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Fatigue crack propagation real-time monitoring method based on structure surface displacement field

A technology for fatigue crack growth and real-time monitoring, applied in measuring devices, optical testing flaws/defects, instruments, etc., can solve problems such as complex measurement process, small-scale yield, and difficulty in detecting crack tips, so as to improve test efficiency and shorten test time. Time, the effect of eliminating measurement errors

Active Publication Date: 2021-12-31
BEIHANG UNIV
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Problems solved by technology

However, during fatigue cyclic loading, the plastic zone at the crack tip will lead to small-scale yielding, resulting in the crack closure phenomenon
In the collected crack image, the gray level distribution of the closed area of ​​the crack is the same as that of the background, which makes it difficult to detect the real crack tip based on the gray level edge detection method
[0006] In summary, the traditional fatigue crack length measurement method has a complicated measurement process, and the measurement accuracy is difficult to guarantee; the existing method based on digital image processing is difficult to measure the real fatigue crack

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  • Fatigue crack propagation real-time monitoring method based on structure surface displacement field
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  • Fatigue crack propagation real-time monitoring method based on structure surface displacement field

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Embodiment Construction

[0026] The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0027] The present invention can realize the coordinate positioning of the fatigue crack tip, the measurement of the fatigue crack length and the real-time display of the fatigue crack propagation path during the fatigue crack propagation process. According to an embodiment of the present invention, a real-time monitoring of the fatigue crack propagation based on the structural surface displacement field method is further explained. Such as figure...

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Abstract

The invention relates to a fatigue crack propagation real-time monitoring method based on a structure surface displacement field, which comprises the following steps: (1), building a fatigue crack propagation test platform, and clearly displaying a crack monitoring area; (2), acquiring a fatigue crack propagation image; (3), calculating a surface displacement field of the test piece; (4), realizing fatigue crack tip positioning under different cycles; (5), carrying out crack length measurement under different cycles; and (6), displaying the crack propagation path in real time. According to the invention, real-time monitoring of fatigue crack propagation can be realized, the defect that the fatigue crack propagation test needs to measure the crack length through a termination test is overcome, and the efficiency of the fatigue crack propagation test is improved; a crack length measurement error caused by a crack closing phenomenon is eliminated, and the measurement precision of a macro-scale fatigue crack test is improved to a micron dimension; the method is high in measurement precision, high in response speed, simple to operate and wide in application range.

Description

technical field [0001] The invention relates to the technical field of aerospace engines, in particular to a method for real-time monitoring of fatigue crack growth and real-time measurement of fatigue crack length based on structural surface displacement field, which is a method capable of improving the detection efficiency of material mechanical properties and improving the accuracy of material fatigue life assessment Methods. Background technique [0002] Different types of damage (such as cracks, corrosion, pits, wear, etc.) often occur in the key components of aero-engines during their service, among which fatigue cracks are one of the most common forms of damage. Carrying out structural fatigue crack growth tests and exploring the fatigue fracture law of materials is of great significance to improving the reliability and service life of structures. Among them, the fatigue crack length is an important mechanical index to study the law of fatigue growth. Therefore, it ...

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Application Information

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IPC IPC(8): G01B11/02G01N21/88G01N21/95
CPCG01B11/02G01N21/8851G01N21/9515
Inventor 胡殿印赵炎毛建兴王荣桥
Owner BEIHANG UNIV