Tool to hold several mounting clamps simultaneously against an aircraft fuselage frame element

Patent metadata

Field	Value
Publication number	US-9527606-B2
Application number	US-201414448779-A
Country	US
Kind code	B2
Filing date	Jul 31, 2014
Priority date	Aug 1, 2013
Publication date	Dec 27, 2016
Grant date	Dec 27, 2016

Abstract

To reduce the time and cost of manufacture of an aircraft fuselage, a tool for positioning mounting clamps to attach a fuselage frame element onto a fuselage skin and/or onto stiffeners is provided. Accordingly, the tool includes a ramp and several systems for holding clamps in position distributed along the ramp, where each system includes a mobile device for applying pressure to the clamp, together with an adjustment device coupled to the mobile device such that its separation from the ramp is adjustable.

First claim

The invention claimed is:

1. A tool for positioning mounting clamps used for attaching an aircraft fuselage frame element onto a fuselage skin and/or onto one or more fuselage stiffeners fitted to the fuselage skin, the tool comprising:
a ramp; and
one or more position-holding systems configured to hold the mounting clamps in position, wherein the one or more position-holding systems are distributed along the ramp, and wherein each of the one or more position-holding systems comprises a mobile device for applying pressure to a respective mounting clamp, together with an adjustment device coupled to the mobile device, such that a separation of the mobile device from the ramp is adjustable.

2. The tool according to claim 1 , wherein at least several of the one or more position-holding systems are installed such that the at least several of the one or more position-holding systems are slideable on the ramp.

3. The tool according to claim 1 , wherein each of the mobile devices for applying pressure includes a first plate coupled to the adjustment device, one or more contact parts configured to contact the mounting clamps to apply pressure to the respective mounting clamps, together with an offsetting mechanism connecting the one or more contact parts to the first plate, wherein the offsetting mechanism is installed such that the offsetting mechanism rotates relative to the one or more contact parts and/or relative to the first plate.

4. The tool according to claim 3 , wherein the offsetting mechanism comprises one or more connecting rods forming a pendular system.

5. The tool according to claim 3 , wherein the first plate comprises a holding portion configured to cooperate with the one or more fuselage stiffeners.

6. The tool according to claim 5 , wherein the holding portion of the first plate is configured such that the holding portion is configured to slide along an associated stiffener.

7. The tool according to claim 1 , wherein each of the one or more position-holding systems comprises a second plate installed on the ramp and coupled to the adjustment device.

8. The tool according to claim 7 , wherein the second plate comprises a holding portion configured to cooperate with the one or more fuselage stiffeners.

9. The tool according to claim 8 , wherein the holding portion of the second plate is designed such that the holding portion is configured to slide along an associated stiffener.

10. The tool according to claim 1 , further comprising between five and fifteen position-holding systems.

11. An assembly for positioning on a fuselage in order to be partially integrated in the fuselage, wherein the assembly comprises a fuselage frame element, at least one tool according to claim 1 , together with multiple clamps held in position by the tool, against the fuselage frame element.

12. An assembly according to claim 11 , wherein a ramp of the tool extends over a length substantially identical to that of the fuselage frame element.

13. A method for positioning mounting clamps to attach a fuselage frame element onto a fuselage skin and/or onto one or more fuselage stiffeners fitted to the fuselage skin, the method comprising:
using a tool according to claim 1 ;
moving a ramp of the tool along the fuselage frame element;
pressing the mounting clamps against the fuselage frame element; and
using one or more position-holding systems on the tool.

14. The method according to claim 13 , further comprising implementing the tool when the fuselage frame element is already in position relative to the fuselage skin, or with the fuselage frame element positioned at a distance from the fuselage skin, to form an assembly according to claim 11 , wherein the assembly is transportable in a direction of the fuselage skin.

15. A method for attaching a fuselage frame element onto a fuselage skin and/or onto one or more fuselage stiffeners fitted on the fuselage skin, the method comprising:
implementing the method for positioning mounting clamps according to claim 13 ; and
automatically attaching the mounting clamps onto the fuselage frame element and attaching the mounting clamps onto the fuselage skin and/or onto the one or more fuselage stiffeners fitted to the fuselage skin.

16. A tool for positioning mounting clamps used for attaching an aircraft fuselage frame element onto a fuselage skin and/or onto one or more fuselage stiffeners fitted to the fuselage skin, the tool comprising:
a ramp; and
one or more position-holding system configured to hold the mounting clamps in position, wherein the one or more position-holding system is distributed along the ramp, and wherein each of the one or more position-holding system comprises a mobile device for applying pressure to a respective mounting clamp, together with an adjustment device coupled to the mobile device, such that a separation of the mobile device from the ramp is adjustable;
wherein each of the mobile devices for applying pressure includes a first plate coupled to the adjustment device, one or more contact parts configured to contact the mounting clamps to apply pressure to the respective mounting clamps, together with an offsetting mechanism connecting the one or more contact parts to the first plate, wherein the offsetting mechanism is installed such that the offsetting mechanism rotates relative to the one or more contact parts and/or relative to the first plate.

17. The tool according to claim 16 , wherein the offsetting mechanism comprises one or more connecting rods forming a pendular system.

18. The tool according to claim 16 , wherein the first plate comprises a holding portion configured to cooperate with the one or more fuselage stiffeners.

19. The tool according to claim 18 , wherein the holding portion of the first plate is configured such that the holding portion is configured to slide along an associated stiffener.

Assignees

• Airbus Operations Sas

Inventors

• Marin Yannick
• Guilloteau Damien

Classifications

• B64F5/0009 Primary

  Operations & Transport · mapped topic

• B64C1/061 Primary

  Frames · CPC title

• B64C1/12

  Construction or attachment of skin panels · CPC title

• Y10T29/53978

  including means to relatively position plural work parts · CPC title

• Y10T29/49826

  Assembling or joining · CPC title