Aircraft hinge assembly

Patent metadata

Field	Value
Publication number	US-12030618-B2
Application number	US-202117493368-A
Country	US
Kind code	B2
Filing date	Oct 4, 2021
Priority date	Dec 9, 2020
Publication date	Jul 9, 2024
Grant date	Jul 9, 2024

Abstract

A hinge assembly 8a for an aircraft component comprises first and second hinge plates 9, 10, each hinge plate including a plurality of fingers 13 to 17. The fingers of the first and second hinge plates are interleaved. A seal assembly 28 to 32 is provided between at least some of the fingers. The provision of a hinge including interposed fingers allows for a hinge assembly having a complex aerodynamic profile to be made, while the sealing function is performed by the seals filling the gaps between the fingers.

First claim

The invention claimed is:

1. A hinge assembly for an aircraft component comprising:
first and second hinge plates,
a plurality of fingers on each of the first and second hinge plates, wherein the fingers of the first hinge plate are interleaved with the fingers of the second hinge plate; and
a seal assembly between the plurality of fingers on the first hinge plate and the plurality of fingers on the second hinge plate,
wherein the seal assembly includes a plurality of finger seals attached to the plurality of fingers of the first hinge plate, and
wherein the plurality of finger seals is configured to seal against the fingers of the second hinge plate.

2. The hinge assembly as claimed in claim 1 , in which the first and second hinge plates each have an aerodynamic surface, and the seal assembly is flush with the aerodynamic surfaces of at least one of the first and second hinge plates.

3. The hinge assembly as claimed in claim 1 , in which each of the finger seals has a triangular cross section and is arranged to make sealing contact with a correspondingly chamfered surface along an edge of one of the fingers of the second hinge plate.

4. The hinge assembly as claimed in claim 1 , in which the fingers of the first and second hinge plates have intervening recesses, and the sealing arrangement further comprises respective fingertip seals attached to at least some of the tips of the fingers of the first and second hinge plate arranged to seal against the corresponding recesses of the other hinge plate.

5. The hinge assembly as claimed in claim 4 , in which at least some of the fingers have a unitary finger seal and a fingertip seal.

6. The hinge assembly as claimed in claim 1 , in which each of the finger seals comprises a resiliently flexible strip.

7. The hinge assembly as claimed in claim 1 , in which each of the finger seals is over-moulded onto a respective one of the fingers.

8. The hinge assembly as claimed in claim 1 , in which the seal assembly further comprises an under-seal assembly between undersides of the first and second hinge plates.

9. The hinge assembly as claimed in claim 8 , in which at least one of the fingers includes a finger extension to extend beneath one of the first and second hinge plates, and the under-seal assembly comprises at least one extension seal between a respective one of the finger extensions and the underside of an opposing one of the first and second hinge plates.

10. The hinge assembly as claimed in claim 9 , in which the at least one of the fingers has a unitary extension seal and fingertip seal.

11. The hinge assembly as claimed in claim 1 , further comprising reinforcing elements arranged to support the fingers.

12. The hinge assembly as claimed in claim 11 in which the reinforcing elements extend transversely from the fingers, and the finger seals extend along a portion of the reinforcing elements.

13. The hinge assembly as claimed in claim 1 , further comprising lugs attached to at least one of the fingers, the lugs configured to accommodate a hinge pin.

14. The hinge assembly as claimed in claim 13 , in which an axis of the hinge is underneath the first and second hinge plates.

15. A moveable aircraft component including the hinge assembly as claimed in claim 1 .

16. An aircraft wing comprising:
a main body, and
a wingtip device attached to the main body by the hinge assembly claimed in claim 1 .

17. The aircraft including the aircraft wing as claimed in claim 16 .

18. An aircraft including a moveable component having a hinge assembly as claimed in claim 1 .

19. The aircraft as claimed in claim 18 , in which the seal assembly and the fingers are configured to form sealing connections tilted away from a direction of incoming air when the aircraft is in flight.

20. A hinge assembly configured to connect a fixed wing to a wing tip device of an aircraft, the hinge assembly comprising:
a first hinge plate with first fingers, wherein the first hinge plate is fixed to one of the fixed wing and the wing tip device and the first fingers extend towards the other of the fixed wing and the wing tip device;
a second hinge plate with second fingers that interleave with the first fingers, wherein the second hinge plate is attached to the other of the fixed wing and the wing tip device and the second fingers extend towards the one of the fixed wing and the wing tip device, and
a seal assembly including finger seals each attached to and extending a length of a respective one of the first fingers and each of the finger seals extends towards a respective one of the second fingers to seal a gap between the respective first finger and the respective second finger.

Assignees

• Airbus Operations Ltd
• Airbus Operations Sas

Inventors

• Older Russell
• Morrell Paul
• Holland Ryan
• Marks Oliver
• Combes Pierre-Antoine
• De Almeida Guillaume

Classifications

• B64C3/56 Primary

  Folding or collapsing to reduce overall dimensions of aircraft · CPC title

• E05Y2900/502

  for aircraft or spacecraft · CPC title

• E05D11/00

  Additional features or accessories of hinges {(edge protecting devices E06B3/88)} · CPC title

• E05D7/00

  Hinges or pivots of special construction (used for special suspension arrangements E05D15/00; so as to be self-closing E05F1/06, E05F1/12; with means for raising wings before being turned E05F7/02) · CPC title

• E05D5/04

  Flat flaps · CPC title