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Non-destructive testing of steel products - Method for ultrasonic testing of torsional residual stress distribution of shaft
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GB/T 43900-2024
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Basic data Standard ID | GB/T 43900-2024 (GB/T43900-2024) | Description (Translated English) | Non-destructive testing of steel products - Method for ultrasonic testing of torsional residual stress distribution of shaft | Sector / Industry | National Standard (Recommended) | Classification of Chinese Standard | H26 | Classification of International Standard | 77.040.20 | Word Count Estimation | 10,184 | Date of Issue | 2024-04-25 | Date of Implementation | 2024-11-01 | Issuing agency(ies) | State Administration for Market Regulation, China National Standardization Administration |
GB/T 43900-2024: Non-destructive testing of steel products - Method for ultrasonic testing of torsional residual stress distribution of shaft ---This is a DRAFT version for illustration, not a final translation. Full copy of true-PDF in English version (including equations, symbols, images, flow-chart, tables, and figures etc.) will be manually/carefully translated upon your order.
ICS 77:040:20
CCSH26
National Standards of People's Republic of China
Nondestructive testing of steel products - Torsional residual stress in shaft components
Ultrasonic testing method for distribution status
Released on 2024-04-25
2024-11-01 Implementation
State Administration for Market Regulation
The National Standardization Administration issued
Foreword
This document is in accordance with the provisions of GB/T 1:1-2020 "Guidelines for standardization work Part 1: Structure and drafting rules for standardization documents"
Drafting:
Please note that some of the contents of this document may involve patents: The issuing organization of this document does not assume the responsibility for identifying patents:
This document was proposed by the China Iron and Steel Association:
This standard is under the jurisdiction of the National Technical Committee on Steel Standardization (SAC/TC183):
This document was drafted by: Beijing Institute of Technology, China Petroleum Materials Co:, Ltd:, Deyang Product Quality Supervision and Inspection Institute, CRRC Yongji Electric
Machinery Co:, Ltd:, Metallurgical Industry Information Standards Research Institute, Inner Mongolia First Machinery Group Co:, Ltd:, China Ordnance Science Research Institute Ningbo
Branch, Beijing North Vehicle Group Co:, Ltd:, Shanxi Diesel Engine Industry Co:, Ltd:, AECC Shenyang Liming Aero-Engine Co:, Ltd:
Company, China Energy Group Science and Technology Research Institute Co:, Ltd:, CRRC Tangshan Locomotive and Rolling Stock Co:, Ltd:, Jinan Second Machine Tool Group Co:, Ltd:
company:
The main drafters of this document are: Xu Chunguang, Guo Jianguang, Song Wenyuan, Xie Dong, Liu Haining, Dong Li, Li Peilu, Yin Peng, Shan Zhipeng, Bai Long, Li Zhe,
Deng Tao, Zhang Yunlong, Sun Dong, He Chi, Zhang Yafeng, Sun Mingxue, Xue Jianzhong, Li Hongwei, Liu Shiyuan, Dong Dexiu, Li Yang, Xu Hongjiang, Li Zongqiang,
Lu Yuren, Guo Jianlong, Zhang Guangxiang, Yang Guangcan, and Li Shuangyi:
Nondestructive testing of steel products - Torsional residual stress in shaft components
Ultrasonic testing method for distribution status
1 Scope
This document specifies the general requirements, testing equipment, test specimens, testing methods, and testing methods for ultrasonic testing of torsional residual stress distribution in shaft components:
Test procedures and test reports:
This document is applicable to ultrasonic testing of steel shaft components in the torsional residual stress distribution state with a frequency range of 0:1MHz~20:0MHz:
The non-destructive testing and monitoring of the service torsional stress of shaft components caused by external loads can refer to this document:
The parts can also be used for reference:
2 Normative references
The contents of the following documents constitute the essential clauses of this document through normative references in this document:
For referenced documents without a date, only the version corresponding to that date applies to this document; for referenced documents without a date, the latest version (including all amendments) applies to
This document:
GB/T 228:1 Tensile test of metallic materials Part 1: Room temperature test method
GB/T 7232 Terminology for heat treatment of metals
GB/T 9445 Qualification and certification of non-destructive testing personnel
GB/T 10128 Room temperature torsion test method for metallic materials
GB/T 12604:1 Nondestructive testing terminology Ultrasonic testing
GB/T 27664:1 Non-destructive testing - Performance and inspection of ultrasonic testing equipment - Part 1: Instrument
GB/T 32073 Nondestructive testing of residual stress by ultrasonic critical refraction longitudinal wave testing method
GB/T 38811 Acoustic beam control method for residual stress in metallic materials
3 Terms and definitions
The terms and definitions defined in GB/T 7232 and GB/T 12604:1 and the following apply to this document:
3:1
The stress distributed along a certain angle within a certain depth range on the surface of a shaft component:
Note: Commonly used detection angles are 0°, 45°, and 90°:
4 Detection Principle
According to Snel's law, in order to generate and receive ultrasonic critical refracted longitudinal waves inside the surface of the shaft component being tested, the detection probe can
The surface is placed in a direction at any angle to the axis, as shown in Figure 1a): According to the principle of acoustic elasticity, when the residual stress direction of the shaft component
When the direction is consistent with the longitudinal wave, tensile stress slows down the propagation speed of ultrasonic waves or prolongs the propagation time (t), while compressive stress speeds up the propagation speed of ultrasonic waves:
Or the propagation time (t) is shortened: If the ultrasonic propagation time (t0) in the shaft component with zero stress (σ0) is known, the ultrasonic propagation time (t0) of the shaft component under test can be calculated based on the time difference:
The residual stress (σ) in the component is calculated by formula (1):
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