System for out of autoclave bonded repairs

Patent metadata

Field	Value
Publication number	US-10189123-B2
Application number	US-201615286098-A
Country	US
Kind code	B2
Filing date	Oct 5, 2016
Priority date	Oct 5, 2015
Publication date	Jan 29, 2019
Grant date	Jan 29, 2019

Abstract

A system for out of autoclave bonded repairs which including a fixing structure (1) to the composite area to be repaired, including a frame (4) and fixing parts (5, 19) attached to the frame (4), a movable structure (2) able to be attached either to the fixing structure (1) or to the patch manufacturing table (3), which includes three shafts (6, 6′, 6″) and three engines (7, 7′, 7″) configured to be able to move the tooling support in the three axes X, Y and Z, and a tooling support of either scanning tool (9), milling tool (10), patch cutting tool (11) or composite patch handle tool (11), and a patch manufacturing structure (3).

First claim

The invention claimed is:

1. A system for out of autoclave bonded repairs comprising:
a first fixing structure configured to be fixed to a composite damaged area to be repaired, the first fixing structure including a frame and fixing parts attached to the frame;
a movable structure including:
a first rotating shaft connected to a first engine configured to rotate the first rotating shaft and attached to second fixing structures,
a tooling support attached to the first rotating shaft, wherein the tooling support includes a second rotating shaft connected to a second engine configured to rotate the second shaft, and the tooling support configured to mount tooling including at least one of a scanning tool, a milling tool, a patch cutting tool and a composite patch handle tool attached to the second rotating shaft, and
second fixing structures each including fixing parts linked to each other through a third rotating shaft connected to a third engine configured to rotate the third shaft been the fixing parts, wherein the second fixing structures are configured to be attached to either or both the frame of the fixing structure of the damaged part and a patch manufacturing structure;

wherein the first, second and third rotating shafts are each oriented along a different one of the three axes X, Y, Z according to a cartesian coordinate system for a three-dimensional space to move the tooling in three dimensions; and
the patch manufacturing structure including a fixing tool configured to fix the movable structure to the patch manufacturing structure.

2. The system according to claim 1 wherein the patch manufacturing structure comprises:
a bench comprising platform and a displacement mechanism configured to move the platform from one side to the other side of the bench, and
a platform for laying up composite layers comprising fasteners configured to attach to the displacement mechanism of the bench.

3. The system according to claim 2 wherein the patch manufacturing structure includes a mould disposed on the bench opposite to the platform, and displacement mechanisms attached to the bench configured to move the mould up and down.

4. The system according to claim 3 wherein the mould is a resin mould.

5. The system according to claim 1 wherein the scanning tool comprises a dual laser scanner head.

6. The system according to claim 1 wherein the fixing parts attached to the frame of the fixing structure comprises vents and counterweights.

7. The system according to claim 1 wherein the patch handle tool comprises two vents for handling the patch.

8. A method for removing and restoring damaged part of a composite structure with a system comprising:
(i) a first fixing structure including a frame and fixing parts attached to the frame;
(ii) a movable structure including a first rotating shaft connected to a first engine configured to rotate the first rotating shaft and attached to second fixing structures;
(ii) a tooling support attached to the first rotating shaft and including a second rotating shaft connected to a second engine configured to rotate the second shaft, wherein the second rotating shaft moves a tooling, and
(iv) the second fixing structures each include fixing parts linked to each other through a third rotating shaft connected to a third engine configured to rotate the third shaft, wherein the second fixing structures are configured to be attached to the frame of the first fixing structure and to a patch manufacturing structure;
wherein the first, second and third rotating shafts are each oriented along a different one of the three axes X, Y, Z according to a Cartesian coordinate system for a three-dimensional space to move the tooling in three dimensions;
wherein the method comprises:
attaching the fixing parts of the first fixing structure to the composite structure such that the frame of the first fixing structure is over the damaged part of the composite structure;
mounting the moveable structure to the first fixing structure by using the second fixing structures to attach the moveable structure to the first fixing structure;
scanning the damaged area by moving a scanning tool over the damaged area while the scanning tool is attached to the second rotating shaft and the scanning tool is moved by rotating one or more of the first, second and third shafts while the moveable structure is mounted to the first fixing structure,
removing at least portions of the damaged area from the composite part by milling the damaged area using a milling tool while moving the milling tool which is attached to the second rotating shaft and moving the milling tool to mill the damaged area by rotating one or more of the first, second and third shafts while the moveable structure is mounted to the first fixing structure,
unmounting the moveable structure from the first fixing structure by releasing the second fixing structures from the first fixing structure;
mounting the moveable structure to the patch manufacturing structure by using the second fixing structures to attach the moveable structure to the patch manufacturing structure;
manufacturing a patch configured to replace the scanned damaged area, by using a patch cutting tool mounted to the second rotating shaft to cut a patch from a material mounted to the patch manufacturing structure, wherein the patch cutting tool is moved by rotating one or more of the first, second and third shafts while the patch cutting tool is mounted on the second rotating shaft and while the moveable structure is mounted on the patch manufacturing structure, and
attaching the patch to the mechanized area formed in the composite structure.

9. The method according to claim 8 wherein the scanning step comprises the steps of scanning though a scanning tool comprising a dual laser scanner head generating a three-dimensional (3D) image or model of the damaged area.

10. The method according to claim 8 wherein the step of removing the damaged area comprises the step of removing layers of the damaged area by using a milling tool generating a mechanized area and generating a new 3D image or model of the mechanized area.

11. The method according to claim 10 wherein the step of manufacturing the patch comprises layup composite layers over either a platform or a resin mould and cut the composite layers with the same volume as the mechanized area according to the generated 3D image or model scanned in the removal step, obtaining a patch.

12. The method according to claim 11 wherein the step of manufacturing the patch comprises manufacturing a resin mould according to the scanned mechanized area and then lay-up the composite layers over the mould.

13. A method to repair a composite material part comprising:
mounting a first fixing structure to the composite material part, wherein the first fixing structure is mounted over a damaged area of the composite material part;
attaching to the first fixing structure a moveable structure supporting a tooling support, wherein the tooling support is configured to support a scanner, a material removal tool and a patch cutting tool;
while the movable structure is attached to the first fixing structure, removing layers from the composite material part using the material removal tool held by the tooling support and being moved across the composite material part by the movable structure, wherein the removed layers include the damaged area;
scanning the composite material after removal of the layers using the scanner held by the tooling support to collect data indicative of a shape of a removed portion of the composite material by using the moveable structure to move the scanner over the compos

Assignees

• Airbus Operations Sl

Inventors

• Rodriguez Bellido Ana
• Sanchez Gomez Jose
• Avila Dominguez Rafael
• Vila Papell Enric
• Anguiano Zarranz Rebeca
• FORCEN CARVALHO Juan Ignacio

Classifications

• B32B2605/18

  Aircraft · CPC title

• B29C73/26

  for mechanical pretreatment · CPC title

• B25H1/00

  Work benches; Portable stands or supports for positioning portable tools or work to be operated on thereby · CPC title

• Y10T29/49734

  and removing damaged material · CPC title

• B29C2073/264

  for cutting out or grooving the area to be repaired · CPC title