 34 inclines each rotor in an airframe lateral direction while elastically deforming the elastic element by anti-torque of each propeller, as well as, attenuates vibration of each rotor due to inclination by the attenuation element.SELECTED DRAWING: Figure 1 【課題】旋回性能を向上可能なマルチコプターを提供する。【解決手段】マルチコプター１０では、プロペラ１４ＦＬ，ＦＲ，ＲＬ，ＲＲ及び該プロペラを駆動するモータ１６ＦＬ，ＦＲ，ＲＬ，ＲＲを各々が有する複数のロータ１２ＦＬ，ＦＲ，ＲＬ，ＲＲが、機体１８のフレーム２０に取り付けられている。このフレームには、弾性要素及び減衰要素を含んだフレーム連結機構３４（ロータ傾動機構）が設けられている。このフレーム連結機構３４は、各プロペラの反トルクによって弾性要素を弾性変形させつつ各ロータを機体の左右方向に傾動させると共に、当該傾動に伴う各ロータの振動を減衰要素によって減衰する。【選択図】図１