CN113053471B - Method for nondestructive on-line detection of Brinell hardness of fan spindle - Google Patents

Method for nondestructive on-line detection of Brinell hardness of fan spindle Download PDF

Info

Publication number
CN113053471B
CN113053471B CN202110303247.0A CN202110303247A CN113053471B CN 113053471 B CN113053471 B CN 113053471B CN 202110303247 A CN202110303247 A CN 202110303247A CN 113053471 B CN113053471 B CN 113053471B
Authority
CN
China
Prior art keywords
brinell hardness
hardness
model
brinell
test
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN202110303247.0A
Other languages
Chinese (zh)
Other versions
CN113053471A (en
Inventor
王凡
张志伟
耿文远
袁永健
周宏伟
丛琳琳
徐军
赵国庆
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Inner Mongolia Metal Material Research Institute
Original Assignee
Inner Mongolia Metal Material Research Institute
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Inner Mongolia Metal Material Research Institute filed Critical Inner Mongolia Metal Material Research Institute
Priority to CN202110303247.0A priority Critical patent/CN113053471B/en
Publication of CN113053471A publication Critical patent/CN113053471A/en
Application granted granted Critical
Publication of CN113053471B publication Critical patent/CN113053471B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G16INFORMATION AND COMMUNICATION TECHNOLOGY [ICT] SPECIALLY ADAPTED FOR SPECIFIC APPLICATION FIELDS
    • G16CCOMPUTATIONAL CHEMISTRY; CHEMOINFORMATICS; COMPUTATIONAL MATERIALS SCIENCE
    • G16C60/00Computational materials science, i.e. ICT specially adapted for investigating the physical or chemical properties of materials or phenomena associated with their design, synthesis, processing, characterisation or utilisation
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N1/00Sampling; Preparing specimens for investigation
    • G01N1/28Preparing specimens for investigation including physical details of (bio-)chemical methods covered elsewhere, e.g. G01N33/50, C12Q
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N1/00Sampling; Preparing specimens for investigation
    • G01N1/28Preparing specimens for investigation including physical details of (bio-)chemical methods covered elsewhere, e.g. G01N33/50, C12Q
    • G01N1/286Preparing specimens for investigation including physical details of (bio-)chemical methods covered elsewhere, e.g. G01N33/50, C12Q involving mechanical work, e.g. chopping, disintegrating, compacting, homogenising
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N1/00Sampling; Preparing specimens for investigation
    • G01N1/28Preparing specimens for investigation including physical details of (bio-)chemical methods covered elsewhere, e.g. G01N33/50, C12Q
    • G01N1/32Polishing; Etching
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N3/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N3/40Investigating hardness or rebound hardness
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/20Design optimisation, verification or simulation
    • G06F30/23Design optimisation, verification or simulation using finite element methods [FEM] or finite difference methods [FDM]
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2203/00Investigating strength properties of solid materials by application of mechanical stress
    • G01N2203/0058Kind of property studied
    • G01N2203/0076Hardness, compressibility or resistance to crushing

Abstract

The invention relates to a method for nondestructive on-line detection of Brinell hardness of a fan spindle, which is characterized by comprising the following steps: the method comprises the steps of (1) constructing a constitutive model based on real tissue evolution by analyzing a Brinell hardness method and a Richner hardness method and a fitting method and a relation between a fitting model and a process and parameters; constructing a prediction model; finally, embedding the model into a finite element system through a finite element analysis technology to obtain hardness distribution rules under different process conditions. The advantages are that: the technical problem that the Brinell hardness of the main shaft of the fan cannot be detected accurately in a nondestructive and online manner in the prior art is solved on the whole, and a basis is provided for realizing accurate assessment of the in-service state of the main shaft of the fan, enhancing the accurate control of a quality tool on the use process and prolonging the fatigue life of the in-service parts. Compared with the prior art, the invention can greatly reduce the cost of manpower and material resources, improve the efficiency, and fill the blank of nondestructive online detection of the Rich hardness of the main shaft of the fan.

Description

Method for nondestructive on-line detection of Brinell hardness of fan spindle
Technical Field
The invention relates to a method for nondestructive on-line detection of Brinell hardness of a fan spindle, in particular to a method for nondestructive on-line detection of Brinell hardness of a fan spindle with a material mark of 42CrMo4, belonging to the technical field of hardness testing of metal materials.
Background
For in-service units, whether in thermal power, wind power or other industries, if the in-service units are inspected in the future, a nondestructive method is adopted to detect the in-service units, for example: hardness detection, nondestructive detection, on-site metallographic detection, and the like. Because of the proportional relationship between hardness and strength, engineering is often used to measure the performance. The portable hardness tester has the advantages of small volume, light weight, simple and convenient test, convenient carrying, high detection efficiency, slight damage to test surfaces and the like, so that the portable hardness tester is widely applied to the field detection of in-service equipment.
The prior art is limited by the prior art, and the prior detection technology cannot accurately carry out nondestructive online detection on the Brinell hardness of the main shaft of the fan with the material mark of 42CrMo 4.
Although portable hardness testing devices are widely used in field testing of in-service equipment, no standard is currently available that uses hardness values as a basis for determination. In general, it is important to accurately convert the Brinell hardness value into the Brinell hardness value to determine whether the conversion is performed. The conversion between the Brinell hardness and Brinell hardness is now in accordance with GB/T17394.4-2014 section 4 of the test for the Brinell hardness of metallic materials: the hardness values obtained in Table 1 in the conversion Table are, however, the test objects applicable to Table 1 are "carbon steel, low alloy steel and cast steel", and are not applicable to fan spindles strictly; if the conversion is carried out according to table 1, deviation is liable to be caused, and the actual hardness of the measured part cannot be reflected. Therefore, a comparison test is needed to find out the conversion relation between the Brinell hardness and the Brinell hardness, which is consistent with the comparison test, so as to fill the blank of the Brinell hardness test standard of the fan main shaft material.
Although GB/T17394.4-2014 section 1 of the Brinell hardness test for metallic materials: the requirements concerning comparative tests have not been mentioned in test methods, but since GB/T17394.4-1998 "test method for hardness of metal" has clear requirements for comparative tests: "for a specific material, to convert the Lev hardness value to other hardness values more accurately, a comparative test must be performed to obtain a corresponding conversion relationship. ".
Disclosure of Invention
The invention aims to provide a method for nondestructive on-line detection of Brinell hardness of a fan spindle, in particular to a method for nondestructive on-line detection of Brinell hardness of a fan spindle with the material mark of 42CrMo4, which provides a basis for accurately evaluating the in-service state of the fan spindle and accurately controlling the using process of a reinforcing quality tool on the basis of elucidating the relation between the Brinell hardness method (dynamic test method) and the Brinell hardness method (static test method) and the fitting method and the fitting model and different processes and parameters.
The object of the invention is achieved by the following means:
a method for nondestructive on-line detection of Brinell hardness of a fan spindle is characterized in that a constitutive model based on real tissue evolution is constructed by analyzing the Brinell hardness method (dynamic test method) and the Brinell hardness method (static test method) and fitting the relationship between the fitting method and the fitting model and the process and parameters; constructing a prediction model; finally, embedding the model into a finite element system through a finite element analysis technology to obtain hardness distribution rules under different process conditions.
The analysis specifically refers to: and analyzing the hardness distribution characteristics, the change rule and the like.
The constitutive model of the real tissue evolution is based on the implementation of different processes, and comprises the following steps: annealing, normalizing and tempering.
The prediction model refers to: and according to the relation between the Brinell hardness and the Richter hardness of the material, combining the expression of the constitutive model to obtain a confidence interval of the material at normal temperature, and further obtaining an equation of the Richter hardness.
The embedding is specifically to obtain a regression equation with a hypothesis test value P greater than 0.05 by using the significance of the hypothesis test verification equation based on the finite element technology.
The invention relates to a system for realizing the method, which comprises the following steps: the device comprises a process implementation processing unit, a Brinell hardness and Lev hardness test detection unit, a Brinell hardness and Lev hardness modeling unit and a verification unit, wherein: the process implementation processing unit outputs a microstructure change rule and transmits the microstructure change rule to the Brinell hardness and Brinell hardness test detection unit, the Brinell hardness and Brinell hardness test detection unit outputs the hardness change rule and transmits the hardness change rule to the Brinell hardness and Brinell hardness modeling unit, and the Brinell hardness and Brinell hardness modeling unit outputs an analytical expression and transmits the analytical expression to the verification unit through a finite element technology and compares the analytical expression with an output result of the Brinell hardness and Brinell hardness test detection unit.
The beneficial effects of the invention are as follows:
the invention integrally solves the technical problem that the Brinell hardness of a main shaft of a fan with the material mark of 42CrMo4 cannot be detected accurately in a nondestructive and online manner in the prior art.
Compared with the prior art, the method establishes the constitutive model suitable for the Brinell hardness and the Brinell hardness of the main shaft of the 42CrMo4 finished product fan based on the real evolution rule of the microstructure in the treatment process, and can accurately predict the Brinell hardness distribution value of the main shaft of the 42CrMo4 finished product fan. The invention provides a basis for realizing accurate assessment of the in-service state of the fan main shaft, enhancing the accurate control of a quality tool on the use process and improving the fatigue life of the in-service part. Compared with the prior art, the invention can greatly reduce the cost of manpower and material resources, improve the efficiency, and fill the blank of nondestructive online detection of the Rich hardness of the main shaft of the fan.
Drawings
FIG. 1 is a schematic flow chart of the present invention.
Detailed Description
Example 1
As shown in fig. 1, the embodiment relates to a method for nondestructive on-line detection of brinell hardness of a fan spindle with a material mark of 42CrMo4, wherein the material consists of a large amount of sorbite and a small amount of ferrite, and the specific operation comprises the following steps:
and step one, cutting a fan main shaft material with the material mark of 42CrMo4 to prepare 3 groups of samples. And respectively carrying out annealing treatment, normalizing treatment and quenching and tempering treatment on the 3 groups of samples. 1 block is selected from the 3 groups to be cut, inlaid, polished and corroded to prepare a metallographic specimen, and the metallographic specimen is placed under an optical microscope to observe the microstructure morphology of the specimen.
Step two, on the basis of the step one, respectively carrying out surface processing on 3 groups of samples through a milling machine and a grinding machine, and carrying out a test on the samples in a Brinell hardness machine to obtain Brinell hardness data; and then respectively placing 3 groups of samples on a Brinell hardness machine, carrying out a Brinell hardness test on the premise of not influencing the detection result near each Brinell hardness point, carrying out a plurality of Brinell hardness tests near each Brinell hardness point, and recording the average value of the test as 1 group of effective values of the Brinell hardness to obtain the Brinell hardness data corresponding to the Brinell hardness data.
Thirdly, building a constitutive model suitable for a fan main shaft material with a material mark of 42CrMo4 based on the weight relation, wherein the model comprises model fitting relativity, and the expression is as follows:
where r is the model fitting correlation, x i In order to obtain the value of the hardness of the steel,is the average value of the Lev hardness value, y i Is Brinell hardness value, < >>The average value of the Brinell hardness values is shown.
The weight relation comprises: the weighting characteristics and the degree to which their weights deviate from a single point.
The modeling process is specifically as follows:
(1) since the least squares method is weighted according to distance from somewhere in the middle, the weights thereof are related to the significant deviation that a single point has, the numerical fitting method is selected as the least squares method;
(2) according to the definition and the property of the hardness, the fitting model is selected as a primary function, and therefore, the model established on the basis is as follows: y=a+bx, where a, b are constants, x is the brinell hardness number, and y is the brinell hardness number.
(3) Under different process conditions, the uniformity of the materials is different, the predicted result has fluctuation, a confidence interval with the probability of 95% can be introduced for correction, the range of the confidence interval is obtained, and the expression is as follows:will->Substituting the model formula y=a+bx gives δ, where +.>Delta is a constant that is a predicted value for model equation y=a+bx.
(4) According to the constitutive model expression: y=a+bx, brought into confidence intervalAnd in the second step, the Brinell hardness value and the Li hardness value can obtain a 42CrMo4 fan main shaft material constitutive equation of various microstructure evolution.
Step four, based on finite element technology, adopting hypothesis test to test the constitutive equation, wherein the hypothesis test expression is: t>t α/2 (n-2), wherein t is a t-test method statistic and n is an experimental number.
The present example was divided into 3 groups (1 group of samples for each 3) of 9 pieces of samples, and the sample size was 200 ﹡ 100 ﹡ mm, and 30 groups of data were finally obtained by measurement. Through specific practical experiments, the obtained experimental data under different process conditions are shown as follows:
the analytical expression: y= -290.76+1.06x, where x is the brinell hardness number and y is the brinell hardness number;
wherein r is a model fitting correlation; when the data amount is larger than 25, the correlation coefficient is larger than 0.4, namely, the two groups of data are considered to be correlated, and the closer the correlation coefficient is to 1, the stronger the correlation is.
Confidence interval is +.>Delta=29.12 (HBW 5/750), where +.>Delta is a constant that is a predicted value for model equation y=a+bx.
Hypothesis testing: let α=0.05, |t|= 39.767 =t 0.025 (28) Where α is the confidence probability, t is the t-test method statistic, n is the number of experiments, i.e., the P value is greater than 0.05, where P is the hypothesis test value. It is obvious to illustrate the regression equation.
In conclusion, the characteristic of the relation between the Brinell hardness and the Brinell hardness of the material with the material grade of 42CrMo4 fan main shaft material is different from that of carbon steel, low alloy steel and cast steel materials, and the method is based on weight relation and different process analytic modeling methods, introduces a correlation prediction method and finite element technology hypothesis test, so that the method has higher prediction precision of the Brinell hardness of the material grade of 42CrMo4 fan main shaft material in a nondestructive online detection manner, and omits a Brinell hardness test final detection means with high cost and complex operation.
The foregoing embodiments may be partially modified in numerous ways by those skilled in the art without departing from the principles and spirit of the invention, the scope of which is defined in the claims and not by the foregoing embodiments, and all such implementations are within the scope of the invention.

Claims (6)

1. A method for nondestructively and online detecting Brinell hardness of a fan spindle is characterized by comprising the following steps: the method comprises the steps of (1) constructing a constitutive model based on real tissue evolution by analyzing a Brinell hardness method and a Richner hardness method and a fitting method and a relation between a fitting model and a process and parameters; constructing a prediction model; finally, embedding the model into a finite element system through a finite element analysis technology to obtain hardness distribution rules under different process conditions; the material mark of the fan main shaft is 42CrMo4; the specific operation comprises the following steps:
cutting a fan main shaft material with the material mark of 42CrMo4 into 3 groups of samples, and respectively carrying out annealing treatment, normalizing treatment and quenching and tempering treatment on the 3 groups of samples; 1 block is selected from the 3 groups to be cut, inlaid, polished and corroded to prepare a metallographic specimen, and the metallographic specimen is placed under an optical microscope to observe the microstructure morphology of the specimen;
step two, on the basis of the step one, respectively carrying out surface processing on 3 groups of samples through a milling machine and a grinding machine, and carrying out a test on the samples in a Brinell hardness machine to obtain Brinell hardness data; respectively placing 3 groups of samples on a Brinell hardness machine, carrying out a Brinell hardness test on the premise of not influencing a detection result near each Brinell hardness point, carrying out a plurality of Brinell hardness tests near each Brinell hardness point, and recording the average value of the test as 1 group of effective values of the Brinell hardness to obtain the Brinell hardness data corresponding to the Brinell hardness data;
thirdly, building a constitutive model suitable for a fan main shaft material with a material mark of 42CrMo4 based on the weight relation, wherein the model comprises model fitting relativity, and the expression is as follows:
where r is the model fitting correlation, x i In order to obtain the value of the hardness of the steel,is the average value of the Lev hardness value, y i The hardness of the steel is given as the Brinell hardness value,is the average value of Brinell hardness values;
the weight relation comprises: the weighting characteristics and the degree of deviation of their weights from a single point;
the modeling process is specifically as follows:
(1) selecting a numerical fitting method as a least square method;
(2) selecting a fitting model as a primary function, and establishing a model as follows: y=a+bx, where a, b are constants, x is the brinell hardness number, y is the brinell hardness number;
(3) and (3) introducing a confidence interval with the probability of 95% for correction to obtain a range of the confidence interval, wherein the expression is as follows:will->Substituting the model formula y=a+bx gives δ, where +.>Delta is a constant that is a predicted value for model equation y=a+bx;
(4) according to the constitutive model expression: y=a+bx, brought into confidence intervalAnd the Brinell hardness value and the Li hardness value in the second step can obtain 42CrMo4 fan main shaft material constitutive equation of various microstructure evolution;
step four, based on finite element technology, adopting hypothesis test to test the constitutive equation, wherein the hypothesis test expression is: t>t α/2 (n-2), wherein t is a t-test method statistic and n is an experimental number.
2. The method for nondestructive on-line detection of brinell hardness of a spindle of a blower of claim 1, wherein: the analysis refers to: and analyzing the hardness distribution characteristics and the change rule.
3. The method for nondestructive on-line detection of brinell hardness of a spindle of a blower of claim 1, wherein: the constitutive model of the real tissue evolution is based on the implementation of different processes, and comprises the following steps: annealing, normalizing and tempering.
4. The method for nondestructive on-line detection of brinell hardness of a spindle of a blower of claim 1, wherein: the prediction model refers to: and according to the relation between the Brinell hardness and the Richter hardness of the material, combining the expression of the constitutive model to obtain a confidence interval of the material at normal temperature, and further obtaining an equation of the Richter hardness.
5. The method for nondestructive on-line detection of brinell hardness of a spindle of a blower of claim 1, wherein: the embedding is based on finite element technology, and the significance of the hypothesis test verification equation is utilized to obtain a regression equation with the hypothesis test value P being greater than 0.05.
6. The method for nondestructive on-line detection of brinell hardness of a spindle of a blower of claim 1, wherein: a system for implementing the method, comprising: the device comprises a process implementation processing unit, a Brinell hardness and Lev hardness test detection unit, a Brinell hardness and Lev hardness modeling unit and a verification unit, wherein: the process implementation processing unit outputs a microstructure change rule and transmits the microstructure change rule to the Brinell hardness and Brinell hardness test detection unit, the Brinell hardness and Brinell hardness test detection unit outputs the hardness change rule and transmits the hardness change rule to the Brinell hardness and Brinell hardness modeling unit, and the Brinell hardness and Brinell hardness modeling unit outputs an analytical expression and transmits the analytical expression to the verification unit through a finite element technology and compares the analytical expression with an output result of the Brinell hardness and Brinell hardness test detection unit.
CN202110303247.0A 2021-03-22 2021-03-22 Method for nondestructive on-line detection of Brinell hardness of fan spindle Active CN113053471B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202110303247.0A CN113053471B (en) 2021-03-22 2021-03-22 Method for nondestructive on-line detection of Brinell hardness of fan spindle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202110303247.0A CN113053471B (en) 2021-03-22 2021-03-22 Method for nondestructive on-line detection of Brinell hardness of fan spindle

Publications (2)

Publication Number Publication Date
CN113053471A CN113053471A (en) 2021-06-29
CN113053471B true CN113053471B (en) 2024-01-02

Family

ID=76514586

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202110303247.0A Active CN113053471B (en) 2021-03-22 2021-03-22 Method for nondestructive on-line detection of Brinell hardness of fan spindle

Country Status (1)

Country Link
CN (1) CN113053471B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114112722B (en) * 2021-10-29 2024-01-02 上海汇众萨克斯减振器有限公司 Regression equation-based maximum yield stress evaluation method for metal rod bending

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20070070490A (en) * 2005-12-29 2007-07-04 한국표준과학연구원 Test-cycle calibrator for hydraulic brinell hardness tester
CN102419282A (en) * 2011-08-22 2012-04-18 中原特钢股份有限公司 Manufacturing method of reference block for on-site conversion of Leeb hardness to Brinell hardness
CN105243195A (en) * 2015-09-16 2016-01-13 大连理工大学 Prediction method for micro-milling and work-hardening nickel-based superalloy
EP3671178A1 (en) * 2018-12-20 2020-06-24 SSAB Technology AB Test system and method for measuring and calculating hardness of material
CN111678823A (en) * 2020-06-22 2020-09-18 上海交通大学 Method for measuring microhardness of surface layer of titanium alloy milled
CN112100885A (en) * 2020-08-28 2020-12-18 北京航空航天大学 Numerical simulation method for surface hardness of high-energy shot blasting

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20070070490A (en) * 2005-12-29 2007-07-04 한국표준과학연구원 Test-cycle calibrator for hydraulic brinell hardness tester
CN102419282A (en) * 2011-08-22 2012-04-18 中原特钢股份有限公司 Manufacturing method of reference block for on-site conversion of Leeb hardness to Brinell hardness
CN105243195A (en) * 2015-09-16 2016-01-13 大连理工大学 Prediction method for micro-milling and work-hardening nickel-based superalloy
EP3671178A1 (en) * 2018-12-20 2020-06-24 SSAB Technology AB Test system and method for measuring and calculating hardness of material
CN111678823A (en) * 2020-06-22 2020-09-18 上海交通大学 Method for measuring microhardness of surface layer of titanium alloy milled
CN112100885A (en) * 2020-08-28 2020-12-18 北京航空航天大学 Numerical simulation method for surface hardness of high-energy shot blasting

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
基于锥形压入的材料力学性能测试方法研究;姚博;蔡力勋;包陈;;航空学报(第08期);全文 *
结构材料维氏硬度与屈服应力的关系分析;薛河;庄泽城;曹婷;郭瑞;崔英浩;龚晓燕;;西安科技大学学报(第02期);全文 *

Also Published As

Publication number Publication date
CN113053471A (en) 2021-06-29

Similar Documents

Publication Publication Date Title
CN111751199B (en) Fatigue life prediction method based on EIFS distribution
Mazal et al. Use of acoustic emission method for identification of fatigue micro-cracks creation
CN105891321B (en) The micro-magnetic detection scaling method of ferrimagnet structural mechanical property
CN113053471B (en) Method for nondestructive on-line detection of Brinell hardness of fan spindle
McMurtrey et al. The effect of pit size and density on the fatigue behaviour of a pre‐corroded martensitic stainless steel
CN111027208B (en) Method for determining and prolonging service life of in-service mechanical equipment key structure element under fatigue load action
CN110763758B (en) Method for determining relation between defects and fatigue performance based on nondestructive testing
CN110686948A (en) Method for detecting strength of welding area
CN110568083A (en) acoustic emission detection method for online monitoring of corrosion fatigue damage of steel
CN112816553A (en) Heat-resistant steel aging grade evaluation method based on support vector machine
JPS61139743A (en) Method and apparatus fr evaluating residual life of machine structure receiving repeated load
Sorsa et al. A data-based modelling scheme for estimating residual stress from Barkhausen noise measurements
Siefert et al. Optimization of vickers hardness parameters for micro-and macro-indentation of grade 91 steel
CN109541013A (en) A kind of ferromagnetic alloy steel dislocation density detection method
CN113155444B (en) Calibration method for detecting grinding burn of carburized and quenched gear by magnetic-elastic method
RU2234079C2 (en) Method and device for determination of remaining service life of thin-walled envelopes made from reservoir and pipe steels
JPH1123776A (en) Composite diagnostic system of reactor internal equipment
Álvarez et al. Fatigue life estimation of pre-corroded 42CrMo4 subjected to accelerated pitting corrosion method
CN109870257B (en) Method for predicting distribution of quenching residual stress in thickness direction of plate
CN110308044A (en) Increasing material manufacturing product early stage stress based on metal magnetic memory test concentrates method of discrimination
Locke¹ Statistical measurement control
CN117592820B (en) Bridge damage disease intelligent recognition system based on computer data analysis
CN117370871B (en) Quality analysis method and system for special steel
CN117168980A (en) Method for predicting notch tensile strength of material through damage amplification
Tscherter A process and investigation into the influence of cast surface condition on fatigue life

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant