Method for determining crack propagation characteristics of turbine engine rotor

A technology for cracks in turbine engines and rotors, applied in strength characteristics, testing of mechanical components, testing of machine/structural components, etc., can solve problems such as difficult identification of cracks and their size, difficulty in determining the location and size of cracks, etc., to achieve Determining the effect of strong ability and high precision

Active Publication Date: 2019-10-25
ZHEJIANG UNIV
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Problems solved by technology

The ultrasonic method can identify defects and cracks more sensitively, but due to the scattering and refraction of waves, it is difficult to determine the position and size of defects and cracks; the X-ray method can locate defects more accurately, but it is not sensitive to non-opening cracks. It is difficult to identify the crack and its size; the above-mentioned internal crack growth characteristics and surface crack growth internal characteristics can be determined with an accuracy of several millimeters, or even tens of millimeters, so that this problem is still only a qualitative analysis

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  • Method for determining crack propagation characteristics of turbine engine rotor
  • Method for determining crack propagation characteristics of turbine engine rotor

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Embodiment Construction

[0023] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0024] Such as figure 1 As shown, a method for determining the crack propagation characteristics of a turbine engine rotor specifically includes defect fabrication, forging blank fabrication of structural parts, test block design, test block fabrication, bench orthogonal fatigue test, establishment of corresponding relationship of all-focus phased array detection, CT 3D reconstruction detection correspondence establishment, test block fracture analysis, structural part fabrication, structural part defect identification, structural part fatigue test, structural part internal crack detection, structural part surface crack detection, structural part fracture analysis.

[0025] The defects constructed in the present invention are inclusions that are brittle in nature and weak in fatigue resistance, and are cylinders of a series of sizes (such as ...

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Abstract

The present invention discloses a method for determining crack propagation characteristics of a turbine engine rotor. The method comprises defect fabrication, structural member forging blank fabrication, test block design, test block fabrication, gantry orthogonal fatigue test, and full focus phased array detection correspondence establishment, CT three-dimensional reconstruction detection correspondence establishment, test block fracture analysis, structural parts fabrication, structural part defect identification, structural part fatigue test, structural part internal crack detection, structural part surface crack detection, structural part fracture analysis. The method solves the problem of determining location and size of defects and cracks. The method achieves the purpose of quantitative analysis of internal cracks and internal characteristics of surface cracks and achieves the purpose of mastering the crack propagation law and further achieving damage tolerance design. The methodhas strong crack propagation characteristics determination ability, and solves shortcomings of the existing crack propagation characteristics determination technology.

Description

technical field [0001] The invention belongs to the technical field for indicating or measuring workpiece characteristics, and specifically relates to a method for determining crack propagation characteristics of a turbine engine rotor. Background technique [0002] Due to material and processing factors, there are defects of a certain size (initial damage) in the structure. After the structure has been in service for a period of time, cracks are easy to initiate at the defect, and the crack expansion to a certain size will cause fatigue damage to the structure. Therefore, the service life of the structure with defects is much less than the low cycle fatigue design life. For the turbine engine rotor structure with harsh working conditions and high safety requirements, it is necessary to use the damage tolerance design method to analyze the crack growth process in the structural design and troubleshooting analysis, so as to achieve important parameters such as reasonable ove...

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Application Information

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IPC IPC(8): G01N23/046G01N3/08G01M13/00
CPCG01M13/00G01N3/08G01N21/91G01N23/046G01N2203/0005G01N2203/0066G01N2203/0073G01N2203/0298G01N2203/0641G01N2203/0682G01N2223/1016G01N2223/646
Inventor 吴英龙宣海军
Owner ZHEJIANG UNIV
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