Method for producing part of an aircraft fuselage and tool for implementing said method

Patent metadata

Field	Value
Publication number	US-10029414-B2
Application number	US-201514600442-A
Country	US
Kind code	B2
Filing date	Jan 20, 2015
Priority date	Jan 21, 2014
Publication date	Jul 24, 2018
Grant date	Jul 24, 2018

Abstract

The subject matter disclosed herein relates to a method for assembling at least one panel and frames for producing part of an aircraft fuselage, the method including shaping the panel on support surfaces of a tool, wherein it includes holding each frame clamped against at least one sliding support surface arranged in a transverse plane, the sliding support surfaces of the various frames and the support surfaces being secured to the same tool and positioned relative to one another, and in putting in place permanent attachment elements for connecting the panel and the frames. The subject matter disclosed herein also proposes a tool for implementing the assembly method.

First claim

The invention claimed is:

1. A method for assembling at least one panel and frames, which are part of an aircraft fuselage, the method comprising:
shaping the at least one panel on support surfaces of a tool, the support surfaces having at least one radius of curvature in a transverse plane, the frames following a reference line of curvature;
holding each frame clamped against at least one sliding support surface arranged in a transverse plane, the sliding support surfaces and the support surfaces being secured to the same tool and positioned relative to one another; and
putting in place permanent attachment elements for connecting the at least one panel to the frames.

2. The assembly method according to claim 1 , comprising positioning each frame with respect to its sliding support surface after having shaped the panel.

3. The assembly method according to claim 2 , comprising positioning each frame by immobilizing it along its line of curvature while allowing a translational movement in a radial direction.

4. The assembly method according to claim 3 , wherein each frame is positioned with respect to a positioner arranged equidistant from the ends of the frame, and wherein the ends are subsequently unrolled so as to come into contact with the panel.

5. The assembly method according to claim 3 , comprising using at least one brace for holding each frame clamped against the sliding support surface, the brace comprising a counter-support in contact with the frame which allows the frame to move in translation in the radial direction.

6. The assembly method according to claim 1 , comprising using straps for holding the panel clamped against the support surfaces.

Assignees

• Airbus Operations Sas

Inventors

• De Mattia Denis

Classifications

• B29L2031/3082

  Fuselages · CPC title

• B29C67/0011 Primary

  for shaping plates or sheets · CPC title

• B64F5/10 Primary

  Manufacturing or assembling aircraft, e.g. jigs therefor · CPC title

• B29C33/308

  Adjustable moulds (for injection moulding B29C45/376) · CPC title

• B29C33/307

  Mould plates mounted on frames; Mounting the mould plates; Frame constructions therefor (shaping plates for making moulds B29C33/3842; thin walled moulds B29C33/0011) · CPC title