Wing tip device

Patent metadata

Field	Value
Publication number	US-11345461-B2
Application number	US-201916561227-A
Country	US
Kind code	B2
Filing date	Sep 5, 2019
Priority date	Sep 21, 2018
Publication date	May 31, 2022
Grant date	May 31, 2022

Abstract

A wing tip device for attaching to an aircraft wing comprising a first wing tip device element having a root end and a tip end; a second wing tip device element coupled to the tip end of the first wing tip device element; wherein the second wing tip device element has an inboard portion extending inboard from the tip end of the first wing tip device element and/or an outboard portion extending outboard from the tip end of the first wing tip device element, when viewed in the wing planform direction.

First claim

The invention claimed is:

1. A wing tip device for attaching to an aircraft wing comprising:
a first wing tip device element having a root end and a tip end;
a second wing tip device element coupled to the tip end of the first wing tip device element;
wherein the second wing tip device element has an inboard portion extending inboard from the tip end of the first wing tip device element and an outboard portion extending outboard from the tip end of the first wing tip device element, when viewed in a wing planform direction;
wherein the first wing tip device element includes a trailing edge portion of the tip end of the first wing tip device element inboard of another portion of the first wing tip device element which is at an outermost spanwise extent of the first wing tip device element when viewed in the wing planform direction, and
wherein the outboard portion of the second wing tip device element extends up to the outermost spanwise extent of the first wing tip device element.

2. The wing tip device according to claim 1 , wherein the wing tip device has a first vertex between the first wing tip device element and the inboard portion of the second wing tip device element.

3. The wing tip device according to claim 1 , wherein the wing tip device has a second vertex between the first wing tip device element and the outboard portion of the second wing tip device element.

4. The wing tip device according to claim 1 , wherein the second wing tip device element is substantially planar.

5. The wing tip device according to claim 4 , wherein the plane of the second wing tip device element is normal to a cant angle at the tip end of the first wing tip device element.

6. The wing tip device according to claim 1 , wherein the first wing tip device element is twisted between the root end of the first wing tip device element and the tip end of the first wing tip device element.

7. The wing tip device according to claim 1 , wherein the first wing tip device element is twisted about an axis parallel to the wing planform direction so that the first wing tip device has a toe-out angle.

8. The wing tip device according to claim 1 , wherein a wetted area of the second wing tip device element is less than 40% of the wetted area of the first wing tip device element.

9. The wing tip device according to claim 1 , wherein a wetted area of the inboard portion is greater than a wetted area of the outboard portion.

10. The wing tip device according to claim 1 , wherein the second wing tip device element extends aft, when viewed in the wing planform direction, of the tip of the first wing tip device element.

11. The wing tip device according to claim 1 , wherein the outboard portion has an aft swept region.

12. The wing tip device according to claim 1 , wherein the inboard portion has an aft swept region.

13. The wing tip device according to claim 1 , wherein the tip end of the first wing tip device element has a cant angle of at least 20 degrees.

14. The wing tip device according to claim 1 , wherein the first wing tip device element is at least one of a non-planar wing tip extension, a winglet, a winglet having a substantially planar portion and a non-planar wing tip extension, a blended winglet, a split winglet having an uplet and a downlet, a downlet, and a raked wingtip.

15. The wing tip device according to claim 1 , wherein the first wing tip device element includes an uplet and a downlet, and
wherein the second wing tip device element is coupled to a tip end of the uplet or downlet.

16. The wing tip device according to claim 15 , wherein a tip of the uplet and a tip of the downlet are located at substantially the same spanwise location, when viewed in the wing planform direction.

17. The aircraft wing comprising a wing root end and a wing tip end, and the wing tip device according to claim 1 attached to the wing tip end.

18. A fixed wing aircraft comprising the aircraft wing according to claim 17 .

19. The fixed wing aircraft according to claim 18 , wherein the spanwise extent of the wing in the ground shape conforms to an airport compatibility gate limit.

Assignees

• Airbus Operations Ltd

Inventors

• Commis Ben

Classifications

• B64C3/38 Primary

  Adjustment of complete wings or parts thereof · CPC title

• B64C1/26

  Attaching the wing or tail units or stabilising surfaces · CPC title

• B64C3/58

  provided with fences or spoilers (adjustable for control purposes B64C9/00) · CPC title

• B64C23/069 Primary

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

• B64C5/08 Primary

  mounted on, or supported by, wings · CPC title