Thermographic Component Evaluation for Remaining Service Life Prediction

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Solution Overview

Problem

Existing non-destructive testing methods for aircraft power plant components do not effectively predict the future performance or service life of components with internal defects such as cracks and voids, despite providing insights into structural integrity.

Innovation Solution

A method using infrared thermography combined with mechanical excitation and machine learning to quantify the remaining service life of components by analyzing thermographic images, where a machine learning algorithm is trained on historical data associating previous images with service lives.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of information

If existing non-destructive testing methods are used to inspect component structural integrity, then defects can be detected, but the future performance and remaining service life of the component cannot be predicted

Engineering Contradiction:
Improveinformation on future performanceVSAvoidprediction accuracy
Core Design Contradiction:
Loss of informationVSReliability

Solution Approach 1:

The system performs preliminary mechanical excitation and thermal imaging before the component reaches its failure point, capturing thermographic data that correlates with remaining service life. This allows prediction of future performance based on current thermal response characteristics, rather than waiting for actual failure or using post-failure analysis.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent replaces traditional mechanical testing methods that require actual stress loading with a thermal imaging-based assessment system. By using mechanical excitation to induce thermal responses and analyzing these responses through machine learning, the system substitutes direct mechanical performance testing with a non-intrusive thermal field measurement approach.

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

2Measurement precision

If mechanical excitation is applied to induce thermal response for thermographic imaging, then remaining service life can be estimated, but additional equipment and process complexity are required

Engineering Contradiction:
Improveremaining service life estimationVSAvoidtesting system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The mechanical excitation device serves multiple functions: it provides structural support for the component, applies controlled excitation forces to induce thermal responses, and acts as a mounting platform for sensors. This multi-functionality reduces the need for separate dedicated testing equipment, thereby reducing overall system complexity despite the advanced measurement capabilities.

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The component itself serves as the test object and the source of information. By using the component's own thermal response to mechanical excitation as the measurement signal, the system eliminates the need for external test specimens, artificial defects, or complex simulation setups. The component's natural thermal behavior under excitation provides the necessary data for service life prediction.

Inventive Principle:
Principle #25Self-service

3Measurement precision

If thermographic imaging is used to capture thermal responses, then defect characteristics can be identified, but the location and type of defects affect the accuracy of remaining service life prediction

Engineering Contradiction:
Improvedefect detection accuracyVSAvoiddefect characterization difficulty
Core Design Contradiction:
Measurement precisionVSDifficulty of detecting and measuring

Solution Approach 1:

The patent introduces thermal response patterns as an intermediary between the physical defect and the remaining service life prediction. Instead of directly measuring defect geometry or material properties, the system captures thermal wave propagation patterns that are influenced by defect characteristics. These thermal patterns serve as mediators that encode defect information in a form that machine learning algorithms can process to predict service life, bypassing the difficulty of direct defect characterization.

Inventive Principle:
Principle #24Intermediary (Mediator)

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

Enables accurate estimation of the health condition and remaining service life of components, improving reliability in non-destructive testing and health monitoring by predicting future performance based on thermal responses induced by mechanical excitation.

Implementation Method 1

Mechanically exciting the component may include inducing frictional heating at the defect.

Methodology Applied
Scientific EffectFrictional heating: Friction

Implementation Method 2

acquiring at a computer from an infrared sensor a thermographic image of a part of the component containing the defect and taken while the component exhibits the thermal response

Methodology Applied
Scientific EffectThermal response: Thermal Radiation

Data Source

PatentUS20260065451A1System and method for evaluating components using thermography
Publication Date: 2026.03.05 PRATT & WHITNEY CANADA CORP
  • US20260065451A1 patent drawing
  • US20260065451A1 patent drawing
  • US20260065451A1 patent drawing

AI summary

Systems and methods for non-destructive evaluation of components using infrared thermography are provided. A method includes mechanically exciting the component, and using an infrared sensor to acquire a thermographic image of part of the component containing a defect. Using a machine learning algorithm, a health condition of the component is determined based on the new thermographic image. The machine learning algorithm is trained using machine learning and historical data associating previous thermographic images with previous remaining service lives for the component.