Infrared Sensor Thermal Data Machine Learning Crack Detection

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Solution Overview

Problem

Current methods for detecting defects, such as cracks, in aircraft structures under repetitive stress are time-consuming and expensive, often requiring manual inspection and back-calculations to estimate defect onset, which are not efficient or timely.

Innovation Solution

A system utilizing an infrared sensor to monitor structural components and process thermal data with machine learning models, specifically unsupervised and supervised techniques, to detect the onset and propagation of cracks, providing automated and timely defect identification.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If manual inspection and back-calculations are used to detect defects, then defect detection can be performed, but the process is time-consuming and expensive

Engineering Contradiction:
Improvedefect detection capabilityVSAvoidinspection time
Core Design Contradiction:
Measurement precisionVSLoss of time

Solution Approach 1:

The patent replaces manual mechanical inspection methods with an automated optical sensing system. An infrared sensor captures thermal data from the structure during fatigue cycling, and a processor automatically analyzes the thermal data to detect defects. This substitution eliminates the need for manual inspection and back-calculations, significantly reducing inspection time while maintaining defect detection capability.

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

2Measurement precision

If manual inspection methods are used, then defect detection is possible, but highly skilled engineers are required making the process expensive

Engineering Contradiction:
Improvedefect detection capabilityVSAvoidcost-effectiveness
Core Design Contradiction:
Measurement precisionVSEase of manufacture

Solution Approach 1:

The system enables self-service defect detection by automatically capturing thermal data during fatigue cycling and processing it through machine learning models. The processor independently identifies defects without requiring highly skilled engineers to perform manual inspection and back-calculations. This automation reduces dependency on expensive expert personnel while maintaining accurate defect detection.

Inventive Principle:
Principle #25Self-service

3Measurement precision

If traditional inspection methods are used, then defects can be detected, but it is rare to discover a defect at the moment it occurred

Engineering Contradiction:
Improvedefect detection capabilityVSAvoidtiming information of defect onset
Core Design Contradiction:
Measurement precisionVSLoss of information

Solution Approach 1:

The system performs preliminary action by continuously monitoring the structure with infrared sensing during fatigue cycling before defects propagate to detectable sizes. The thermal data is captured in real-time during the fatigue process, allowing defects to be detected at or near their onset moment rather than at later stages during periodic inspections. This preserves the timing information of when defects occurred.

Inventive Principle:
Principle #10Preliminary action

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

The system enables automated and efficient detection of crack onset and propagation, reducing the need for manual inspection and back-calculations, thereby improving the speed and cost-effectiveness of defect identification in aircraft structures.

Implementation Method 1

monitoring the structure with an infrared sensor to provide thermal data of the structure within a field of view of the infrared sensor

Methodology Applied
Scientific EffectInfrared radiation detection: Infrared Radiation

Data Source

PatentUS11314906B2System and method for detecting defects in structures subject to repetitive stress
Publication Date: 2022.04.26 GULFSTREAM AEROSPACE CORP
  • US11314906B2 patent drawing
  • US11314906B2 patent drawing
  • US11314906B2 patent drawing

AI summary

Exemplary embodiments of a system and method are provided for detecting cracks and crack propagation in aircraft structures subject to repetitive stress. A method for detecting onset or propagation of defects in a structure includes monitoring the structure with an infrared sensor to provide thermal data of the structure within a field of view of the infrared sensor. A processor is used to process the thermal data memory to extract features from the thermal data and utilize at least one machine learning model to detect onset or propagation of defects in the structure. A system includes an infrared sensor having a field of view of the structure and a processor coupled to the infrared sensor and a memory, which contains instructions that cause the processor to process thermal data from the infrared sensor to extract features from the thermal data and utilize at least one machine learning model to detect onset or propagation of the defects in the structure.