Composite Tape Layup Guard Bands for Undetected Gap Anomalies

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Solution Overview

Problem

Existing manufacturing processes for composite parts, such as aircraft panels, fail to accurately account for anomalies like whiskers and missing fiber due to poly backing, leading to unnecessary rework and potential nonconformance, as automated optical inspection systems often miss these issues.

Innovation Solution

A method and system using a two-stage hurdle model and bootstrapping to simulate anomaly data, calculating guard bands that account for undetected whiskers and missing fiber, ensuring compliance with manufacturing requirements with a known confidence level.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Extent of automation

If automated optical inspection systems are used to inspect preform layers, then inspection speed and automation are improved, but measurement precision deteriorates because the systems cannot detect undetected anomalies like whiskers and missing fiber

Engineering Contradiction:
Improveautomation of inspectionVSAvoiddetection of anomalies
Core Design Contradiction:
Extent of automationVSMeasurement precision

Solution Approach 1:

The inspection approach is segmented into two stages: automated optical inspection for rapid screening of obvious defects, and statistical guard band analysis for accounting for undetected anomalies. This segmentation allows each method to operate in its optimal domain while compensating for the other's limitations.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

A statistical guard band model acts as an intermediary between the automated inspection system and the final quality decision. The model incorporates anomaly data from historical processes to compensate for the inspection system's inability to detect certain defects, thereby bridging the gap between automated screening and precise quality assurance.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Manufacturing precision

If strict specification limits are enforced based on automated inspection results, then manufacturing precision is improved, but productivity deteriorates due to unnecessary rework of parts that would have been acceptable

Engineering Contradiction:
Improvecompliance with specificationVSAvoidproduction efficiency
Core Design Contradiction:
Manufacturing precisionVSProductivity

Solution Approach 1:

The guard band is calculated in advance based on historical anomaly data and inspection system characteristics. This preliminary statistical adjustment allows the inspection criteria to be optimized before production, preventing overly strict rejection criteria that would cause unnecessary rework while ensuring adequate quality control.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The inspection acceptance criteria are adjusted by incorporating a statistical guard band parameter that accounts for undetected anomalies. This parameter modification transforms the rigid specification limit into a more nuanced acceptance threshold that balances quality assurance with production efficiency.

Inventive Principle:
Principle #35Parameter changes

3Reliability

If retroactive rework is performed on parts with detected anomalies, then product quality is improved, but loss of time increases due to post-inspection rework

Engineering Contradiction:
Improveproduct qualityVSAvoidrework time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The guard band calculation and anomaly modeling are performed preliminarily based on historical data, allowing the inspection system to be properly calibrated before production begins. This prevents the need for time-consuming retroactive rework by ensuring that inspection criteria accurately reflect actual quality risks from the outset.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS20250387988A1Automated tape laying machine panel manufacture with guard bands
Publication Date: 2025.12.25 THE BOEING CO
  • US20250387988A1 patent drawing
  • US20250387988A1 patent drawing
  • US20250387988A1 patent drawing

AI summary

Techniques for manufacturing a composite part using a tape laying process are presented. The techniques can include: laying up a preform layer from composite tape; inspecting the preform layer for gaps; comparing the gap measurement with a gap guard band, where the gap guard band is determined by: obtaining anomaly data that includes measurements of fiber that has not been deposited on a respective preform during prior preform lay-up processes; fitting a multi-component model to the anomaly data; simulating a preform manufacture based on the multi-component model; calculating summary statistics on gap width accounting for undetected anomalies; and determining a guard band based on the summary statistics on gap width accounting for undetected anomalies and based on a manufacturing requirement; determining that the preform layer complies with the manufacturing requirement; repeating the laying up, the inspecting, the comparing, and the determining; and heating the preform to form a composite part.