Optimization of ply orientations for multi-layer composite parts

Patent metadata

Field	Value
Publication number	US-10467350-B2
Application number	US-201615018075-A
Country	US
Kind code	B2
Filing date	Feb 8, 2016
Priority date	Feb 8, 2016
Publication date	Nov 5, 2019
Grant date	Nov 5, 2019

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.

First claim

The invention claimed is:

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.

Assignees

• Boeing Co

Inventors

• Kang Laura Sumi
• Blom Adriana Willempje

Classifications

• B64C3/20 Primary

  Integral or sandwich constructions · CPC title

• G06F2113/28

  Fuselage, exterior or interior · CPC title

• G06F2113/26

  Composites · CPC title

• G06F2119/18

  Manufacturability analysis or optimisation for manufacturability · CPC title

• G06F30/15

  Vehicle, aircraft or watercraft design · CPC title