Method and assembly for attaching fuel system components to a rib before the assembly is joined to an aircraft wing

Patent metadata

Field	Value
Publication number	US-9527576-B2
Application number	US-201313961199-A
Country	US
Kind code	B2
Filing date	Aug 7, 2013
Priority date	Aug 15, 2012
Publication date	Dec 27, 2016
Grant date	Dec 27, 2016

Abstract

A method of installing fuel system components in an aircraft wing in which the fuel system components are attached to ribs before the ribs are assembled into the wing. The ribs are structural ribs for the wing and may be assembled to form a combined rib and fuel system component assembly before the assembly is added to the wing.

First claim

The invention claimed is:

1. A method of manufacturing an aircraft wing assembly comprising ribs and other structural elements, the method including:
attaching a fuel system component to at least one of the ribs to form at least one preinstalled rib, wherein the at least one rib includes a pair of rib portions and each rib portion includes a wall, wherein the preinstalled rib is formed by joining the walls together such that the fuel system component is between the walls, and wherein the rib portions each have a height corresponding to a thickness of the aircraft wing;
delivering the at least one preinstalled rib to a wing assembly location at which the other structural elements are located; and
assembling the at least one preinstalled rib and the other structural elements at said wing assembly location.

2. The method of claim 1 , wherein the attachment of the fuel system component to at least one of ribs to form the at least one preinstalled rib, comprises attaching the fuel system component to at least one of the walls.

3. The method of claim 1 , including attaching the fuel system component to one of the walls before the one of the walls is joined to another one of the walls of the rib portions.

4. The method of claim 1 , wherein the fuel system component is an electrical component, and at least one of the pair of rib portions includes a channel or conduit for the passage of a cable or fuel pipe, and the method includes routing the cable or fuel pipe through the channel or conduit prior to joining the walls of the rib portions.

5. A preinstalled structural rib configured for delivery to an aircraft wing assembly location at which ribs and other structural elements of an aircraft wing assembly are located for the manufacture of an aircraft wing assembly using said preinstalled structural rib, the ribs and the other structural elements, wherein the preinstalled structural rib comprises:
a pair of rib portions each having a wall, the wall of one of the rib portions facing and being attached to the wall of the other rib portion, wherein the rib portions each have a height corresponding to a thickness of the aircraft wing assembly;
a space between the rib portions; and
a fuel system component mounted to at least one of the walls and in the space between the rib portions.

6. An aircraft wing comprising a plurality of the preinstalled structural ribs according to claim 5 , wherein the preinstalled structural ribs are joined to each other in spaced relation with the other structural elements.

7. A method of manufacturing an aircraft wing assembly comprising a preinstalled rib, ribs and other structural elements, the method comprising:
attaching a fuel system component to a wall of a rib portion of a pair of rib portions, wherein each of the rib portions has a height corresponding to a thickness of the aircraft wing assembly;
after attaching the fuel system component, forming the preinstalled rib by joining together the pair of rib portions wherein the wall faces a corresponding wall of another rib portion of the pair of rib portions;
delivering the preinstalled rib to a wing assembly location at which the ribs and the other structural elements are located; and
assembling the preinstalled rib with the ribs and the other structural elements at the wing assembly location.

8. The method of claim 7 wherein the attachment of the fuel system component to the wall is performed to position the fuel system component in an enclosed space formed between the walls of the rib portions when the rib portions are joined.

9. A method for manufacture of an aircraft wing assembly comprising:
forming a preinstalled rib by joining walls of a pair of rib portions with a fuel system component between the walls, such that the pair of rib portions and the fuel system component form the preinstalled rib, wherein the rib portions each have a height corresponding to a thickness of the aircraft wing assembly;
delivering the preinstalled rib to a wing assembly location at which other structural elements of the aircraft wing assembly are located; and
assembling the preinstalled rib and the other structural elements at said wing assembly location.

10. The method of claim 9 wherein the assembling step further includes assembling an additional rib.

11. The method of claim 9 wherein the attaching step includes forming a plurality of preinstalled ribs by attaching additional fuel system components to additional ribs.

12. The method of claim 11 wherein the preinstalled ribs constitute all ribs in the aircraft wing assembly and the other structural elements do not include ribs.

13. The method of claim 9 wherein the aircraft wing assembly is a portion of a wing of an aircraft.

Assignees

• Airbus Operations Ltd

Inventors

• Haskins Richard

Classifications

• B64C3/187 Primary

  Ribs · CPC title

• B64D37/06

  Constructional adaptations thereof · CPC title

• Y10T29/49826

  Assembling or joining · CPC title

• B64C3/34

  Tanks constructed integrally with wings, e.g. for fuel or water · CPC title