[go: up one dir, main page]

CN1587988A - Sample for measuring fatigue crack expansion rate in corrosion liquid and test method - Google Patents

Sample for measuring fatigue crack expansion rate in corrosion liquid and test method Download PDF

Info

Publication number
CN1587988A
CN1587988A CN 200410060569 CN200410060569A CN1587988A CN 1587988 A CN1587988 A CN 1587988A CN 200410060569 CN200410060569 CN 200410060569 CN 200410060569 A CN200410060569 A CN 200410060569A CN 1587988 A CN1587988 A CN 1587988A
Authority
CN
China
Prior art keywords
sample
test
crack
fatigue
growth rate
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.)
Granted
Application number
CN 200410060569
Other languages
Chinese (zh)
Other versions
CN1278114C (en
Inventor
张亚军
梁健
白杰
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.)
725th Research Institute of CSIC
Original Assignee
725th Research Institute of CSIC
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 725th Research Institute of CSIC filed Critical 725th Research Institute of CSIC
Priority to CN 200410060569 priority Critical patent/CN1278114C/en
Publication of CN1587988A publication Critical patent/CN1587988A/en
Application granted granted Critical
Publication of CN1278114C publication Critical patent/CN1278114C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Landscapes

  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)

Abstract

一种测量腐蚀液中疲劳裂纹扩展速率的试样及试验方法,在其试样远离裂纹扩展面的上侧采用整体设计的方法设置有电子引伸计的装卡刀口;根据试验机控制系统采集到的大量的试验数据,求解出所设计试样的柔度系数,建立归一化裂纹长度和柔度系数之间的函数关系,实现在腐蚀液中进行疲劳裂纹扩展速率(da/dN)试验时裂纹长度的检测自动化,据此所建立的试验方法,为该类试验的顺利进行提供了保证。与目前国内大多单位在腐蚀液中测量疲劳裂纹扩展速率(da/dN)用目测法检测裂纹长度相比,明显提高了测量裂纹长度的精度,同时也大大降低了劳动强度。利用试验结果,能够更准确地对服役在腐蚀介质中的船舶进行安全设计和寿命评估。

A sample and test method for measuring the fatigue crack growth rate in corrosive liquid. The upper side of the sample away from the crack propagation surface adopts the method of integral design to set the clamping knife edge of the electronic extensometer; according to the data collected by the control system of the testing machine Based on a large amount of test data, the flexibility coefficient of the designed sample is solved, and the functional relationship between the normalized crack length and the flexibility coefficient is established to realize the fatigue crack growth rate (da/dN) test in the corrosive liquid. The length detection is automated, and the test method established based on it provides a guarantee for the smooth progress of this type of test. Compared with most domestic units currently measuring the fatigue crack growth rate (da/dN) in the corrosive solution and using the visual method to detect the crack length, the accuracy of measuring the crack length is significantly improved, and the labor intensity is also greatly reduced. Using the test results, the safety design and life assessment of ships serving in corrosive media can be more accurately carried out.

Description

测量腐蚀液中疲劳裂纹扩展速率的试样及试验方法Specimen and test method for measuring fatigue crack growth rate in corrosive solution

技术领域:Technical field:

本发明涉及金属材料腐蚀试验测试方法技术领域,一种测量腐蚀液中疲劳裂纹扩展速率的试样及试验方法。The invention relates to the technical field of metal material corrosion test methods, and relates to a sample and a test method for measuring the fatigue crack growth rate in corrosive liquid.

背景技术:Background technique:

目前在我国的GB/T6398-2000(金属材料疲劳裂纹扩展速率试验方法)中规定的标准紧凑拉伸C(T)试样的引伸计装卡刀口在关于裂纹扩展面对称的两侧,在腐蚀液中进行疲劳裂纹扩展速率(da/dN)试验时,疲劳裂纹长度用柔度法测量的情形只限于在卧式疲劳试验机上进行;如果在立式疲劳试验机上进行这种试验,价格昂贵的引伸计(进口的约5000美金,国产的也要上千元人民币)往往会因受到腐蚀液的侵蚀而降低其线性度、灵敏度或彻底损坏;而国内绝大多数疲劳试验机都是立式的,因此,在腐蚀液中进行疲劳裂纹扩展速率(da/dN)试验时,用柔度法测量疲劳裂纹长度几乎是不可能的。鉴于这种情况,国内大多数单位进行这类试验时,一般不用引伸计通过柔度技术测量疲劳裂纹长度,而是借助光学显微镜用目测法来观察裂纹的扩展情况。但是,金属材料的疲劳裂纹往往比较细,尤其是铜合金、钛合金等材料的疲劳裂纹,在空气中已经很不容易观察清楚,并且由于腐蚀液常常会因为悬浮其中的金属材料试样的腐蚀产物而变得混浊不清,这使得用目测法观察疲劳裂纹长度更为困难,因此很难保证目测法观察疲劳裂纹长度的精度,劳动强度也很大。At present, in China's GB/T6398-2000 (metal material fatigue crack growth rate test method), the extensometer clamping knife edge of the standard compact tensile C(T) sample is on both sides of the crack growth plane. When the fatigue crack growth rate (da/dN) test is carried out in the corrosive solution, the fatigue crack length is measured by the flexibility method only on the horizontal fatigue testing machine; if this test is carried out on the vertical fatigue testing machine, the price is expensive High-quality extensometers (imported about 5,000 U.S. dollars, and domestic ones cost thousands of yuan) tend to reduce their linearity, sensitivity or be completely damaged due to erosion by corrosive liquids; while most domestic fatigue testing machines are vertical Therefore, it is almost impossible to measure the fatigue crack length by the compliance method when performing the fatigue crack growth rate (da/dN) test in the corrosive solution. In view of this situation, when most domestic units conduct such tests, they generally do not use extensometers to measure the fatigue crack length through flexibility techniques, but use optical microscopes to observe the crack growth by visual inspection. However, the fatigue cracks of metal materials are often relatively thin, especially the fatigue cracks of copper alloys, titanium alloys and other materials, which are not easy to observe clearly in the air, and because the corrosive liquid is often corroded by the suspended metal material samples The product becomes turbid and unclear, which makes it more difficult to observe the length of fatigue cracks by visual inspection, so it is difficult to ensure the accuracy of fatigue crack length observation by visual inspection, and the labor intensity is also very high.

目前,国内涉及在试验测试领域测量疲劳裂纹长度的文献很少,特别是对柔度技术的研究和利用柔度技术进行腐蚀环境下裂纹长度自动检测方面的研究尚未见到。At present, there are few domestic literatures related to the measurement of fatigue crack length in the field of test and testing, especially the research on flexibility technology and the automatic detection of crack length in corrosive environment using flexibility technology have not been seen.

发明内容:Invention content:

为了解决上述存在的问题,本发明提供一种测量腐蚀液中疲劳裂纹扩展速率的试样及试验方法,这种试样可以使价格昂贵的电子引伸计远离腐蚀液面,避免因受到腐蚀液侵蚀而损坏,最终使试验失败的难题;相对目测法测量疲劳裂纹长度而言,该方法可明显提高测量疲劳裂纹长度的精度,同时也大大降低劳动强度。In order to solve the above existing problems, the present invention provides a sample and test method for measuring the fatigue crack growth rate in corrosive liquid. And the damage will eventually make the test fail. Compared with the visual method of measuring the fatigue crack length, this method can significantly improve the accuracy of measuring the fatigue crack length, and also greatly reduce the labor intensity.

本发明是采用如下技术方案实现的:The present invention is realized by adopting the following technical solutions:

所述的测量腐蚀液中疲劳裂纹扩展速率的试样,在其试样远离裂纹扩展面的上侧采用整体设计的方法设置有电子引伸计的装卡刀口;根据试验机控制系统采集到的大量的试验数据,利用进口设备的多项试验测试软件,求解出所设计试样的柔度系数如下:The sample for measuring the fatigue crack growth rate in the corrosive liquid is provided with a clamping knife edge of an electronic extensometer on the upper side of the sample away from the crack propagation surface; Using the test data of the imported equipment, the flexibility coefficient of the designed sample is calculated as follows:

柔度系数符号  C0     C1      C2     C3      C4     C5 Symbol of compliance coefficient C 0 C 1 C 2 C 3 C 4 C 5

柔度系数数值  0.9927  -4.8803  17.031  -189.39  781.63  -821.74Value of flexibility coefficient 0.9927 -4.8803 17.031 -189.39 781.63 -821.74

同时,建立归一化裂纹长度和柔度系数之间的函数关系,实现在腐蚀液中进行疲劳裂纹扩展速率(da/dN)试验时裂纹长度的检测自动化。At the same time, the functional relationship between the normalized crack length and the flexibility coefficient is established to realize the automatic detection of the crack length when performing the fatigue crack growth rate (da/dN) test in the corrosive solution.

实施所述的测量腐蚀液中疲劳裂纹扩展速率的试样的试验方法按照下列步骤进行:Implement the test method of the sample for measuring the fatigue crack growth rate in the corrosive solution according to the following steps:

(1)采用电火花线切割的方式引发试样的初始裂纹;(1) The initial crack of the sample is induced by wire electric discharge cutting;

(2)将求解出的所设计试样的柔度系数输入到事先编好的试验程序中;(2) Input the calculated flexibility coefficient of the designed sample into the pre-programmed test program;

(3)测量试样厚度、宽度参数,并输入到事先编好的程序中;(3) Measure the thickness and width parameters of the sample, and input them into the pre-programmed program;

(4)将腐蚀循环系统、相关的试样卡具及试样与立式疲劳试验机相连接;(4) Connect the corrosion circulation system, related sample fixtures and samples with the vertical fatigue testing machine;

(5)将腐蚀液加入循环系统和装有试样的腐蚀盒中,循环系统中的腐蚀液要足够多,腐蚀盒中的腐蚀液要保证时时浸泡住裂纹扩展面;(5) Add the corrosive solution to the circulation system and the corrosion box containing the sample. The corrosive solution in the circulation system should be sufficient, and the corrosive solution in the corrosion box should be guaranteed to soak the crack propagation surface from time to time;

(6)将电子引伸计装卡在试样上侧的刀口处;(6) Install the electronic extensometer at the knife edge on the upper side of the sample;

(7)设置好预制疲劳裂纹的各个参数,包括应力强度因子范围ΔK、控制方式、采用频率、波形及预制疲劳裂纹的长度;(7) Set various parameters of prefabricated fatigue cracks, including stress intensity factor range ΔK, control mode, frequency, waveform and length of prefabricated fatigue cracks;

(8)启动试验机,开始预制疲劳裂纹,时时观测当前的裂纹扩展长度,注意整个腐蚀循环系统,以防腐蚀液渗漏而侵蚀试验机;(8) Start the testing machine, start prefabricating fatigue cracks, observe the current crack extension length from time to time, pay attention to the entire corrosion cycle system, to prevent corrosion of the testing machine due to leakage of corrosive liquid;

(9)预制完成疲劳裂纹后,根据当前的结果,设定试验时所需要的载荷范围、应力比、频率的参数;(9) After the fatigue cracks are prefabricated, according to the current results, set the parameters of the load range, stress ratio, and frequency required for the test;

(10)再次启动试验机,开始正式试验;(10) Start the testing machine again and start the formal test;

(11)试验结束后,根据所采集到的试验数据,按照帕里斯(Paris)经验方程的表达形式拟合出试验材料的疲劳裂纹扩展速率曲线及其方程,最后出具相应的试验报告。(11) After the test, according to the collected test data, fit the fatigue crack growth rate curve and equation of the test material according to the expression form of the Paris (Paris) empirical equation, and finally issue the corresponding test report.

所述的测量腐蚀液中疲劳裂纹扩展速率的试样,该试样柔度系数的求解步骤如下:For the sample measuring the fatigue crack growth rate in the corrosive solution, the solution steps of the flexibility coefficient of the sample are as follows:

(1)测量所设计试样的厚度B、宽度W及采用任何方法所引发的有效裂纹长度a,并事先测试出试验材料的弹性模量E;(1) Measure the thickness B, width and the effective crack length a caused by any method of the designed sample, and test the elastic modulus E of the test material in advance;

(2)将所设计的试样采用电火花线切割的方法引发裂纹,每隔a/W=0.025引发一次,并重新测量引发的裂纹长度a,作为所用的实际值;(2) Initiate cracks on the designed sample by wire electric discharge cutting, initiate once every a/W=0.025, and re-measure the induced crack length a, as the actual value used;

(3)将引发裂纹后的试样装在试验机上,并将电子引伸计装卡在试样的刀口处,清零;(3) Install the sample after the crack is induced on the testing machine, and install the electronic extensometer at the knife edge of the sample, and reset it;

(4)对引发裂纹后的试样在弹性范围内缓慢拉伸,此时需要以较高的采点速率采集作用在试样上的载荷P、引伸计的变形量V;(4) Slowly stretch the sample after crack initiation within the elastic range. At this time, it is necessary to collect the load P acting on the sample and the deformation V of the extensometer at a higher sampling rate;

(5)按照公式Ux=1/[(BEVx/P)1/2+1]求解出试样的无量纲柔度值Ux;(5) Solve the dimensionless flexibility value Ux of the sample according to the formula Ux=1/[(BEV x /P) 1/2 +1];

(6)每次引发裂纹后,都要求解出一个归一化裂纹长度a/W值;(6) After each crack is initiated, a normalized crack length a/W value is required to be solved;

(7)当归一化裂纹长度a/W=0.75时,试验可以停止;(7) When the normalized crack length a/W=0.75, the test can be stopped;

(8)对所求得的数据组(a/W,Ux)进行一元五次递增多项式回归,其回归系数便可以作为该试样的柔度系数;(8) Carry out a quintic incremental polynomial regression on the obtained data set (a/W, Ux), and its regression coefficient can be used as the flexibility coefficient of the sample;

(9)对多块试样按如上步骤进行,可分别得到各个试样的六个柔度系数;(9) Carry out the above steps for multiple samples, and six flexibility coefficients of each sample can be obtained respectively;

(10)对多块试样的柔度系数进行均值化处理,就得到了最终所求解的六个柔度系数C0、C1、C2、C3、C4、C5(10) The compliance coefficients of multiple samples are averaged to obtain the final six compliance coefficients C 0 , C 1 , C 2 , C 3 , C 4 , and C 5 .

由于采用了上述技术方案,本发明具有如下积极效果:Owing to adopting above-mentioned technical scheme, the present invention has following positive effect:

本发明设计出的在腐蚀液(海水、盐水、江水等)中测量疲劳裂纹扩展速率(da/dN)的试样,将电子引伸计的装卡刀口提到了远离裂纹扩展面的上侧,解决了在立式疲劳试验机上用柔度法测量疲劳裂纹长度时、价格昂贵的引伸计常因腐蚀液侵蚀而损坏、从而导致试验失败的难题。该试样也可以用在卧式疲劳试验机上。The sample designed by the present invention to measure the fatigue crack growth rate (da/dN) in the corrosive liquid (sea water, salt water, river water, etc.) mentions the clamping edge of the electronic extensometer to the upper side away from the crack propagation surface, so as to solve the problem When using the flexibility method to measure the fatigue crack length on the vertical fatigue testing machine, the expensive extensometer is often damaged by the corrosion of the corrosive liquid, which leads to the failure of the test. This sample can also be used on a horizontal fatigue testing machine.

利用求解出的试样柔度系数,建立起了归一化裂纹长度和柔度系数的函数方程,从理论上为通过柔度技术测量疲劳裂纹长度奠定了基础,从而使得在腐蚀液中进行疲劳裂纹扩展速率(da/dN)试验时裂纹长度的检测实现了自动化,与目前国内大多单位在腐蚀液中测量疲劳裂纹扩展速率(da/dN)用目测法检测裂纹长度相比,明显提高了测量裂纹长度的精度,同时也大大降低了劳动强度。The function equation of the normalized crack length and the flexibility coefficient was established by using the sample flexibility coefficient obtained from the solution, which theoretically laid the foundation for measuring the fatigue crack length through the flexibility technology, so that fatigue in the corrosive solution The detection of the crack length in the crack growth rate (da/dN) test has been automated, and compared with most domestic units currently measuring the fatigue crack growth rate (da/dN) in the corrosive solution and using the visual method to detect the crack length, the measurement has been significantly improved. The accuracy of the crack length also greatly reduces the labor intensity.

在腐蚀液中测量疲劳裂纹扩展速率试样的设计成功、柔度系数的正确求得及据此所建立的试验方法,为该类试验的顺利进行提供了保证。利用试验结果,能够更准确地对服役在腐蚀介质中的船舶进行安全设计和寿命评估。The successful design of the sample for measuring the fatigue crack growth rate in the corrosive solution, the correct calculation of the flexibility coefficient and the test method established accordingly provide a guarantee for the smooth progress of this type of test. Using the test results, the safety design and life assessment of ships serving in corrosive media can be more accurately carried out.

附图说明:Description of drawings:

图1是标准的紧凑拉伸C(T)试样图;Figure 1 is a standard compact tensile C(T) sample diagram;

图2是测量腐蚀液中疲劳裂纹扩展速率的试样及试验方法中所设计的试样图;Fig. 2 is the sample diagram designed in the sample and test method for measuring the fatigue crack growth rate in corrosive liquid;

图3是标准的紧凑拉伸C(T)试样的疲劳裂纹扩展速率(da/dN)-ΔK曲线图;Fig. 3 is the fatigue crack growth rate (da/dN)-ΔK curve diagram of the standard compact tensile C (T) specimen;

图4是测量腐蚀液中疲劳裂纹扩展速率的试样的疲劳裂纹扩展速率(da/dN)-ΔK曲线图。Fig. 4 is a curve diagram of the fatigue crack growth rate (da/dN)-ΔK of the sample for measuring the fatigue crack growth rate in the corrosive solution.

具体实施方式:Detailed ways:

1、测量腐蚀液中疲劳裂纹扩展速率(da/dN)的试样形式1. Sample form for measuring fatigue crack growth rate (da/dN) in corrosive liquid

在腐蚀液中用标准的紧凑拉伸C(T)试样进行疲劳裂纹扩展速率(da/dN)试验,用目测法观测疲劳裂纹长度,一方面通过光学显微镜读到的裂纹长度的精度不能保证,另一方面劳动强度也相当大。如图1中所示,该试样的引伸计装卡刀口(①处)在关于裂纹扩展面对称的两侧。在立式疲劳试验机上测量腐蚀液(②处为腐蚀液面)中的疲劳裂纹扩展速率(da/dN)时,价格昂贵的引伸计往往会受到腐蚀液的侵蚀。如果将引伸计的装卡刀口移动到裂纹扩展面的上侧,首先便可以保证价格昂贵的引伸计不被侵蚀。另外,如果能够求解出这种试样的柔度系数,就可以采用柔度技术来测量腐蚀液中的疲劳裂纹长度,这样就可以保证裂纹长度测量的精度,同时也会大大降低用目测法测量时所付出的大量辛勤劳动。In the corrosive solution, the fatigue crack growth rate (da/dN) test is carried out on the standard compact tensile C(T) specimen, and the fatigue crack length is observed by visual inspection. On the one hand, the accuracy of the crack length read by the optical microscope cannot be guaranteed. On the other hand, the labor intensity is also quite large. As shown in Figure 1, the extensometer clamping knife edge (①) of the sample is on both sides of the symmetric crack propagation plane. When measuring the fatigue crack growth rate (da/dN) in the corrosive liquid (2 is the corrosive liquid level) on the vertical fatigue testing machine, the expensive extensometer is often eroded by the corrosive liquid. If the clamping edge of the extensometer is moved to the upper side of the crack propagation surface, firstly, the expensive extensometer can be guaranteed not to be corroded. In addition, if the flexibility coefficient of this sample can be solved, the fatigue crack length in the corrosive liquid can be measured by the flexibility technology, which can ensure the accuracy of the crack length measurement, and will greatly reduce the visual inspection method. A lot of hard work put in.

于是,在标准的紧凑拉伸C(T)试样的基础上,我们设计出了测量腐蚀液中疲劳裂纹扩展速率(da/dN)的试样,如图2中所示,电子引伸计的装卡刀口(③处)采用整体设计的方法设计在了远离裂纹扩展面的上侧,这样,一方面解决了价格昂贵的电子引伸计遭受腐蚀液(④为腐蚀液面)侵蚀的难题,另一方面也为用柔度技术测量疲劳裂纹长度打下了基础。我们根据试验机控制系统采集到的归一化裂纹长度、试样的无量纲柔度、未知参数柔度系数等大量的试验数据,在严密推理与实践的基础上,充分利用进口设备的多项试验测试软件的功能特点,求解出了所设计试样的柔度系数。所设计试样的典型特征是:将用来间接测量疲劳裂纹长度的电子引伸计装卡刀口采用整体性设计的方法设计在了远离裂纹扩展面的上侧,这样在试验过程中一方面可以保证价格昂贵的引伸计远离腐蚀液面,避免在测量疲劳裂纹长度的过程中因受到腐蚀液侵蚀而降低其线性度、灵敏度或彻底损坏的可能,另一方面也能够较好地保证在整个试验过程中引伸计不会因脱落而使试验失败,同时也便于装卸操作。该试样的设计成功,为在腐蚀液中进行疲劳裂纹扩展速率(da/dN)试验时自动检测裂纹长度提供了可能。Therefore, on the basis of the standard compact tensile C(T) specimen, we designed a specimen for measuring the fatigue crack growth rate (da/dN) in the corrosive solution, as shown in Figure 2, the electronic extensometer The clamping knife edge (3) is designed on the upper side away from the crack propagation surface by the method of overall design, thus, on the one hand, it solves the problem that the expensive electronic extensometer is corroded by the corrosive liquid (4 is the corrosive liquid surface), and on the other hand On the one hand, it also lays the foundation for measuring the fatigue crack length with the flexibility technique. Based on a large amount of test data collected by the control system of the testing machine, such as the normalized crack length, the dimensionless flexibility of the sample, and the flexibility coefficient of unknown parameters, on the basis of strict reasoning and practice, we make full use of the multiple The function characteristics of the test software are used to solve the flexibility coefficient of the designed sample. The typical feature of the designed sample is: the electronic extensometer clamping knife edge used for indirect measurement of the fatigue crack length is designed on the upper side away from the crack propagation surface by the method of integral design, so that on the one hand, it can be guaranteed during the test The expensive extensometer is far away from the corrosive liquid surface, avoiding the possibility of reducing its linearity, sensitivity or complete damage due to the corrosion of the corrosive liquid during the measurement of the fatigue crack length. The middle extensometer will not fail the test due to falling off, and it is also convenient for loading and unloading operations. The successful design of the sample provides the possibility to automatically detect the crack length when performing the fatigue crack growth rate (da/dN) test in the corrosive solution.

2、所设计试样的柔度系数2. The flexibility coefficient of the designed sample

经过大量的推理与试验验证,所求解试样的柔度系数精度高、可靠性强、具有广泛的实用性:可以应用于不同的金属材料、不同试样尺寸的所有和所设计试样形式相同、大小成比例的试样。利用所求解出的六个试样柔度系数,建立起了归一化裂纹长度和柔度系数的函数方程,从理论上为用柔度技术测量疲劳裂纹长度奠定了基础,从而为在腐蚀液中进行疲劳裂纹扩展速率(da/dN)试验时疲劳裂纹长度的自动测量提供了可能。将试验机的控制系统采集到作用在试样上的载荷、引伸计张开位移等必要的数据应用于通过所求理论公式编写的计算机程序,就能随时自动计算出试样当前裂纹的扩展长度,并可时时显示在计算机桌面上。最后经过计算和处理,就可以得到试验材料在腐蚀液中的疲劳裂纹扩展速率。所设计试样柔度系数的求得,使得在腐蚀液中进行疲劳裂纹扩展速率(da/dN)试验时裂纹长度的检测实现了自动化的同时,也明显提高了裂纹长度的测量精度,大大降低了劳动强度。After a lot of reasoning and experimental verification, the flexibility coefficient of the solved sample has high precision, strong reliability, and wide practicability: it can be applied to different metal materials, different sample sizes, and all samples with the same form as the designed sample , Proportional to the size of the sample. The function equation of the normalized crack length and flexibility coefficient was established by using the flexibility coefficients of the six samples solved, which theoretically laid the foundation for the measurement of the fatigue crack length by the flexibility technology, so as to be used in the corrosion solution It is possible to automatically measure the fatigue crack length in the fatigue crack growth rate (da/dN) test. Apply the necessary data collected by the control system of the testing machine such as the load acting on the sample and the opening displacement of the extensometer to the computer program written by the required theoretical formula, and the current crack extension length of the sample can be automatically calculated at any time , and can be displayed on the computer desktop from time to time. Finally, after calculation and processing, the fatigue crack growth rate of the test material in the corrosive solution can be obtained. The determination of the flexibility coefficient of the designed sample makes the detection of the crack length automatic when performing the fatigue crack growth rate (da/dN) test in the corrosive liquid, and at the same time, it also significantly improves the measurement accuracy of the crack length and greatly reduces the crack length. labor intensity.

发明设计试样的柔度系数如下:The flexibility coefficient of the inventive design sample is as follows:

柔度系数符号  C0     C1      C2     C3      C4     C5 Symbol of compliance coefficient C 0 C 1 C 2 C 3 C 4 C 5

柔度系数数值  0.9927  -4.8803  17.031  -189.39  781.63  -821.74Value of flexibility coefficient 0.9927 -4.8803 17.031 -189.39 781.63 -821.74

3、所设计试样柔度系数的求解步骤3. The solution steps of the flexibility coefficient of the designed sample

(1)测量所设计试样的厚度B、宽度W及采用任何方法所引发的有效裂纹长度a,并事先测试出试验材料的弹性模量E;(1) Measure the thickness B, width and the effective crack length a caused by any method of the designed sample, and test the elastic modulus E of the test material in advance;

(2)将所设计的试样采用电火花线切割的方法引发裂纹,每隔a/W=0.025引发一次,并重新测量引发的裂纹长度a,作为所用的实际值;(2) Initiate cracks on the designed sample by wire electric discharge cutting, initiate once every a/W=0.025, and re-measure the induced crack length a, as the actual value used;

(3)将引发裂纹后的试样装在试验机上,并将电子引伸计装卡在试样的刀口处,清零;(3) Install the sample after the crack is induced on the testing machine, and install the electronic extensometer at the knife edge of the sample, and reset it;

(4)对引发裂纹后的试样在弹性范围内缓慢拉伸,此时需要以较高的采点速率(比如100数据点/sec)采集作用在试样上的载荷P、引伸计的变形量V;(4) Slowly stretch the sample after crack initiation within the elastic range. At this time, it is necessary to collect the load P acting on the sample and the deformation of the extensometer at a higher sampling rate (such as 100 data points/sec). volume V;

(5)按照公式Ux=1/[(BEVVx/P)1/2+1]求解出试样的无量纲柔度值Ux;(5) Solve the dimensionless flexibility value Ux of the sample according to the formula Ux=1/[(BEVV x /P) 1/2 +1];

(6)每次引发裂纹后,都要求解出一个归一化裂纹长度a/W值;(6) After each crack is initiated, a normalized crack length a/W value is required to be solved;

(7)当归一化裂纹长度a/W=0.75时(正式试验时该值一般不会超过0.70),试验可以停止;(7) When the normalized crack length a/W=0.75 (the value generally will not exceed 0.70 during the formal test), the test can be stopped;

(8)对所求得的数据组(a/W,Ux)进行一元五次递增多项式回归,其回归系数便可以作为该试样的柔度系数;(8) Carry out a quintic incremental polynomial regression on the obtained data set (a/W, Ux), and its regression coefficient can be used as the flexibility coefficient of the sample;

(9)对多块试样按如上步骤进行,可以分别得到各个试样的六个柔度系数;(9) Carry out the above steps for multiple samples, and six flexibility coefficients of each sample can be obtained respectively;

(10)对多块试样的柔度系数进行均值化处理,就得到了最终所求解的六个柔度系数C0、C1、C2、C3、C4、C5(10) The compliance coefficients of multiple samples are averaged to obtain the final six compliance coefficients C 0 , C 1 , C 2 , C 3 , C 4 , and C 5 .

4、试验方法4. Test method

利用所设计出的试样及其柔度系数,按照下列步骤就可以完成在腐蚀液中进行的疲劳裂纹扩展速率(da/dN)试验:Using the designed sample and its flexibility coefficient, the fatigue crack growth rate (da/dN) test in the corrosive solution can be completed according to the following steps:

(1)采用电火花线切割的方式引发试样的初始裂纹;(1) The initial crack of the sample is induced by wire electric discharge cutting;

(2)将求解出的所设计试样的柔度系数输入到事先编好的试验程序中;(2) Input the calculated flexibility coefficient of the designed sample into the pre-programmed test program;

(3)测量试样厚度、宽度等参数,并输入到事先编好的程序中;(3) Measure parameters such as sample thickness and width, and input them into the pre-programmed program;

(4)将腐蚀循环系统、相关的试样卡具及试样与立式疲劳试验机相连接;(4) Connect the corrosion circulation system, related sample fixtures and samples with the vertical fatigue testing machine;

(5)将腐蚀液加入循环系统和装有试样的腐蚀盒中,循环系统中的腐蚀液要足够多,腐蚀盒中的腐蚀液要保证时时浸泡住裂纹扩展面;(5) Add the corrosive solution to the circulation system and the corrosion box containing the sample. The corrosive solution in the circulation system should be sufficient, and the corrosive solution in the corrosion box should be guaranteed to soak the crack propagation surface from time to time;

(6)将电子引伸计装卡在试样上侧的刀口处;(6) Install the electronic extensometer at the knife edge on the upper side of the sample;

(7)设置好预制疲劳裂纹的各个参数,包括应力强度因子范围ΔK、控制方式、采用频率、波形及预制疲劳裂纹的长度等;(7) Set various parameters of prefabricated fatigue cracks, including stress intensity factor range ΔK, control mode, frequency, waveform and length of prefabricated fatigue cracks, etc.;

(8)启动试验机,开始预制疲劳裂纹,时时观测当前的裂纹扩展长度,注意整个腐蚀循环系统,以防腐蚀液渗漏而侵蚀试验机;(8) Start the testing machine, start prefabricating fatigue cracks, observe the current crack extension length from time to time, pay attention to the entire corrosion cycle system, to prevent corrosion of the testing machine due to leakage of corrosive liquid;

(9)预制完成疲劳裂纹后,根据当前的结果,设定试验时所需要的载荷范围、应力比、频率等参数;(9) After the fatigue cracks are prefabricated, according to the current results, set the required load range, stress ratio, frequency and other parameters for the test;

(10)再次启动试验机,开始正式试验;(10) Start the testing machine again and start the formal test;

(11)试验结束后,根据所采集到的试验数据,按照帕里斯(Paris)经验方程的表达形式拟合出试验材料的疲劳裂纹扩展速率曲线及其方程,最后出具相应的试验报告。(11) After the test, according to the collected test data, fit the fatigue crack growth rate curve and equation of the test material according to the expression form of the Paris (Paris) empirical equation, and finally issue the corresponding test report.

从我们发明设计的试样形式可以看到,该试样可以无庸置疑地用在腐蚀液中的疲劳试验而保证电子引伸计不被腐蚀液所侵蚀。为了验证所设计试样柔度系数及试验方法的正确性与可行性,我们选择了一种结构钢材料,加工成了一组标准的紧凑拉伸试样和一组我们发明设计的试样。由于在立式试验机上标准的紧凑拉伸试样在腐蚀液中无法测量试验材料的疲劳裂纹扩展速率,而金属材料在空气中和在腐蚀液中的疲劳裂纹扩展速率又往往相差很大。因此,我们认为,如果用标准的紧凑拉伸试样用柔度技术在空气中测试了试验材料的疲劳裂纹扩展速率(da/dN),然后再用我们发明设计的试样及其柔度系数采用同样的试验条件进行测试,由于试验材料是一样的,如果测试结果的一致性很好,就能够表明我们所发明的试样及试验方法是正确的。It can be seen from the sample form of our invention that the sample can undoubtedly be used in the fatigue test in the corrosive solution to ensure that the electronic extensometer is not corroded by the corrosive solution. In order to verify the correctness and feasibility of the designed specimen flexibility coefficient and test method, we selected a structural steel material and processed it into a set of standard compact tensile specimens and a set of specimens designed by us. Since the standard compact tensile specimen on the vertical testing machine cannot measure the fatigue crack growth rate of the test material in the corrosive solution, and the fatigue crack growth rate of the metal material in the air and in the corrosive solution is often very different. Therefore, we believe that if the fatigue crack growth rate (da/dN) of the test material is tested in air using the compliance technique with standard compact tensile specimens, then with our inventively designed specimen and its coefficient of compliance Using the same test conditions to test, since the test materials are the same, if the consistency of the test results is very good, it can show that the sample and test method we invented are correct.

试验设备为立式的MTS810电液伺服疲劳试验机。The test equipment is a vertical MTS810 electro-hydraulic servo fatigue testing machine.

采用上述试验方法步骤进行试验。The test was carried out using the steps of the above-mentioned test method.

采用的试验条件如下:The test conditions used are as follows:

试验载荷范围ΔP=12.0KN,应力比R=0.1,波形为正弦波,频率f=10Hz,室温空气中试验。Test load range ΔP = 12.0KN, stress ratio R = 0.1, waveform is sine wave, frequency f = 10Hz, test in air at room temperature.

试验结果(包括da/dN-ΔK曲线图及其方程)如图3和图4中所示,从图3和图4可见,两种试样的数据组(da/dN,ΔK)的分布完全一样。考虑到试验材料的组织均匀性及每块试样的加工误差,得到的试验材料在两种不同试样形式下(对应不同的柔度系数)的裂纹扩展速率是一致的。这充分表明,我们所设计发明的测量腐蚀液中金属材料的疲劳裂纹扩展速率的试样是实用的,柔度系数是可靠的,所建立起来的试验方法具有可靠性和可行性。The test results (including the da/dN-ΔK curve diagram and its equation) are shown in Figure 3 and Figure 4, as can be seen from Figure 3 and Figure 4, the distribution of the data sets (da/dN, ΔK) of the two samples is completely Same. Considering the uniformity of the structure of the test material and the processing error of each sample, the crack growth rate of the obtained test material in two different sample forms (corresponding to different flexibility coefficients) is consistent. This fully shows that the sample we designed and invented to measure the fatigue crack growth rate of metal materials in corrosive liquid is practical, the flexibility coefficient is reliable, and the established test method is reliable and feasible.

Claims (3)

1、一种测量腐蚀液中疲劳裂纹扩展速率的试样,其特征在于:所述的试样,在其试样远离裂纹扩展面的上侧采用整体设计的方法设置有电子引伸计的装卡刀口;根据试验机控制系统采集到的大量的试验数据,利用进口设备的多项试验测试软件,求解出所设计试样的柔度系数如下:1. A sample for measuring the fatigue crack growth rate in corrosive liquid, characterized in that: the sample is provided with a clamping device for an electronic extensometer on the upper side of the sample away from the crack propagation surface by adopting an overall design method Knife edge: According to a large amount of test data collected by the control system of the testing machine, using a number of test software of imported equipment, the flexibility coefficient of the designed sample is calculated as follows: 柔度系数符号  C0     C1      C2     C3     C4    C5 Symbol of compliance coefficient C 0 C 1 C 2 C 3 C 4 C 5 柔度系数数值  0.9927  -4.8803  17.031  -189.39 781.63 -821.74Flexibility coefficient value 0.9927 -4.8803 17.031 -189.39 781.63 -821.74 同时,建立归一化裂纹长度和柔度系数之间的函数关系,实现在腐蚀液中进行疲劳裂纹扩展速率(da/dN)试验时裂纹长度的检测自动化。At the same time, the functional relationship between the normalized crack length and the flexibility coefficient is established to realize the automatic detection of the crack length when performing the fatigue crack growth rate (da/dN) test in the corrosive solution. 2、实施权利要求1所述的测量腐蚀液中疲劳裂纹扩展速率的试样的试验方法,其特征在于:该试验方法按照下列步骤进行:2, implement the test method of the sample of fatigue crack growth rate in the measurement corrosion solution described in claim 1, it is characterized in that: this test method is carried out according to the following steps: (1)采用电火花线切割的方式引发试样的初始裂纹;(1) The initial crack of the sample is induced by wire electric discharge cutting; (2)将求解出的所设计试样的柔度系数输入到事先编好的试验程序中;(2) Input the calculated flexibility coefficient of the designed sample into the pre-programmed test program; (3)测量试样厚度、宽度参数,并输入到事先编好的程序中;(3) Measure the thickness and width parameters of the sample, and input them into the pre-programmed program; (4)将腐蚀循环系统、相关的试样卡具及试样与立式疲劳试验机相连接;(4) Connect the corrosion circulation system, related sample fixtures and samples with the vertical fatigue testing machine; (5)将腐蚀液加入循环系统和装有试样的腐蚀盒中,循环系统中的腐蚀液要足够多,腐蚀盒中的腐蚀液要保证时时浸泡住裂纹扩展面;(5) Add the corrosive solution to the circulation system and the corrosion box containing the sample. The corrosive solution in the circulation system should be sufficient, and the corrosive solution in the corrosion box should be guaranteed to soak the crack propagation surface from time to time; (6)将电子引伸计装卡在试样上侧的刀口处;(6) Install the electronic extensometer at the knife edge on the upper side of the sample; (7)设置好预制疲劳裂纹的各个参数,包括应力强度因子范围ΔK、控制方式、采用频率、波形及预制疲劳裂纹的长度;(7) Set various parameters of prefabricated fatigue cracks, including stress intensity factor range ΔK, control mode, frequency, waveform and length of prefabricated fatigue cracks; (8)启动试验机,开始预制疲劳裂纹,时时观测当前的裂纹扩展长度,注意整个腐蚀循环系统,以防腐蚀液渗漏而侵蚀试验机;(8) Start the testing machine, start prefabricating fatigue cracks, observe the current crack extension length from time to time, pay attention to the entire corrosion cycle system, to prevent corrosion of the testing machine due to leakage of corrosive liquid; (9)预制完成疲劳裂纹后,根据当前的结果,设定试验时所需要的载荷范围、应力比、频率的参数;(9) After the fatigue cracks are prefabricated, according to the current results, set the parameters of the load range, stress ratio, and frequency required for the test; (10)再次启动试验机,开始正式试验;(10) Start the testing machine again and start the formal test; (11)试验结束后,根据所采集到的试验数据,按照帕里斯(Paris)经验方程的表达形式拟合出试验材料的疲劳裂纹扩展速率曲线及其方程,最后出具相应的试验报告。(11) After the test, according to the collected test data, fit the fatigue crack growth rate curve and equation of the test material according to the expression form of the Paris (Paris) empirical equation, and finally issue the corresponding test report. 3、根据权利要求1所述的测量腐蚀液中疲劳裂纹扩展速率的试样,其特征在于:该试样柔度系数的求解步骤如下:3. The sample for measuring the fatigue crack growth rate in corrosive liquid according to claim 1, characterized in that: the steps for solving the flexibility coefficient of the sample are as follows: (1)测量所设计试样的厚度B、宽度W及采用任何方法所引发的有效裂纹长度a,并事先测试出试验材料的弹性模量E;(1) Measure the thickness B, width and the effective crack length a caused by any method of the designed sample, and test the elastic modulus E of the test material in advance; (2)将所设计的试样采用电火花线切割的方法引发裂纹,每隔a/W=0.025引发一次,并重新测量引发的裂纹长度a,作为所用的实际值;(2) Initiate cracks on the designed sample by wire electric discharge cutting, initiate once every a/W=0.025, and re-measure the induced crack length a, as the actual value used; (3)将引发裂纹后的试样装在试验机上,并将电子引伸计装卡在试样的刀口处,清零;(3) Install the sample after the crack is induced on the testing machine, and install the electronic extensometer at the knife edge of the sample, and reset it; (4)对引发裂纹后的试样在弹性范围内缓慢拉伸,此时需要以较高的采点速率采集作用在试样上的载荷P、引伸计的变形量V;(4) Slowly stretch the sample after crack initiation within the elastic range. At this time, it is necessary to collect the load P acting on the sample and the deformation V of the extensometer at a higher sampling rate; (5)按照公式Ux=1/[(BEVx/P)1/2+1]求解出试样的无量纲柔度值Ux;(5) Solve the dimensionless flexibility value Ux of the sample according to the formula Ux=1/[(BEV x /P) 1/2 +1]; (6)每次引发裂纹后,都要求解出一个归一化裂纹长度a/W值;(6) After each crack is initiated, a normalized crack length a/W value is required to be solved; (7)当归一化裂纹长度a/W=0.75时,试验可以停止;(7) When the normalized crack length a/W=0.75, the test can be stopped; (8)对所求得的数据组(a/W,Ux)进行一元五次递增多项式回归,其回归系数便可以作为该试样的柔度系数;(8) Carry out a quintic incremental polynomial regression on the obtained data set (a/W, Ux), and its regression coefficient can be used as the flexibility coefficient of the sample; (9)对多块试样按如上步骤进行,可分别得到各个试样的六个柔度系数;(9) Carry out the above steps for multiple samples, and six flexibility coefficients of each sample can be obtained respectively; (10)对多块试样的柔度系数进行均值化处理,就得到了最终所求解的六个柔度系数C0、C1、C2、C3、C4、C5(10) The compliance coefficients of multiple samples are averaged to obtain the final six compliance coefficients C 0 , C 1 , C 2 , C 3 , C 4 , and C 5 .
CN 200410060569 2004-10-14 2004-10-14 Sample for measuring fatigue crack expansion rate in corrosion liquid and test method Expired - Fee Related CN1278114C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 200410060569 CN1278114C (en) 2004-10-14 2004-10-14 Sample for measuring fatigue crack expansion rate in corrosion liquid and test method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 200410060569 CN1278114C (en) 2004-10-14 2004-10-14 Sample for measuring fatigue crack expansion rate in corrosion liquid and test method

Publications (2)

Publication Number Publication Date
CN1587988A true CN1587988A (en) 2005-03-02
CN1278114C CN1278114C (en) 2006-10-04

Family

ID=34603486

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 200410060569 Expired - Fee Related CN1278114C (en) 2004-10-14 2004-10-14 Sample for measuring fatigue crack expansion rate in corrosion liquid and test method

Country Status (1)

Country Link
CN (1) CN1278114C (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102426137A (en) * 2011-08-31 2012-04-25 中国船舶重工集团公司第七二五研究所 Testing and measuring method capable of axially loading low cycle fatigue crack initiation
CN103439202A (en) * 2013-08-19 2013-12-11 北京航空航天大学 System for testing fatigue in corrosion environment
CN103439199A (en) * 2013-08-19 2013-12-11 北京航空航天大学 System for testing fatigue crack propagation in corrosion environment
CN103884610A (en) * 2012-12-21 2014-06-25 中国直升机设计研究所 Determination method of composite material II-type cracking threshold value and S-N curve
CN104404582A (en) * 2014-11-19 2015-03-11 中国航空工业集团公司沈阳飞机设计研究所 Method for optimizing high-corrosion resistance cadmium titanium plating layers of ultrahigh-strength steel
CN104458562A (en) * 2014-11-28 2015-03-25 中国航空工业集团公司北京航空材料研究院 Measuring method for opening stress of crack
CN104704342A (en) * 2012-09-04 2015-06-10 斯奈克玛 High frequency method for determining the non-propagation threshold of fatigue cracks
CN110376062A (en) * 2019-07-22 2019-10-25 中国航发沈阳发动机研究所 A kind of resonant fatigue test crackle pre-setting method
CN110987634A (en) * 2019-11-15 2020-04-10 河海大学 Test device and test method for hydraulic fracture of gravel-doped core wall
CN111665132A (en) * 2020-06-17 2020-09-15 天津大学 Method for measuring fatigue crack propagation of opening corner
CN113514353A (en) * 2021-04-25 2021-10-19 中信戴卡股份有限公司 A kind of crack monitoring equipment and test equipment for automobile fatigue test
CN116840084A (en) * 2023-06-30 2023-10-03 华东理工大学 Method and system for rapidly evaluating stress corrosion sensitivity of fatigue damage component

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102426137B (en) * 2011-08-31 2013-06-05 中国船舶重工集团公司第七二五研究所 Testing and measuring method capable of axially loading low cycle fatigue crack initiation
CN102426137A (en) * 2011-08-31 2012-04-25 中国船舶重工集团公司第七二五研究所 Testing and measuring method capable of axially loading low cycle fatigue crack initiation
CN104704342A (en) * 2012-09-04 2015-06-10 斯奈克玛 High frequency method for determining the non-propagation threshold of fatigue cracks
CN104704342B (en) * 2012-09-04 2017-11-07 斯奈克玛 For the high-frequency methods for the non-propagating threshold value for determining fatigue crack
CN103884610A (en) * 2012-12-21 2014-06-25 中国直升机设计研究所 Determination method of composite material II-type cracking threshold value and S-N curve
CN103884610B (en) * 2012-12-21 2016-06-29 中国直升机设计研究所 A kind of composite II type cracking threshold and S-N curve determination method
CN103439199A (en) * 2013-08-19 2013-12-11 北京航空航天大学 System for testing fatigue crack propagation in corrosion environment
CN103439202A (en) * 2013-08-19 2013-12-11 北京航空航天大学 System for testing fatigue in corrosion environment
CN104404582A (en) * 2014-11-19 2015-03-11 中国航空工业集团公司沈阳飞机设计研究所 Method for optimizing high-corrosion resistance cadmium titanium plating layers of ultrahigh-strength steel
CN104458562A (en) * 2014-11-28 2015-03-25 中国航空工业集团公司北京航空材料研究院 Measuring method for opening stress of crack
CN110376062A (en) * 2019-07-22 2019-10-25 中国航发沈阳发动机研究所 A kind of resonant fatigue test crackle pre-setting method
CN110987634A (en) * 2019-11-15 2020-04-10 河海大学 Test device and test method for hydraulic fracture of gravel-doped core wall
CN111665132A (en) * 2020-06-17 2020-09-15 天津大学 Method for measuring fatigue crack propagation of opening corner
CN113514353A (en) * 2021-04-25 2021-10-19 中信戴卡股份有限公司 A kind of crack monitoring equipment and test equipment for automobile fatigue test
CN116840084A (en) * 2023-06-30 2023-10-03 华东理工大学 Method and system for rapidly evaluating stress corrosion sensitivity of fatigue damage component

Also Published As

Publication number Publication date
CN1278114C (en) 2006-10-04

Similar Documents

Publication Publication Date Title
CN1587988A (en) Sample for measuring fatigue crack expansion rate in corrosion liquid and test method
CN104075941B (en) Fracture toughness of brittle materials and residual stress in-situ synchronization method of testing and device
CN110672441A (en) Characterization method of crack tip state in fatigue crack propagation process
CN105784521B (en) A kind of full-automatic injection resistance meter of concrete and setting time measurement method
CN102393341A (en) Device for testing hardness, fracture toughness and residual stress of brittle material with indentation method
CN107860707A (en) The heteropical method of aluminum alloy surface microcell galvanic corrosion is characterized using wire beam electrode
CN102426137B (en) Testing and measuring method capable of axially loading low cycle fatigue crack initiation
CN108375595B (en) Test method for surface stress distribution of metal workpieces along the depth direction
CN104777046B (en) Fatigue crack propagation mechanism testing method based on small time scale
CN109520856A (en) A kind of small sample On Creep Crack Growth test method
CN105021455A (en) Experimental apparatus for simulating stress corrosion of metal material under actual working conditions
CN111965022B (en) Device and method for evaluating hydrogen induced crack propagation behavior under force-electricity coupling
CN110595908A (en) Quasi-in-situ test method for high-temperature loss-delay cracking of a nickel-based alloy welding material
CN204731205U (en) A kind of casting ultrasonic flaw detection artificial defect Determination mechanism
CN206891852U (en) A kind of cantilever bending fatigue experimental device and home position observation device
CN103969128A (en) Method for detecting bending mechanical property of sample
CN1766550A (en) Evaluation Method of Critical Stress Intensity and Sensitivity Factor of Stress Corrosion Cracking of Oil Well Pipe
TWI855411B (en) Method and system for measuring the depth of a damaged layer on a wafer surface
CN116840084A (en) Method and system for rapidly evaluating stress corrosion sensitivity of fatigue damage component
CN209182151U (en) A Measuring Device for Apparent Resistivity in Rock Damage and Destruction Test
CN104502273A (en) Method for representing bonding strength of hard film through interfacial stress of elasticoplastic deformation
CN115406820A (en) Indoor accelerated environmental damage detection and evaluation method for aluminum alloy threaded part
CN111141612B (en) Device and method for testing hydrogen sulfide stress corrosion resistance of oil well pipe
CN201955329U (en) Ultrasonic detecting equipment
CN205562458U (en) Simple and easy electrochemistry testing arrangement

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
EE01 Entry into force of recordation of patent licensing contract

Assignee: Luoyang Qiwei Anti-Corrosion Engineering Material Co., Ltd.

Assignor: No.725 Inst. China Shipping Heavy Industry Group Corp.

Contract fulfillment period: 2008.8.12 to 2016.8.11 contract change

Contract record no.: 2008410000032

Denomination of invention: Sample for measuring fatigue crack expansion rate in corrosion liquid and test method

Granted publication date: 20061004

License type: Exclusive license

Record date: 20081112

LIC Patent licence contract for exploitation submitted for record

Free format text: EXCLUSIVE LICENSE; TIME LIMIT OF IMPLEMENTING CONTACT: 2008.8.12 TO 2016.8.11; CHANGE OF CONTRACT

Name of requester: LUOYANG QIWEI CORROSION PROTECTION ENGINEERING MAT

Effective date: 20081112

C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20061004

Termination date: 20091116