Composite Bonding via B-Staged Partial Cure

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Solution Overview

Problem

Conventional adhesive bonding methods for fiber-reinforced polymeric composites require surface preparation and can be hindered by contamination, leading to weak bonds and reliability issues, especially in aerospace applications where chemical bonding is essential for structural integrity.

Innovation Solution

A B-staged bonding method that partially cures composite substrates to a specific cure level (25%-70%) before bonding, allowing for chemical bonding between the matrix resin and adhesive without the need for surface preparation, thereby creating a robust and reliable bond.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If conventional adhesive bonding methods are used with surface preparation, then bond strength can be improved, but manufacturing complexity and time increase due to additional surface treatment steps

Engineering Contradiction:
Improvebond strengthVSAvoidmanufacturing complexity
Core Design Contradiction:
StrengthVSDevice complexity

Solution Approach 1:

The composite substrates are pre-conditioned to a specific moisture content range (3-12%) before bonding, which prepares the material in advance to achieve optimal bond strength without requiring additional surface treatment steps during the bonding process

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The invention changes the moisture content parameter of the composite substrate to a specific range (3-12%), which fundamentally alters the bonding mechanism to enable direct bonding without surface preparation while maintaining or improving bond strength

Inventive Principle:
Principle #35Parameter changes

2Reliability

If surface preparation steps are performed, then bonding reliability can be improved, but production time and productivity are reduced

Engineering Contradiction:
Improvebonding reliabilityVSAvoidproduction time
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The moisture conditioning is performed in advance on the composite substrates, allowing them to be ready for immediate bonding without waiting during the bonding process, thus maintaining reliability while reducing overall production time

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The invention extracts and eliminates the surface preparation step from the bonding process by using moisture-controlled substrates that can be bonded directly, removing the time-consuming intermediate step while preserving bonding reliability

Inventive Principle:
Principle #2Taking out (Extraction)

3Strength

If traditional bonding methods with mechanical fasteners are used, then structural integrity can be ensured, but weight increases and stress concentrations occur

Engineering Contradiction:
Improvestructural integrityVSAvoidcomponent weight
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The invention replaces mechanical fastening systems with a chemical adhesive bonding system that uses moisture-controlled composite substrates, eliminating the need for holes, fasteners, and associated stress concentrations while reducing overall component weight

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

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 method enhances mechanical properties such as lap shear strength and fracture toughness, providing a cohesive failure mode and improved handling of composite materials, while eliminating the need for surface treatment and reducing contamination risks.

Implementation Method 1

A B-staged bonding method that partially cures composite substrates to a specific cure level (25%-70%) before bonding, allowing for chemical bonding between the matrix resin and adhesive

Methodology Applied
Scientific EffectCuring: Chemical Bonding

Data Source

PatentEP2922685B1Bonding of composite materials
Publication Date: 2019.04.17 CYTEC IND INC
  • EP2922685B1 patent drawingFigure 1
  • EP2922685B1 patent drawingFigure 2
  • EP2922685B1 patent drawingFigure 3

AI summary

A composite bonding process is disclosed. At least one of two curable, resin-based composite substrates is partially cured to a degree of cure of at least 10% but less than 75% of full cure. The composite substrates are then joined to each other with a curable adhesive there between. Co-curing of the joined substrates is carried out to form a bonded composite structure, whereby the adhesive is chemically bonded to and mechanically diffused with the resin matrix of the composite substrates, resulting in a chemically bonded interface between the adhesive and each composite substrate. Furthermore, bonding can occur with the presence of contaminants on the joined surfaces.