Method and apparatus for fabricating contoured laminate structures

• US 10,464,265 B2
• Filed: 04/01/2016
• Issued: 11/05/2019
• Est. Priority Date: 01/07/2013
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Buttrick, James N., Stewart, Dennis Wayne, Modin, Andrew E., Banks, David Paul, Depase, Edoardo, Sanchez, Jesus
• Primary Examiner(s): Musser, Barbara J
• Application Number:
  US15/089,399
• Publication Number:
  US 20160214330A1
• Time in Patent Office: 1,313 Days
• Field of Search: None
• CPC Class Codes: B29C 69/00 Combinations of shaping techniques not provided for in a single one of main groups B29C39/00 - B29C67/00, e.g. associations of moulding and joining techniques; Apparatus therefore B29C48/001 takes precedence
• CPC Class Codes: B29C 70/06 Fibrous reinforcements only
• CPC Class Codes: B29C 70/38 Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns application heads for tyres B29D30/28
• CPC Class Codes: B29C 70/541 Positioning reinforcements in a mould, e.g. using clamping means for the reinforcement positioning inserts in moulds B29C33/12; lay-up on a mould B29C70/30
• CPC Class Codes: B29D 99/0003 Producing profiled members, e.g. beams
• CPC Class Codes: B29K 2105/12 of short lengths, e.g. chopped filaments, staple fibres or bristles
• CPC Class Codes: B29K 2307/04 Carbon
• CPC Class Codes: B29L 2031/3082 Fuselages
• CPC Class Codes: Y02T 50/40 Weight reduction
• CPC Class Codes: Y10T 156/1002 with permanent bending or reshaping or surface deformation of self sustaining lamina

Abstract

A plurality of identical fabrication modules are linked together and configurable to fabricate any of a plurality of differing laminate structures in a family of structures having common features. Each of the fabrication modules is locally adapted to fabricate a section of the laminate structure on a corresponding tool. A controller controls and coordinates automated operation of the fabrication modules.

Claims

1. A system for fabricating a plurality of distinct parts, comprising:

a plurality of distinct lay-up tools respectively corresponding to the plurality of parts to be fabricated;

a plurality of forming modules configured to be combined together to define a plurality of distinct formers respectively corresponding to the plurality of parts and the plurality of lay-up tools, each of the formers being adapted for laying down material on a corresponding one of the lay-up tools, wherein each of the forming modules includes a corresponding track in which a portion of a forming member is locally mounted; and

the forming member adapted for forming material over a particular lay-up tool from among the plurality of lay-up tools to form a particular part from among the plurality of parts, the forming member extending along the plurality of forming modules, the forming member being mounted on the corresponding tracks of the forming modules for movement over the particular lay-up tool along at least two axes, wherein the forming member is removably mounted in the tracks to allow interchangeability of a plurality of different forming members respectively having different shapes.

2. The system of claim 1, wherein:

the forming modules are substantially identical, and

each of the plurality of distinct formers is configured by coupling the forming modules to a corresponding distinct lay-up tool.

3. The system of claim 1, wherein the forming modules are mounted on bases allowing the forming modules to move in multiple directions.

4. The system of claim 1, wherein forming modules are rigidly linked together.

5. The system of claim 1, wherein each of the forming modules includes a forming head section adapted to form the material on the particular lay-up tool.

6. The system of claim 5, wherein each of the forming head sections includes compliance.

7. The system of claim 6, wherein the compliance is removed when the forming modules are coupled to the lay-up tool.

8. The system of claim 1, wherein the part is a laminated structure.

9. The system of claim 1, wherein the part is a carbon fiber reinforced plastic.

10. A method of fabricating a composite laminate structure, comprising:

arranging a plurality of substantially identical forming modules to generally match a tool on which composite plies are to be formed to fabricate the laminate structure, wherein each of the forming modules includes a track;

linking the forming modules together to form a single former for forming an entire composite laminate structure;

mounting a continuous forming member within the track on the forming modules, the continuous forming member defining a spline extending substantially an entire length of the former, the forming member being mounted on each of the forming modules for movement over the tool along at least two axes, wherein the forming member is removably mounted in the tracks to allow interchangeability of a plurality of forming members respectively having different shapes; and

using the forming member to form and compact the composite plies on the tool.

11. The method of claim 10, further comprising:

placing the composite plies on a ply carrier, and

wherein using the forming member includes engaging and sweeping the ply carrier along with the composite plies over the tool.

12. A system for fabricating a plurality of distinct parts, comprising:

a plurality of distinct lay-up tools respectively corresponding to the plurality of parts to be fabricated;

a flexible ply carrier adapted to hold at least one laminate ply thereon;

a plurality of forming modules configured to be combined together to define a plurality of distinct formers respectively corresponding to the plurality of parts and the plurality of lay-up tools, wherein each of the forming modules includes a pair of spaced apart tracks adapted to releasably hold the ply carrier, each of the formers being adapted for laying down material on a particular lay-up tool from among the plurality of lay-up tools;

a forming member adapted for forming laminate plies over a particular lay-up tool from among the plurality of lay-up tools to form a particular part from among the plurality of parts, the forming member extending along the plurality of forming modules, the forming member being mounted on the forming modules for movement over the particular lay-up tool along at least two axes; and

a plurality of ply carrier control assemblies for holding the ply carrier in tension as of the forming member forms the at least one laminate ply over the particular lay-up tool.

13. The system of claim 12, wherein:

the forming modules are substantially identical, and

each of the plurality of distinct formers is configured by coupling forming modules to a corresponding distinct lay-up tool.

14. The system of claim 12, wherein the forming modules are mounted on bases allowing the forming modules to move in multiple directions.

15. The system of claim 12, wherein forming modules are rigidly linked together.

16. The system of claim 12, wherein each of the forming modules includes a forming head section adapted to form the material on the particular lay-up tool.

17. The system of claim 16, wherein each of the forming head sections includes compliance.

18. The system of claim 17, wherein the compliance is removed when the forming modules are coupled to the lay-up tool.

19. The system of claim 12, wherein the part is a laminated structure.

20. The system of claim 12, wherein the part is a carbon fiber reinforced plastic.

21. A method of fabricating a composite laminate structure, comprising:

arranging a plurality of substantially identical forming modules to generally match a tool on which composite plies are to be formed to fabricate the laminate structure, wherein each of the forming modules includes a pair of spaced apart tracks, the tracks having a ply carrier held thereon;

linking the forming modules together to form a single former for forming an entire composite laminate structure;

mounting a continuous forming member within the track on the forming modules, the continuous forming member defining a spline extending substantially an entire length of the former, portions of the forming member being mounted on each of the forming modules for movement over the tool along at least two axes;

holding the ply carrier in tension on the tracks while the forming member forms a laminate ply over the tool; and

using the forming member to form and compact the laminate ply on the tool.

22. The method of claim 21, further comprising:

placing the laminate ply on the ply carrier, and

wherein using the forming member includes engaging and sweeping the ply.