To provide a motorized aircraft capable of optimizing aerodynamic performance of a wing in an emergency, for example, in each flight phase or during a blast action, without depending on the shape of the wing, and an aerodynamic performance control method.SOLUTION: A motorized aircraft 1 comprises: one or more electric propulsion systems 20 that have a propeller or a fan 21 for propulsion, arranged to contribute to lifts of main wings 11 and 12, and an electric motor 22 for driving the propeller or the fan 21; and a control part that adjusts the electric propulsion system 20 so that total thrust generated by the electric propulsion system 20 or an aerodynamic force generated on the main wings 11 and 12 can be a predetermined value or fall within a predetermined range, on the basis of a relationship between a variable associated with an operational state of the electric propulsion system 20 and the aerodynamic force generated on the main wings 11 and 12.SELECTED DRAWING: Figure 2
【課題】翼の空力性能を、翼の形状に依存せずに、各飛行フェイズあるいは突風作用時等の非常時に最適化することができる電動化航空機及びその空力性能制御方法を提供すること。【解決手段】電動化航空機1は、主翼11、12の揚力に寄与するように配置された推進用のプロペラ又はファン21と、プロペラ又はファン21を駆動する電動モータ22とを有する1又は2以上の電動推進系20と、電動推進系20の運転状態に関する変数と主翼11、12に発生する空気力との関係に基づいて、電動推進系20による合計推力又は主翼11、12の空気力が所定の値又は所定の範囲になるように、電動推進系20を調節する制御部とを具備する。【選択図】図2
MOTORIZED AIRCRAFT AND AERODYNAMIC PERFORMANCE CONTROL METHOD
電動化航空機及びその空力性能制御方法
2021-04-15
Patent
Electronic Resource
Japanese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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