A motorized aircraft is controlled by a drive control means (120) that rotationally drives a propulsion system propeller. The propulsion system propeller is driven by a plurality of electric motors (130). Total output of the plurality of electric motors (130) and required output satisfy the following relationship: Pmax(n−1)/n>Preq (where Pmax is the total output (kW) of the electric motors, n is the number of electric motors, and Preq is the required output (kW)).
Motorized Aircraft and Method for Determining Output and Number of Electric Motors in Motorized Aircraft
2017-07-06
Patent
Electronic Resource
English
European Patent Office | 2018
|European Patent Office | 2016
|MOTORIZED AIRCRAFT, AND CONTROL METHOD OF REGENERATIVE ELECTRIC POWER OF MOTORIZED AIRCRAFT
European Patent Office | 2018
|D2R: A 50 Passengers Electric Motorized Commercial Aircraft
British Library Conference Proceedings | 2014
|