Structure

• US 10,308,345 B2
• Filed: 07/07/2015
• Issued: 06/04/2019
• Est. Priority Date: 07/08/2014
• Status: Active Grant

• Current Assignee: Airbus Operations Limited (Airbus SE)
• Original Assignee: Airbus Operations Limited (Airbus SE)
• Inventors: Marks, Oliver
• Primary Examiner(s): Badawi, Medhat
• Application Number:
  US14/793,581
• Publication Number:
  US 20160009365A1
• Time in Patent Office: 1,428 Days
• CPC Class Codes: B64C 2001/0072 from composite materials
• CPC Class Codes: B64C 3/18 Spars; Ribs; Stringers
• CPC Class Codes: B64C 3/182 Stringers, longerons
• CPC Class Codes: B64C 3/187 Ribs
• CPC Class Codes: B64C 3/26 Construction, shape, or attachment of separate skins, e.g. panels
• CPC Class Codes: B64C 5/00 Stabilising surfaces
• CPC Class Codes: Y02T 50/40 Weight reduction

Abstract

The invention relates to a structure having a panel, a stringer and a rib. The stringer has a stringer flange that is joined to an inner surface of the panel and a stringer web that extends away from the stringer flange. The rib has a rib web and a rib foot. The rib foot has a rib foot flange that is joined to the stringer web, first and second rib foot base parts that are joined to the inner surface of the panel or to the stringer flange and a rib foot web that is joined to the rib web. The rib foot is formed as a single folded piece such that the rib foot flange is connected to the rib foot web by a first folded corner, the first rib foot base part is connected to the rib foot flange by a second folded corner and the second rib foot base part is connected to the rib foot web by a third folded corner.

Claims

1. A structure comprising:

a panel;

a stringer comprising a stringer flange joined to the panel and a stringer web extending away from the stringer flange;

a rib comprising a rib web and a rib foot, the rib foot having a rib foot flange joined to the stringer web;

first and second rib foot base parts joined to the panel or to the stringer flange; and

a rib foot web joined to the rib web;

wherein the rib foot flange is connected to the rib foot web by a first corner that includes at least one layer which runs continuously from the rib foot flange into the rib foot web via the first corner;

wherein the first rib foot base part is connected to the rib foot flange by a second corner that includes at least one layer which runs continuously from the first rib foot base part into the rib foot flange via the second corner; and

wherein the second rib foot base part is connected to the rib foot web by a third corner that includes at least one layer which runs continuously from the second rib foot base part into the rib foot web via the third corner.

2. The structure according to claim 1, wherein the first rib foot base part abuts the second rib foot base part or is joined to the second rib foot base part.

3. The structure according to claim 1, wherein the rib foot comprises at least one layer which runs around the first, second, and third corners.

4. The structure according to claim 1, wherein the first rib foot base part is joined to the second rib foot base part by a co-cured joint.

5. The structure according to claim 1, wherein the rib foot flange is joined to the stringer web by a co-bonded or co-cured joint.

6. The structure according to claim 1, wherein the first and second rib foot base parts are joined to the panel or to the stringer flange by a co-bonded or co-cured joint.

7. The structure according to claim 1, wherein:

the rib foot is formed from a composite material comprising a plurality of fibres,

some of the fibres run continuously from the rib foot flange into the rib foot web via the first corner,

some of the fibres run continuously from the first rib foot base part into the rib foot flange via the second corner, and

some of the fibres run continuously from the second rib foot base part into the rib foot web via the third corner.

8. The structure according to claim 1, wherein the rib foot comprises a further rib foot flange joined to the stringer web, the further rib foot flange and the rib foot flange extending on opposite sides of the rib foot web.

9. The structure according to claim 8, wherein the second rib foot flange is joined to the stringer web by a co-bonded or co-cured joint.

10. The structure according to claim 1, wherein the rib foot comprises a further rib foot base part joined to the panel or to the stringer flange, the further rib foot base part and the first and second rib foot base parts extending on opposite sides of the rib foot web.

11. The structure according to claim 1, wherein the rib foot comprises a pair of back-to-back parts, each of which comprises:

a rib foot flange joined to the stringer web;

first and second rib foot base parts joined to the panel or to the stringer flange; and

a rib foot web joined to the rib web,

wherein the rib foot flange is connected to the rib foot web by a first corner including at least one layer, which is continuous from the rib foot flange into the rib foot web via the first corner,

wherein the first rib foot base part is connected to the rib foot flange by a second corner including at least one layer, which is continuous from the first rib foot base part into the rib foot flange via the second corner,

wherein the second rib foot base part is connected to the rib foot web by a third corner including at least one layer which is continuous from the second rib foot base part into the rib foot web via the third corner, and

wherein the rib foot webs of the pair of back-to-back parts are joined to each other and to the rib web.

12. The structure according to claim 1, wherein the structure is an aerodynamic aircraft structure.

13. The structure according to claim 12, wherein the aerodynamic aircraft structure is an aircraft wing box.

14. An aircraft comprising a fuselage and the structure according to claim 12, wherein the structure is attached to and extends away from the fuselage.

17. The structure according to claim 12, wherein the aerodynamic aircraft structure is an aircraft horizontal stabilizer.

18. The structure according to claim 12, wherein the aerodynamic aircraft structure is an aircraft vertical stabilizer.

15. A method of forming a structure, the method including steps of:

providing a panel, a stringer comprising a stringer flange and a stringer web, and a rib comprising a rib web;

forming a rib foot comprising a rib foot flange, a rib foot web, and first and second rib foot base parts;

connecting the rib foot flange to the rib foot web by a first corner including at least one layer, which is continuous from the rib foot flange into the rib foot web via the first corner;

connecting the first rib foot base part to the rib foot flange by a second corner including at least one layer, which is continuous from the first rib foot base part into the rib foot flange via the second corner; and

connecting the second rib foot base part to the rib foot web by a third corner including at least one layer, which is continuous from the second rib foot base part into the rib foot web via the third corner;

joining the stringer flange to the panel;

joining the rib foot flange to the stringer web;

joining the first and second rib foot base parts to the inner surface of the panel or to the stringer flange; and

joining the rib foot web to the rib web.

16. The method according to claim 15, wherein the rib foot flange, the rib foot web, the first rib foot base part, and the second rib foot base part are formed as a single piece, which is subsequently bent or folded to form the first, second, and third corners.