Airfoil for flow control including a common inlet/outlet device connected to a porous section

1. An airfoil for flow control, comprising

an outer skin in contact with an ambient air flow, wherein the outer skin extends between a leading edge and a trailing edge with two opposite lateral sides, and surrounds an interior space, and wherein the outer skin comprises a porous section in the area of the leading edge,

a pressure chamber arranged in the interior space, wherein the pressure chamber is fluidly connected to the porous section,

an air inlet/outlet device provided in the outer skin, wherein the air inlet/outlet device is fluidly connected to the pressure chamber, wherein an overpressure in the pressure chamber causes the air to discharge through the porous section into the ambient air flow, and

wherein an underpressure in the pressure chamber causes the air of the ambient air flow to be suctioned in through the porous section, and wherein the air the air inlet/outlet device is configured to selectively let air in from the ambient air flow or discharge air into the ambient air flow, and

wherein the air inlet/outlet device comprises an opening that is flush with the outer skin,

wherein, the air inlet/outlet device further comprises a door having a first door portion and a second door portion,

wherein the first door portion is mounted to the outer skin by a first hinge arranged on a side of the door facing the leading edge, and

wherein the first door portion is connected to the second door portion by a second hinge.

2. The airfoil according to claim 1 ,

wherein the door is pivotable between a closed position where the ambient air flow is inhibited from passing through the outer skin and entering the airfoil, and an inlet position where the ambient air flow may pass through the outer skin into the airfoil, and

wherein in the closed position the door is flush with the outer skin, and in the inlet position a channel is formed between the door and an edge of the opening for ambient air flow to pass through the outer skin into the airfoil.

3. The airfoil according to claim 1 , wherein the first hinge has a vertical first hinge axis.

4. The airfoil according to claim 1 , wherein the second hinge has a vertical second hinge axis that is spaced in parallel from the first hinge axis.

5. The airfoil according to claim 1 , wherein the air outlet is formed by the second door portion being pivotable outwards relative to the first door portion out of the closed position of the door, wherein the second door portion is movable between the closed position of the door, where air is inhibited from passing through the outer ski to or from the ambient air flow, and an outlet position, where the second door portion is pivoted relative to the first door portion outwards into the ambient air flow, so that air from inside the airfoil may pass through the outer skin to the ambient air flow.

6. The airfoil according to claim 1 , wherein the air outlet is formed by the door being pivotable about the first hinge outwards into the ambient air flow, so that air from inside the airfoil may pass through the outer skin to the ambient air flow.

7. The airfoil according to claim 1 , wherein the inlet/outlet device has two opposite walls that proceed in a diverging manner in a direction from the leading edge to the trailing edge.

8. The airfoil according to claim 7 , wherein the two opposite walls proceed in the form of a wave in the direction from the leading edge to the trailing edge such that the distance between the two opposite walls first increases with an increasing slope and subsequently increases with a decreasing slope.

9. An airfoil for flow control, comprising

an outer skin in contact with an ambient air flow, wherein the outer skin extends between a leading edge and a trailing edge with two opposite lateral sides, and surrounds an interior space, and wherein the outer skin comprises a porous section in the area of the leading edge,

a pressure chamber arranged in the interior space, wherein the pressure chamber is fluidly connected to the porous section,

an air inlet/outlet device provided in the outer skin, wherein the air inlet/outlet device is fluidly connected to the pressure chamber, wherein an overpressure in the pressure chamber causes the air to discharge through the porous section into the ambient air flow, and

wherein an under pressure in the pressure chamber causes the air of the ambient air flow to be suctioned in through the porous section, and wherein the air the air inlet/outlet device is configured to selectively let air in from the ambient air flow or discharge air into the ambient air flow,

wherein the air inlet/outlet device comprise an opening that is flush with the outer skin, and

wherein the inlet/outlet device is arranged further to a root of the airfoil than the porous section.

10. The airfoil according to claim 1 , wherein the air inlet/outlet device is connected to the pressure chamber via a duct.

11. The airfoil according to claim 9 , wherein the air inlet/outlet device is connected to the pressure chamber via a duct.

12. The airfoil according to claim 11 , wherein at least parts of the inlet duct and the outlet duct are formed integrally.

13. An aircraft comprising an airfoil according to claim 1 .