Flow separation control device for an airfoil

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United States of America Patent

PATENT NO 11338909
SERIAL NO

15425964

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Abstract

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A combination of an airfoil, turbine blade, or compressor blade with a flow separation control device includes an airfoil, a flow separation control device, and an injection system. The airfoil includes a body with an upper surface and a lower surface that extend from a leading edge to a trailing edge. The flow separation control device includes a plurality of openings on the upper surface of the body. The injection system includes an inlet tube, a pump in gaseous communication with the inlet tube, and a flow regulator in gaseous communication with the pump and the plurality of capillary tube.

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Patent Owner(s)

Patent OwnerAddress
ALHUSSAN KHALED ABDULLAHRIYADH

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Alhussan, Khaled Abdullah Riyadh, SA 14 11

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