The Strain Rate Effect on the Compression Properties of Basalt/Carbon Fiber Reinforced Composites

Applied Composite Materials - Adding a basalt fiber layer (BF) to carbon-Fiber-reinforced plastic (CFRP) material can effectively improve its extensibility. In the work described in this study, a...     

New Strengthening Techniques with FRP Laminates and Interfacial Fracture Theories

The use of FRP composites in the form of sheet or plate bonded to the large-scale RC structures is becoming an increasing attractive solution to the strengthening of existing structures. Compared with traditional steel plate strengthening, FRP possesses excellent behavior such as lightness in weight, high strength-to-weight and stiffness-to-weight ratio, high corrosion and fatigue resistance, electronic neutrality, and great efficiency in construction. A important failure mode for FRP-strengthened structures is debondings.Therefore, the LEFM and NLFM are utilized to treat this problem. Closed form expressions for energy release rate, load-carrying capacity, load-displacement relation and interfacial crack propagation are obtained, in which a local shear stress-slip law with softening is adopted.     

温度对碳纤维平纹布正交层合板拉伸疲劳性能的影响

温度环境可降低复合材料的疲劳性能,在确定复合材料结构寿命时须考虑温度的影响.本试验测量了碳纤维平纹布正交层合板在低温干态(CTD)、常温干态(RTD)和高温干态(ETD)环境下的拉伸疲劳性能,获得了三种环境下复合材料的S-N曲线,分析了温度对复合材料疲劳性能的影响.基于试验结果,建立了温度条件下复合材料疲劳性能有限元分析模型,对复合材料的疲劳寿命进行了估算并分析了其损伤机理.线性拟合结果显示:在106 疲劳寿命下,与RTD环境疲劳最大应力相比,CTD环境疲劳最大应力略有降低,而ETD环境疲劳最大应力下降明显. CTD环境下,试验件的疲劳破坏断口比较齐整,纤维基本在同一纵向位置断裂,断口附近基体基本完好,无分层现象;RTD环境下,试验件断口处也没有明显分层现象;ETD环境下,试验件出现了明显的分层,同时还有纤维拔出,且断口处基体开裂程度严重.有限元分析表明,CTD环境下试验件的疲劳断裂呈现脆断的特征,断裂截面平整,断裂区域窄;RTD与ETD环境下试验件的纤维疲劳断裂损伤的断裂截面不平整,断口不一,断裂区域相对较宽.     

Loading Rate Dependence of Mode II Fracture Behavior in Interleaved Carbon Fibre/Epoxy Composite Laminates

The mode II delamination fracture toughness (G _IIC ) for interleaved and non-interleaved CFRP were measured at loading rates ranging from 0.2 to 125 mm/min. It was observed that interleaving could enhance G _IIC for CFRP significantly. Furthermore, G _IIC was observed to be independent of the loading rate for the non-interleaved CFRP. For the interleaved CFRP, the loading rate has a strong influence on G _IIC , and the loading rate dependence can be explained in terms of the fracture surface morphologies.     

炭纤维特性与炭纤维/环氧树脂界面断裂能关联分析

采用基于WND(Wagner-Nairn-Detassis)能量模型的单丝断裂法,测试了5种国产炭纤维、2种国外炭纤维与航空结构用环氧树脂复合体系的界面断裂能,通过SEM,AFM,IR以及XPS等手段分析了7种炭纤维的表面物理化学特性,并研究了炭纤维特性与界面断裂能的关联。结果表明:对于所研究的炭纤维/环氧树脂体系,去除炭纤维表面上浆剂后界面断裂能下降,说明上浆剂可以在一定程度上提高界面的韧性。此外,实验范围内,纤维拉伸强度较高时,测得的界面断裂能较高,炭纤维表面粗糙度较高时,测得界面断裂能较高,说明纤维拉伸性能和表面粗糙度对界面韧性有重要影响,而与这两种因素相比,上浆剂的种类影响相对较小。研究结果为高性能国产炭纤维的研发和炭纤维/树脂匹配性的评价提供了重要的实验数据。     

Effect of Strain Rate and Preloading on the Fracture Toughness of ZrO2-Based Ceramics

We study the variation of the fracture toughness K_Ic ofZrO₂ - Y₂ O₃ ceramics (density 98%) as a function of the testing machine crosshead speed (0.005–50 mm/min) and preloading at K_I < K_c. The fracture toughness is shown to be practically constant in the speed range from 0.05 to 5 mm/min. At a loading rate of 50 mm/min, the quantity K_Ic substantially decreases (by a factor of more than two), whereas at a rate of 0.005 mm/min it slightly increases. Preloading leads to a 1.5-fold increase in K_Ic. Variation of the fracture toughness is associated with structural transformations.     

冲击速度和应变率对六边形蜂窝共面缓冲性能的影响

目的通过改变压缩方向的厚度,即共面方向的蜂窝层数,来研究冲击速度和应变率对六边形蜂窝共面缓冲性能的影响。方法借助软件Ansys/LS-DYNA来模拟六边形蜂窝在应变率恒定时冲击速度对蜂窝共面缓冲性能的影响,以及六边形蜂窝在速度值恒定时应变率对蜂窝共面缓冲性能的影响。结果设定3组应变率恒值(300,500,1000 s-1)研究不同冲击速度对蜂窝动态峰应力的影响,随着速度的增加,动态峰应力也增加。设定3组冲击速度恒值(3,50,100 m/s)研究不同应变率对蜂窝动态峰应力的影响,随着应变率增加,动态峰应力基本不变。结论在试件材料选用双线性硬化的铝基材料,壁材视为应变率不敏感的模型下,应变率对正六边形蜂窝的动态力学性能和缓冲性能基本无影响。     

Effect of the Strain Rate and Temperature on the Physicomechanical Properties of Glass-Fiber-Reinforced Plastics

We study the influence of the strain rate and temperature on the physicomechanical properties of structural composites based on the PN-11 polyester resin. We deduce new empirical formulas for the strain rate and temperature dependences of the characteristics of polymeric composite materials. These formulas enable us, for any given temperature and strain rate, to determine the coefficient g characterizing the behavior of the stress intensity factor K _I (or its critical value K _Ic ) as a function of the testing temperature and strain rate within the indicated range. It is shown that the application of the proposed approach to the analysis of quasibrittle fracture of polymeric composite materials, i.e., the investigation of physical nonlinearity caused by the influence of the strain rate and temperature, makes it possible to obtain more precise estimates of the stress intensity factors under the analyzed conditions.     

Effect of Strain Rate on the Mechanical Properties of Ti-24Al-11Nb

The effect of strain rate on the bend ductility and notch fracture toughness of Ti-24Al-11 Nb wasstudied,it was found that the strain rate with a range of 1.17×10~(-5)～1.17 ×10~(-3) at 20℃ had nega-tive influence on both properties based on different microstructures.     

原位法表征碳／碳复合材料界面性能的研究

用单丝顶出和束顶出法分别测试了细编穿刺碳／碳（Ｃ／Ｃ）复合材料不同层次的界面粘结性能，研究了生产工艺对不同层次界面性能的影响，建立了顶出试验的力学模型，并用有限元方法分析了界面上应力的分布情况，对可能的界面破坏模式进行了预测，为最终优化Ｃ／Ｃ复合材料的生产工艺提供了依据。     

冷等离子处理对炭纤维表面及复合材料性能的影响

空气气氛下对T300炭纤维进行不同时间的等离子处理。对处理后的炭纤维表面进行了扫描电镜(SEM)观察,对表面活性基团进行了红外光谱测试。结果显示,随着处理时间的增长,纤维表面沟槽长度加长,程度加深,表面粗糙度增大。纤维表面并没有明显的活性基团产生。将处理后的炭纤维制备成单向增强板,测得试样的弯曲模量达到109GPa;弯曲强度在处理时间为16min之内增加较快达到1241.5MPa,超过16min之后开始下降。等离子处理前后的力学性能相比,弯曲模量提高了50.97%,弯曲强度提高了46.89%。实验结果显示,等离子处理16min能够得到比较好的界面结合性能和力学性能。     

阳极氧化对高聚物基碳纤维复合材料界面性能的影响

采用阳极氧化法对Ｔ－３００高强度碳纤维和Ｍ－４０高模量碳纤维进行了表面处理。发现该方法能剥除Ｔ－３００碳纤维表面的高涂层，涂覆耐热涂层后可提高Ｔ－３００／聚酰亚胺复合材料界面的抗热氧化性能，并且可使基体改性的珠Ｍ－４０／酚醛环氧复合材料界面强度和冲击强度同时获得提高。     

碳纤维增强镁合金层合板及其基本力学性能

对碳纤维增强镁合金金属层合板FML(Fiber Metal Laminates)进行了初步的探索和研究.在几种不同层数和体分比下,制备了碳环氧/镁合金层合板这种轻型结构材料,通过对这种新材料的初步力学性能的试验测试,给出了碳纤维增强镁合金金属层合板的应力-应变曲线,以及强度极限、弹性模量与纤维/环氧复合材料百分含量的关系.     

应变速率对一种无铼单晶高温合金低周疲劳性能的影响

研究了一种无铼镍基单晶高温合金在1223 K、不同应变速率(5×10^-4s^-1、1×10^-3s^-1、5×10^-3s^-1、1×10^-2s^-1)条件下的低周疲劳行为。结果表明:在四种应变速率条件下,合金均表现出循环稳定。随着应变速率的增加,合金的疲劳寿命逐渐增加,且其半寿命稳定滞后回线环内面积逐渐减少,表明低应变速率合金更容易积累蠕变塑性变形。疲劳裂纹源均萌生于试样表面,随着应变速率的增加,疲劳过程中产生的塑性变形越来越少,疲劳裂纹扩展区的面积逐渐增大。低应变速率时,较大的塑性变形导致合金取向发生明显的偏转,诱发多滑移系开动进而形成位错网;反之,高应变速率时,合金没有产生明显的塑性变形,只有单一方向的位错塞积形成位错束。     

碳纤维阳极氧化法处理对复合材料界面性能的影响

利用阳极氧化法对碳纤维进行表面改性处理,研究了碳纤维处理前后表面化学组成,纤维复丝拉伸强度和复合材料的层间剪切强度（ＩＬＳＳ）。结果表明,经阳极氧化处理碳纤维表面的含氧、含氮极性官能团数目增加,纤维复丝拉伸强度有所下降,复合材料的ＩＬＳＳ值提高。同时通过实验结果分析,阐明阳极氧化处理使复合材料界面性能改善的机理。     

Localization of Strain Rate at Mesoscale and Its Effect on the Measured Strain Rate Sensitivity During Superplastic Deformation

Microstructural observations on specimens deformed in regions I, II and III of superplasticity suggest that the dislocation activity is restricted to limited grains in region I but spreads to almost all grains in the region III. Analysis has been carried out to show that the transition from the localized plastic flow in region I to relatively homogeneous plastic flow in region III significantly contributes to the high strain rate sensitivity observed in region II.     

Stacking Sequence Effect on the Fracture Behavior of Narrow L-Shaped Cross-Ply Laminates: Experimental Study

Strength of Materials - The stacking sequence effect of narrow L-shaped laminates on the fracture mode was studied. Two laminate stacking sequences were designed to analyze different fracture...     

高应变率下阻尼铝合金的动态力学性能研究

针对航空用高阻尼铝合金在高应变率载荷下的服役特征,研究了两种高阻尼铝合金在高应变率下的动态力学性能.采用分离式霍布金森(Hopkinson)压杆对高阻尼铝合金进行了动态压缩实验,获得了应变率(140,275,500s-1)对材料应力-应变曲线的影响规律,并同普通铸造铝合金ZL101A的动态压缩力学性能进行比较分析.结果表明:高阻尼铝合金在高应变率下的力学性能明显优于普通铸造铝合金;第一种高性能阻尼铝合金的动态压缩力学性能优异.第二种高性能阻尼铝合金随着应变率的提高,材料的弹性模量和应力均有所下降,但是形变强化效果显著.