Composite Laminate Configuration Using Machine Learning Models

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Solution Overview

Problem

The design of laminate configurations for composite material structures, particularly FRP pipes for optical observation satellites, is arduous due to the lack of a general relational expression depicting the relationship between demanded specifications and laminate configurations.

Innovation Solution

A method involving machine learning to derive a relational expression between physical property values and laminate configurations, using a database of theoretical, numerical, and actual measurement data to facilitate efficient design of composite material laminated structures, and a designing device to automate this process.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Extent of automation

If a design assistance method using relational expressions is used, then design automation is improved, but the method is limited because general relational expressions are not available

Engineering Contradiction:
Improvedesign automationVSAvoidapplicability to different structures
Core Design Contradiction:
Extent of automationVSAdaptability or versatility

Solution Approach 1:

The invention changes the approach from using fixed relational expressions to using machine learning models that can adapt to different parameters and structures. The system learns optimal laminate configurations by training on diverse datasets, enabling it to handle various composite material structures without requiring pre-defined relational expressions for each case.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The invention replaces the traditional mechanical/design-based approach of manually deriving relational expressions with an intelligent system using machine learning. This substitution allows the system to automatically learn complex relationships between laminate configurations and physical properties without requiring explicit mathematical formulations.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Manufacturing precision

If manual designing of laminate configuration is performed, then design precision can be achieved, but the designing process becomes arduous and time-consuming

Engineering Contradiction:
Improvelaminate configuration precisionVSAvoiddesign time
Core Design Contradiction:
Manufacturing precisionVSLoss of time

Solution Approach 1:

The invention performs preliminary actions by pre-training machine learning models on extensive datasets of laminate configurations and their physical properties. This pre-training enables the system to quickly provide accurate design recommendations without requiring time-consuming manual calculations or iterations during the actual design phase.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The invention creates a virtual model or copy of the design process through machine learning algorithms that simulate and learn from optimal laminate configurations. This digital copy allows rapid evaluation and optimization of design options without physical prototyping or extensive manual computation.

Inventive Principle:
Principle #26Copying

Data Source

PatentEP3960452B1Method for manufacturing composite material laminate structure, designing and manufacturing device for composite material laminate structure
Publication Date: 2026.02.25 MITSUBISHI ELECTRIC CORP
  • EP3960452B1 patent drawingFigure 1~2
  • EP3960452B1 patent drawingFigure 3~4
  • EP3960452B1 patent drawingFigure 5~6

AI summary

Provided is a method of designing a composite material laminated structure, the method including: a machine learning step of performing machine learning on a plurality of pieces of data each of which includes a pair of a physical property value of the composite material laminated structure and a laminate configuration of the composite material laminated structure, to obtain a relational expression depicting a relationship between the physical property value and the laminate configuration, the composite material laminated structure including a plurality of layers that are laminated; and a laminate configuration information calculation step of calculating, based on the relational expression and an objective value of the physical property value, laminate configuration information which is information of the laminate configuration that enables the objective value to be obtained.