The invention relates to an aircraft lift surface and to an aircraft comprising such a lift surface, the aircraft lift surface comprising: an aerodynamic surface (11) having a first electrode (21) embedded at the surface thereof; and a control surface (12) articulated to the aerodynamic surface (11), characterized in that the control surface (12) comprises a second electrode (22) embedded at its surface, and the first electrode (21) and the second electrode (22) are arranged and adapted to generate a plasma (36) in the air when a predetermined electrical tension, referred to as ionization tension, is applied between the first electrode (21) and the second electrode (22).
本发明涉及一种飞行器升力表面和一种包括这种升力表面的飞行器,该飞行器升力表面包括:空气动力学表面(11),该空气动力学表面(11)具有嵌入在其表面处的第一电极(21);以及控制表面(12),该控制表面(12)铰接至空气动力学表面(11),其特征在于,控制表面(12)包括嵌入在其表面处的第二电极(22),并且第一电极(21)和第二电极(22)布置成并且适于当在第一电极(21)与第二电极(22)之间施加被称为电离张力的预定电张力时在空气中产生等离子体(36)。
Aircraft lift surface and aircraft comprising such lift surface
飞行器升力表面和包括这种升力表面的飞行器
2024-11-26
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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