Virtual Design Allowables for Composite Materials
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Solution Overview
Problem
Current finite element methods (FEM) systems lack the capability to effectively determine virtual design allowables for composite materials, which are essential for assessing the safe operational limits of structural objects made from these materials, particularly in terms of properties like stiffness, stress, and thermal conductivity.
Innovation Solution
A method and system that utilize a reverse engineering process to determine micromechanical material properties from available test data, generate finite element models, and analyze them to produce a set of virtual allowables, including properties such as stiffness, strength, and thermal conductivity, by integrating these properties into a FEM system.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Measurement precision
If virtual design allowables are determined for composite materials using FEM systems, then the accuracy of material simulations is improved, but the complexity of the system increases
Solution Approach 1:
The system segments the determination of design allowables into distinct virtual test procedures (tension, compression, shear, bearing, etc.) that can be independently defined and executed. Each test type represents a separate module in the test matrix, allowing the complex overall process to be broken down into manageable, reusable components that can be selectively applied to different composite material architectures.
Solution Approach 2:
The system enables parameter changes by allowing users to modify test conditions, material properties, and architectural parameters in the virtual test matrix. The FEM models can be reconfigured with different micromechanical properties, loading conditions, and constraints to simulate various real-world testing scenarios, providing flexibility without requiring system redesign.
2Reliability
If a comprehensive test matrix is created to determine all necessary design allowables, then the reliability of composite material assessment is improved, but the time required for analysis increases
Solution Approach 1:
The system performs preliminary action by pre-defining a comprehensive test matrix that includes all necessary virtual tests (tension, compression, shear, bearing, etc.) before the actual FEM analysis. The test matrix is prepared in advance with all loading conditions, constraints, and evaluation criteria specified, allowing the analysis to proceed systematically without delays for test setup or interpretation during the computation phase.
Solution Approach 2:
The system applies discarding and recovering by selectively executing only the relevant tests from the comprehensive test matrix based on the specific composite material architecture and application requirements. Not all tests need to be performed for every material - the system can discard unnecessary tests while recovering and reusing the pre-defined test frameworks and FEM models for future analyses of similar materials.
3Manufacturing precision
If micromechanical material properties are determined through reverse engineering from available test data, then the manufacturing precision of virtual models is improved, but the difficulty of detecting and measuring properties increases
Solution Approach 1:
The system applies inversion by using reverse engineering - instead of directly measuring micromechanical properties through complex micromechanical testing, the system takes readily available macroscopic test data (from standard composite material tests) and inverts the analysis to back-calculate the underlying micromechanical properties. This reverses the traditional measurement approach, making the difficult-to-measure properties accessible through standard test data and FEM-based inverse analysis.
Data Source
AI summary
A method for determining virtually a set of design allowables for a composite material is disclosed. The method includes receiving information about the composite material and a given set of architectures, available test data of the composite material, and a test matrix identifying desired tests to be performed virtually on the composite material and different set of architectures. Using the material information and available test data, a reverse engineering process is used to determine micromechanical material properties. Finite element models of relevant test specimens are generated according to the test matrix and integrating the micromechanical material properties, and are analyzed. A set of allowables and associated properties is generated based on the finite element analyses results.


