Development of the Propeller Integrated with Diaphragm Pump

Abstract

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