晶须增强铝基复合材料的热压缩变形行为研究

采用试验和数值模拟相结合的方法研究了纵向、横向和倾斜分布的晶须增强铝基复合材料热压缩变形行为.研究表明:SiCw/6061Al复合材料300℃压缩的应力-应变行为与晶须取向角密切相关;在热变形过程中,纵向分布晶须折断严重,导致复合材料表现为应变软化行为;而倾斜于压缩方向30°的晶须折断和转动明显,引起相应复合材料应变软化;横向分布晶须没有转动而折断程度很小,使复合材料呈现出加工硬化行为.     

晶须取向对SiCw/6061Al复合材料热压缩变形行为的影响

采用SEM 和 Magiscan-2A 图像分析系统研究了晶须取向对SiCw/6061Al复合材料在300℃压缩变形行为的影响.结果表明:晶须取向影响着晶须折断程度和转动角度; 随着晶须取向角的增加,晶须转动和折断行为所导致的软化效果下降.同时晶须取向也影响复合材料的热压缩应力-应变曲线的形状.在热压缩变形过程中,晶须取向角为0°和30°的复合材料表现出明显应变软化现象, 晶须取向角为45°的复合材料无明显软化现象.晶须取向角为90℃的复合材料表现出应变硬化现象.     

SiC晶须对SiCw/6061Al复合材料拉伸和压缩变形行为的影响

通过试验研究了SiCw/6061Al复合材料和6061Al基体的拉伸和压缩变形行为.结果表明,SiCw/6061Al复合材料和6061Al的拉伸变形行为相同,而压缩变形曲线上出现应力峰,这与不同应力状态下SiC晶须的转动有关.拉伸时SiC晶须逐渐转向与外力平行方向使SiCw/6061Al复合材料的应力增大,而压缩时SiC晶须转向与外力垂直方向使其应力减小,而不是由动态再结晶引起.     

高压原位合成Al3Ni晶须增强AI基复合材料

在１－６ＧＰａ范围内原位合成Ａｌ３Ｎｉ晶须增强Ａｌ基复合材料。原位合成的Ａｌ２Ｎｉ晶须尺寸小，在高致密度的复合中分布弥散；并研究了对Ａｌ３Ｎｉ昌须尺寸及晶发布取向的影响。     

石墨烯增强铝基复合材料的制备及热变形研究

为了探究石墨烯增强铝基复合材料的制备工艺及其热变形行为,本文采用湿混球磨结合真空热压烧结法制备了0.5wt.％石墨烯增强铝基复合材料,并利用场发射扫描电子显微镜、能谱仪和X射线衍射仪对其进行微观组织观察、成分和物相分析,用Gleeble 3800热模拟机对复合材料进行等温压缩试验,建立了材料的本构方程并分析其热变形机理...     

7075Al/SiCp复合材料的热压缩变形流变应力和组织行为

采用圆柱试样在Gleeble-1500热模拟机上对喷射沉积7075Al/SiCp复合材料进行高温压缩变形实验,实验条件为:变形温度300～450℃,应变速率0.001～1s-1.结果表明:7075Al/SiCp复合材料的流变应力大小受到变形温度和应变速率的强烈影响,流变应力随应变的增加而逐渐增加,出现一峰值后逐渐下降;流变应力随变形温度的升高、应变速率的降低而降低.可用Zener-Hollomon参数的双曲正弦形式来描述7075Al/SiCp复合材料高温压缩变形流变应力.随着变形温度的升高和应变速率的降低,7075Al/SiCp复合材料热变形过程中SiCp的分布逐渐均匀化,有利其热加工性能的改善.     

高压原位合成Al_3Ni晶须增强Al基复合材料

在 1～ 6 GPa高压范围内原位合成 Al3Ni晶须增强 Al基复合材料。原位合成的 Al3Ni晶须尺寸小 ,在高致密度的复合材料中分布弥散 ;并研究了高压对 Al3Ni晶须尺寸及晶须分布取向的影响。     

晶须增韧陶瓷基复合材料裂纹扩展行为模型

在考虑晶须桥联和裂纹转两种增韧机理的基础上，建立了晶须增韧陶瓷复合材料裂纹扩展行为的理论模型，利用该型计算了单边切口梁三点弯曲的Ｒ－阻力曲线和载荷－位移曲线。     

Al/Al2O3复合材料的伪半固态压缩变形力学行为

对37%Al/Al2O3复合材料坯料进行高温压缩,研究其伪半固态压缩变形力学行为.结果表明,该材料在伪半固态温度下的高温压缩过程中,真实应力-真实应变曲线存在四个变化阶段:急剧上升-下降-平稳-缓慢上升,且稳态流动应力及峰值应力随着温度的提高和应变速率的降低显著下降,说明该材料具有应变速率和变形温度敏感性.随着变形量的增加,微观组织中的孔洞逐渐增多.     

正挤压对SiCw/6061Al晶须形貌的影响

为了研究正挤压加工对SiCw/6061Al复合材料晶须形貌的影响规律,通过改变挤压温度、挤压比等工艺条件正挤压成形了挤压铸造法制备的15vol.%SiCw/6061Al复合材料,利用SEM技术观察和分析了正挤压加工前后复合材料的微观组织形貌.研究表明:正挤压加工导致SiC晶须沿着复合材料的塑性流动方向呈现出一定程度的定向排列趋势,并伴随有比较明显的折断现象;挤压温度、挤压比等工艺参数都是影响SiC晶须形貌的主要因素.     

界面对颗粒增强金属基复合材料强化性能的影响

为提高颗粒增强金属基复合材料的力学性能,采用基于微观组织的胞元模型建模方法,并利用有限元软件ABAQUS着重分析了界面层厚度以及界面层强度对复合材料性能的影响,通过对复合材料中各组成部分的应力、应变云图的获取,形象地说明了各部分的变形规律.研究结果表明,在弱界面层下,随着界面层厚度的增加,复合材料的强化效果并不显著,而在强界面层下,随着界面层厚度的增加,强化效果非常明显;就界面层强度来说,界面越强,所表现出的强化效果就越明显,但当界面层强度比基体大得多时,随着界面层强度的增加,虽然复合材料的强化呈递增趋势,但是递增的幅度已逐渐降低.     

高阻尼铝基复合材料在海水中的腐蚀行为

研究了高阻尼铝基复合材料在海水中的腐蚀行为,本实验所用高阻尼铝基复合材料是以6061铝合金为基体,加入SiC颗粒和石墨粉,用粉末冶金方法制备的。测定了高阻尼铝基复合材料在海水中的腐蚀速率度、电极电位和极化曲线,并通过与基体金属的对比来描述它的腐蚀特性。实验表明,在海水介质中,高阻尼铝基复合材料的耐蚀性能比6061铝合金差,孔蚀倾向大。在海水介质中使用高阻尼铝基复合材料必须加以保护。     

原位反应渗透法TiCp/Mg复合材料的制备和性能

利用Ti和C元素粉末间的原位放热反应合成TiCp,结合Mg熔体的自发渗透技术制备了TiCp/Mg以及TiCp/AZ91D两种镁基复合材料,观测了复合材料的相组成和原位反应生成物TiCp的形貌,研究了这两种镁基复合材料的常温压缩性能.结果表明,原位反应自发渗透技术制备的Mg基复合材料组织致密,增强相呈细小的颗粒状和互穿网片状,分布均匀.这是材料的压缩强度得到提高的原因.在常温以及应变速率为0.01 s-1的条件下,TiCp/Mg和TiCp/AZ91D镁基复合材料的压缩强度分别达到598和650 MPa.     

Internal stress behavior of the short ceramic fiber reinforced aluminum alloy under tensile deformation

The in situ measurement of phase stress under tensile deformation on an A6061 alloy reinforced with SiC whiskers (Al/SiCw MMC: Metal Matrix Composite) was performed using the X-ray diffraction technique. In order to raise a preciseness of measurements, we applied a profile fitting technique to separate the nearby located diffraction peak. Tensile deformation on elastic to plastic range was applied by four points bending device and discussed internal stress behavior in the short ceramic fiber reinforced MMC. Phase stress in Al matrix was increased linearly up to 2800×10⁻⁶ in strain and then saturated immediately. On the other hand phase stress in SiC whiskers shows an unstable stress behavior. It was decreased at first because of the Poisson's effect from Al matrix but reversed over 500×10⁻⁶ applied strain. The measured phase stress behavior in elastic region agreed with the calculations using micromechanics based on Eshelby/Mori–Tanaka model except for this unstable internal stress region. The macro stress behavior in plastic region was extremely small than that of the tensile test results. It supposed that the mechanism of strength is not so much the fiber reinforcing as the dispersion strengthening like the Orowan mechanism. Regarding the fatigue property, ΔK_th of the Al/SiC MMC, this was lower than that of the A6061 alloy. On the Al/SiCw MMC specimen, many micro void formations were observed around the fatigue crack tip even under the ΔK_th of A6061. It was considered that these were caused by the high gradient of residual stress on composite process and the unstable stress behavior in low ΔK region.     

Microstructure evolution and hot deformation behavior of carbon nanotube reinforced 2009Al composite with bimodal grain structure

The hot deformation behaviors of the bimodal carbon nanotube reinforced 2009Al(CNT/2009Al)com-posite were studied by establishing processing map and characterizing the microstructure evolution.The results indicate that the grain size in the ultra-fine grained zones was stable during hot deformation,while the coarse grained zones were elongated with their long axis directions tending to be perpendicular to the compression direction.Low temperature with high strain rate(LTHR),as well as high temperature with low strain rate(HTLR)could increase the length/width ratio of the coarse grained zones.However,LTHR and HTLR could cause the instable deformation.The instable deformation at LTHR was induced by severe intragranular plastic deformation and the localized shear crack,while the instable deformation at HTLR resulted from the more deformation component at the coarse grained zones,and the micro-pore initiation due to CNT re-agglomeration at the boundaries between the coarse and the ultra-fine grained zones.