Lift flap bearing apparatus, lift flap assembly, airfoil and aircraft

Patent metadata

Field	Value
Publication number	US-9452823-B2
Application number	US-201214345054-A
Country	US
Kind code	B2
Filing date	Aug 21, 2012
Priority date	Sep 16, 2011
Publication date	Sep 27, 2016
Grant date	Sep 27, 2016

Abstract

A lift flap bearing apparatus is improved with respect to aerodynamics, construction space and assembly, for guiding and adjusting a first lift flap and a second lift flap. The lift flap bearing apparatus comprises a first guiding device for guiding the first lift flap and a second guiding device for guiding the second lift flap. The first and the second guiding devices each have a first curved guide rail and a second curved guide rail.

First claim

The invention claimed is:

1. A lift flap bearing apparatus for guiding and adjusting a first lift flap and a second lift flap, the lift flap bearing apparatus comprising
a first guiding device configured to guide the first lift flap and a second guiding device configured to guide the second lift flap, the first and the second guiding devices each having a first curved guide rail and a second curved guide rail.

2. The lift flap bearing apparatus according to claim 1 , wherein
the first guiding device is disposed on a first side of the lift flap bearing apparatus and the second guiding device is disposed on a second side that is orientated opposite to the first side.

3. The lift flap bearing apparatus according to claim 1 , further comprising
a driving device configured to simultaneously adjust the first and second guiding devices.

4. The lift flap bearing apparatus according to claim 1 , wherein
at least one of the guiding devices comprises a guiding carriage which is displaceably guided by a first rail hinge mounting on a first curved guide rail of the guiding device, and is displaceably guided by a second rail hinge mounting on a second curved guide rail.

5. The lift flap bearing apparatus according to claim 4 , wherein
the at least one guiding carriage comprises a first flap attachment region with at least one first flap attachment device and a second flap attachment region with at least one second flap attachment device, the first and second flap attachment devices being spaced apart, and the first and second flap attachment regions of the guiding carriage being attached to one another so as to be moveable relative to one another in a direction extending transverse to an adjusting direction guided by the guiding device.

6. The lift flap bearing apparatus according to claim 4 , wherein
the first and the second guiding devices are each provided with the guiding carriage, the first guiding carriage of the first guiding device and the second guiding carriage of the second guiding device being rigidly interconnected by a cross-connection.

7. The lift flap bearing apparatus according to claim 1 , further comprising
a basic body that is configured to attach to an airfoil and comprises on a first side the first and the second guide rails of the first guiding device and on a second side, which is orientated opposite to the first side, the first and the second guide rails of the second guiding device.

8. The lift flap bearing apparatus according to claim 7 , further comprising
a carriage assembly comprising the first guiding carriage, the second guiding carriage and the cross-connection that surround the basic body.

9. The lift flap bearing apparatus according to claim 8 , wherein
the driving device is disposed in the basic body and acts on the cross-connection.

10. The lift flap bearing apparatus according to claim 4 , wherein at least one of the following
at least one of the rail hinge mountings comprises at least one roller that acts on at least one roller track of the guide rail associated with the at least one of the rail hinge mountings; and
that at least one of the rail hinge mountings comprises at least one sliding member that acts on a sliding track of the guide rail associated with the at least one of the rail hinge mountings.

11. The lift flap bearing apparatus according to claim 4 , wherein
at least one of the rail hinge mountings is in positive engagement with one of the guide rails in order to absorb lateral transverse forces.

12. The lift flap bearing apparatus according to claim 4 , wherein
the first rail hinge mounting is displaceably supported on a first supporting surface on the first guide rail, while the second rail hinge mounting is displaceably supported on a second supporting surface on the second guide rail, at least one of the first supporting surface being larger than the second supporting surface and the first supporting surface extending over a greater distance in a displacement direction than the second supporting surface.

13. A lift flap assembly comprising:
a first lift flap;
a second lift flap; and
the lift flap bearing apparatus according to claim 1 which is disposed between the first and the second lift flaps.

14. An airfoil for an aircraft, comprising a lift flap assembly according to claim 13 .

15. An aircraft comprising at least one airfoil according to claim 14 .

16. An airfoil for an aircraft, comprising a lift flap bearing apparatus according to claim 1 .

17. An aircraft comprising a lift flap bearing apparatus according to claim 1 .

18. An aircraft comprising a lift flap assembly according to claim 13 .

19. The lift flap bearing apparatus according to claim 2 , further comprising
a driving device configured to simultaneously adjust the first and second guiding devices.

20. The lift flap bearing apparatus according to claim 1 , wherein
at least one of the guiding devices comprises a guiding carriage which is displaceably guided by a first rail hinge mounting on a first curved guide rail of the guiding device, and is displaceably guided by a second rail hinge mounting on a second curved guide rail.

Assignees

• Havar Tamas
• Perez-Sanchez Juan
• Ender Tobias
• Seack Oliver
• Eads Deutschland Gmbh
• Airbus Operations Gmbh

Inventors

• Havar Tamas
• Perez-Sanchez Juan
• Ender Tobias
• Seack Oliver

Classifications

• B64C9/02 Primary

  Mounting or supporting thereof · CPC title

• B64C13/28 Primary

  mechanical · CPC title

• B64C9/16 Primary

  at the rear of the wing · CPC title

• B64C3/54

  Varying in area · CPC title