Aircraft wing

• US 20070023573A1
• Filed: 08/11/2005
• Published: 02/01/2007
• Est. Priority Date: 08/18/2004
• Status: Abandoned Application

• Current Assignee: Airbus Operations Limited (Airbus SE)
• Original Assignee: Airbus Operations Limited (Airbus SE)
• Inventors: Quayle, Alan, Wood, Eric, Neale, Lee
• Application Number:
  US11/201,739
• Publication Number:
  US 20070023573A1
• Time in Patent Office: Days
• US Class Current: 244/124
• CPC Class Codes: B64C 2211/00 Modular constructions of airplanes or helicopters
• CPC Class Codes: B64C 3/00 Wings ornithopter wings B64C33/02
• CPC Class Codes: B64C 3/187 Ribs
• CPC Class Codes: B64C 7/00 Structures or fairings not otherwise provided for

Abstract

An aircraft wing that may be used in large transport aircraft comprising a first wing portion that, in use, forms an inner portion of an aircraft wing, and is attached to a readily replaceable second wing portion comprising a wingtip. The second wing portion may be readily replaceable by a third wing portion comprising a wingtip, the third wing portion having a different functionality from the second wing portion.

Claims

1. A method of changing the functionality of an aircraft including the following steps:

(a) providing an aircraft having a wing comprising

(i) a first wing portion that, in use, forms an inner portion of an aircraft wing, and is attached to

(ii) a readily replaceable second wing portion comprising a wingtip,

(b) providing a third wing portion comprising a wingtip,

(c) detaching the second wing portion; and

(d) securing the third wing portion to the first wing portion, wherein the third wing portion has a different functionality from the second wing portion, and

the functionality of at least one of the second wing portion and the third wing portion is provided by one or more components contained within said at least one of the second wing portion and the third wing portion.

2. A method according to claim 1 wherein each wing portion comprises an upper wingskin and a lower wingskin and is provided with a wingskin support member disposed between said upper and lower wingskins.

3. A method according to claim 2 wherein

the step of detaching the second wing portion is conducted by unfastening at least one fastener acting between a wingskin support member of the first wing portion and a wingskin support member of the second wing portion and

the step of securing the third wing portion to the first wing portion includes a step of forming a joint between the second and third wing portions in which step at least one fastener is fastened between a wingskin support member of the first wing portion and a wingskin support member of the third wing portion.

4. An aircraft wing comprising:

(i) a first wing portion that, in use, forms an inner portion of an aircraft wing, and is attached to

(ii) a readily replaceable second wing portion comprising a wingtip, wherein

the wing is so arranged that the second wing portion is readily replaceable by a third wing portion comprising a wingtip, the third wing portion having a different functionality from the second wing portion, and the functionality of at least one of the second and the third wing portion being provided by one or more components contained within said at least one of the second and the third wing portion.

5. An aircraft wing according to claim 4 wherein each wing portion comprises an upper wingskin and a lower wingskin and is provided with a wingskin support member disposed between said upper and lower wingskins.

6. An aircraft wing according to claim 5 wherein a joint is formed by at least one fastener acting between the first wing portion wingskin support member and the second wing portion wingskin support member.

7. An aircraft wing according to claim 6, wherein the wingskin support member of the second wing portion comprises a peripheral flange adapted to receive said at least one said fastener.

8. An aircraft wing according to claim 4 wherein one or both of the first and second wing portions are provided with a seal member which, on attachment of the first wing portion to the second wing portion, forms a seal between said first and second wing portions.

9. An aircraft wing according to claim 4 wherein the first wing portion is attached to the second wing portion by a plurality of readily releasable fasteners.

10. An aircraft wing according to claim 9, wherein each wing portion comprises an upper wingskin and a lower wingskin and is provided with a wingskin support member disposed between said upper and lower wingskins and the fasteners are disposed around a periphery at least one of said wingskin support members.

11. An aircraft wing according to claim 10 wherein an end of at least one of said fasteners is captured within an enclosure of one of said support members.

12. An aircraft wing according to claim 4 in which at least one spigot is provided to locate the first wing portion with respect to the second wing portion.

13. An aircraft wing according to claim 4 wherein the first wing portion includes an inner wing rib comprising at least one rib foot and an outer wing rib comprising at least one rib foot and said rib foot of said outer wing rib is directed in a direction substantially opposite to said rib foot of said inner wing rib.

14. An aircraft wing according to claim 4, wherein the first wing portion is provided with at least one electrical connector for forming an electrical connection with a corresponding connector in the second or third wing portion.

15. A wing portion suitable for use as the first wing portion of the aircraft wing of claim 4.

16. A wing portion suitable for use as the second wing portion of the aircraft wing of claim 4.

17. An aircraft having an aircraft wing comprising:

(i) a first wing portion that, in use, forms an inner portion of an aircraft wing, and is attached to

(ii) a readily replaceable second wing portion comprising a wingtip, wherein

the wing is so arranged that the second wing portion is readily replaceable by a third wing portion comprising a wingtip, the third wing portion having a different functionality from the second wing portion, and the functionality of at least one of the second and the third wing portion being provided by one or more components contained within said at least one of the second and the third wing portion.

18. An aircraft according to claim 17, wherein the aircraft is a military transport aircraft.

19. An aircraft according to claim 17, wherein the aircraft has a length of greater than 10 metres, a wing span of greater than 10 metres and has a mass, when empty, of at least 10 tonnes.

20. A kit of aircraft parts comprising

(i) a first wing portion that, in use, forms an inner portion of an aircraft wing,

(ii) a second wing portion comprising a wingtip, the second wing portion being readily attachable to, and readily releasable from, the first wing portion, and

(iii) a third wing portion comprising a wingtip, the third wing portion being readily attachable to, and readily releasable from, the first wing portion,

wherein

the third wing portion has a different functionality from the second wing portion, and the functionality of the second wing portion is provided by one or more components contained within the second wing portion.