Automated method to determine composite material constituent properties

• US 8,401,829 B2
• Filed: 01/21/2011
• Issued: 03/19/2013
• Est. Priority Date: 01/21/2010
• Status: Active Grant

• Current Assignee: Autodesk, Inc.
• Original Assignee: Firehole Technologies
• Inventors: Fertig, Ray, Nelson, Emmett, Robbins, Don
• Primary Examiner(s): PATEL, SHAMBHAVI K
• Application Number:
  US13/011,076
• Publication Number:
  US 20110178786A1
• Time in Patent Office: 788 Days
• Field of Search: None
• US Class Current: 703/2
• CPC Class Codes: G06F 2113/24 Sheet material
• CPC Class Codes: G06F 2113/26 Composites
• CPC Class Codes: G06F 30/23 using finite element methods [FEM] or finite difference methods [FDM]

Abstract

A method of determining in situ composite material constituent properties is provided. In one example computer software is provided that automatically determines adjusted material properties or in situ properties of each constituent of a composite material. Methods shown ensure that a finite element model will consistently predict material behavior not just at one desired stress/strain state, but in all simulated states.

Claims

1. A method comprising:

entering a set of composite material properties into a computer memory, including;

a composite modulus in a first direction;

a composite modulus in a second direction normal to the first direction;

a composite shear modulus in a plane that includes the first direction and the second direction;

a composite Poisson ratio in a plane that includes the first direction and the second direction;

entering a composite microstructure into the computer;

processing the set of composite material properties and the composite microstructure to determine adjusted material properties of all constituents of the composite material, wherein a set of fixed constituent property constraints are utilized to obtain the adjusted material properties.

2. The method of claim 1, wherein entering the composite microstructure includes entering a carbon fiber/polymer matrix composite microstructure condition.

3. A computer system, comprising:

a processor;

a memory in communication with the processor, wherein the memory includes instructions stored thereon, the instructions when executed operable to;

accept a set of user input carbon fiber/polymer matrix composite material properties, including;

a composite modulus in a first direction;

a composite modulus in a second direction normal to the first direction;

a composite shear modulus in a plane that includes the first direction and the second direction;

a composite Poisson ratio in a plane that includes the first direction and the second direction;

accept a user input carbon fiber/polymer matrix microstructure;

determine adjusted material properties of one or more of the carbon fiber constituents, wherein a set of fixed constituent property constraints are utilized to obtain the adjusted material properties; and

determine adjusted properties of one or more polymer matrix constituents, wherein the set of fixed constituent property constraints are utilized to obtain the adjusted polymer matrix properties.

4. The computer system of claim 3, wherein the set of user input composite material properties includes additional directional components of elastic modulus, shear modulus and Poisson ratio.

5. The computer system of claim 3, wherein the set of user input composite material properties includes at least one directional component of a thermal expansion coefficient.

6. The computer system of claim 3, wherein accepting a user input composite microstructure includes accepting a woven carbon fiber/polymer matrix composite microstructure condition.