Vertical tail unit for flow control

Patent metadata

Field	Value
Publication number	US-11565795-B2
Application number	US-202117213027-A
Country	US
Kind code	B2
Filing date	Mar 25, 2021
Priority date	Oct 9, 2017
Publication date	Jan 31, 2023
Grant date	Jan 31, 2023

Abstract

A vertical tail unit ( 7 ) for flow control 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 ), and surrounds an interior space ( 29 ), and wherein the outer skin ( 13 ) includes a porous section ( 31 ) in the area of 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 ), wherein the air inlet ( 17 ) is fluidly connected to the pressure chamber ( 15 ), wherein the air outlet ( 19 ) is fluidly connected to the pressure chamber ( 15 ). The vertical tail unit ( 7 ) has reduced drag and an increased efficiency because the air inlet ( 17 ) is formed as an opening ( 35 ) in the outer skin ( 13 ) at the leading edge ( 23 ).

First claim

The invention is:

1. A vertical tail unit for flow control, comprising
an outer skin configured to contact an ambient air flow, wherein the outer skin extends between a leading edge and a trailing edge, and the outer skin 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, wherein the air inlet is formed as an opening in the outer skin at the leading edge,
an air outlet duct including an air outlet provided in the outer skin, wherein the air outlet is fluidly connected via the air outlet duct to the pressure chamber and configured to cause an under-pressure in the pressure chamber such that air of the ambient air flow is sucked in through the porous section, and
an inlet door configured to close the air inlet, wherein the inlet door is mounted to a hinge within the leading edge so that the door opens by pivoting inward relative to the leading edge to create the overpressure in the pressure chamber, wherein the air inlet is aligned with a stagnation point on a leading edge of the vertical tail unit, and
an outlet door configured to close the air outlet duct, wherein the outlet door opens to create the under-pressure in the pressure chamber which causes the ambient air to flow through the porous section and into the pressure chamber.

2. The vertical tail unit according to claim 1 , wherein the air inlet is on the leading edge at a location separate from the porous section.

3. The vertical tail unit according to claim 1 , wherein the air inlet has a circular shape or an oval shape.

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

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

6. The vertical tail unit according to claim 5 , wherein the air outlet duct extends from the air outlet to the pressure chamber.

7. The vertical tail unit according to claim 6 , wherein parts of both the inlet duct and the outlet duct are a single piece component.

8. The vertical tail unit according to claim 1 , wherein the air inlet comprises a door for closing the air inlet.

9. The vertical tail unit according to claim 8 , wherein the door is mounted to a hinge so that the door is pivotable to the inside when the door is opened.

10. The vertical tail unit according to claim 9 , wherein the hinge is mounted to a bottom edge or to a top edge of the air inlet and the hinge has a horizontal hinge axis.

11. The vertical tail unit according to claim 9 , wherein the hinge extends across the air inlet, and the door includes two door wings each mounted to the hinge such that each of the two door wings pivots about the hinge and the two door wings cover the inlet opening while the door is closed.

12. The vertical tail unit according to claim 11 , wherein the hinge has a vertical hinge axis.

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

14. A vertical tail unit for an aircraft comprising
an outer skin configured to contact 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 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 in the outer skin at the leading edge, 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 from the pressure chamber, through the porous section and into ambient air flowing over the porous section, wherein the air inlet is at the leading edge of the vertical tail unit and aligned with a stagnation point on the leading edge;
an inlet door configured to close the air inlet, wherein the inlet door is mounted to a hinge proximate the leading edge and the inlet door is pivotable about the hinge to cause a trailing edge of the inlet door to move inside the leading edge to create the overpressure in the pressure chamber;
an air outlet duct 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, and
an outlet door configured to close the air outlet duct, wherein the outlet door opens to create the under-pressure in the pressure chamber which causes the ambient air to flow through the porous section and into the pressure chamber.

15. The vertical tail unit according to claim 14 , wherein the air inlet is on the leading edge at a location separate from the porous section.

16. The vertical tail unit according to claim 14 , wherein the air inlet is closer to a root of the vertical tail unit than the porous section.

17. The vertical tail unit according to claim 14 , wherein the air inlet is on a portion of the leading edge oriented at an angle from vertical which is greater than an angle from vertical of the porous section.

18. The vertical tail unit according to claim 14 , wherein the inlet door is mounted to the vertical tail along a horizontal hinge axis.

19. The vertical tail unit according to claim 14 , wherein the hinge extends across the air inlet, and the inlet door includes two door wings each mounted to the hinge, wherein the two door wings pivot about the hinge to close and open the inlet opening.

20. The vertical tail unit according to claim 17 , wherein the inlet door is attached to the vertical tail unit by a hinge having a vertical hinge axis.

Assignees

• Airbus Operations Gmbh

Inventors

• Heuer Thomas

Classifications

• B64C21/08 Primary

  adjustable · CPC title

• B64C3/26

  Construction, shape, or attachment of separate skins, e.g. panels · CPC title

• B64C2230/22

  by using a surface having multiple apertures of relatively small openings other than slots · CPC title

• B64C2230/20

  by passively inducing fluid flow, e.g. by means of a pressure difference between both ends of a slot or duct · CPC title

• B64C21/025

  for simultaneous blowing and sucking · CPC title