Composite Pre-Bond Surface Inspection Using Peel Ply Markers

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Solution Overview

Problem

The existing methods for preparing composite structures for bonding often result in weak surface bonding due to incomplete removal of peel ply residue, which is time-consuming and costly to inspect, and require supplementary surface treatments like abrasion or plasma to ensure bonding quality.

Innovation Solution

Incorporating an identifiable marking agent into the peel ply, which is visible upon transfer to the composite substrate, allowing for easy inspection of residue presence and subsequent ablation to ensure a clean surface for bonding.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If supplementary ablation surface treatment is applied after peel ply removal, then bonding strength is improved, but processing time and cost increase

Engineering Contradiction:
Improvebonding strengthVSAvoidprocessing time
Core Design Contradiction:
StrengthVSLoss of time

Solution Approach 1:

The peel ply is pre-treated with an identifiable marking agent before bonding, allowing residue to be easily detected after removal. This preliminary marking enables targeted ablation only where residue exists, rather than requiring blanket surface treatment of the entire bonding area, thus reducing processing time while maintaining bonding strength.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The marking agent on the peel ply automatically transfers to the composite surface during the peeling process, providing self-indication of residue locations. This eliminates the need for separate inspection procedures and enables operators to perform selective ablation only where needed, reducing overall processing time and cost.

Inventive Principle:
Principle #25Self-service

2Strength

If supplementary ablation surface treatment is applied after peel ply removal, then bonding strength is improved, but processing cost increases

Engineering Contradiction:
Improvebonding strengthVSAvoidprocessing cost
Core Design Contradiction:
StrengthVSEase of manufacture

Solution Approach 1:

The marking agent provides automatic visual indication of residue presence and location during the peeling process. This self-indicating system eliminates the need for expensive separate inspection equipment and procedures, allowing operators to perform cost-effective selective ablation only where residue is detected, thereby reducing overall manufacturing costs while ensuring bonding quality.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The marking agent system replaces expensive mechanical or optical inspection systems with a simple visual indication method. The transferred marking provides immediate, clear visibility of residue locations, eliminating the need for complex inspection equipment and reducing processing costs while maintaining bonding strength through targeted treatment.

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

3Reliability

If inspection of pre-bond surface for residue is performed, then bonding quality is ensured, but inspection time and cost increase

Engineering Contradiction:
Improvebonding qualityVSAvoidinspection time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The identifiable marking agent undergoes a color or visual change when transferred to the composite surface during peeling. This visual transformation provides immediate, clear indication of residue presence and location, enabling rapid inspection without time-consuming analytical procedures. Operators can quickly identify and treat only the affected areas, ensuring bonding quality while minimizing inspection time.

Inventive Principle:
Principle #32Color changes

Solution Approach 2:

The marking agent on the peel ply automatically transfers to the composite surface during the peeling process, providing self-indication of residue locations. This eliminates the need for separate, time-consuming inspection procedures and enables operators to quickly identify areas requiring treatment, thereby ensuring bonding quality while significantly reducing inspection time.

Inventive Principle:
Principle #25Self-service

4Productivity

If peel ply residue is not completely removed, then processing time is reduced, but bonding strength decreases

Engineering Contradiction:
Improveprocessing speedVSAvoidbonding strength
Core Design Contradiction:
ProductivityVSStrength

Solution Approach 1:

The marking agent provides automatic visual indication of residue presence during and after the peeling process. This allows operators to quickly identify areas where residue remains and perform targeted ablation only where needed, rather than requiring complete removal of residue from the entire surface. This selective approach maintains bonding strength while minimizing additional processing time.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The marking agent system replaces time-consuming complete surface inspection and treatment with a simple visual indication method. Operators can rapidly identify residue locations through the transferred marking and perform focused ablation only where necessary, ensuring bonding strength is maintained while minimizing the time required for residue removal and surface preparation.

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 facilitates efficient identification and removal of peel ply residue, enhancing bonding strength and durability while reducing inspection and treatment costs by providing a visible marker for residue detection and ablation.

Implementation Method 1

ablating the modified surface to remove the identifiable marking agent and the residue

Methodology Applied
Scientific EffectAblation: Ablation

Data Source

PatentEP2921290B1Method for inspecting a pre-bond surface of a composite structure
Publication Date: 2018.09.12 THE BOEING CO
  • EP2921290B1 patent drawingFigure 1~2
  • EP2921290B1 patent drawingFigure 3
  • EP2921290B1 patent drawingFigure 4

AI summary

A composite structure (10) may include a composite substrate (12), the composite substrate (12) including a surface (24), a peel ply (14), the peel ply (14) including a surface (44), and an identifiable marking agent (32, 52, 54), wherein the surface (44) of the peel ply (14) includes the identifiable marking agent (32, 52, 54), and wherein the peel ply (14) is connected to the composite substrate (12) such that the identifiable marking agent (32, 52, 54) is in contact with the surface (24) of the composite substrate (12).