Composite Curing Simulation Optimizes Residual Stress Profiles

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Solution Overview

Problem

Current methods for manufacturing composite materials are inefficient and costly due to the lack of precise control over the curing process, leading to residual stresses and distortions in composite components, particularly in large structures like aircraft wings and wind turbine blades, which results in premature failure and increased production time.

Innovation Solution

A processor-implemented simulation system that uses machine learning models and finite element analysis to optimize the curing process by identifying the most influencing parameters and iteratively adjusting process cycle parameters to minimize residual stresses and deformations, generating optimized temperature profiles for each thermal zone in the manufacturing setup.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If conventional curing processes are used without optimization, then manufacturing is simpler and faster to implement, but residual stresses and distortions increase leading to premature failure

Engineering Contradiction:
Improvecomponent durabilityVSAvoidprocess complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The system performs preliminary computational analysis and optimization of the curing process before actual manufacturing. By simulating and optimizing cure cycles, temperature distributions, and resin flow patterns in advance, the system determines optimal processing parameters that minimize residual stresses and distortions, thereby improving component reliability without adding complexity during the actual manufacturing execution.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system creates a digital twin or virtual model of the curing process that replicates the physical manufacturing conditions. This computational copy allows for extensive optimization and analysis without affecting the actual manufacturing process, enabling determination of optimal parameters that enhance reliability while keeping the physical process simple.

Inventive Principle:
Principle #26Copying

2Manufacturing precision

If extensive experimental testing is conducted to optimize cure cycles, then manufacturing precision improves, but production time and costs increase significantly

Engineering Contradiction:
Improvedimensional accuracyVSAvoiddevelopment time
Core Design Contradiction:
Manufacturing precisionVSLoss of time

Solution Approach 1:

The system replaces extensive physical experimental testing with computational simulations and numerical models. By using finite element analysis and computational fluid dynamics to model the curing process, the system can predict and optimize dimensional accuracy, residual stress distribution, and cure completeness without requiring numerous physical prototypes and tests, thereby achieving high manufacturing precision while dramatically reducing development time.

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

Solution Approach 2:

The system systematically varies and optimizes processing parameters such as temperature profiles, heating rates, and pressure conditions through computational analysis. This allows for precise control over the curing process to achieve optimal dimensional accuracy and minimize defects, all through virtual experimentation rather than time-consuming physical testing.

Inventive Principle:
Principle #35Parameter changes

3Manufacturing precision

If uniform heating is applied during curing, then the process is simpler to control, but thermal gradients cause resin shrinkage and distortion

Engineering Contradiction:
Improvedimensional fidelityVSAvoidthermal control complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The system implements spatially varying temperature distributions during the curing process, applying different heating rates and temperature levels to different regions of the composite component. By analyzing the specific geometry, fiber orientation, and thickness variations of each region, the system optimizes local thermal conditions to minimize thermal gradients, reduce resin shrinkage, and prevent distortion, thereby achieving high dimensional fidelity while managing thermal control complexity through intelligent regional differentiation.

Inventive Principle:
Principle #3Local quality

4Productivity

If fast curing cycles are used to increase productivity, then production time decreases, but residual stresses increase leading to component failure

Engineering Contradiction:
Improveproduction rateVSAvoidcomponent strength
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

The system employs dynamic and adaptive curing cycles that adjust temperature and pressure parameters in real-time based on the specific component geometry, material properties, and desired quality outcomes. By using computational models to optimize the time-temperature-history, the system achieves fast curing rates that maximize productivity while simultaneously controlling thermal gradients and stress development to maintain component strength and reliability, replacing static conventional cycles with dynamically optimized processes.

Inventive Principle:
Principle #15Dynamics

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This approach reduces the need for extensive experimental testing, minimizes residual stresses and deformations, and enhances the durability of composite components by optimizing the curing process, thereby improving the quality and reducing production time and costs.

Implementation Method 1

During the manufacturing process, heat is applied to composite material which causes the shrinkage in polymer matrix due to thermal effects or cure effects or both depending on the type of polymer

Methodology Applied
Scientific EffectThermal shrinkage: Thermal Contraction

Implementation Method 2

Thermoset polymers, commonly referred as resins, when subjected to cure temperature cycle, undergo exothermic transformation and form cross linking bonds

Methodology Applied
Scientific EffectExothermic transformation: Exothermic Reaction

Data Source

PatentUS11893326B2Systems and methods for generating molded parts comprising reinforced composite materials
Publication Date: 2024.02.06 TATA CONSULTANCY SERVICES LTD
  • US11893326B2 patent drawing
  • US11893326B2 patent drawing
  • US11893326B2 patent drawing

AI summary

Conventionally, manufacturing of molded parts using composite materials has led to poor dimensional accuracy and tensile strength due to improper curing thus resulting in rejection or early/premature failure of composite part. Embodiments of the present disclosure provide simulation-based systems and methods for manufacturing/generating molded parts using reinforced composite materials. The optimized cure cycle is computed for a given component without carrying out numerous experiments. The present disclosure implements multiscale method and surrogate modeling in virtual testing for more accurate and faster manufacturing of molded parts. Process parameters for specified qualities (e.g., minimum residual stresses, minimum deformation, etc.) required for a part are determined along with least process manufacturing time. The resulting optimized time dependent cure cycle for each thermal zone of the heated mold is transferred to a master controller (e.g., system) which controls the entire curing processes with the use of feedback control.