Uniaxial cyclic loading deformation and fatigue life of ECC
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摘要: 高延性水泥基复合材料(ECC)多用于结构的抗震补强,其疲劳性能是工程中关注的重点。为研究其疲劳性能,通过疲劳试验机进行单轴拉伸循环加载试验,利用数字图像相关(DIC)技术实时监测位移发展与开裂行为。分析ECC试件的动力变形、疲劳规律并建立疲劳方程。结果表明:ECC试件的应变和轴向位移发展规律相似,分为初始阶段、稳定发展阶段、加速变形阶段和破坏阶段;动应力比越小,应变发展越快,破坏发生时的累积轴向应变越大;刚度比发展曲线分为三部分:快速下降阶段、稳定下降阶段和破坏阶段;其疲劳寿命可较好服从双参数Weibull分布;通过建立两种形式的疲劳方程:S-lgN和S-lgN-F疲劳方程,将极限疲劳寿命带入平均寿命疲劳方程,针对本文配合比得到疲劳极限应力水平为70.80%,对应的疲劳极限强度为2.69 MPa。Abstract: Engineered cementitious composites (ECC) are mostly used for seismic reinforcement of structures, and their fatigue performance is a major concern in engineering. In order to study the fatigue performance of ECC, the uniaxial tensile cyclic loading test was performed by fatigue testing machine, and the displacement development and cracking behavior in real time were monitored by using digital image correlation (DIC) technology to analyze the dynamic deformation and fatigue law of ECC specimens and establish the fatigue equation. The results show that the strain and axial displacement of ECC specimens develop similarly, which are divided into the initial stage, stable development stage, accelerated deformation stage and damage stage. The smaller the dynamic stress ratio, the faster the strain development and the larger the accumulated axial strain when damage occurs. The stiffness ratio development curve is divided into three parts: Rapid decline stage, stable decline stage and damage stage. The fatigue life of the ECC specimen obeys the two-parameter Weibull distribution well. By establishing two forms of fatigue equations: S-lgN and S-lgN-F fatigue equations, the ultimate fatigue life is brought into the average life fatigue equation, and the fatigue ultimate stress level is 70.80%. The corresponding fatigue ultimate strength is 2.69 MPa.
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表 1 聚乙烯醇(PVA)纤维的各项性能指标
Table 1. Various performance indexes of polyvinyl alcohol (PVA) fiber
Length/mm Diameter/μm Length-diameter ratio/103 Tensile strength/MPa Elastic modulus
/GPaElongation/% Density/(g·cm−3) 12 39 0.31 1600 39 17 0.91 表 2 高延性水泥基复合材料(ECC)试件相对配合比 (kg/m3)
Table 2. Relative fit ratio of engineered cementitious composites (ECC) specimens (kg/m3)
Cement Water Sand PVA fiber Fly ash Water-reducing admixture 662.00 329.19 331.35 45.23 440.90 176.22 表 3 不同应力水平下的ECC疲劳寿命N的Weibull参数分布
Table 3. Weibull distribution test of fatigue life N of ECC under different stress levels
Stress
level SNumber of specimen i Cycles number
Ni$P = 1 - \dfrac{i}{{\left( {1 + K} \right)}}$ $\ln {N_i}$ $\ln \left[ {\ln \left( {1/P} \right)} \right]$ 0.95 1 16 0.83333 2.77259 −1.70198 2 26 0.66667 3.25810 −0.90272 3 38 0.50000 3.63759 −0.36651 4 42 0.33333 3.73767 0.09405 5 64 0.16667 4.15888 0.58320 0.90 1 106 0.83333 4.66344 −1.70198 2 305 0.66667 5.72031 −0.90272 3 405 0.50000 6.00389 −0.36651 4 1054 0.33333 6.96035 0.09405 5 2208 0.16667 7.69984 0.58320
0.851 4035 0.83333 8.30276 −1.70198 2 6524 0.66667 8.78324 −0.90272 3 12054 0.50000 9.39715 −0.36651 4 13518 0.33333 9.51178 0.09405 5 25478 0.16667 10.14557 0.58320
0.801 9225 0.83333 9.12967 −1.70198 2 15652 0.66667 9.65835 −0.90272 3 36584 0.50000 10.50737 −0.36651 4 42536 0.33333 10.65811 0.09405 5 45821 0.16667 10.73250 0.58320
0.751 36598 0.83333 10.50775 −1.70198 2 44750 0.66667 10.70885 −0.90272 3 46524 0.50000 10.74772 −0.36651 4 67546 0.33333 11.12056 0.09405 5 70451 0.16667 11.16267 0.58320
0.701 65894 0.83333 11.09580 −1.70198 2 76954 0.66667 11.25096 −0.90272 3 84572 0.50000 11.34536 −0.36651 4 88258 0.33333 11.38802 0.09405 5 95871 0.16667 11.47076 0.58320 Notes: P—Probability corresponding to the fatigue life NP; K—Total number of fatigue test data obtained at a given stress level. 表 4 ECC疲劳拉伸试验分析结果
Table 4. Analysis results of ECC fatigue tensile test
Stress
level $S$Regression coefficients $b$ $b\ln{N_{\text{a} } }$ Correlation coefficient R 0.95 1.6800 6.362 0.9852 0.90 0.7492 5.111 0.9663 0.85 1.2350 11.860 0.9643 0.80 1.1990 12.620 0.8920 0.75 2.9960 32.960 0.8793 0.70 6.1350 69.860 0.9886 Note: Na—Number of cycle loads. 表 5 不同应力比下ECC的拉伸疲劳寿命
Table 5. Tensile fatigue life of ECC under different stress ratios
Stress
level $S$Average fatigue
life $N$${\text{lg}}N$ ${\text{lg}}S$ 0.95 37.2 1.5705 –0.0223 0.90 815.6 2.9115 –0.0458 0.85 12321.8 4.0907 –0.0706 0.80 29963.6 4.4766 –0.0969 0.75 53173.8 4.7257 –0.1249 0.70 82309.8 4.9155 –0.1549 表 6 不同应力水平S及失效概率F下ECC的疲劳寿命
Table 6. Fatigue life of ECC under different failure probabilities F and stress levels S
Probability
of failure FStress level S 0.95 0.90 0.85 0.80 0.75 0.70 0.05 8 17 1337 3128 22247 54338 0.10 12 46 2395 5702 28289 61103 0.20 18 124 4397 10662 36340 69053 0.30 24 232 6428 15766 42499 74539 0.40 30 374 8598 21273 47912 79034 0.50 35 563 11009 27440 53051 83065 表 7 ECC的S-lgN-F疲劳方程的回归参数
Table 7. Regression parameters of S-lgN-F fatigue equation of ECC
Fatigue equation Failure probability F R2 ${{S}} = - 0.0098{({\rm{lg}}{{N}})^2} - 0.0037{\rm{lg}}{{N}} + 0.9430$ 0.05 0.9701 ${{S}} = - 0.0125{({\rm{lg}}{{N}})^2} + 0.0117{\rm{lg}}{{N}} + 0.9377$ 0.10 0.9749 ${{S}} = - 0.0164{({\rm{lg}}{{N}})^2} + 0.0364{\rm{lg}}{{N}} + 0.9185$ 0.20 0.9752 ${{S}} = - 0.0193{({\rm{lg}}{{N}})^2} + 0.0564{\rm{lg}}{{N}} + 0.8986$ 0.30 0.9721 ${{S}} = - 0.0218{({\rm{lg}}{{N}})^2} + 0.7039{\rm{lg}}{{N}} + 0.8790$ 0.40 0.9672 ${{S}} = - 0.0239{({\rm{lg}}{{N}})^2} + 0.0891{\rm{lg}}{{N}} + 0.8608$ 0.50 0.9605 -
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