IIP情報・知能・精密機器部門講演会講演論文集
Online ISSN : 2424-3140
セッションID: P04_1
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プロペラ吸排気一体型モジュールの開発
*小川 裕雅五十嵐 洋
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This paper addresses the mechanism for obtaining intake amount and thrust by the drone 's motor. The mechanism is composed of a diaphragm pump and a brushless motor. The intake amount can be realized by the rotation force of the motor. The compact mechanism that gets buoyancy and the air-intake from the rotation of the motor is proposed. Finally, the response time of the intake is verified by the rotational velocity by current value

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