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
Elektronische Ressource
Englisch
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