Method and apparatus for fabricating contoured laminate structures

Patent metadata

Field	Value
Publication number	US-9314974-B2
Application number	US-201313901813-A
Country	US
Kind code	B2
Filing date	May 24, 2013
Priority date	Jan 7, 2013
Publication date	Apr 19, 2016
Grant date	Apr 19, 2016

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.

First claim

What is claimed is:

1. An apparatus for fabricating each of a plurality of differing laminate structures in a family of structures having common features, comprising:
a plurality of separate fabrication modules each locally adapted to fabricate a section of the laminate structure on a corresponding tool, the fabrication modules being reconfigurable to fabricate each of the laminate structures in the family thereof, wherein each of the fabrication modules includes a track in which a portion of a forming member is local mounted;
the forming member adapted for forming laminate plies over the tool, the forming member extending along a length of the fabrication modules, portions of the forming member being mounted on each of the fabrication 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
a controller for controlling and coordinating automated operation of the fabrication modules.

2. The apparatus of claim 1 , wherein the forming member is continuous along the length of the fabrication modules.

3. The apparatus of claim 1 , wherein the forming member is adapted to sweep laminate plies over the tool, and includes compliance.

4. The apparatus of claim 1 , wherein each of the fabrication modules includes a clamp adapted for clamping a portion of a laminate ply against a portion of the tool.

5. The apparatus of claim 1 , wherein each of the fabrication modules includes a powered drive coupled with the forming member for sweeping the forming member over the laminate plies and compacting laminate plies on the tool.

6. The apparatus of claim 1 , further comprising:
a flexible ply carrier adapted to hold at least one laminate ply thereon, and
wherein each of the fabrication modules includes a pair of spaced apart tracks adapted to releasably hold the ply carrier, and a ply carrier control assembly for holding the ply carrier in tension as the forming member forms the ply over the tool.

7. The apparatus of claim 6 , wherein:
the forming member is engageable with the ply carrier to sweep the ply carrier along with the ply thereon over the tool, and
the ply carrier control assembly includes drives for adjusting a position of the ply carrier along two axes.

8. The apparatus of claim 1 , wherein each of the fabrication modules further includes:
a force sensor for sensing a level of force applied to the laminate plies by the forming member, and
a position sensor for sensing the position of the forming member.

9. The apparatus of claim 1 , wherein each of the fabrication modules includes a clamp for clamping the fabrication module to the tool.

10. The apparatus of claim 1 , further comprising:
linkage between the fabrication modules for rigidly coupling the fabrication modules together and for aligning the fabrication modules relative to the tool.

11. The apparatus of claim 1 , wherein the fabrication modules are substantially identical and interchangeable with each other.

12. The apparatus of claim 1 , further comprising a central controller for controlling and coordinating the operation of the fabrication modules to collectively fabricate the laminate structure.

13. A method of fabricating each of a plurality of differing parts in a family of parts having common features, wherein each of the parts is fabricated using a unique tool, comprising:
arranging a plurality of separate, substantially identical fabrication modules to substantially match a tool on which one of the parts is to be fabricated, wherein each of the fabrication modules includes a track;
locally mounting portions of a forming member within the track along substantially the entire length of the fabrication modules, the portions of the forming member being mounted on each of the fabrication 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;
adapting each of the fabrication modules to a local section of the tool; and,
controlling and coordinating operation of the fabrication modules to fabricate portions of the part over a corresponding section of the tool.

14. The method of claim 13 , wherein arranging the fabrication modules includes:
moving each of the fabrication modules into proximity to the tool, and
rigidly linking the fabrication modules together.

15. The method of claim 13 , further comprising:
clamping each of the fabrication modules to the tool.

16. The method of claim 13 , wherein adapting the each of the fabrication modules includes learning, by each of the fabrication modules, the location of surfaces on the tool on which the part is to be fabricated.

17. The method of claim 16 , further comprising:
sweeping materials across the surfaces of the tool using the forming member, and
using the forming member to learn the location of the surfaces on the tool.

18. The method of claim 17 , wherein learning the location of the surfaces includes:
sensing a position of the forming member as the forming member sweeps materials across the surfaces of the tool, and
recording the sensed position of the forming member.

19. The method of claim 13 , wherein adapting each of the fabrication modules includes adjusting the elevation of the fabrication modules to a common waterline.

20. The method of claim 13 , wherein the step of locally mounting portions of the forming member within the track along substantially the entire length of the fabrication modules further comprises:
forming a continuous spline defined by the forming member along all of the fabrication modules.

21. The method of claim 13 , wherein:
each of the fabrication modules is a laminate ply former module, and
arranging the fabrication modules includes linking the fabrication modules together to form a single laminate ply former.

22. An apparatus for fabricating each of a plurality of differing laminate structures in a family of structures having common features, comprising:
a flexible ply carrier adapted to hold at least one laminate ply thereon;
a plurality of separate fabrication modules each locally adapted to fabricate a section of the laminate structure on a corresponding tool, wherein each of the fabrication modules includes a pair of spaced apart tracks adapted to releasably hold the ply carrier, the fabrication modules being reconfigurable to fabricate each of the laminate structures in the family thereof;
a forming member adapted for forming laminate plies over the tool, the forming member extending along a length of the fabrication modules, portions of the forming member being mounted on each of the fabrication modules for movement over the tool along at least two axes;
a ply carrier control assembly for holding the ply carrier in tension as the forming member forms the ply over the tool; and
a controller for controlling and coordinating automated operation of the fabrication modules.

23. The apparatus of claim 22 , wherein the forming member is continuous along the length of the fabrication modules.

24. The apparatus of claim 23 , wherein each of the fabrication modules includes a track in which a portion of the forming member is locally mounted.

25. The apparatus of claim 24 , wherein the forming member is removably

Assignees

• Boeing Co

Inventors

• Buttrick James N
• Stewart Dennis Wayne
• Modin Andrew E
• Banks David Paul
• Depase Edoardo
• Sanchez Jesus

Classifications

• B29C70/38 Primary

  Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns {(application heads for tyres B29D30/28)} · CPC title

• B29K2307/04

  Carbon · CPC title

• B29C70/541

  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 title

• Y10T156/1002

  with permanent bending or reshaping or surface deformation of self sustaining lamina · CPC title

• B29D99/0003

  Producing profiled members, e.g. beams · CPC title