发明名称 BOUNDARY LAYER SUCTION SYSTEM
摘要 Boundary layer (6) suction system for being adapted to a surface (1) exposed to the circulation of a fluid, the system comprising a portion of said surface (1) and: - a bifurcation element (2) for bifurcating a mass of fluid flowing along the front face of the surface (1), comprising an aerofoil-shaped cross-section such that the fluid is bifurcated into a first and a second flow, - a slot (3) located on the portion of the surface (1) and upstream the leading edge (5) of the bifurcation element (2), the slot (3) communicating the front and the rear faces of the portion of the surface (1), - means for providing a pressure difference between the front and the rear faces of the surface (1) around the slot (3) such that a suction of the boundary layer (6) is performed through the slot (3) by said pressure difference.
申请公布号 EP3121580(A1) 申请公布日期 2017.01.25
申请号 EP20150382377 申请日期 2015.07.21
申请人 Airbus Operations S.L. 发明人 DIAZ PARRILLA, José María;JARA RODELGO, Álvaro;GALLEGO LORENZO, Miguel Ángel;HERNANZ MANRIQUE, José Ángel
分类号 G01M9/04 主分类号 G01M9/04
代理机构 代理人
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