Composite Monolithic Fabrication With Two-Stage Air-Free Curing

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Solution Overview

Problem

Current methods for fabricating composite monolithic structures incorporate air, which is detrimental to achieving high electrical or mechanical performance parameters, and involve complex process conditions, leading to poor reliability and premature failure under high stress applications.

Innovation Solution

The method involves coating an insulating layer with an uncured binding material, performing a first stage curing process to form a non-tacky binding material, and then disposing the insulating layer on an array of conductive structures. A second stage curing process is performed to form fully cured regions between adjacent conductive structures, effectively eliminating air pockets and enhancing bonding strength.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If current fabrication methods are used, then the process is simpler, but air is incorporated into the composite structure which deteriorates electrical and mechanical performance

Engineering Contradiction:
Improvecomposite structure performanceVSAvoidfabrication process complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The curing process is segmented into multiple stages: an initial curing stage followed by a final curing stage. This segmentation allows air to be removed during the initial stage while the resin maintains sufficient viscosity to prevent re-entrainment, and then allows complete curing in the final stage to achieve optimal mechanical properties without air pockets.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The initial curing stage performs a preliminary action by partially curing the resin before the structure is subjected to high stress or final assembly. This preliminary curing establishes a viscous state that prevents air entrapment while allowing subsequent complete curing to achieve full performance.

Inventive Principle:
Principle #10Preliminary action

2Reliability

If current fabrication methods are used, then processing is faster, but the composite structure exhibits poor reliability under high stress

Engineering Contradiction:
Improvereliability under high stressVSAvoidprocessing time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The curing process is divided into distinct stages with specific objectives: initial curing removes air and establishes viscosity control, while final curing achieves complete polymerization. This segmentation ensures air-free composite structures with optimal mechanical properties, preventing premature failure under high stress despite increased processing time.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The resin's physical and chemical parameters are dynamically controlled during different curing stages. During initial curing, temperature and time parameters are optimized to achieve a viscous state that prevents air entrapment. During final curing, parameters are adjusted to complete polymerization and achieve optimal mechanical strength for high stress applications.

Inventive Principle:
Principle #35Parameter changes

3Ease of manufacture

If air is incorporated in the composite structure, then fabrication is easier, but electrical and mechanical performance parameters are deteriorated

Engineering Contradiction:
Improvefabrication easeVSAvoidelectrical and mechanical performance
Core Design Contradiction:
Ease of manufactureVSManufacturing precision

Solution Approach 1:

The manufacturing process is segmented into initial curing and final curing stages. The initial curing stage creates a viscous resin state that prevents air entrapment during consolidation, while the final curing stage achieves complete polymerization. This segmentation simultaneously improves ease of manufacture by allowing controlled air removal and achieves manufacturing precision by eliminating air pockets that would deteriorate electrical and mechanical performance.

Inventive Principle:
Principle #1Segmentation

4Loss of time

If a single-stage curing process is used, then processing time is reduced, but air pockets remain in the composite structure

Engineering Contradiction:
Improvecuring process timeVSAvoidcomposite structure integrity
Core Design Contradiction:
Loss of timeVSReliability

Solution Approach 1:

The curing process is segmented into two distinct stages: initial curing at controlled conditions to achieve a viscous state that prevents air entrapment, and final curing to complete polymerization. This segmentation ensures complete air removal and optimal composite structure integrity, accepting that total processing time is divided into two stages rather than one accelerated stage.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Curing parameters (temperature, time, pressure) are changed between stages. During initial curing, parameters are set to achieve a specific viscosity range that prevents air re-entrainment. During final curing, parameters are adjusted to complete the polymerization reaction and achieve optimal mechanical and electrical properties, ensuring air-free composite structures.

Inventive Principle:
Principle #35Parameter changes

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 results in composite structures with improved reliability, higher performance, and lower life-cycle costs, while also simplifying the fabrication process with reduced processing time and costs.

Implementation Method 1

performing a first stage curing process on the uncured binding material to form a first stage cured binding material on the insulating layer

Methodology Applied
Scientific EffectCuring process: Phase Change

Implementation Method 2

performing a second stage curing process on the first stage cured binding material to form a second stage cured binding material

Methodology Applied
Scientific EffectCuring process: Phase Change

Data Source

PatentUS20250037915A1Method of fabrication of composite monolithic structures
Publication Date: 2025.01.30 THE MITRE CORPORATION
  • US20250037915A1 patent drawing
  • US20250037915A1 patent drawing
  • US20250037915A1 patent drawing

AI summary

Fabricating composite monolithic structures to achieve optimal electrical, thermal, and mechanical properties through the elimination of air is discussed herein. A method of fabricating a composite structure includes coating an insulating layer with an uncured binding material and performing a first curing process on the uncured binding material to form a first stage cured binding material on the insulating layer without introduction of air pockets in a conventional manufacturing atmospheric environment. The method further includes disposing the insulating layer on an array of conductive structures. The first stage cured binding material is positioned between the insulating layer and the array of conductive structures. The method further includes performing a second curing process on the first stage cured binding material to form a cured binding material, and forming cured regions between adjacent conductive structures of the array of conductive structures.