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Magnetic Hysteresis Analysis for Non-Destructive Evaluation of Aircraft Structural Steels Cover

Magnetic Hysteresis Analysis for Non-Destructive Evaluation of Aircraft Structural Steels

Open Access
|Sep 2024

Figures & Tables

Fig. 1.

The main magnetization, the magnetic hysteresis loop, and the related magnetic characteristics [11]

Fig. 2.

The hysteresis loop changes for steel subjected to cold working or caused by the non-magnetic addition: soft (1) and hardened (2) steels [11]

Fig. 3.

Magnetic measurement system schemes, based on a) permeameter; b) attachable transducer: 1 – the tested object; 2 – magnetizing coil; 3 – yoke of the magnetic circuit; 4 – winding on the tested object for magnetic flux measurement; 5 – magnetic flux density sensor; 6 – movable pole of magnetic circuit.

Fig. 4.

Magnetic Analyzer of type MA-05: a) general view of electronic unit with PC screen; b) an example of measurement results as hysteresis loop with calculated magnetic characteristics

Fig. 5.

The KRM-Ts coercive force meter with attachable U-shaped core magnetic transducer and two calibration specimens of known coercive force

Fig. 6.

Attachable magnetic transducers for KRM-Ts type coercive force meter

Fig. 7.

Spherical and cylindrical gas containers of aircraft selected for NDT inspection

Fig. 8.

The scheme of measurements and results obtained: a) measuring points diagram; b) resulting coercive force distribution along the container length

Results of coercive force measurements

ContainerMaterialHcBAverage HcMin HcMax HcDifferenceDifference
type A/cmA/cmA/cmA/cmA/cm%
140HMA2217.816.318.82.513
40HMA2215.814.516.92.414
40HMA2215.714.316.52.213
240HA2014.614.215.31.17
40HA2015.114.6161.49
40HA2014.813.715.7213
340HA2013.512.8152.215
40HA2014.713.815.71.912
40HA2014.213.514.81.39
430HGSA2418.518.118.90.84
30HGSA2418.51818.90.95
30HGSA2419.118.819.50.74
Language: English
Page range: 1 - 12
Submitted on: Feb 28, 2024
Accepted on: Apr 22, 2024
Published on: Sep 11, 2024
In partnership with: Paradigm Publishing Services
Publication frequency: 4 issues per year

© 2024 Roman Solomakha, Valentyn Uchanin, published by ŁUKASIEWICZ RESEARCH NETWORK – INSTITUTE OF AVIATION
This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 License.