Composite Fiber Distortion Failure Probability Analysis

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Solution Overview

Problem

Current methods lack repeatable and consistent data for determining the impact of fiber distortions on the failure characteristics of composite materials, particularly in critical areas like helicopter rotor blade root ends, due to the absence of models specific to glass reinforced composites, leading to uncertain 'use as is' or 'scrap' dispositions.

Innovation Solution

A coupon fabrication technique with defined distortion is developed, along with a test protocol to determine the shape of the failure probability density curve, simulating marceled fibers and using comparative standard templates to analyze distortion severity and its impact on tensile strength, enabling informed decision-making and improved composite structure design.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If current fatigue and crack propagation models (Miners Rule, Birnbaum-Saunders) are used for composite anomalies, then analysis can be performed using existing metal-based models, but the models are not specific to glass reinforced composite materials and lack empirical data for failure curve determination

Engineering Contradiction:
Improveapplicability of existing modelsVSAvoidaccuracy for composite materials
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The patent changes the fundamental parameters of the analysis by developing new empirical models specifically for glass reinforced composite materials, transitioning from metal-based models to composite-specific models with appropriate failure curves and statistical parameters

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent creates composite-specific analysis models by combining empirical data from coupon testing with statistical methods, developing a hybrid approach that integrates experimental results with probabilistic failure analysis tailored to composite material behavior

Inventive Principle:
Principle #40Composite materials

2Measurement precision

If fiber distortion anomalies are detected in critical structural components, then the location and severity can be identified, but no repair is possible and disposition must be 'use as is' or 'scrap' due to lack of reliable failure data

Engineering Contradiction:
Improvedetection of fiber distortionsVSAvoidconfidence in disposition decisions
Core Design Contradiction:
Measurement precisionVSReliability

Solution Approach 1:

The patent establishes a feedback loop where coupon testing data informs disposition decisions for production components, creating a validated framework where empirical results from controlled experiments feed back into engineering judgments for actual structural assessments

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The patent performs preliminary action by conducting extensive coupon fabrication and testing beforehand to establish failure probability density curves and empirical data, so that when production components are assessed, reliable reference data is already available to guide disposition decisions

Inventive Principle:
Principle #10Preliminary action

3Ease of operation

If case-by-case evaluation is performed for each blade with fiber distortions, then individual assessments can be made, but the process lacks repeatable techniques and consistent data for engineering quality dispositions

Engineering Contradiction:
Improveflexibility in evaluationVSAvoidconsistency of disposition criteria
Core Design Contradiction:
Ease of operationVSManufacturing precision

Solution Approach 1:

The patent segments the evaluation process into standardized categories based on distortion severity, creating discrete classification levels that maintain consistency while allowing flexibility in application to different production scenarios

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent changes the evaluation approach from subjective case-by-case judgment to parameter-based assessment using empirical failure data and statistical parameters, transforming qualitative decisions into quantitative, repeatable engineering criteria

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentUS7509873B2Method and apparatus for failure probability density function determination
Publication Date: 2009.03.31 THE BOEING CO
  • US7509873B2 patent drawing
  • US7509873B2 patent drawing
  • US7509873B2 patent drawing

AI summary

A coupon fabrication with defined distortion in the form of marceled fibers and test protocol is employed to determine the shape of the failure probability density curve to improve the analyses of the risk of fiber distortion anomalies in composite structures. This protocol provides a method to determine the probability of and the severity of the various distorted fiber conditions that might exist on composite structure in fabrication and in service. A distortion characterization matrix is established for determining test shapes and providing defect characterization based on the results of tests on the selected shapes. Coupons for test are created using resin pool.