Seal assembly

Patent metadata

Field	Value
Publication number	US-9745049-B2
Application number	US-201514969422-A
Country	US
Kind code	B2
Filing date	Dec 15, 2015
Priority date	Nov 9, 2010
Publication date	Aug 29, 2017
Grant date	Aug 29, 2017

Abstract

A seal assembly for closing an aperture in an aerodynamic surface of a structure, the seal assembly comprising: a track for attachment to the structure; and a retractable seal including a flexible substrate and a plurality of rods connected to the substrate, wherein at least one of the rods is mounted for running movement along the track, and the seal is moveable between an extended position and a retracted position by moving the at least one rod along the track accompanied by folding/unfolding of the seal substrate, and wherein the seal is biased to its extended position.

First claim

The invention claimed is:

1. A seal assembly for closing an aperture in an aerodynamic surface of a structure, the seal assembly comprising: a track for attachment to the structure; and a retractable seal including a flexible substrate and a plurality of rods connected to the flexible substrate, wherein at least one of the rods is mounted for running movement along the track, the seal is moveable between an extended position and a retracted position by moving the at least one rod along the track accompanied by folding/unfolding of the flexible substrate, and wherein the seal is biased to its extended position, and wherein the seal is self-biasing to the extended position.

2. A seal assembly according to claim 1 , wherein the seal substrate is an elastomer that stores potential energy when the seal is folded and releases that potential energy by unfolding the seal to its extended position.

3. A seal assembly according to claim 1 , wherein the seal further includes a mechanical spring for biasing the seal to the extended position.

4. A seal assembly according to claim 1 , wherein the seal substrate includes one or more integral tensioning webs for biasing the seal to its extended position.

5. A seal assembly according to claim 1 , further comprising a spring mechanism for coupling between the seal and the structure for biasing the seal to its extended position.

6. A seal assembly according to claim 5 , wherein the spring mechanism includes one or more tension springs, or one or more constant force springs.

7. A seal assembly according to claim 1 , wherein the seal has a proximal end and a distal end, the distal end being moveable with respect to the track and with respect to the proximal end.

8. A seal assembly according to claim 7 , wherein the distal end of the seal includes a contact surface for engaging a drive member for retracting the seal.

9. A seal assembly according to claim 8 , wherein the distal end of the seal includes a magnet for co-operating with a ferromagnetic material in the drive member for extending the seal.

10. A seal assembly according to claim 7 , wherein the track includes an end stop, which limits the travel of the distal end of the seal along the track.

11. A seal assembly according to claim 1 , wherein the rods include one or more first rods which extend from the substrate into engagement with the track, and one or more second rods which are arranged to move away from the track as the seal is retracted.

12. A seal assembly according to claim 11 , wherein each second rod does not extend from either side of the substrate.

13. A seal assembly according to claim 11 , wherein each second rod extends from either side of the substrate and is arranged to contact an outside of the track when the seal is in its extended position.

14. A seal assembly according to claim 11 , wherein a first rod is disposed at either end of the seal.

15. A seal assembly according to claim 11 , wherein the first rods and the second rods are arranged alternately along the length of the seal.

16. A seal assembly according to claim 11 , wherein the first rods are arranged to freely rotate relative to the substrate.

17. A seal assembly according to claim 11 , wherein the second rods are fixed relative to the substrate.

18. A seal assembly according to claim 1 , wherein the seal further comprises a stiffener member between adjacent rods.

19. A seal assembly according to claim 1 , wherein the seal further includes a relief in a surface of the substrate adjacent at least one of the rods to aid in folding the substrate.

20. An aerofoil having a device moveable between a retracted position and an extended position with respect to a leading edge of the aerofoil, the aerofoil leading edge having an aperture for accommodating a portion of the device when the device is in its retracted position, and a seal assembly in accordance with any preceding claim for closing at least a portion of the aperture when the device is in its extended position.

21. An aerofoil according to claim 20 , wherein the seal substrate does not extend beyond a profile of the aerofoil leading edge as the seal moves between its extended and retracted positions.

22. An aerofoil according to claim 21 , wherein the seal substrate substantially conforms to the leading edge profile when the seal is in its extended position.

23. An aerofoil according to claim 20 , wherein the device includes a drive surface for contacting the seal so as to cause the seal to retract upon retraction of the device.

24. An aerofoil according to claim 20 , wherein the seal is adapted to completely seal the aperture when the device is partially extended and sealed against the aerofoil leading edge.

25. An aerofoil according to claim 20 , wherein the seal extends around the aerofoil leading edge to a position adjacent the device trailing edge when the device is fully extended and forms a slot with the aerofoil leading edge.

26. An aerofoil according to claim 20 , wherein the aerofoil is an aircraft wing, and the device is a leading edge slat.

Assignees

• Airbus Operations Ltd

Inventors

• Wilson James
• Quayle Alan
• Hadley Paul

Classifications

• B29C70/26

  Non-fibrous reinforcements only {(B29C35/0272, B29C61/0625, B29C70/887 take precedence; combined with fibres B29C70/023)} · CPC title

• B64C7/00 Primary

  Structures or fairings not otherwise provided for · CPC title

• B64C9/22

  at the front of the wing · CPC title

• B64C9/02

  Mounting or supporting thereof · CPC title

• B64C3/50

  by leading or trailing edge flaps · CPC title