Optimization of ply orientations for multi-layer composite parts

• US 10,467,350 B2
• Filed: 02/08/2016
• Issued: 11/05/2019
• Est. Priority Date: 02/08/2016
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Kang, Laura Sumi, Blom, Adriana Willempje
• Primary Examiner(s): Cook, Brian S
• Application Number:
  US15/018,075
• Publication Number:
  US 20170228473A1
• Time in Patent Office: 1,366 Days
• Field of Search: 703 1
• CPC Class Codes: B64C 3/20 Integral or sandwich constructions
• CPC Class Codes: B64F 5/10 Manufacturing or assembling aircraft, e.g. jigs therefor
• CPC Class Codes: G06F 2113/26 Composites
• CPC Class Codes: G06F 2113/28 Fuselage, exterior or interior
• CPC Class Codes: G06F 2119/18 Manufacturability analysis or optimisation for manufacturability
• CPC Class Codes: G06F 30/00 Computer-aided design [CAD]
• CPC Class Codes: G06F 30/15 Vehicle, aircraft or watercraft design
• CPC Class Codes: Y02P 90/02 Total factory control, e.g. smart factories, flexible manufacturing systems [FMS] or integrated manufacturing systems [IMS]
• CPC Class Codes: Y02T 90/00 Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation

Abstract

Systems and methods are provided for composite part design. One embodiment is an apparatus that designs a composite part. The apparatus includes a controller configured to generate a design for the part. The controller subdivides the part into blocks that each comprise a contiguous stack of layers within the part, identifies rules that constrain how layers that have different fiber orientations are stacked within the part, generates a guide for a block that prescribes a fiber orientation for each layer of the block, and identifies sublaminates comprising that are compatible with the guide for the block. The controller subdivides the part into panels, and selects one of the compatible sublaminates for one of the panels of the block, based on compatible sublaminates for neighboring panels.

Claims

1. A method comprising:

designing a multi-layer composite part by;

prior to performing optimization of plies for the composite part;

pre-generating a library of sublaminates comprising consecutive ply sequences;

subdividing the part along its depth into blocks that each comprise a contiguous stack of layers within the part;

identifying rules that constrain how layers that have different fiber orientations are stacked within the part;

generating a guide for a block that prescribes a fiber orientation for each layer of the block and that complies with the rules after the library has been pre-generated;

excluding sublaminates that are not compatible with the guide for the block from the library, wherein sublaminates that are compatible with the guide are subsets of the layers in the guide; and

excluding sublaminates that do not comply with the rules from the library; and

performing optimization of the plies for the composite part by;

subdividing the part into panels that each comprise a fraction of the area of the composite part; and

selecting one of the compatible sublaminates from the library for one of the panels of the block, based on compatible sublaminates for neighboring panels.

2. The method of claim 1 wherein:

selecting one of the compatible sublaminates comprises;

selecting a compatible sublaminate that reduces an aggregate boundary length of ply shapes within a layer of the composite part.

3. The method of claim 1 wherein:

selecting one of the compatible sublaminates comprises;

selecting a compatible sublaminate that reduces an aggregate number of cuts performed to generate ply shapes within the composite part.

4. The method of claim 1 wherein:

selecting one of the compatible sublaminates comprises;

selecting a compatible sublaminate that increases an average course length for ply shapes within the composite part.

5. The method of claim 1 wherein:

selecting one of the compatible sublaminates comprises;

selecting a compatible sublaminate that reduces an aggregate number of internal corners for ply shapes within the composite part.

6. The method of claim 1 wherein:

the sublaminates include empty layers where fiber is not applied to the panel.

7. The method of claim 1 wherein:

the sublaminates are configured to be stacked on top of each other within the composite part without violating the rules.

8. An apparatus comprising:

an interface configured to receive input indicating a geometry of a multi-layer composite part;

a controller configured to, prior to performing optimization of plies for the composite part;

pre-generate a library of sublaminates comprising consecutive ply sequences, subdivide the part into blocks along its depth that each comprise a contiguous stack of layers within the part, identify rules that constrain how layers that have different fiber orientations are stacked within the part, generate a guide for a block that prescribes a fiber orientation for each layer of the block and that complies with the rules after the library has been pre-generated, exclude sublaminates that are not compatible with the guide for the block from the library, wherein sublaminates that are compatible with the guide are subsets of the layers in the guide, and exclude sublaminates that do not comply with the rules from the library

the controller is further configured to perform optimization of the plies for the composite part by;

subdividing the part into panels that each comprise a fraction of the area of the composite part, and selecting one of the compatible sublaminates from the library for one of the panels of the block, based on compatible sublaminates for neighboring panels; and

a memory configured to store the design as a combination of selected sublaminates for use by an Automated Fiber Placement (AFP) machine constructing the part.

9. The apparatus of claim 8 wherein:

the controller is configured to select a compatible sublaminate by selecting a compatible sublaminate that that reduces an aggregate boundary length of ply shapes within a layer of the composite part.

10. The apparatus of claim 8 wherein:

the controller is configured to select a compatible sublaminate by selecting a compatible sublaminate that reduces an aggregate number of cuts performed to generate ply shapes within the composite part.

11. The apparatus of claim 8 wherein:

the controller is configured to select a compatible sublaminate by selecting a compatible sublaminate that increases an average course length for ply shapes within the composite part.

12. The apparatus of claim 8 wherein:

the controller is configured to select a compatible sublaminate by selecting a compatible sublaminate that reduces an aggregate number of internal corners for ply shapes within the composite part.

13. The apparatus of claim 8 wherein:

the compatible sublaminates include empty layers where fiber is not applied to the panel.

14. The apparatus of claim 8 wherein:

the compatible sublaminate are capable of being stacked together with each other within the composite part without violating the rules.

15. A non-transitory computer readable medium embodying programmed instructions which, when executed by a processor, are operable for performing a method comprising:

designing a multi-layer composite part by;

prior to performing optimization of plies for the composite part;

pre-generating a library of sublaminates comprising consecutive ply sequences;

subdividing the part along its depth into blocks that each comprise a contiguous stack of layers within the part;

identifying rules that constrain how layers that have different fiber orientations are stacked within the part;

generating a guide for a block that prescribes a fiber orientation for each layer of the block and that complies with the rules, after pre-generating the library of sublaminates;

excluding sublaminates that are not compatible with the guide for the block from the library, wherein sublaminates that are compatible with the guide are subsets of the layers in the guide; and

excluding sublaminates that do not comply with the rules from the library; and

performing optimization of the plies for the composite part by;

subdividing the part into panels that each comprise a fraction of the area of the composite part; and

selecting one of the compatible sublaminates from the library for one of the panels of the block, based on compatible sublaminates for neighboring panels.

16. The medium of claim 15, wherein:

selecting one of the compatible sublaminates comprises;

selecting a compatible sublaminate that reduces an aggregate boundary length of ply shapes within a layer of the composite part.

17. The medium of claim 15, wherein:

selecting one of the compatible sublaminates comprises;

selecting a compatible sublaminate that reduces an aggregate number of cuts performed to generate ply shapes within the composite part.

18. The medium of claim 15, wherein:

selecting one of the compatible sublaminates comprises;

selecting a compatible sublaminate that increases an average course length for ply shapes within the composite part.

19. The medium of claim 15, wherein:

selecting one of the compatible sublaminates comprises;

selecting a compatible sublaminate that reduces an aggregate number of internal corners for ply shapes within the composite part.

20. The medium of claim 15 wherein:

the sublaminates include empty layers where fiber is not applied to the panel.

21. A method comprising:

receiving input indicating a geometry of a multi-layer composite part;

prior to performing optimization of plies for the composite part;

pre-generating a library of sublaminates comprising consecutive ply sequences;

generating a design indicating an arrangement of ply sequences for the part;

subdividing the part along its depth into blocks that each comprise a contiguous stack of layers within the part;

identifying rules that constrain how layers that have different fiber orientations are stacked within the part;

identifying sets of fiber orientations for a block that comply with the rules and are from the library;

subdividing the block into panels that each comprise a fraction of the area of the composite part;

performing optimization of plies for the composite part by;

selecting one of the sets of fiber orientations for one of the panels, based on sets of fiber orientations for neighboring panels; and

configuring a memory to store the design for use by an Automated Fiber Placement (AFP) machine constructing the part.

22. The method of claim 21, wherein

selecting one of the compatible sublaminates comprises:

selecting a compatible sublaminate that reduces an aggregate boundary length of ply shapes within a layer of the composite part.