Related Experiment Video
Updated: Jun 30, 2026

Fabrication and Characterization of a Conformal Skin-like Electronic System for Quantitative, Cutaneous Wound Management
Published on: September 2, 2015
Research on Alternating Current Field Measurement Method for Buried Defects of Titanium Alloy Aircraft Skin
Chunhui Liao1, Ruize Wang1, Cheng Lv2
1Hubei Key Laboratory of Modern Manufacturing Quantity Engineering, School of Mechanical Engineering, Hubei University of Technology, Wuhan 430068, China.
A new alternating current field measurement probe effectively detects surface and buried defects in titanium alloy aircraft skins. This technology identifies cracks as small as 3mm long and 2mm deep, ensuring aircraft structural integrity.
Area of Science:
- Materials Science
- Aerospace Engineering
- Non-Destructive Testing
Background:
- Titanium alloys are critical for aerospace components like engines and structures.
- Aircraft skins face degradation from corrosion and stress, leading to cracks and defects.
- Effective detection of these defects is crucial for flight safety.
Purpose of the Study:
- To design and validate an alternating current field measurement (ACFM) probe for detecting surface and buried defects in thin-walled titanium alloy plates.
- To investigate the impact of defect characteristics and excitation frequency on ACFM signals.
- To optimize the ACFM probe for enhanced sensitivity and reliability in detecting flaws in aircraft skins.
Main Methods:
- Development of an ACFM detection probe based on alternating current field measurement principles.
- Establishment of a finite element simulation model using COMSOL 5.6 for TC4 titanium alloy plates with buried defects.
- Systematic investigation of defect length, depth, and excitation frequency effects on characteristic ACFM signals.
- Optimization of the detection probe design through simulation and experimental validation.
Main Results:
- The ACFM probe demonstrated high sensitivity to varying lengths and depths of buried defects.
- Successfully detected small cracks (3 mm length, 2 mm depth) and deeper flaws (10 mm length, 4 mm depth).
- Simulation and experimental data confirmed the probe's effectiveness in identifying subsurface flaws.
Conclusions:
- The designed ACFM probe is a viable tool for detecting both surface and buried defects in thin-walled titanium alloy structures.
- The study confirms the probe's capability to identify critical flaws in aircraft skins, enhancing safety and maintenance protocols.
- This ACFM technology offers a promising solution for non-destructive evaluation in the aerospace industry.
More Related Videos
11:34Subsurface Defect Localization by Structured Heating Using Laser Projected Photothermal Thermography
Published on: May 15, 2017
12:18Co-localizing Kelvin Probe Force Microscopy with Other Microscopies and Spectroscopies: Selected Applications in Corrosion Characterization of Alloys
Published on: June 27, 2022
Related Concept Videos
Calculation of Electric Flux
Electronic Distance Measuring Instruments