To provide a motorized aircraft capable of generating an aerodynamic force without excess or deficiency, without diminishing fuel consumption performance, and an attitude control method for the same.SOLUTION: In a motorized aircraft 1, an electric propulsion system 20, which comprises a propulsion propeller 21 and an electric motor 22 for driving it, is arranged at a front edge of a wing 10 so that a race generated by the electric propulsion system 20 can act on the wing 10. A control part 30 enables thrust of the thrust of the electric propulsion system 20 to be adjusted to a negative value.SELECTED DRAWING: Figure 1
【課題】燃費性能を損なうことなく、空気力を過不足なく発生することができる電動化航空機及びその姿勢制御方法を提供すること。【解決手段】電動化航空機1では、翼10の前縁に、推進用のプロペラ21及びこれを駆動する電動モータ22により構成される電動推進系20を、この電動推進系20による後流が翼10に作用するよう配置している。制御部30は、電動推進系20の推力を負の値まで調節することが可能である。【選択図】図1
MOTORIZED AIRCRAFT AND ATTITUDE CONTROL METHOD FOR THE SAME
電動化航空機及びその姿勢制御方法
2021-04-15
Patent
Electronic Resource
Japanese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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