CN104007028B - Micro-member tensile test device - Google Patents
Micro-member tensile test device Download PDFInfo
- Publication number
- CN104007028B CN104007028B CN201410271032.5A CN201410271032A CN104007028B CN 104007028 B CN104007028 B CN 104007028B CN 201410271032 A CN201410271032 A CN 201410271032A CN 104007028 B CN104007028 B CN 104007028B
- Authority
- CN
- China
- Prior art keywords
- micro
- fixedly connected
- carrying platform
- fixed
- article carrying
- 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
Links
- 238000009864 tensile test Methods 0.000 title claims abstract description 11
- 230000003068 static effect Effects 0.000 claims abstract description 21
- 238000005259 measurement Methods 0.000 claims abstract description 9
- 239000000919 ceramic Substances 0.000 claims description 11
- 229910000831 Steel Inorganic materials 0.000 claims description 6
- 239000010959 steel Substances 0.000 claims description 6
- 238000012360 testing method Methods 0.000 abstract description 27
- 238000009434 installation Methods 0.000 abstract description 7
- 238000000034 method Methods 0.000 description 14
- 210000003128 head Anatomy 0.000 description 13
- 239000000463 material Substances 0.000 description 6
- 238000006073 displacement reaction Methods 0.000 description 4
- 238000013461 design Methods 0.000 description 3
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 2
- 238000005452 bending Methods 0.000 description 2
- 238000003801 milling Methods 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 238000010998 test method Methods 0.000 description 2
- 239000000956 alloy Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000009661 fatigue test Methods 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 238000011065 in-situ storage Methods 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000004579 marble Substances 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 230000005476 size effect Effects 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 210000003454 tympanic membrane Anatomy 0.000 description 1
Landscapes
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
Abstract
微构件拉伸测试装置,涉及一种微构件力学性能测试装置。本发明可实现对微米尺度构件的力学性能静态参量测量及疲劳特性的探究。两根导轨固定在L形底座上;精密驱动单元固定在右载物平台上,动载物台与精密驱动单元固接,静、动载物台上有一用于固定微构件的定位槽,静载物台与微力传感器固接,微力传感器与力传感器固定块固接,力传感器固定块与左载物平台固接,光栅尺安装在精密驱动单元前侧或后侧面上,右载物平台上固定有读数头安装架,度数头固定在读数头安装架上;右载物平台与丝杠螺母副的丝杠螺母固接,右载物平台通过四个右滑块与两根导轨滑动连接,步进电机驱动丝杠螺母副运动,左载物平台相对导轨固定不动。本发明用于微构件力学性能测试。
The utility model relates to a micro-component tensile testing device, relating to a micro-component mechanical property testing device. The invention can realize the measurement of the static parameters of the mechanical properties of the micron-scale components and the exploration of the fatigue characteristics. The two guide rails are fixed on the L-shaped base; the precision drive unit is fixed on the right loading platform, the moving stage is fixedly connected with the precision driving unit, and there is a positioning groove for fixing micro components on the static and moving stages. The stage is fixedly connected to the micro force sensor, the micro force sensor is fixed to the force sensor fixed block, the force sensor fixed block is fixed to the left loading platform, the grating scale is installed on the front or rear side of the precision drive unit, and the right loading platform The reading head installation frame is fixed, and the degree head is fixed on the reading head installation frame; the right loading platform is fixedly connected with the screw nut of the screw nut pair, and the right loading platform is slidingly connected with two guide rails through four right sliders. The stepper motor drives the lead screw nut pair to move, and the left loading platform is fixed relative to the guide rail. The invention is used for testing the mechanical properties of micro components.
Description
技术领域 technical field
本发明涉及一种微构件力学性能测试装置。 The invention relates to a device for testing the mechanical properties of micro components.
背景技术 Background technique
惯导系统高弹性合金微构件在地面加载测试中极容易断裂失效,惯性传感器中微构件的特征尺寸大致在亚微米到毫米的范围内。当细微到微米/纳米尺度后,由于尺寸效应,微构件材料本身的物理性质及其受环境影响的程度等都会发生很大改变,其力学特性以及所受体积力和表面力的相对关系等也会发生显著的变化。宏观条件下材料的力学性能参数已远远不能满足MEMS系统结构的设计要求,而由微小试件带来的一系列技术问题使得传统的测试方法和装置也已不再适用。 The highly elastic alloy micro-components of the inertial navigation system are very easy to fracture and fail in the ground loading test, and the characteristic size of the micro-components in the inertial sensor is roughly in the range of submicron to millimeter. When it is micron/nanoscale, due to the size effect, the physical properties of the micro-component material itself and the degree to which it is affected by the environment will change greatly, and its mechanical properties and the relative relationship between the body force and surface force will also change. Significant changes will occur. The mechanical performance parameters of materials under macroscopic conditions are far from meeting the design requirements of MEMS system structures, and a series of technical problems caused by tiny test pieces make traditional testing methods and devices no longer applicable.
近年来,国内外学者越来越重视微构件材料力学性能的研究,提出了一些新的测试方法和测试装置。但是,各种方法测得的数据分散性较大,甚至连最基础的弹性模量都没有一个一致公认的结果。在微构件设计和进行可靠性分析时,由于缺乏有关微构件材料力学性能的基础数据,目前还没有建立起一个有效的设计准则,导致成品率低,可靠性差,这严重阻碍了MEMS的发展。 In recent years, scholars at home and abroad have paid more and more attention to the research on the mechanical properties of micro-component materials, and proposed some new testing methods and testing devices. However, the data measured by various methods are highly dispersed, and even the most basic modulus of elasticity does not have a consistent and recognized result. In micro-component design and reliability analysis, due to the lack of basic data on the mechanical properties of micro-component materials, an effective design criterion has not been established, resulting in low yield and poor reliability, which seriously hinders the development of MEMS.
材料的力学性能测试中常用的方法包括单轴拉伸法、纳米压痕法、鼓膜法、微梁弯曲法和衬底曲率法等。其中,最常用的方法是单轴拉伸法,微拉伸实验是测量微米级材料弹性模量、泊松比、屈服强度和断裂强度最直接的方法,拉伸实验的数据容易解释,测试结果比弯曲实验可靠。但是由于试样尺寸微小,微构件的对中、装夹、微位移驱动以及微小载荷和微位移的测量等一系列技术难题使得传统的测试方法和装置也已不再适用。目前测试装置还没有统一的标准,而且大部分测试装置结构都比较复杂,所需仪器都很昂贵,测试数据分散性很大。如何最大限度的减少测试误差,保证获得精确一致的测试结果,提高测试效率,使测试数据能够迅速加以处理而进行反馈监控或直接应用于生产实践,这些问题对科研人员来说是亟待突破的难关也是挑战。 The commonly used methods in testing the mechanical properties of materials include uniaxial tensile method, nanoindentation method, tympanic membrane method, microbeam bending method and substrate curvature method, etc. Among them, the most commonly used method is the uniaxial tensile method. The micro-tensile test is the most direct method to measure the elastic modulus, Poisson's ratio, yield strength and breaking strength of micron-scale materials. The data of the tensile test is easy to interpret, and the test results More reliable than bending experiments. However, due to the small size of the sample, a series of technical difficulties such as the centering, clamping, micro-displacement driving of micro-components, and the measurement of micro-load and micro-displacement make traditional testing methods and devices no longer applicable. At present, there is no uniform standard for testing devices, and most of the testing devices have complex structures, expensive instruments, and large dispersion of test data. How to minimize test errors, ensure accurate and consistent test results, improve test efficiency, and enable test data to be processed quickly for feedback monitoring or directly applied to production practice, these problems are difficulties that need to be overcome urgently for researchers It is also a challenge.
发明内容 Contents of the invention
本发明的目的是提供一种微构件拉伸测试装置,以实现对微米尺度构件的力学性能静态参量测量及疲劳特性的探究。 The purpose of the present invention is to provide a micro-component tensile testing device to realize the measurement of static parameters of mechanical properties of micro-scale components and the exploration of fatigue characteristics.
本发明解决上述问题采取的技术方案是: The technical scheme that the present invention solves the problems referred to above is:
本发明的微构件拉伸测试装置,它包括精密驱动单元、微力传感器、直线光栅测量装置、高精度电移台、载物台、力传感器固定块、两个固定件,所述的高精度电移台包括左载物平台、右载物平台、丝杠螺母副、L形底座、支撑座、步进电机、四个左滑块、四个右滑块、两根导轨,所述的载物台包括动载物台和静载物台,所述的直线光栅测量装置包括光栅尺读数头安装架、读数头和光栅尺, The micro-component tensile testing device of the present invention includes a precision drive unit, a micro-force sensor, a linear grating measuring device, a high-precision electric stage, a stage, a force sensor fixing block, and two fixing pieces. The high-precision electric The moving table includes a left loading platform, a right loading platform, a screw nut pair, an L-shaped base, a support seat, a stepping motor, four left sliders, four right sliders, and two guide rails. The stage includes a moving object stage and a static stage, and the linear grating measuring device includes a grating ruler reading head installation frame, a reading head and a grating ruler,
所述的L形底座的长板水平设置,所述的两根导轨平行于L形底座的长边并固定在L形底座的长板上;所述的左载物平台和右载物平台左右并列设置,所述的精密驱动单元固定在右载物平台上表面,所述的动载物台与精密驱动单元的左侧面固定连接,所述的静载物台与动载物台相邻且相对应设置,静载物台与动载物台的上表面对应位置分别加工有一用于固定微构件的定位槽;所述的静载物台、微力传感器及力传感器固定块由右至左依次设置在左载物平台的上表面,且静载物台与微力传感器固定连接,微力传感器与力传感器固定块固定连接,力传感器固定块与左载物平台的上表面固定连接,所述的光栅尺安装在精密驱动单元的前侧面或后侧面上,右载物平台上与光栅尺位于同侧的侧面上固定有读数头安装架,所述的度数头与光栅尺相对设置并固定在读数头安装架上;所述的右载物平台的下表面与丝杠螺母副的螺母固定连接,丝杠螺母副的丝杠一端与支撑座转动连接,丝杠螺母副的丝杠另一端与L形底座的短板转动连接,支撑座与L形底座的长板固定连接,右载物平台的下表面与呈矩形设置的四个右滑块固定连接,四个右滑块与两根导轨滑动连接,所述的步进电机固定于L形底座的短板上,步进电机驱动丝杠螺母副运动;左载物平台的下表面与呈矩形设置的四个左滑块固定连接,四个左滑块设置在两根导轨上,设置在同一根导轨上的两个左滑块之间安装有一与导轨固定连接的固定件,工作中左载物平台相对导轨固定不动,右载物平台相对导轨进行运动。 The long plate of the L-shaped base is arranged horizontally, and the two guide rails are parallel to the long sides of the L-shaped base and fixed on the long plate of the L-shaped base; the left loading platform and the right loading platform are left and right Arranged side by side, the precision driving unit is fixed on the upper surface of the right loading platform, the moving loading platform is fixedly connected to the left side of the precision driving unit, and the static loading platform is adjacent to the moving loading platform And set correspondingly, the corresponding positions of the upper surface of the static stage and the moving stage are respectively processed with a positioning groove for fixing the micro components; the static stage, the micro force sensor and the force sensor fixing block are arranged from right to left They are sequentially arranged on the upper surface of the left loading platform, and the static loading platform is fixedly connected with the micro force sensor, the micro force sensor is fixedly connected with the force sensor fixed block, and the force sensor fixed block is fixedly connected with the upper surface of the left object loading platform. The grating ruler is installed on the front side or rear side of the precision drive unit, and the reading head installation frame is fixed on the side on the same side as the grating ruler on the right loading platform, and the degree head is set opposite to the grating ruler and fixed on the reading head. On the head mounting frame; the lower surface of the right loading platform is fixedly connected with the nut of the lead screw nut pair, one end of the lead screw of the lead screw nut pair is rotatably connected with the support seat, and the other end of the lead screw of the lead screw nut pair is connected to the L The short plate of the L-shaped base is rotatably connected, the support seat is fixedly connected with the long plate of the L-shaped base, the lower surface of the right loading platform is fixedly connected with four right sliders arranged in a rectangular shape, and the four right sliders slide with two guide rails connection, the stepper motor is fixed on the short plate of the L-shaped base, and the stepper motor drives the screw nut pair to move; the lower surface of the left loading platform is fixedly connected with four left sliders arranged in a rectangular shape, and the four The left slider is set on two guide rails, and there is a fixing piece fixedly connected with the guide rails between the two left sliders set on the same guide rail. During operation, the left loading platform is fixed relative to the guide rails, and the right loading platform Movement relative to the guide rail.
本发明相对于现有技术的有益效果是:本发明不仅可实现微构件微拉伸静态测试,并且与动态测试结合,利用精密驱动单元带动动载物台对微构件进行0-4kHz的拉拉疲劳加载,微构件夹持可靠;采用高精度的力传感器(精度5mN),实现载荷的精确测量;采用高精度直线光栅测量装置实现微位移的精确检测,分辨率为5nm,便于安装调试。该装置不仅能实现微构件静态参量的测量,如弹性模量、屈服强度、断裂强度的测量,而且还能实现对疲劳特性的探究,如疲劳强度。 Compared with the prior art, the beneficial effect of the present invention is: the present invention can not only realize the micro-stretch static test of the micro-component, but also combine with the dynamic test, and use the precision drive unit to drive the moving stage to pull the micro-component at 0-4kHz Fatigue loading, reliable clamping of micro-components; high-precision force sensor (accuracy 5mN) to achieve accurate measurement of load; high-precision linear grating measurement device to achieve accurate detection of micro-displacement, with a resolution of 5nm, easy to install and debug. The device can not only realize the measurement of static parameters of micro-components, such as the measurement of elastic modulus, yield strength, and fracture strength, but also realize the exploration of fatigue characteristics, such as fatigue strength.
附图说明 Description of drawings
图1是本发明的微构件拉伸测试装置的总体装配图; Fig. 1 is the overall assembly drawing of micro-component tensile testing device of the present invention;
图2是图1中的精密驱动单元装配图; Fig. 2 is an assembly drawing of the precision drive unit in Fig. 1;
图3是图1的A处局部放大图。 FIG. 3 is a partial enlarged view of A in FIG. 1 .
上述图中涉及到的部件名称及标号分别为: The names and labels of the components involved in the above figure are:
L形底座1、步进电机2、支撑座3、力传感器固定块4、微力传感器5、静载物台6、微构件7、动载物台8、精密驱动单元9、柔性铰链9-1、垫片9-2、钢珠9-3、安装孔9-4、预紧螺钉9-5、压电陶瓷9-6、丝杠螺母副10、右载物平台11、右滑块12、光栅尺读数头安装架13、导轨14、读数头15、光栅尺16、固定件17、左滑块18、左载物平台19。 L-shaped base 1, stepping motor 2, support seat 3, force sensor fixed block 4, micro force sensor 5, static stage 6, micro component 7, moving stage 8, precision drive unit 9, flexible hinge 9-1 , Gasket 9-2, Steel Ball 9-3, Mounting Hole 9-4, Pretightening Screw 9-5, Piezoelectric Ceramic 9-6, Screw Nut Pair 10, Right Loading Platform 11, Right Slider 12, Grating Ruler reading head installation frame 13, guide rail 14, reading head 15, grating ruler 16, fixture 17, left slide block 18, left loading platform 19.
具体实施方式 detailed description
如图1~图3所示,微构件拉伸测试装置,它包括精密驱动单元9、微力传感器5、直线光栅测量装置、高精度电移台、载物台、力传感器固定块4、两个固定件17,所述的高精度电移台包括左载物平台19、右载物平台11、丝杠螺母副10、L形底座1、支撑座3、步进电机2、四个左滑块18、四个右滑块12、两根导轨14,所述的载物台包括动载物台8和静载物台6,所述的直线光栅测量装置包括光栅尺读数头安装架13、读数头15和光栅尺16, As shown in Figures 1 to 3, the micro-component tensile testing device includes a precision drive unit 9, a micro force sensor 5, a linear grating measuring device, a high-precision electric stage, a stage, a force sensor fixed block 4, two Fixture 17, the high-precision electric shift table includes a left loading platform 19, a right loading platform 11, a screw nut pair 10, an L-shaped base 1, a support seat 3, a stepping motor 2, and four left sliders 18. Four right sliders 12, two guide rails 14, the described object stage includes a moving object stage 8 and a static object stage 6, and the described linear grating measuring device includes a grating ruler reading head mounting frame 13, a reading Head 15 and grating ruler 16,
所述的L形底座1的长板水平设置,所述的两根导轨14平行于L形底座1的长边并固定在L形底座1的长板上;所述的左载物平台19和右载物平台11左右并列设置,所述的精密驱动单元9固定在右载物平台11上表面,所述的动载物台8与精密驱动单元9的左侧面固定连接,所述的静载物台6与动载物台8相邻且相对应设置,静载物台6与动载物台8的上表面对应位置分别加工有一用于固定微构件7的定位槽,利用微细铣削技术,加工出定位槽;所述的静载物台6、微力传感器5及力传感器固定块4由右至左依次设置在左载物平台19的上表面,且静载物台6与微力传感器5固定连接,微力传感器5与力传感器固定块4固定连接,力传感器固定块4与左载物平台19的上表面固定连接,所述的光栅尺16安装在精密驱动单元9的前侧面或后侧面上,右载物平台11上与光栅尺16位于同侧的侧面上固定有读数头安装架13,所述的度数头15与光栅尺16相对设置并固定在读数头安装架13上;所述的右载物平台11的下表面与丝杠螺母副10的螺母固定连接,丝杠螺母副10的丝杠一端与支撑座3转动连接,丝杠螺母副10的丝杠另一端与L形底座1的短板转动连接,支撑座3与L形底座1的长板固定连接,右载物平台11的下表面与呈矩形设置的四个右滑块12固定连接,四个右滑块12与两根导轨14滑动连接,进行导向,所述的步进电机2固定于L形底座1的短板上,步进电机2驱动丝杠螺母副10运动;左载物平台19的下表面与呈矩形设置的四个左滑块18固定连接,四个左滑块18设置在两根导轨14上,设置在同一根导轨14上的两个左滑块18之间安装有一与导轨14固定连接的固定件17,工作中左载物平台19相对导轨14固定不动,右载物平台11相对导轨14进行运动。 The long plate of the L-shaped base 1 is arranged horizontally, and the two guide rails 14 are parallel to the long sides of the L-shaped base 1 and fixed on the long plate of the L-shaped base 1; the left loading platform 19 and The right loading platform 11 is arranged side by side, the precision driving unit 9 is fixed on the upper surface of the right loading platform 11, the moving loading platform 8 is fixedly connected to the left side of the precision driving unit 9, and the static The stage 6 is adjacent to the moving stage 8 and is arranged correspondingly. The corresponding positions of the upper surfaces of the static stage 6 and the moving stage 8 are respectively processed with a positioning groove for fixing the micro-component 7, and the micro-milling technology is used to , process the positioning groove; the static loading table 6, the micro force sensor 5 and the force sensor fixing block 4 are arranged on the upper surface of the left loading platform 19 from right to left, and the static loading table 6 and the micro force sensor 5 Fixedly connected, the micro force sensor 5 is fixedly connected with the force sensor fixed block 4, the force sensor fixed block 4 is fixedly connected with the upper surface of the left loading platform 19, and the grating ruler 16 is installed on the front side or the rear side of the precision drive unit 9 On the right loading platform 11, a reading head installation frame 13 is fixed on the side on the same side as the grating ruler 16, and the degree head 15 is arranged opposite to the grating ruler 16 and is fixed on the reading head installation frame 13; The lower surface of the right loading platform 11 is fixedly connected with the nut of the lead screw nut pair 10, one end of the lead screw of the lead screw nut pair 10 is rotatably connected with the support seat 3, and the other end of the lead screw of the lead screw nut pair 10 is connected with the L-shaped base The short plate of 1 is rotationally connected, the support base 3 is fixedly connected with the long plate of the L-shaped base 1, the lower surface of the right loading platform 11 is fixedly connected with four right sliders 12 arranged in a rectangular shape, and the four right sliders 12 are connected with Two guide rails 14 are slidingly connected to guide, and the stepping motor 2 is fixed on the short plate of the L-shaped base 1, and the stepping motor 2 drives the screw nut pair 10 to move; the lower surface of the left loading platform 19 is in contact with the Four left sliders 18 that are arranged in a rectangle are fixedly connected, and four left sliders 18 are arranged on two guide rails 14, and a fixed connection with guide rail 14 is installed between the two left sliders 18 on the same guide rail 14. As for the fixing part 17, the left object loading platform 19 is fixed relative to the guide rail 14 during work, and the right object loading platform 11 moves relative to the guide rail 14.
所述的微力传感器5为商用传感器,微力传感器5型号是GSO-1000-T。 The micro force sensor 5 is a commercial sensor, and the model of the micro force sensor 5 is GSO-1000-T.
所述的精密驱动单元9包括柔性铰链机构9-1、预紧螺钉9-5、压电陶瓷9-6、两个垫片9-2、两个钢珠9-3、三个安装孔9-4,所述的柔性铰链机构9-1中部设有凹槽,所述的压电陶瓷9-6设置于柔性铰链机构9-1的凹槽内,压电陶瓷9-6两端分别通过钢珠9-3、垫片9-2与柔性铰链机构9-1的凹槽内壁相接触,柔性铰链机构9-1上设有三个用于与右载物平台11固定连接的安装孔9-4,安装孔9-4内穿入螺钉,柔性铰链机构9-1通过螺钉与右载物平台11固定连接,柔性铰链机构9-1的右端面加工有螺纹孔,所述的预紧螺钉9-5与柔性铰链机构9-1的螺纹孔螺纹连接,预紧螺钉9-5通过垫片9-2及钢珠9-3预压紧压电陶瓷9-6。 The precision drive unit 9 includes a flexible hinge mechanism 9-1, pre-tightening screws 9-5, piezoelectric ceramics 9-6, two gaskets 9-2, two steel balls 9-3, three mounting holes 9- 4. The middle part of the flexible hinge mechanism 9-1 is provided with a groove, the piezoelectric ceramic 9-6 is arranged in the groove of the flexible hinge mechanism 9-1, and the two ends of the piezoelectric ceramic 9-6 pass through steel balls respectively. 9-3. The gasket 9-2 is in contact with the inner wall of the groove of the flexible hinge mechanism 9-1. The flexible hinge mechanism 9-1 is provided with three mounting holes 9-4 for fixed connection with the right loading platform 11. Screws are penetrated in the mounting holes 9-4, and the flexible hinge mechanism 9-1 is fixedly connected with the right loading platform 11 by screws. It is threadedly connected with the threaded hole of the flexible hinge mechanism 9-1, and the pre-tightening screw 9-5 pre-compresses the piezoelectric ceramic 9-6 through the gasket 9-2 and the steel ball 9-3.
精密驱动单元9不仅可以实现简单拉伸位移的驱动,而且可以实现微构件的一定频率的疲劳加载。 The precision driving unit 9 can not only realize the driving of simple tensile displacement, but also realize the fatigue loading of micro-components at a certain frequency.
本测试装置可与CCD测试系统或其他测试设备进行集成,便于实现原位监测。 The test device can be integrated with a CCD test system or other test equipment to facilitate in-situ monitoring.
具体测试方法一:本测试装置放置在大理石隔振平台上,实验室环境洁净、恒温。首先打开控制系统总电源,压电陶瓷控制电源预热30分钟。调整动、静载物台的位置,使其标记中心线重合(最好利用CCD辅助调整)。然后,用镊子将微细铣削工艺加工的微构件取出,用胶粘在动、静载物台的定位槽中。通过调整,将动、静载物台的中心线与微构件中心重合(最好在CCD相机视场对中),在CCD辅助下进行测试。利用压电陶瓷驱动器控制精密驱动单元,对微构件进行拉-拉循环疲劳加载,当循环周次达到设定值时,疲劳测试结束。再进行微拉伸测试,精密驱动单元带动动载物台对微构件进行拉伸,直至微构件拉断,记录测试数据并进行数据处理。最后用丙酮溶液浸润被拉断的微构件,5分钟后用镊子将微构件取下,测试过程结束。 Specific test method 1: The test device is placed on a marble vibration isolation platform, and the laboratory environment is clean and constant temperature. First turn on the main power supply of the control system, and the piezoelectric ceramic control power supply is preheated for 30 minutes. Adjust the position of the dynamic and static stage so that the marked center lines coincide (it is best to use the CCD to assist in the adjustment). Then, take out the micro-component processed by the micro-milling process with tweezers, and stick it in the positioning groove of the dynamic and static stage with glue. Through adjustment, the centerline of the dynamic and static stage coincides with the center of the micro-component (preferably centered in the field of view of the CCD camera), and the test is performed with the assistance of the CCD. The piezoelectric ceramic driver is used to control the precision drive unit, and the micro-components are subjected to pull-pull cycle fatigue loading. When the number of cycles reaches the set value, the fatigue test ends. Then carry out the micro-tensile test, the precision drive unit drives the moving stage to stretch the micro-component until the micro-component breaks, record the test data and perform data processing. Finally, soak the broken micro-component with acetone solution, remove the micro-component with tweezers after 5 minutes, and the test process ends.
具体测试方法二:准备工作同方法一,对微构件直接进行微拉伸测试,测量试件的静态力学性能。 Specific test method 2: The preparation work is the same as method 1, and the micro-components are directly subjected to micro-tensile tests to measure the static mechanical properties of the specimens.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201410271032.5A CN104007028B (en) | 2014-06-18 | 2014-06-18 | Micro-member tensile test device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201410271032.5A CN104007028B (en) | 2014-06-18 | 2014-06-18 | Micro-member tensile test device |
Publications (2)
Publication Number | Publication Date |
---|---|
CN104007028A CN104007028A (en) | 2014-08-27 |
CN104007028B true CN104007028B (en) | 2016-05-18 |
Family
ID=51367785
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201410271032.5A Active CN104007028B (en) | 2014-06-18 | 2014-06-18 | Micro-member tensile test device |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN104007028B (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104297065B (en) * | 2014-10-28 | 2016-09-14 | 郑州轻工业学院 | A piezoelectric driven micro-tensile testing device |
WO2016123265A1 (en) * | 2015-01-29 | 2016-08-04 | Newport Corporation | Integrated picomotor mount |
CN106059382B (en) * | 2016-06-06 | 2017-09-01 | 长春工业大学 | Rhombus hinge chute type orthogonal drive piezoelectric stick-slip linear motor and its compound excitation method |
CN107464759A (en) * | 2017-09-18 | 2017-12-12 | 科广电子(东莞)有限公司 | A kind of device for drawing semi-conducting electrode lead |
IT201700108535A1 (en) * | 2017-09-28 | 2019-03-28 | Univ Degli Studi Di Trento | DEVICE TO DETERMINE THE MECHANICAL PROPERTIES OF NANOMATERIALS AND RELATIVE METHOD |
CN109655112A (en) * | 2019-01-25 | 2019-04-19 | 嘉兴学院 | Adjustable measuring device that is a kind of while measuring piezoelectric actuator load and output displacement |
CN110082208A (en) * | 2019-05-14 | 2019-08-02 | 中国石油大学(北京) | Miniature SMA comprehensive characteristic test device |
CN111504826B (en) * | 2020-05-13 | 2021-07-06 | 吉林大学 | An online automatic detector for mechanical parameters of materials under complex working conditions |
CN113624600B (en) * | 2021-07-21 | 2024-04-26 | 西安工程大学 | Three-dimensional solid device of functional microfilament |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7752916B2 (en) * | 2007-08-31 | 2010-07-13 | The Board Of Trustees Of The University Of Illinois | Apparatus and method for material testing of microscale and nanoscale samples |
US8297130B2 (en) * | 2008-11-12 | 2012-10-30 | The United States Of America As Represented By The Secretary Of The Air Force | Microtesting rig with variable compliance loading fibers for measuring mechanical properties of small specimens |
CN102507339A (en) * | 2011-10-27 | 2012-06-20 | 哈尔滨工业大学 | Nanoscale micro-stretching device |
CN103091178A (en) * | 2013-01-15 | 2013-05-08 | 天津大学 | Mechanical-thermal composite in-situ loading system |
-
2014
- 2014-06-18 CN CN201410271032.5A patent/CN104007028B/en active Active
Also Published As
Publication number | Publication date |
---|---|
CN104007028A (en) | 2014-08-27 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN104007028B (en) | Micro-member tensile test device | |
CN103994929B (en) | Mechanics Performance Testing device and the method with this device to test micro structures mechanical characteristic | |
CN104007015B (en) | Mechanics Performance Testing device and the method by this device to test micro structures natural frequency | |
CN103487315B (en) | A kind of material mechanical performance proving installation | |
CN102221499B (en) | Alignment loading device used for stretching test of nanoscale, micron-size thin film materials | |
CN203337456U (en) | Extensometer type displacement detecting device | |
CN105973694A (en) | Nano indentation testing device under stretch-four-point bending preload | |
CN101216390A (en) | Micro-element dynamic performance off-chip tensile test experimental bench | |
CN103335898A (en) | In-situ testing device for micro-mechanical properties of materials under tension-shear combined loading mode | |
CN203551383U (en) | In-situ testing instrument for micromechanical property of material under multi-load and multi-physical field coupling action | |
CN202330188U (en) | Micro-torsion mechanical property testing device | |
CN101059381A (en) | Piezoelectric film cantilever beam type micro-force sensor micro-force loading device | |
CN108931453A (en) | Small-sized pin disk-type friction abrasion tester | |
CN206671088U (en) | A kind of miniature thin plate bending stiffness measurement device of Bit andits control | |
CN104851823A (en) | X and Y double-axis linkage non-contact wafer warping degree measuring equipment | |
CN107543752A (en) | Nano-hardness tester special fixture | |
CN105547858A (en) | Measuring device and testing method for glass micro channel bending mechanical property | |
CN113484235B (en) | Device for measuring ice adhesion strength on surface of wind turbine blade | |
CN203249835U (en) | In-situ three-point bending test device for materials under the coupling of mechanical and thermal fields | |
CN103983526A (en) | Cross-scale micro-nano-scale in-situ shearing mechanical performance testing platform | |
CN103293065B (en) | Outward bending testing device of microstructural mechanical property sheet | |
CN104007014B (en) | Micro structures comprehensive mechanical property proving installation | |
CN204374047U (en) | A kind of micro tribology measurement mechanism | |
CN106885741A (en) | A kind of portable minisize thin plate rate tester and its method of work | |
CN106644715B (en) | A portable scratch-in test system |
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 |