ELECTRIC AIRCRAFT AND POWER SUPPLY DEVICE

PROBLEM TO BE SOLVED: To reduce the weight of an electric aircraft.SOLUTION: The present invention provides an electric aircraft comprising a plurality of rotary wings, a motor that rotates each of the rotary wings, a support shaft that supports each rotary wing and motor, a motor control unit that...

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Bibliographic Details
Main Authors SAKAI HIROTAKA, MISAWA DAIKI, MORI YASUSHI, KUSUMI YASUYUKI
Format Patent
LanguageEnglish
Japanese
Published 28.12.2016
Subjects
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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Summary:PROBLEM TO BE SOLVED: To reduce the weight of an electric aircraft.SOLUTION: The present invention provides an electric aircraft comprising a plurality of rotary wings, a motor that rotates each of the rotary wings, a support shaft that supports each rotary wing and motor, a motor control unit that controls the rotation of each motor, a plurality of power supply lines that supply each pair of motors with power, and a plurality of battery modules each connected to a power supply line.SELECTED DRAWING: Figure 5 【課題】電動式航空機を軽量化する。【解決手段】複数の回転翼と、回転翼をそれぞれ回転させるモータと、回転翼およびモータをそれぞれ支持する支持軸と、モータの回転を制御するモータ制御部と、モータの対毎に電力を供給する複数の電力供給ラインと、電力供給ライン毎に接続される複数のバッテリモジュールとを備えた電動式航空機である。【選択図】図５
Bibliography:Application Number: JP20150108195