Integral suction device with acoustic panel

1. An inlet flow control system for a nacelle comprising:

a panel defining a portion of an interior surface of the nacelle, wherein said panel comprises a noise attenuation layer including a plurality of cells for dissipating noise energy within the nacelle, a face sheet including a plurality of openings for communicating noise energy through to the plurality of cells, and a back sheet supporting the plurality of cells and including openings in communication with the plurality of cells, wherein each of the plurality of cells include uninterrupted solid walls extending between the face sheet and the back sheet;

a plenum in communication with the back sheet and each of the openings in the back sheet that correspond to each of the plurality of cells

a vacuum source in communication with said plenum and generating a pressure differential desired to draw air through said panel and away from the interior surface of the nacelle.

2. The system as recited in claim 1 , wherein said panel comprises a face sheet disposed over said noise attenuation layer, wherein said face sheet includes a plurality of openings for communicating noise energy through to said noise attenuation layer.

3. The system as recited in claim 1 , wherein said noise attenuation layer comprises a plurality of cells defined by a plurality of walls disposed transverse to the interior surface of the nacelle.

4. The system as recited in claim 3 , wherein said plurality of walls include openings for communicating air between the plurality of cells.

5. The system as recited in claim 3 , including a back sheet supporting the noise attenuation layer, wherein said back sheet includes a plurality of openings providing communication with said vacuum source.

6. The system as recited in claim 1 , wherein said vacuum source comprises a vacuum pump.

7. The system as recited in claim 1 , wherein said vacuum source comprises an ejector.

8. The system as recited in claim 1 , including a passage for exhausting air drawn through said panel flowing along the inner surface of the nacelle.

9. A nacelle for a gas turbine engine comprising:

an intake opening for directing air to the gas turbine engine;

an inner surface including a noise attenuation panel including a plurality of cells covered on the inner surface by a face sheet including a plurality of openings, and supported on by a back sheet including a plurality of openings corresponding to each of the plurality of cells, the face sheet in communication with air flowing along said inner surface;

a plenum defining an open cavity disposed along the back sheet that is in communication with each of the openings within the back sheet; and

a vacuum source for generating a pressure differential that is in communication with the plenum for drawing a part of air flow along said inner surface through said noise attenuation panel.

10. The nacelle as recited in claim 9 , wherein said noise attenuation panel comprises a plurality of cells covered by a face sheet, wherein said face sheet includes a plurality of openings for communicating sound energy and air flow to said plurality of cells.

11. The nacelle as recited in claim 10 , wherein said noise attenuation panel comprises a plenum in communication with said vacuum source.

12. The nacelle as recited in claim 10 , wherein said noise attenuation panel includes a back panel for supporting said plurality of cells, said back panel including a plurality of openings in communication with said vacuum source.

13. The nacelle as recited in claim 12 , including a plenum disposed within said nacelle and in communication with said back panel.

14. The nacelle as recited in claim 13 , including a passage in communication with said plenum for exhausting air drawn through said noise attenuation panel away from said inner surface.

15. The nacelle as recited in claim 14 , wherein the passage comprises an outlet open to an exterior surface of the nacelle.