Computerized ply pattern generation

• US 5,038,291 A
• Filed: 04/03/1989
• Issued: 08/06/1991
• Est. Priority Date: 04/03/1989
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Beck, James M., Wang, Weiping
• Primary Examiner(s): Smith, Jerry
• Assistant Examiner(s): GORDON, PAUL P
• Application Number:
  US07/332,084
• Time in Patent Office: 855 Days
• Field of Search: 364/512, 364/513, 364/476, 364/522, 364/518, 364/521, 364/476, 364/577, 364/578, 340/729
• US Class Current: 700/98
• CPC Class Codes: B29C 70/30 Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
• CPC Class Codes: G05B 19/41 characterised by interpolation, e.g. the computation of intermediate points between programmed end points to define the path to be followed and the rate of travel along that path G05B19/25, G05B19/31, G05B19/37, G05B19/39, G05B19/40 take precedence
• CPC Class Codes: G05B 2219/49002 Map unfolded surface on flat surface to make dies, composite objects, free form
• CPC Class Codes: G05B 2219/49007 Making, forming 3-D object, model, surface
• CPC Class Codes: G05B 2219/49011 Machine 2-D slices, build 3-D model, laminated object manufacturing LOM

Abstract

A computerized process to generate ply patterns for manufacturing industrial parts by stacking and molding a large number of plies is based on solid modeling. The outermost shell of the part is unfolded to a planar pattern using a surface development procedure. The part is decomposed based on the ply thickness; the shell with the ply thickness is removed from the solid model once the surface is unfolded. A set of ply patterns are formed by repeating the unfolding process until no more volume remains. More accurate patterns are produced in less time, especially plies for complexly shaped composite parts such as aircraft engine components.

Claims

1. A computerized ply pattern generation process to be used in the manufacture of industrial parts by stacking and joining a plurality of plies comprising:

providing a 3-dimensional solid model of the part and a mid-surface thereof;

decomposing said part model into nested shells each having a thickness approximately equal to the net thickness of the plies;

unfolding said shells in sequence to respective planar patterns using a surface development procedure; and

determining contours of the planar patterns which are the boundaries of the respective plies.

2. The process of claim 1 wherein said decomposing comprises deriving two sets of the nested shells, one set on either side of said mid-surface, and said unfolding to planar patterns and determining contours is performed for both sets.

3. The process of claim 1 further comprising cutting out the plies from a flexible flat sheet of material and stacking the plies.

4. The process of claim 1 wherein every shell has a surface which is divided into patches, and said surface development procedure comprises integrating along patch borders and adjusting initial conditions to ensure that end points of different integration paths converge.

5. A computerized ply pattern generation process to be used in the manufacture of industrial parts by stacking and joining many plies comprising:

providing a 3-dimensional solid model of the part and first and second curved outer surfaces and a curved mid-surface thereof;

decomposing said part model into nested 3-dimensional shells by calculating distances from said outer surfaces to said mid-surface at a network of points and producing contours of said shells by interpolating along said distances;

developing said shells in sequence to respective planar patterns using a surface development procedure and dividing every shell surface into 3-dimensional patches which are mapped to 2-dimensional unfolded surfaces and aligned; and

determining contours of the planar patterns which are the boundaries of the respective plies.

6. The process of claim 5 further comprising cutting out the plies from flexible flat sheet material and stacking the plies.

7. The process of claim 5 wherein said outer surfaces are doubly curved and said developing comprises integrating along patch borders and adjusting initial conditions to ensure that end points of different integration paths converge.

8. The process of claim 7 further comprising trimming surfaces outside the boundary of every ply.

9. The process of claim 8 further comprising deforming the patch borders and merging to form a continuous ply.

10. A computerized ply pattern generation process to be used in the manufacture of composite parts by stacking and pressure molding pre-impregnated plies comprising:

providing a 3-dimensional solid model of the part and first and second curved outer surfaces and a curved mid-surface thereof;

decomposing said part model into nested 3-dimensional shells having a thickness approximately equal to that of the plies, by calculating distances from said outer surfaces to said mid-surface at a network of points and producing contours of said shells by interpolating along said distances;

developing said shells in sequence to respective planar ply patterns using a surface development procedure and dividing every shell surface into 3-dimensional patches which are mapped to 2-dimensional unfolded surfaces and aligned, said development procedure comprising integrating along patch borders and adjusting initial conditions to ensure that end points of different integration paths converge; and

determining contours of the planar ply patterns which are boundaries of the respective plies.

11. The process of claim 10 where said shells all have the same thickness.

12. The process of claim 10 further comprising cutting out the ply patterns from flat sheets of material and stacking the plies.

13. The process of claim 10 further comprising trimming the surfaces outside the boundary of every ply.

14. The process of claim 13 further comprising deforming the patch borders and merging to form a continuous ply.