Joint

Patent metadata

Field	Value
Publication number	US-9701392-B2
Application number	US-201615217823-A
Country	US
Kind code	B2
Filing date	Jul 22, 2016
Priority date	Mar 28, 2011
Publication date	Jul 11, 2017
Grant date	Jul 11, 2017

Abstract

A joint including first and second rib components, the first rib having an abutment surface and a plurality of lugs disposed adjacent to the abutment surface; and the second rib having an abutment surface and a plurality of lugs disposed adjacent to the abutment surface, wherein the abutment surfaces of the respective ribs are abutting and joined with a tension joint, and wherein the lugs are pinned to form a pinned lug joint by aligning respective holes in the plurality of lugs such that the lugs of the first and second ribs are interleaved and have one or more pins passing through the aligned lug holes. The joint may be used for attaching a wing tip device to the outboard end of an aircraft wing.

First claim

The invention is:

1. A joint comprising:
first and second rib components,
the first rib component having an abutment surface and a plurality of lugs disposed adjacent to the abutment surface; and
the second rib component having an abutment surface and a plurality of lugs disposed adjacent to the abutment surface,
wherein the abutment surfaces of the respective first and second rib components are abutting and joined with a tension fitting wherein at least a member of the tension fitting is under tension, and
wherein the lugs are pinned to form a pinned lug joint by aligning respective holes in the plurality of lugs such that the lugs of the first and second rib components are interleaved and have one or more pins passing through the aligned lug holes.

2. The joint according to claim 1 , wherein the lugs of the respective first or second rib components project beyond the abutment surfaces of the respective first or second rib components.

3. The joint according to claim 1 , wherein the tension fitting includes a plurality of tension bolts.

4. The joint according to claim 3 , further comprising a nut associated with each tension bolt.

5. The joint according to claim 1 , wherein the pinned lug joint comprises two or more groups of lugs on each side of the joint.

6. The joint according to claim 5 , wherein the groups of lugs are spaced apart by a distance greater than a spacing between the lugs within each group.

7. The joint according to claim 5 , wherein one of the pins is associated with each of the groups of lugs.

8. The joint according to claim 1 , wherein at least one of the one or more pins includes a nut.

9. The joint according to claim 1 , wherein the pinned lug joint further comprises a pin retaining device associated with the one or more pins.

10. The joint according to claim 1 , wherein each of the first and second rib components is integrally formed.

11. The joint according to claim 1 , wherein the first and second rib components define a space between the abutment surfaces and the plurality of lugs, wherein the space is configured to receive one or more systems.

12. The joint according to claim 1 , wherein the first and second rib components are aircraft components.

13. An aircraft wing comprising:
a wing box structure, the wing box structure including front and rear spars, a plurality of ribs extending between the front and rear spars, and an upper wing cover and a lower wing cover each extending between the front and rear spars, and
a wing tip device attached to an outboard end of the wing, wherein the wing tip device is joined to the wing by a joint in accordance with claim 1 in which the first rib component is an outboard rib component of the wing and the second rib component is an inboard rib component of the wing tip device.

14. The aircraft wing according to claim 13 , wherein the wing tip device includes an upper cover and a lower cover, and outer surfaces of the upper and lower covers of the wing and wing tip device are substantially flush across the joint.

15. The aircraft wing according to claim 13 , wherein the wing tip device includes an essentially planar winglet and a curved transition region arranged between the wing and the winglet.

16. The aircraft wing according to claim 15 , wherein the transition region has a curvature of increasing local dihedral in an outboard direction.

17. The aircraft wing according to claim 13 , wherein within the joint, the tension joint is disposed nearest the upper wing cover and the pinned lug joint is disposed nearest the lower wing cover.

18. The aircraft wing according to claim 17 , wherein the tension fitting includes a plurality of tension joint fitting bolts spaced in a chord-wise direction, and wherein one of the tension fitting bolts is located in a bolt hole with a tighter tolerance than the other tension fitting bolts.

19. The aircraft wing according to claim 18 , wherein the tighter tolerance tension fitting bolt is disposed in a central part of the tension fitting in the chord-wise direction.

20. The joint according to claim 1 wherein the tension fitting includes a tension bolt.

21. The joint according to claim 20 wherein a nut is arranged with the bolt such that the bolt is under tension.

22. The joint according to claim 1 wherein the tension fitting forces the abutment surfaces into abutment.

23. The joint according to claim 1 wherein the tension fitting is one of a plurality of the tension fittings.

24. A joint comprising:
first and second rib components,
the first rib component includes a first abutment surface and a first row of lugs adjacent the first abutment surface, wherein the lugs in the first row each have a hole and the holes are aligned along a centerline; and
the second rib component includes a second abutment surface and a second row of lugs adjacent the second abutment surface, wherein the lugs of the second row each have a hole and the holes are aligned along the centerline;
a pin aligned with the centerline and extending through at least one of the holes in the first row of lugs and at least one of the holes in the second row of lugs;
a tension fitting aligned with the first and second abutment surfaces, wherein the tension fitting includes a member under tension and the tension fitting applies a force biasing together the first and second abutment surfaces such that the first and second abutment surfaces are in contact with each other.

Assignees

• Airbus Operations Ltd
• Airbus Operations Sas

Inventors

• Whitlock Rhona
• Del Tin Massimo
• Dalton Peter
• Ford George
• Hill Michael John
• Huntbatch Adrian
• Breeze Laurence
• Depeige Alain

Classifications

• B64C23/069

  using one or more wing tip airfoil devices, e.g. winglets, splines, wing tip fences or raked wingtips · CPC title

• B64C3/187 Primary

  Ribs · CPC title

• B64C3/26 Primary

  Construction, shape, or attachment of separate skins, e.g. panels · CPC title

• B64C23/065

  at the wing tips · CPC title

• Y02T50/164

  Cross-Sectional Technologies · mapped topic