Aircraft hinge assembly

Patent metadata

Field	Value
Publication number	US-11708145-B2
Application number	US-202117495449-A
Country	US
Kind code	B2
Filing date	Oct 6, 2021
Priority date	Dec 9, 2020
Publication date	Jul 25, 2023
Grant date	Jul 25, 2023

Abstract

A hinge assembly 8 a for an aircraft component including first and second hinge plates 9, 10 , having an aerodynamic surface. A first seal assembly 28 to 32 is provided and arranged to seal between the aerodynamic surfaces of the hinge plates. A second seal assembly 38 to 42 is arranged to seal between the undersides of the hinge plates in order to reduce pressure leakage between voids under the hinge. The provision of two seal assemblies, each having a dedicated function, addresses the competing demands made on the sealing arrangement of an aircraft hinge assembly in use.

First claim

The invention is:

1. A hinge assembly for an aircraft component, the hinge assembly comprising:
first and second hinge plates each having an aerodynamic surface; and
a seal assembly including:
a first seal between the aerodynamic surface of the first hinge plate and the aerodynamic surface of the second hinge plate, and
a second seal between an underside of the first hinge plate and an underside of the second hinge plate.

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

3. The hinge assembly as claimed in claim 1 , further comprising:
a first extended part of the first hinge plate extending under the second hinge plate; and
a second extended part of the second hinge plates extending under the first hinge plate,
wherein the second seal includes a first seal element between the first extended part of first hinge plate and the underside of the second hinge plate.

4. The hinge assembly as claimed in claim 1 , in which each of the first and second hinge plates comprises a plurality of fingers, the fingers of the first hinge plate interleave with the fingers of the second hinge plate,
wherein the first seal is between a finger of the first hinge plate and a finger of the second hinge plate.

5. The hinge assembly as claimed in claim 4 , in which the first seal comprises:
a finger seal attached to a respective one of the fingers of the first hinge plate, wherein the finger seal is sandwiched between the respective one of the fingers and one of the fingers on the second hinge plate.

6. The hinge assembly as claimed in claim 5 , in which the finger seals each have a triangular cross section, and is arranged to make sealing contact with a chamfered surface along an edge of one of the fingers adjacent the respective one of the fingers having the finger seal.

7. The hinge assembly as claimed in claim 5 , in which the finger seal comprises a resiliently flexible strip.

8. The hinge assembly as claimed in claim 5 , in which the finger seal is over-moulded onto one of the fingers.

9. The hinge assembly as claimed in claim 4 , further comprising:
at least one recess between the fingers on each of the first or second hinge plate, and
the first seal includes a fingertip seal attached to a tip region of one of the fingers in the first hinge plate, and the fingertip seal is sandwiched between the finger to which the finger seal is attached and an apex of one of the recesses in the second hinge plate.

10. The hinge assembly as claimed in claim 9 , in which a plurality of the fingers each includes the first seal, and the first seal on each of the plurality of the fingers is a unitary, single piece seal including the fingertip seal and the finger seal.

11. The hinge assembly as claimed in claim 4 , further comprising:
a finger extension on at least one of the fingers of the first hinge plate, wherein the extension extends beneath the second hinge plate, and
the second seal includes an extension seal on the finger extension, wherein the extension seal is sandwiched between the finger extension and the underside of the second hinge plate.

12. The hinge assembly as claimed in claim 11 , in which the extension seal includes a resiliently flexible lip.

13. The hinge assembly as claimed in claim 11 , in which the extension seal is over-moulded onto the finger extension.

14. The hinge assembly as claimed in claim 11 , in which the extension seal is aligned with a tip of the finger having the extension and the finger extension.

15. The hinge assembly as claimed in claim 4 , further comprising a lug attached to at least some of the fingers, wherein each the lugs is configured to accommodate a hinge pin.

16. The hinge assembly as claimed in claim 15 , in which a rotational axis about which one of the first and second hinge plate rotates is underneath the first and second hinge plates.

17. A moveable aircraft component including the hinge assembly of claim 1 .

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

19. An aircraft including the aircraft wing as claimed in claim 18 .

20. The aircraft as claimed in claim 19 , in which the hinge plates are arranged to form sealing connections tilted away from a direction of incoming air when the aircraft is in flight.

21. An aircraft including a moveable component having the hinge assembly in claim 1 .

22. An aircraft wing comprising:
a fixed wing including a tip;
a wing tip device including and end;
a first hinge assembly configured to attached the wing tip device to the fixed wing to allow the wing tip device to pivot with respect to the fixed wing, wherein the first hinge assembly includes:
the first hinge assembly attached to the tip of the fixed wing, wherein the first hinge assembly includes:
a first hinge plate with fingers each having an outer aerodynamic surface;
first seals each mounted to a side edge of each of a respective one of the fingers of the first hinge plate, wherein each of the first seals extends a length of the respective finger and is flush with the aerodynamic surface of the respective finger;
finger extensions each extending outward from a respective one of the fingers, wherein the finger extension is offset inward of the fixed wing from the aerodynamic surface of the respective finger,
second seals each mounted to a respective one of the finger extensions;
recesses between the fingers, and
lugs wherein each of the fingers is mounted onto a respective one of the lugs; and

a second hinge assembly attached to the end of the wing tip device,
wherein the second hinge assembly includes:
a second hinge plate with fingers each having an outer aerodynamic surface, wherein at the fingers of the second hinge plate interleave with the fingers of the first hinge plate such that at least one of the fingers of the second hinge plate is positioned in a recess of the first hinge plate,
first seals each mounted to a side edge a respective one of the fingers of the second hinge plate, wherein each of the first seals extends a length of the respective finger, is flush with the aerodynamic surface of the respective finger, and is configured to be sandwiched between the respective finger of the second hinge plate and one of the fingers of the first hinge plate;
finger extensions each extending from an end of a respective finger of the second hinge plate, wherein the finger extension of the second hinge plate are each offset inward of the wing tip device from the aerodynamic surface of the respective finger of the second hinge plate, and
second seals each mounted to a respective one of the finger extensions of the second hinge plate, wherein the second seal is configured to be sandwiched between the finger extension of the second hinge plate to which the second seal is mounted and an underside of the first hinge plate; and
lugs wherein each of the fingers of the second hinge plate is mounted onto a respective one of the lugs.

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

• B64C9/02

  Mounting or supporting thereof · CPC title

• F16C11/04 Primary

  Pivotal connections (hinges for doors, windows or wings E05D) · CPC title

• B64C23/072 Primary

  the wing tip airfoil devices being moveable in their entirety · CPC title

• B64C3/546

  by foldable elements · CPC title