CN110487643A - A kind of micron order fiber cutting strength test method - Google Patents
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- 238000010998 test method Methods 0.000 title claims abstract description 13
- 239000000523 sample Substances 0.000 claims abstract description 11
- 238000004458 analytical method Methods 0.000 claims abstract description 6
- 238000010008 shearing Methods 0.000 claims abstract description 6
- 230000006835 compression Effects 0.000 claims abstract description 3
- 238000007906 compression Methods 0.000 claims abstract description 3
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract 19
- 239000000463 material Substances 0.000 claims description 8
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- 238000005259 measurement Methods 0.000 claims description 3
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- 238000004364 calculation method Methods 0.000 claims description 2
- 238000007373 indentation Methods 0.000 claims description 2
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- 238000000399 optical microscopy Methods 0.000 claims 1
- 238000012360 testing method Methods 0.000 abstract description 12
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 18
- 239000010937 tungsten Substances 0.000 description 18
- 229910052721 tungsten Inorganic materials 0.000 description 18
- GRYLNZFGIOXLOG-UHFFFAOYSA-N Nitric acid Chemical compound O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 0.000 description 6
- 229910017604 nitric acid Inorganic materials 0.000 description 6
- 238000000034 method Methods 0.000 description 5
- 230000003287 optical effect Effects 0.000 description 5
- 239000003795 chemical substances by application Substances 0.000 description 3
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 2
- 229920001651 Cyanoacrylate Polymers 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- 239000004830 Super Glue Substances 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 239000004831 Hot glue Substances 0.000 description 1
- 150000007513 acids Chemical class 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000004090 dissolution Methods 0.000 description 1
- FGBJXOREULPLGL-UHFFFAOYSA-N ethyl cyanoacrylate Chemical compound CCOC(=O)C(=C)C#N FGBJXOREULPLGL-UHFFFAOYSA-N 0.000 description 1
- 239000003733 fiber-reinforced composite Substances 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 239000012943 hotmelt Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000004088 simulation Methods 0.000 description 1
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- G01N3/00—Investigating strength properties of solid materials by application of mechanical stress
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Abstract
Description
技术领域technical field
本发明涉及纤维测试方法,具体为一种微米级纤维剪切强度测试方法。The invention relates to a fiber testing method, in particular to a micron-scale fiber shear strength testing method.
背景技术Background technique
连续纤维增强复合材料在沿纤维轴向方向(纵向)拥有较强的力学性能,而在垂直于纤维方向(横向)的强度较差,这成为复合材料在复杂环境中使用时的安全隐患之一,故测量纤维的剪切应力是非常必要的。不同直径微米级纤维的剪切强度按照传统方法也难以测量。Continuous fiber-reinforced composite materials have strong mechanical properties along the fiber axial direction (longitudinal direction), but poor strength perpendicular to the fiber direction (transverse direction), which becomes one of the safety hazards when composite materials are used in complex environments , so it is necessary to measure the shear stress of the fiber. It is also difficult to measure the shear strength of micron-scale fibers with different diameters according to traditional methods.
发明内容Contents of the invention
发明目的:为了克服现有技术中存在的不足,本发明目的是提供一种能够对复杂应力状态下纤维的失效准则进行分析微米级纤维剪切强度测试方法。Purpose of the invention: In order to overcome the deficiencies in the prior art, the purpose of the invention is to provide a micron-scale fiber shear strength test method capable of analyzing the failure criteria of fibers under complex stress states.
技术方案:本发明所述的一种微米级纤维剪切强度测试方法,包含以下步骤:Technical solution: A method for testing the shear strength of micron-scale fibers according to the present invention comprises the following steps:
(1)逐步改变底座间距大小直到待测纤维横截面的剪切应力突然变大,此时即待测纤维处于剪切状态下的底座间距,有限元分析待测纤维处于剪切状态下的底座间距,底座由高弹性模量且不与酸反应的材料制成,优选为钨片;(1) Gradually change the distance between the bases until the shear stress of the cross-section of the fiber to be tested suddenly increases. At this time, the base distance of the fiber to be tested is in a shear state, and the finite element analysis is performed on the base of the fiber to be tested in a shear state. spacing, the base is made of a material with a high modulus of elasticity and does not react with acids, preferably a tungsten sheet;
(2)对用于固定待测纤维的底座进行预处理,底座上黏贴待测纤维的平面要保证平行,进行剪切的两个平面要垂直,平面的表面粗糙度小于待测纤维半径的10%,待测纤维直径为1~900μm;(2) Pre-treat the base used to fix the fiber to be tested. The plane on which the fiber to be tested is pasted must be parallel, the two planes for shearing must be vertical, and the surface roughness of the plane is less than 1/2 of the radius of the fiber to be tested. 10%, the diameter of the fiber to be tested is 1-900μm;
(3)测量底座中间间隙的大小,底座中间间隙小于等于待测纤维半径的5倍,用光学显微镜测量间隙的大小,判断间隙的间距是否满足要求;(3) Measure the size of the gap in the middle of the base, the gap in the middle of the base is less than or equal to 5 times the radius of the fiber to be measured, measure the size of the gap with an optical microscope, and judge whether the gap meets the requirements;
(4)固定待测纤维,采用光学显微镜在400倍以上放大倍数下观察待测纤维,确定待测纤维是否已被固定;(4) fix the fiber to be tested, and use an optical microscope to observe the fiber to be tested at a magnification of more than 400 times to determine whether the fiber to be tested has been fixed;
(5)微米级待测纤维剪切试验在纳米力学测试系统上进行,纳米压痕仪探针对待测纤维的中央压缩加载至待测纤维压断,压入深度为5×10-4mm,并测量出将待测纤维剪断所需的剪切力Fs,探针的尺寸为底座中间间隙的0.9~0.95倍;(5) The shear test of the micron-scale fiber to be tested is carried out on the nanomechanical testing system. The probe of the nano-indenter is compressed and loaded to the center of the fiber to be tested until the fiber to be tested is broken, and the indentation depth is 5×10 -4 mm. And measure the shear force F s required to cut the fiber to be tested, the size of the probe is 0.9 to 0.95 times the gap in the middle of the base;
(6)待测待测纤维的剪切强度T的计算公式为:(6) The calculation formula of the shear strength T of the fiber to be measured is:
其中,rf为待测纤维半径,Fs为将待测纤维剪断所需的剪切力,测量和固定通过光学显微镜在400倍以上放大倍数下观察;Among them, r f is the radius of the fiber to be tested, and F s is the shear force required to cut the fiber to be tested, and the measurement and fixation are observed by an optical microscope at a magnification of more than 400 times;
(7)重复上述步骤,多次测量求平均值。(7) Repeat the above steps, and take the average value of multiple measurements.
工作原理:用探针对待测纤维进行压缩加载时,底座弹性模量大产生的应变可以忽略不计,保证了在压缩加载时底座的两个面始终垂直,从而使待测纤维在剪切状态下发生断裂。Working principle: When the probe is used to compress and load the fiber to be tested, the strain caused by the large elastic modulus of the base can be ignored, which ensures that the two surfaces of the base are always vertical during the compression load, so that the fiber to be tested is in a shear state. Fracture occurs.
有益效果:本发明和现有技术相比,具有如下显著性特点:能够测试准确微米级纤维的剪切强度,进而可以对复杂应力状态下纤维的失效准则分析提供材料的基础力学性能参数。Beneficial effects: Compared with the prior art, the present invention has the following remarkable features: it can test the shear strength of accurate micron-sized fibers, and can provide basic mechanical performance parameters of materials for failure criterion analysis of fibers under complex stress states.
附图说明Description of drawings
图1是本发明的流程图;Fig. 1 is a flow chart of the present invention;
图2是本发明夹具4的结构示意图;Fig. 2 is the structural representation of clamp 4 of the present invention;
图3是本发明底座的结构示意图;Fig. 3 is the structural representation of base of the present invention;
图4是本发明的有限元模型图。Fig. 4 is a finite element model diagram of the present invention.
具体实施方式Detailed ways
以下实施例中,待测纤维1半径rf取为3.5μm。In the following embodiments, the radius r f of the fiber 1 to be tested is taken as 3.5 μm.
表1有限元模拟获得剪切应力随间隙宽度变化规律Table 1. Variation law of shear stress with gap width obtained by finite element simulation
(1)有限元分析:先用UG建立待测纤维1,底座2和探针3的模型如图3所示,待测纤维1剪切失效的切向位移为5×10-4mm,对探针3施加一个方向沿待测纤维1切向,大小为5×10-4mm的位移约束,然后求解待测纤维1剪切应力,通过改变底座2间距的大小来模拟底座2间隙对待测纤维1切应力的影响,结果如表1所示,从表1可以看出,所模拟的待测纤维1在底座2间隙为0.018mm时横截面的切应力突然增大,可以确定这个间距为待测纤维1处于剪切状态下底座2的最小间距;(1) Finite element analysis: first use UG to establish the model of the fiber 1 to be tested, the base 2 and the probe 3 as shown in Figure 3, the tangential displacement of the fiber 1 to be tested to shear failure is 5×10 -4 mm, for Probe 3 imposes a direction along the tangential direction of the fiber 1 to be tested, with a displacement constraint of 5×10 -4 mm in size, and then solves the shear stress of the fiber 1 to be tested, and simulates the gap between the base 2 and the base 2 to be tested by changing the distance between the base 2 The influence of the shear stress of fiber 1, the results are shown in Table 1. It can be seen from Table 1 that the shear stress of the cross-section of the simulated fiber 1 to be tested increases suddenly when the gap between the base 2 is 0.018mm. It can be determined that the distance is The minimum spacing of the base 2 when the fiber 1 to be tested is in a shear state;
(2)底座2的处理:底座2的材料须选取弹性模量大的材料,夹具4须选取有磁性的金属且易加工,这里选取底座2材料为钨,夹具4材料为钢,钨弹性模量大,且不与硝酸发生反应,钨无磁性不能固定在磨床上,而钢有磁性,能把钨片固定在磨床上加工,先加工一个夹具4,然后用夹具4将钨片夹住如图2~3所示,将夹具4固定在磨床上,将A平面进行精磨使其表面粗糙度不大于0.35μm(待测纤维1半径的10%),随后将这对钨片的A平面对齐用强力胶水黏在夹具4上,接着将钨片的B进行精磨保证平面的表面粗糙度和平面度与塞规的表面粗糙度和平面度一致,这样处理的顺序特征在于可以保证A、B两个平面的垂直度使待测纤维1在下压时处于剪切状态,然后用这对钨片的平面B钨片将塞规固定住,并用夹子将钨片夹紧,把夹紧的钨片B平面与镶嵌槽底接触并轻轻下压钨片以保证这对钨片的B平面与镶嵌槽底座2在同一个平面上并用镶嵌剂将钨片镶嵌在槽中,待镶嵌剂固化后把镶嵌块取出并泡在溶硝酸中使间隙中的塞规融掉,得到间距为0.018mm的底座2,塞规的特性在于可以与浓硝酸发生反应,而镶嵌剂和钨片不与硝酸反应;(2) Treatment of the base 2: the material of the base 2 must be selected from a material with a large elastic modulus, and the clamp 4 must be selected from a magnetic metal and easy to process. Here, the material of the base 2 is selected to be tungsten, and the material of the clamp 4 is steel. The amount of tungsten is large and does not react with nitric acid. Tungsten is non-magnetic and cannot be fixed on the grinding machine, while steel is magnetic and can fix the tungsten sheet on the grinding machine for processing. As shown in Figures 2 to 3, the fixture 4 is fixed on the grinding machine, and the A plane is finely ground so that its surface roughness is not greater than 0.35 μm (10% of the radius of the fiber 1 to be tested), and then the A plane of the pair of tungsten sheets The alignment is glued on the fixture 4 with super glue, and then the B of the tungsten sheet is finely ground to ensure that the surface roughness and flatness of the plane are consistent with the surface roughness and flatness of the plug gauge. The characteristic of this processing sequence is that A, The verticality of the two planes of B makes the fiber 1 to be tested in a shear state when it is pressed down, and then fix the plug gauge with the plane B tungsten sheet of the pair of tungsten sheets, and clamp the tungsten sheet with a clip, and clamp the clamped tungsten sheet The B plane of the piece is in contact with the bottom of the mosaic groove and gently press down on the tungsten piece to ensure that the B plane of the pair of tungsten pieces is on the same plane as the base 2 of the mosaic groove, and the tungsten piece is embedded in the groove with a mounting agent. Take out the mosaic block and soak it in dissolved nitric acid to melt the plug gauge in the gap, and get the base 2 with a distance of 0.018mm. The characteristic of the plug gauge is that it can react with concentrated nitric acid, while the mosaic agent and tungsten sheet do not react with nitric acid. ;
这样处理的顺序特征在于可以保证A、B两个平面的垂直度使待测纤维1在下压时处于剪切状态,利用丙酮可与强力胶的主要成分α-氰基丙烯酸乙酯发生反应来使钨片从夹具4上脱落,塞规可与硝酸发生反应而钨片和镶嵌剂不与硝酸反应,保证间隙中的塞规成功溶解,不同间隙可以采用不同厚度的塞规来控制;The sequence of such processing is characterized in that the verticality of the two planes A and B can be guaranteed so that the fiber 1 to be tested is in a shear state when it is pressed down, and acetone can react with the main component of superglue α-cyanoacrylate ethyl ester to make The tungsten piece falls off from the fixture 4, the plug gauge can react with nitric acid, but the tungsten piece and the mounting agent do not react with nitric acid, ensuring the successful dissolution of the plug gauge in the gap, different gaps can be controlled by plug gauges of different thickness;
(3)采用光学显微镜在不小于400倍数下观察间距,确定间隙的实际距离,与0.018mm进行比较,判断是否相差不大;(3) Use an optical microscope to observe the distance at a multiple of not less than 400, determine the actual distance of the gap, compare it with 0.018mm, and judge whether there is little difference;
(4)用镊子小心夹取单根待测纤维1横跨在间隙上,并将待测纤维1一端通过热熔胶黏贴在底座2上,随后将待测纤维1拉直,并用热熔胶固定另一端,在底座2横向上间隔一定距离均匀固定待测纤维1;采用光学显微镜在不小于400倍放大倍数下观察待测纤维1,确定待测纤维1是否已固定;(4) Use tweezers to carefully pick up a single fiber 1 to be tested across the gap, and stick one end of the fiber 1 to be tested on the base 2 with hot-melt adhesive, then straighten the fiber 1 to be tested, and use a hot-melt Fix the other end with glue, and evenly fix the fiber 1 to be tested at a certain distance in the lateral direction of the base 2; use an optical microscope to observe the fiber 1 to be tested at a magnification of not less than 400 times, and determine whether the fiber 1 to be tested is fixed;
(5)将制备好的待测纤维1剪切试样在纳米压痕仪上采用尺寸略小于180μm的探针3进行压缩加载,此时待测纤维1处于剪切状态,将通过纳米力学测试系统进行的待测纤维1剪切试验,测出将待测纤维1剪断所需剪切力;(5) The prepared shear sample of the fiber 1 to be tested is compressed and loaded on the nanoindenter using a probe 3 with a size slightly smaller than 180 μm. At this time, the fiber 1 to be tested is in a shear state and will pass the nanomechanical test. The shear test of the fiber 1 to be tested is carried out by the system, and the shear force required to cut the fiber 1 to be tested is measured;
(6)根据公式计算待测纤维1剪切强度,其中,rf为纤维半径,Fs为将纤维剪断所需的剪切力。(6) According to the formula Calculate the shear strength of the fiber 1 to be tested, where r f is the fiber radius, and F s is the shear force required to cut the fiber.
表2是用上述实施例的方法进行纤维剪切试验得到的测试数据及纤维剪切强度,将在钨片横向上间隔一定距离均匀固定纤维按从左往右的顺序依次编号,分别为T300-S-1、T300-S-2、T300-S-3、T300-S-4、T300-S-5,从表中可看出,T300纤维的纤维剪切强度为675.42MPa,标准差为122.30MPa;T700纤维的剪切强度为942.94MPa,标准差为153.62MPa。Table 2 is the test data and fiber shear strength obtained from the fiber shear test using the method of the above example. The fibers are uniformly fixed at a certain distance in the transverse direction of the tungsten sheet and numbered in sequence from left to right, respectively T300- S-1, T300-S-2, T300-S-3, T300-S-4, T300-S-5, it can be seen from the table that the fiber shear strength of T300 fiber is 675.42MPa, and the standard deviation is 122.30 MPa; the shear strength of T700 fiber is 942.94MPa, and the standard deviation is 153.62MPa.
表2纤维剪切强度试验数据Table 2 fiber shear strength test data
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CN111157362A (en) * | 2020-01-14 | 2020-05-15 | 南京航空航天大学 | A nano-indenter-based interface shear strength measuring device and testing method |
CN112945756A (en) * | 2021-02-21 | 2021-06-11 | 扬州升飞检测技术有限公司 | Method for testing shear strength of high-temperature ceramic material |
CN113218767A (en) * | 2021-06-07 | 2021-08-06 | 中国空气动力研究与发展中心超高速空气动力研究所 | In-situ test method for interface shear strength of fiber reinforced ceramic matrix composite |
CN113609688A (en) * | 2021-08-09 | 2021-11-05 | 大连理工大学 | Method for accurately judging fiber shearing and bending failure in microscopic cutting simulation of composite material |
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CN111157362A (en) * | 2020-01-14 | 2020-05-15 | 南京航空航天大学 | A nano-indenter-based interface shear strength measuring device and testing method |
CN111157362B (en) * | 2020-01-14 | 2021-05-25 | 南京航空航天大学 | Nano-indentation instrument-based interface shear strength measuring device and testing method |
CN112945756A (en) * | 2021-02-21 | 2021-06-11 | 扬州升飞检测技术有限公司 | Method for testing shear strength of high-temperature ceramic material |
CN113218767A (en) * | 2021-06-07 | 2021-08-06 | 中国空气动力研究与发展中心超高速空气动力研究所 | In-situ test method for interface shear strength of fiber reinforced ceramic matrix composite |
CN113609688A (en) * | 2021-08-09 | 2021-11-05 | 大连理工大学 | Method for accurately judging fiber shearing and bending failure in microscopic cutting simulation of composite material |
CN113609688B (en) * | 2021-08-09 | 2024-03-29 | 大连理工大学 | Accurate judging method for fiber shearing and bending failure in composite material microscopic cutting simulation |
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