The invention relates to a vortex generator for an aircraft. The vortex generator for the aircraft comprises a first flow deflector and a second flow deflector, the second flow deflector is installedto be perpendicular to the first flow deflector, the second flow deflector is in an isosceles triangle shape, and the symmetric center line of the isosceles triangle is located in the plane of the first flow deflector. The vortex generator has the following beneficial technical effect: the gas-flow separation control capacity is enhanced.
本发明涉及用于飞机的涡流发生器。所述用于飞机的涡流发生器包括第一导流片和第二导流片,所述第二导流片安装成垂直于所述第一导流片,所述第二导流片呈等腰三角形,所述等腰三角形的对称中心线位于所述第一导流片的平面内。本发明能起到以下有益技术效果:增强对气流分离的控制能力。
Vortex generator for aircraft
用于飞机的涡流发生器
24.07.2020
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
Vortex generator, aircraft and control method of aircraft
Europäisches Patentamt | 2024
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