SiC颗粒增强Al-Fe-V-Si复合材料的SiC/Al界面形貌

采用喷射沉积工艺制备SiCp/Al-Fe-V-Si复合材料,并通过热压和热轧工艺对沉积坯进行致密化;通过高分辨电镜观察其SiC/Al界面形貌,并对比热暴露后的界面形貌。结果表明:复合材料主要存在两种SiC/Al界面,一种是厚度为3nm左右的晶态Si界面层,且在界面附近的基体中生成细小的Al4C3相;另一种是厚度为5nm的非晶态SiO2界面层,部分溶解的SiC颗粒向附近Al基体中注入游离态的Si,在界面附近形成Si的浓度梯度;两种界面都具有良好的润湿性,界面结合强度高;经640℃热暴露10h后,SiC/Al界面处生成的粗大Al4C3脆性相降低界面结合强度,从而降低复合材料的力学性能。     

SiC_p/2024Al复合材料界面的表征及评价（英文）

采用粉末冶金方法制备体积分数为35%的Si Cp/2024 Al复合材料。利用高分辨透射电镜对复合材料中Si Cp与Al基体、析出相与Al基体之间的界面微结构进行表征,采用拉伸弹性模量和布氏硬度测试对界面状况进行评估。结果表明,所得复合材料中Si C与Al的界面整体状况良好。复合材料中SiC/Al界面分为3种类型:大部分干净界面、少量轻微反应型界面以及极少量的非晶层界面。在干净界面中,Si C和Al的结合机制为紧密原子匹配形成的半共格界面,且Si C和Al无固定或择优的取向关系。在轻微反应型界面中,MgA l2O4尖晶石与Si C和Al均形成半共格界面,作为中间媒介很好地连接Si C和Al。复合材料经510°C固溶2 h再在190°C时效9 h后,许多圆盘状纳米析出相和棒针状纳米析出相弥散分布于基体中,且与基体的界面为错配度较小的半共格界面。此时,复合材料的布氏硬度达到峰值。     

高性能SiC增强Al基复合材料的显微组织和热性能

采用模压成型和无压浸渗工艺制备了高体积分数SiC增强Al基复合材料(AlSiC),对其物相和显微结构进行研究。结果表明:用上述方法制备的AlSiC复合材料组织致密,两种粒径的SiC颗粒均匀分布于Al基质中,界面结合强度高;SiC增强颗粒与Al基质界面反应控制良好,未出现Al4C3等脆性相。分析指出:Al合金中Si元素的存在有利于防止脆性相Al4C3的形成,Mg元素的加入提高了Al基体和SiC增强体之间的润湿性。所获得复合材料的平均热膨胀系数为9.31×10 6K 1,热导率为238 W/(m.K),密度为2.97 g/cm3,表现出了良好的性能,完全满足高性能电子封装材料的要求。     

不同SiCp预处理的SiCp/Al复合材料界面特征及耐蚀性

采用无压渗透法制备了经不同SiCp表面预处理的SiCp/Al复合材料,研究了SiC颗粒表面预处理对SiCp/Al复合材料界面特征及其腐蚀行为的影响。结果表明,高温氧化处理使SiC颗粒边界钝化,颗粒表面形成均匀SiO2氧化膜,复合材料界面结合良好,而未表面处理和酸洗的复合材料界面孔隙多,界面结合较差。经高温氧化SiC颗粒表面预处理的SiCp/Al复合材料耐腐蚀性能最好,酸洗次之,未表面处理最差。高温氧化处理形成的SiO2氧化膜对SiC颗粒起着保护作用,抑制了SiCp/Al界面Al4C3相形成,对复合材料耐腐蚀性能有利。     

含高体积分数SiC_p的Al复合材料微观组织及弯曲性能

利用无压浸渗法制备高体积分数SiC的SiC_p/Al复合材料.采用XRD和SEM对复合材料的相组成、微观组织及断口形貌进行分析,研究颗粒粒径分布和基体合金成分对复合材料抗弯性能的影响.结果表明:以Al-10Si-8Mg(质量分数,%)合金为基体制备的复合材料组织均匀,致密度好,无明显气孔缺陷;界面反应产物为Mg2Si、MgAl_2O_4和Fe,其弯曲强度高于以Al-10Si合金为基体制备的复合材料的弯曲强度;SiC_p/Al复合材料的弯曲强度随着SiC颗粒粒径的增大而减小;复合材料整体上表现出脆性断裂的特征.     

Cf+SiCp/Al复合材料的微观组织与力学性能

采用挤压铸造法制备了SiC颗粒混杂增强T700/Al和M40/Al复合材料,研究了材料的微观组织与力学性能.结果表明,复合材料组织致密,纤维分布均匀.铸造态复合材料存在界面反应,透射电镜和XRD分析表明M40/Al的界面反应物尺寸和数量均小于T700/Al,M40Cf与铝具有较好的化学相容性.拉伸试验表明,M40/Al的抗拉强度高于T700/Al,这是由于界面反应物的数量改变了复合材料的断裂机制.     

SiC/Ti6Al4V复合材料界面反应产物的形成序列及扩散路径

通过SiC/Ti6Al4V钛基复合材料的制备及在不同条件下的热处理试验，利用SEM，EDS及XRD分析技术研究复合材料界面反应产物相的形成及反应元素的扩散路径。结果表明：反应元素如C，Ti，Si在界面反应层中出现浓度波动，合金元素Al并没有显著扩散进入界面反应产物层，而是在界面反应前沿堆积，其界面反应产物被确认为Ti3SiC2，TiCx，Ti5Si3C，和Ti3Si；在界面反应初期，存在着TiC＋Ti5Si3Cx双相区，当形成各界面反应产物单相区时，SiC／Ti6Al4V复合材料界面反应扩散的完整路径应为：SiC ｜ Ti3SiC2 ｜ Ti5Si3Cx ｜ TiCx ｜ Ti3Si｜ Ti6Al4V＋TiCx；界面反应产物层的生长受扩散控制，遵循抛物线生长规律，其生长激活能Q^k及k0分别为290.935 kJ·mol^-1,2.49× 10^-2 m·s^-1/2.     

喷涂Al/SiC复合材料的制备与组织分析

采用等离子喷涂技术和亚音速火焰喷涂技术制备了高性能Al/SiC复合材料.利用OM,SEM,TEM,XRD等仪器详细分析了上述两种技术制备的Al/SiC复合材料微观组织.结果显示,亚音速火焰喷涂技术和等离子喷涂技术均可制备出SiC体积分数大于50%的Al/SiC复合材料,所制备的Al/SiC复合材料组织致密、颗粒均匀分布、SiC颗粒和Al之间的界面结合良好.XRD研究表明,等离子喷涂Al/SiC复合材料中存在着Al,SiC,晶体Si等相.亚音速火焰喷涂Al/SiC复合材料中的相是由Al,SiC和少量的Al2O3组成.与等离子喷涂相比,亚音速火焰喷涂Al/SiC复合材料的孔隙率较高,氧化程度较高.此外等离子喷涂Al/SiC复合材料中有一定量纳米尺度的晶粒和颗粒.     

SiC_p/Al基复合材料的铝浴自蔓延反应制备及其热学性能

将SiC和Ti的混合粉末压坯浸入铝液中 ,引发SiC和Ti的自蔓延反应 ,制备了低膨胀、高导热和高含量SiCp/Al基复合材料。自蔓延反应产物Ti5Si3和TiC在SiC颗粒表面原位形成涂层 ,改善了SiCp/Al界面的润湿性。SiC颗粒自重沉降 ,可形成高SiC含量的复合材料。考察了复合材料的热膨胀系数、导热系数及其与自蔓延反应之间的关系。结果表明 ,自蔓延反应对材料的热膨胀系数影响不大 ,但剧烈的自蔓延反应会损害材料的导热性能 ,如果适当控制反应程度 ,可以制备低膨胀、高导热的SiCp/Al基复合材料。     

K2ZrF6助浸SiC涂层碳纤维增强Al复合材料的研究

研究了用K_2ZrF_6助浸法制造C/Al复合材料的工艺和K_2ZrF_6的助浸机理结果表明:K_2ZrF_6处理后,C,Al间的润湿性仍比SiC,Al间的差C,Al间的润湿主要靠大量的界面化学反应、这使得复合材料的制造十分困难;而SiC、Al间的润湿靠微量的SiC在Al中的溶解K在纤维或涂层中的扩散也可能起助浸作用Al液在极短时间内对SiC涂层后的纤维束或纤维预制件浸渍良好同时,将基体Si合金化后,获得了完整的CF/SiC/Al界面,圆满解决了C/Al复合材料的界面相容性和制造中的问题     

SiC_p/2024铝合金复合材料粉末混合半固态挤压法制备

研究了SiCp/ 2 0 2 4铝合金复合材料的粉末混合 半固态挤压成形工艺及所制备材料的组织和界面特征。不同温度下半固态挤压的挤压力与位移曲线表明 ,半固态挤压过程的成形力低且稳定。SEM和TEM电镜观察结果表明 ,该工艺可以获得增强颗粒分布均匀、基体组织致密、界面结合良好且无界面反应的复合材料型材。分析了半固态挤压后复合材料的力学性能 ,结果表明 :与基体合金相比 ,复合材料的弹性模量、屈服强度、抗拉强度均有很大提高 ;与其它工艺生产的该复合材料相比 ,所制备的复合材料的塑性相对较高。     

The influence of the reinforcing particle shape and interface strength on the fracture behavior of a metal matrix composite

A numerical analysis of the reinforcing particle shape and interface strength effects on the deformation and fracture behavior of an Al/Al₂O₃ composite is performed. Three-dimensional calculations are carried out for five elastic–brittle particles embedded into the elastic–plastic matrix, the reinforcing particle shape being varied from spherical to strongly irregular. It is shown that microstructural heterogeneity of the composite gives rise to a complex stress–strain state in the vicinity of particle boundaries and hence to near-interface areas undergoing tensile deformation both in tension and compression. Within the strain range under study, compressive strength is not achieved, either in compression or in tension, i.e., all cracks grow only under tensile stress. Particle fracture is found to occur by two mechanisms: interface debonding and particle cracking. Individual and combined effects of the particle shape, interface strength, and loading conditions on the fracture mechanisms are analyzed.     

Microstructure,mechanical properties and two-body abrasive wear behaviour of hypereutectic Al—Si—SiC composite

The microstructure, mechanical properties, and the effects of sliding distance and material removal mechanism on two-body abrasive wear behaviour of hypereutectic Al—Si—SiC composite and its matrix alloy were investigated. The hypereutectic Al—Si—SiC composite was prepared by stir casting route. The hardness, ultimate tensile strength and yield strength of the composite are increased by 17%, 38%, and 30% respectively compared with those of the matrix alloy, while the elongation of the composite is decreased by 48% compared with that of the matrix alloy. The wear rate of the materials is increased with increasing the abrasive size and the applied load and does not vary with the sliding distance. The wear surfaces and wear debris of the materials were characterized by high-resolution field emission scanning electron microscopy (HR FESEM) and wear mechanism was analyzed for low and high load regimes.     

SiC纤维表面改性对SiCw／Al复合材料界面强度的影响

用ＳｉＯ２，Ｃ对ＳｉＣ纤维进行表面处理后制备成ＳｉＣｗ／Ａｌ复合材料，对其拉伸形变断裂过程的声发射行为进行了研究，并测定了纤维断裂强度和纤维基体间的界面切变强度。结果表明界面切变强度，纤维断裂强度和界面性能对纤维的表面处理十分敏感，富ＳｉＯ２处理的ＳｉＣ纤维的界面性能得到改善，而富碳处理的界面变脆。     

有限元模拟SiC增强Al基复合材料的力学行为

采用有限元方法和轴对称单胞模型模拟了增强体(SiC)形状、体积分数以及不同基体类型对铝基复合材料力学行为的影响。模拟结果表明:增强体的加入会阻碍基体的塑性流变,使基体内发生非均匀变形,在增强体尖角处出现应力集中;椭圆柱形增强体对基体塑性变形的阻力最大,传递载荷的能力最强,因此强化效果最好。在一定范围内,随着增强体体积分数的增加,基体与增强体之间的比表面积增大,有利于载荷的传递;增强体体积分数的增加导致颗粒间距减小,几何必须位错自由运动的路径减少,复合材料的强度也随之增加。此外,不同类型基体自身的塑性流变能力不同,Al-Zn-Mg基体强度最高,在拉伸变形过程中,受到增强体的阻碍作用最大,会有更多的载荷从基体传递到增强体,以Al-Zn-Mg为基体的复合材料的强度最高。     

Influence of pulse impact on properties of liquid phase pulse impact diffusion welding SiCp/AlSi7Mg and its welding mechanism

Abstract

The influence of pulse impact on the microstructure and properties of welded joints of aluminium matrix composite SiC_p/AlSi7Mg by liquid phase pulse impact diffusion welding (LPPIDW) and its welding mechanism had been studied. It showed that during LPPIDW, under the effect of pulse impact, the interface state between SiC particle and matrix was prominent, the initial pernicious contact state of reinforcement particles had been changed from reinforcement (SiC)/reinforcement (SiC) to reinforcement (SiC)/matrix/reinforcement (SiC), and the harmful microstructure or brittle phase was restrained from the welded joint. Moreover, the density of dislocation in the matrix neighbouring to and away from the interface was higher than that of its parent composite and the dislocation entwisted each other intensively. Furthermore, the deformation mainly occurred in the matrix grain and the matrices around SiC particles engendering intensive aberration offered a high density nucleus area for matrix crystal in favour of forming nanograins, which improved the properties of welded joints distinctly, resulting in welding the composite successfully. Consequently, the tensile strength of the welded joints was up to 179 MPa, which was ～74˙6% of the strength of SiC_p/AlSi7Mg (as stir cast), and its corresponding radial deformation was less than 3%, suitable for the demand of deformation of welded specimens.     

热挤压变形对搅拌铸造SiCp/2024复合材料显微组织与力学性能的影响

利用搅拌铸造?热挤压工艺制备SiCp/2024复合材料板材。通过金相观察(OM)、扫描电镜(SEM)及力学性能测试等手段研究了该复合材料热挤压变形前后的显微组织与力学性能。结果表明,复合材料铸坯主要由大小为80μm~100μm的等轴晶组成,晶界第二相粗大呈非连续状分布,SiC颗粒较均匀地分布于基体合金,大部分SiC颗粒沿晶界分布,少数颗粒分布于晶内;热挤压变形后,显微孔洞等铸造缺陷和SiC颗粒团聚现象明显消除,SiC颗粒及破碎的第二相沿热挤压方向呈流线分布,复合材料的强度和塑性显著提高;拉伸断口表明,热挤压变形有利于改善SiC颗粒与基体合金的界面结合;SiCp/2024复合材料主要的断裂方式为SiC颗粒断裂和SiC/Al的界面脱粘。     

Effect of limited matrix–reinforcement interfacial reaction on enhancing the mechanical properties of aluminium–silicon carbide composites

An unconventional approach to strengthening Al/SiC composites through controlled matrix–reinforcement interfacial reactions was studied. Composites with two distinct interfacial microstructures were prepared by varying the contact time between the SiC particles and molten aluminium during processing. The formation of a thin Al₄C₃ reaction layer along the particle–matrix interface was found to increase the composite yield strength, ultimate tensile strength, work-hardening rate and work-to-fracture, and change the fracture pattern from one involving interfacial decohesion to one where particle breakage was dominant. These changes were attributed to a stronger interface bond, which is thought to result from the tendency for the Al₄C₃ reaction layer to form semicoherent interfaces and orientation relationships with the aluminium matrix and SiC particles and for it to be mechanically “keyed-in” to both these phases. The stronger interface bond also enhanced the levels of plastic constraint which, when coupled with the greater work hardening, promoted local matrix failure, thereby reducing the composite ductility.     

Microstructures and mechanical properties of Al 2519 matrix composites reinforced with Ti-coated SiC particles

Ti-coated SiC_p particles were developed by vacuum evaporation with Ti to improve the interfacial bonding of SiC_p/Al composites. Ti-coated SiC particles and uncoated SiC particles reinforced Al 2519 matrix composites were prepared by hot pressing, hot extrusion and heat treatment. The influence of Ti coating on microstructure and mechanical properties of the composites was analyzed by scanning electron microscopy (SEM) and energy dispersive spectroscopy (EDS). The results show that the densely deposited Ti coating reacts with SiC particles to form TiC and Ti₅Si₃ phases at the interface. Ti-coated SiC particle reinforced composite exhibits uniformity and compactness compared to the composite reinforced with uncoated SiC particles. The microstructure, relative density and mechanical properties of the composite are significantly improved. When the volume fraction is 15%, the hardness, fracture strain and tensile strength of the SiC_p reinforced Al 2519 composite after Ti plating are optimized, which are HB 138.5, 4.02% and 455 MPa, respectively.     

搅拌铸造SiC_p/A356复合材料的显微组织及力学性能

采用搅拌铸造技术制备质量分数为15%的SiCp增强A356铝基复合材料,并对所制备的复合材料进行后续热挤压变形。通过金相观察(OM),扫描电镜(SEM)及力学性能测试等手段,对该复合材料显微组织与力学性能进行了研究。结果表明,所制备的复合材料铸态组织中,SiCp较均匀地分布于基体中,SiCp与Al界面处存在Si原子的富集;热挤压变形后,显微气孔等铸造缺陷明显减少,材料致密度显著提高,SiCp沿热挤压方向呈流线分布特征,颗粒均匀分散性明显提高;采用535℃×5h固溶+180℃×5h时效处理后,热挤压棒材的力学性能为:σs=370MPa,σb=225MPa,δ=5.3%,时效后析出强化相大小约为200nm,且弥散分布于基体中;断口分析表明,SiCp/A356铝基复合材料的断裂主要是由基体的塑性断裂及SiCp的断裂导致的。