VERTICAL TAIL UNIT FOR FLOW CONTROL

Abstract

A vertical tail unit (7) including an outer skin (13) in contact with an ambient air flow (21), wherein the outer skin (13) extends between a leading edge (23) and a trailing edge (25) with opposite lateral sides (27a, 27b), and surrounds an interior space (29), and wherein the outer skin (13) has a porous section at the leading edge (23), a pressure chamber (15) arranged in the interior space (29), wherein the pressure chamber (15) is fluidly connected to the porous section (31), an air inlet (17) provided in the outer skin (13) and fluidly connected to the pressure chamber (15), and an air outlet (19) provided in the outer skin (13) and fluidly connected to the pressure chamber (15).

Claims

1. A vertical tail unit comprising an outer skin configured to be in contact with an ambient air flow, wherein the outer skin extends between a leading edge and a trailing edge with opposite lateral sides, and surrounds an interior space, and wherein the outer skin comprises a porous section in an 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 provided in the outer skin, wherein the air inlet is fluidly connected to the pressure chamber and configured to cause an overpressure in the pressure chamber such that air discharges through the porous section into the ambient air flow, and an air outlet provided in the outer skin, wherein the air outlet is fluidly connected to the pressure chamber and configured to cause an underpressure in the pressure chamber such that air of the ambient air flow is sucked in through the porous section, wherein the air inlet is formed as an opening that is arranged in one lateral side of the outer skin and is flush with the outer skin.

2. The vertical tail unit according to claim 1, wherein the air inlet comprises an inward-pivoting door, wherein the inward pivoting door is pivotable between a closed position where the ambient air flow is inhibited from passing through the outer skin and entering the vertical tail unit, and an opened position where the ambient air flow passes through the outer skin into the vertical tail unit, and wherein in the closed position the door is flush with the outer skin, and in the opened 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 vertical tail unit.

3. The vertical tail unit according to claim 2, wherein the door is mounted to the vertical tail unit by a hinge, wherein the hinge is arranged at that side of the door facing the leading edge.

4. The vertical tail unit according to claim 2, wherein the hinge has a vertical hinge axis.

5. The vertical tail unit according to claim 1, wherein the opposite side walls diverge from the leading edge towards the trailing edge.

6. The vertical tail unit according to claim 5, wherein the side 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 side walls first increases with an increasing slope and subsequently increases with a decreasing slope.

7. The vertical tail unit according to claim 1, wherein the air inlet is arranged further to a root of the vertical tail unit than the porous section.

8. The vertical tail unit according to claim 1, wherein the air inlet is connected to the pressure chamber via an inlet duct.

9. The vertical tail unit according to claim 8, wherein the air outlet is connected to the pressure chamber via an outlet duct.

10. The vertical tail unit according to claim 9, wherein at least parts of the inlet duct and the outlet duct are formed integrally.

11. An aircraft comprising a vertical tail unit according to claim 1.

12. A vertical tail unit for an aircraft comprising an outer skin configured to be in contact with ambient air flowing over the aircraft during flight, wherein the outer skin forms a leading edge and includes opposite lateral sides extending from the leading edge towards a trailing edge of the vertical tail unit, wherein the outer skin comprises a porous section in an area of the leading edge; an interior volume within the outer skin; a pressure chamber in the interior space fluidly connected to the porous section, an air inlet scoop in the outer skin, wherein the air inlet scoop is recessed in the outer skin and has an opening facing a flow direction of ambient air flowing over the outer skin at the air inlet scoop and the air inlet scoop is fluidly connected to the pressure chamber and configured to cause an overpressure in the pressure chamber such that air discharges from the pressure chamber, through the porous section and into ambient air flowing over the porous section, and an air outlet duct including a discharge opening facing away from a flow direction of ambient air flowing over the outlet duct, wherein the air outlet duct is fluidly connected to the pressure chamber and configured to cause an under pressure in the pressure chamber such that ambient air flowing over the porous section is sucked in through the porous section and into the pressure chamber, wherein the air inlet scoop is arranged one of the opposite lateral sides and of the outer skin and that is flush with the outer skin.

Description

SUMMARY OF THE DRAWINGS

[0018] Hereinafter, an embodiment(s) of the present invention is described in more detail by means of a drawing. The drawing shows in

[0019] FIG. 1 a side view of the tail section of an aircraft according to the invention,

[0020] FIG. 2 a detailed cross sectional view of an air inlet of the aircraft from FIG. 1 with a door in an opened position, and

[0021] FIG. 3 the air inlet from FIG. 2 with the door in a closed position, and

[0022] FIG. 4 a detailed perspective view of the air inlet shown in FIG. 2 with the door in the opened position.

DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTION

[0023] In FIG. 1 an embodiment of an aircraft 1 according to the invention is illustrated. The aircraft 1 comprises a fuselage 3, a horizontal tail unit 5, and a vertical tail unit 7 according to an embodiment of the invention. The vertical tail unit 7 comprises a vertical stabilizer 9 and a rudder 11 pivotally mounted to the vertical stabilizer 9. The vertical tail unit 7 is configured for hybrid laminar flow control and comprises an outer skin 13, a pressure chamber 15, an air inlet 17, and an air outlet 19.

[0024] The outer skin 13 is in contact with an ambient air flow 21 and extends between a leading edge 23 and a trailing edge 25. Further, the outer skin 13 has two opposite lateral sides 27a, 27b and surrounds an interior space 29. The outer skin 13 further comprises a porous section 31 in the area of the leading edge 23 for letting air through the outer skin 13.

[0025] The pressure chamber 15 is arranged in the interior space 29 for holding an overpressure or an underpressure with respect to the pressure of the ambient air flow 21 in front of the porous section 31. The pressure chamber 15 is fluidly connected to the porous section 31.

[0026] The air outlet 19 is arranged in the outer skin 13 for letting out air into the ambient air flow 21. The air outlet 19 is fluidly connected to the pressure chamber 15 and configured to cause, in flight of the associated aircraft 1, an underpressure in the pressure chamber 15 such that air from the ambient air flow 21 is sucked in through the porous section 31 into the pressure chamber 15. The air outlet 19 includes a pivotable flap 33 that can be opened in the direction of the trailing edge 25.

[0027] The air inlet 17 is arranged in the outer skin 13 for letting air from the ambient air flow 21 into the vertical tail unit 7. The air inlet 17 is fluidly connected to the pressure chamber 15 and configured to cause, in flight of the associated aircraft 1, an overpressure in the pressure chamber 15, such that air from the pressure chamber 15 discharges through the porous section 31 to the ambient air flow 21. The air inlet 17 is formed as an opening 35 that is arranged in one lateral side 27a of the outer skin 13 and that is flush with the outer skin 13.

[0028] As shown in FIGS. 2 and 3, the air inlet 17 comprises an inward-pivoting door 37 that can be pivoted between a closed position 39 (FIG. 3) where an ambient air flow 21 is inhibited from passing through the outer skin 13 and entering the vertical tail unit 7, and an opened position 41 (FIG. 2) where the ambient air flow 21 may pass through the outer skin 13 into the vertical tail unit 7. In the closed position 39 the door 37 is flush with the outer skin 13, and in the opened position 41 a channel 43 is formed between the door 37 and an edge 45 of the opening 35, for ambient air flow 21 to pass through the outer skin 13 into the vertical tail unit 7. The door 37 is mounted to the vertical tail unit 7 by a hinge 47. The hinge 47 is arranged at that side of the door 37 facing the leading edge 23, so that the channel 43 opens in the direction of the leading edge 23. The hinge 47 has a vertical hinge axis 49.

[0029] As shown in FIG. 1, the air inlet 17 is arranged further to a root 51 of the vertical tail unit 7 than the porous section 31. The air inlet 17 is connected to the pressure chamber 15 via an inlet duct 53 that proceeds from the air inlet 17 upwards to the pressure chamber 15. The air outlet 19 is connected to the pressure chamber 15 via an outlet duct 55. Wide parts of the inlet duct 53 and the outlet duct 55 are formed integrally. The air inlet 17 and the air outlet 19 are arranged at the same lateral side 27a in FIG. 1, however, they might also be arranged at opposite lateral sides 27a, 27b.

[0030] As shown in FIG. 4, the air inlet 17 has two opposite side walls 57a, 57b that proceed in a diverging manner in a direction from the leading edge 23 to the trailing edge 25. The side walls 57a, 57b proceed in the form of a wave in the direction from the leading edge 23 to the trailing edge 25 such that the distance between the side walls 57a, 57b first increases with an increasing slope and subsequently increases with a decreasing slope.

[0031] While at least one exemplary embodiment of the present invention(s) is disclosed herein, it should be understood that modifications, substitutions and alternatives may be apparent to one of ordinary skill in the art and can be made without departing from the scope of this disclosure. This disclosure is intended to cover any adaptations or variations of the exemplary embodiment(s). In addition, in this disclosure, the terms comprise or comprising do not exclude other elements or steps, the terms a or one do not exclude a plural number, and the term or means either or both. Furthermore, characteristics or steps which have been described may also be used in combination with other characteristics or steps and in any order unless the disclosure or context suggests otherwise. This disclosure hereby incorporates by reference the complete disclosure of any patent or application from which it claims benefit or priority.