Vertical tail unit for flow control

Patent metadata

Field	Value
Publication number	US-10967955-B2
Application number	US-201816153988-A
Country	US
Kind code	B2
Filing date	Oct 8, 2018
Priority date	Oct 9, 2017
Publication date	Apr 6, 2021
Grant date	Apr 6, 2021

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).

First claim

The invention claimed is:

1. A vertical tail unit comprising:
an outer skin configured to contact an ambient air flow, wherein the outer skin forms a leading edge and opposite lateral sides each extending from the leading edge to a trailing edge, wherein 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 in and flush with one of the lateral sides, 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;
an air outlet in the outer skin fluidly connected to the pressure chamber, having a closed mode during the overpressure in the pressure chamber and an open mode which creates an under pressure in the pressure chamber causing air of the ambient air flow is sucked in through the porous section, and
an inward-pivoting door including a leading end and a trailing edge, wherein the door is pivotable about the leading end between a closed position where the ambient air flow is inhibited from passing through the air inlet and entering the vertical tail unit, and an opened position where the ambient air flow passes through the air inlet and into the vertical tail unit,
wherein, in the closed position, the door is flush with the outer skin and closes the air inlet, and
wherein, in the opened position, the inward-pivoting door is pivoted about the leading end and the trailing edge is inward of the air inlet to form a channel between the door and the air inlet for ambient air to pass through the air inlet, into the channel and into the vertical tail unit.

2. The vertical tail unit according to claim 1 , wherein the door is mounted to the vertical tail unit by a hinge, wherein the hinge is arranged at a side of the door facing the leading edge.

3. The vertical tail unit according to claim 1 , wherein the hinge has a vertical hinge axis.

4. The vertical tail unit according to claim 1 , wherein the air inlet includes opposite side walls that diverge from each other in a direction extending from the leading edge towards the trailing edge.

5. The vertical tail unit according to claim 4 , wherein the side walls of the air inlet each have a curvature in the direction from the leading edge to the trailing edge.

6. 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.

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

8. The vertical tail unit according to claim 7 , wherein the air outlet is connected to the pressure chamber via an outlet duct.

9. The vertical tail unit according to claim 8 , wherein at least parts of the inlet duct and the outlet duct are formed integrally.

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

11. 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 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 opening in one of the lateral sides of the outer skin and the air inlet opening is flush with the outer skin of the one of the lateral sides, wherein the air inlet opening has a forward end facing the leading edge and a trailing edge facing the trailing edge;
an air inlet door, which when closed, closes the air inlet opening and is flush with the outer skin and the air inlet door, when open, is recessed into the outer skin to open the air inlet, the air inlet door has a forward end proximate to the forward end of the air inlet opening and a trailing edge adjacent the trailing edge of the air inlet opening when the air inlet door is closed, wherein a channel is formed between the air inlet opening and the air inlet door when the air inlet door is opened by pivoting the air inlet door proximate the forward edge and moving the trailing edge inward of the air inlet opening and the outer skin, and, while the air inlet door is opened, ambient air flowing over the outer skin passes through the air inlet, through the channel and into the pressure chamber 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, while the air outlet duct is open, ambient air flowing over the porous section is sucked in through the porous section and into the pressure chamber.

Assignees

• Airbus Operations Gmbh

Inventors

• Heuer Thomas

Classifications

• B64C21/00 Primary

  Influencing air flow over aircraft surfaces by affecting boundary layer flow · 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

• B64C2230/22

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

• B64C21/08 Primary

  adjustable · CPC title

• B64C2230/06

  by explicitly adjusting fluid flow, e.g. by using valves, variable aperture or slot areas, variable pump action or variable fluid pressure · CPC title