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1.
对国内外有关SiC颗粒增强铝基复合材料摩擦磨损的研究现状进行了系统的综述,分别介绍了内部因素(包括颗粒粒径、颗粒含量、颗粒形貌和基体材料)和外部因素(包括载荷、速度、温度和电流)对SiC颗粒增强铝基复合材料摩擦磨损性能的影响,并总结了SiC颗粒增强铝基复合材料在交通运输、航空航天和电子等领域中的应用。  相似文献   

2.
颗粒增强铝基复合材料研究进展   总被引:28,自引:1,他引:28  
综述了颗粒增强铝基复合材料研究现状,从增强体选择,材料制备方法,机械性能,应用研究等各个领域,详细阐述了复合材料的特点,并指出了今后复合材料的研究方向。  相似文献   

3.
采用微波烧结的方法,在烧结温度分别为680℃,710℃,740℃,770℃,800℃制备了15%的SiCp/Al复合材料。探讨温度对材料的致密度和力学性能的影响。结果表明:致密度和材料硬度及冲击韧性随温度变化呈马鞍形,在770℃样品的密度和硬度及冲击韧性达到最佳值,分别为2.62g/cm3,42.6MPa,40J/cm2。结论:用微波烧结SiCp/Al复合材料可在短时间内使样品达到烧结致密化,缩短烧结时间,节约能源。  相似文献   

4.
纳米SiC颗粒增强铝基复合材料制备工艺研究   总被引:1,自引:0,他引:1  
本文介绍纳米复合材料的发展现状,重点介绍几种固态法制备纳米SiC颗粒增强铝基复合材料的工艺.分析铝基复合材料的显微组织,综合评价纳米SiC颗粒增强铝基复合材料制备工艺中存在的几个重要问题,并提出解决方案.在展望其应用前景基础上,指出制备技术未来的发展方向.  相似文献   

5.
纳米SiC颗粒增强铝基复合材料制备工艺进展   总被引:1,自引:0,他引:1  
余志勇  郝斌  崔华  周香林  张济山 《材料导报》2006,20(Z2):206-208,218
介绍了纳米SiC颗粒增强铝基复合材料的发展现状,重点介绍和评述了国内外几种制备工艺的研究现状和应用,分析了纳米SiC颗粒增强铝基复合材料的微观结构,指出了纳米SiC颗粒增强铝基复合材料研究中存在的几个重要问题,展望了其未来的发展趋势.  相似文献   

6.
颗粒增强铝基原位复合材料   总被引:10,自引:0,他引:10  
原位反应合成的颗粒增强铝基复合材料的弹性模量,比强度和高温强度均高,是航空,汽车工业上很有发展潜力的新型结构材料。综述了它的制备方法,组织结构及力学性能方面的研究进展。  相似文献   

7.
泡沫SiC颗粒增强铝基复合材料的制备工艺和拉伸强度   总被引:5,自引:0,他引:5  
介绍了一种新的泡沫金属材料-泡沫SiC颗粒增强铝基复合,泡沫的孔隙率为60%-85%。用TiH2作发泡剂,采用直接发泡工艺制备。由于复合材料熔体自身粘度较大,不需要采用任何增粘措施,发泡工艺简单,易于操作,该泡沫材料比普通泡沫铝或铝合金具有更高的抗拉、抗压强度。  相似文献   

8.
本研究报告通过试验建立了采用重量法铝基复合材料中SiC的分析方法,加入回收和实际样品分析结果表明,建立的方法准确可靠,可满足复合材料的分析需要.  相似文献   

9.
颗粒类型对颗粒增强铝基复合材料性能的影响   总被引:1,自引:0,他引:1  
本文对粉末冶金法制备的SiC和TiC颗粒增强铝基复合材料进行了研究。试验表明,在颗粒含量相同、尺寸相当的条件下,TiC增强Al基复合材料的强度和模量均低于SiC增强Al基复合材料,但其屈强比却明显高于SiC增强Al基复合材料。高温长时间等温处理对TiC颗粒增强纯Al复合材料的强度没有明显的影响。  相似文献   

10.
SiC颗粒增强铝基复合材料冲击拉伸力学性能的试验研究   总被引:5,自引:1,他引:5  
对SiC颗粒增强铝基复合材料在应变速率为150~1000s^-1范围内的冲击拉伸力学性能进行了试验研究,得到了材料从弹塑变形直至断裂的完整的应力应变曲线,结果表明SiC颗粒增强铝基复合材料是一种应变率敏感材料,随着应变速率的提高,材料的屈服应力,破坏应力以及破坏应变均为相应提高,断口分析表明,SiCp/Al的破坏形式的比较复杂,是一种颗粒的脆性破坏与铝合金基体的韧性破坏共存,强界面与弱界面共存的混  相似文献   

11.
碳化硅颗粒增强铝基复合材料的航空航天应用   总被引:87,自引:4,他引:87  
综合评述了近年来碳化硅颗粒增强铝基复合材料在航空航天领域所获得的一系列成功应用,并较为详尽地介绍了它们的具体应用情况以及对相关产品与装备所产生的积极作用。此外,还例举、分析和展望了该种复合材料在我国航空航天飞行器惯寻系统、光机结构及电子元器件中的几个颇具前景的应用方向。  相似文献   

12.
颗粒增强金属基复合材料的干摩擦性能与磨损机理   总被引:13,自引:0,他引:13  
颗粒增强金属基复合材料(PMMC5)具有优良的耐磨性,在摩擦磨损领域有着广阔的应用前景。本文评述了近年来关于PMMCs干摩擦磨损行为的研究结果,从材料因素和外部条件两个角度分析了各种因素对材料耐磨性、摩擦系数和配偶件磨损的影响,总结了不同条件下复合材料的磨损机制,并提出了设计摩擦磨损性能优良的PMMCs体系的可能途径。  相似文献   

13.
Abstract: In this work, we describe the fatigue behaviour of silicon carbide (SiCP)‐reinforced A359 aluminium alloy matrix composite considering its microstructure and thermo‐mechanical properties. A variety of heat treatments have been performed for the 20 vol. % SiCp composite, which resulted in different strength and elongation behaviour of the material. The fatigue behaviour was monitored, and the corresponding S–N curves were experimentally derived for all heat treatments. The fatigue strength was found to depend strongly on the heat treatment. In addition, the fatigue behaviour was monitored non‐destructively via the use of lock‐in thermography. The heat wave, generated by the thermo‐mechanical coupling and the intrinsic dissipated energy during mechanical loading of the sample, is detected by a thermal camera.  相似文献   

14.
喷射沉积成形颗粒增强金属基复合材料制备技术的发展   总被引:9,自引:2,他引:9  
分析了喷射沉积成形颗粒增强金属基复合材料制备技术的研究现状。系统地介绍了原位反应喷射沉积成形过程中进行的各类反应。在总结国内外喷射沉积成形颗粒增强金属基复合材料制备技术优缺点的基础上,发展了熔铸-原位反应喷射沉积成形金属基复合材料制备新技术。  相似文献   

15.
原位TiB2颗粒增强铝基复合材料形核机制及转变动力学   总被引:4,自引:0,他引:4  
阐述了原位合成制备TiB2颗粒增强铝基复合材料自生相的形核机制以及转变动力学,从热力学和动力学的一般角度来分析TiB2的形成机制,依据扩散原理讨论TiB2转变动力学,反应润湿及反应活化能。  相似文献   

16.
铝基复合材料增强体涂层与界面   总被引:4,自引:0,他引:4  
基体与增强体间的界面对金属基复合材料的性质起着重要的作用。为改善复合材料增强体与基体合金的浸润性,避免有害界面产物的形成,往往通过增强体表面涂层处理加以解决。本文综述了增强体涂层种类、涂覆方法及其对复合材料的界面和性能的影响。  相似文献   

17.
A processing route has been developed for the fabrication of metallic fibre mat reinforced glass matrix composites. For the model experiments reported here, a commercially available satin woven stainless steel 316L fibre mat was used as the reinforcement and soda-lime glass as the matrix. The process involves two steps: (1) the infiltration of the intra- and inter-tows regions of the fibre mats with silica sol using electrophoretic deposition and (2) the fabrication of a composite by cold uniaxial pressing and pressureless sintering of impregnated fibre mats sandwiched between layers of the matrix glass powder. The sintering took place in air at 670°C, and composite materials of sufficient integrity could be obtained without damaging the fibres. The deposited silica remained amorphous at the processing temperature providing a porous interface between the glass matrix and the metallic reinforcement. Obervation of fracture surfaces revealed that both fibre pull-out and fibre deformation occur, which should lead to a significant toughness enhancement. The presence of the interfacial silica layer, deposited using electrophoresis, is thought to be responsible for this behaviour.  相似文献   

18.
Fracture Behavior of Particle Reinforced Metal Matrix Composites   总被引:3,自引:0,他引:3  
The contributions of the reinforcement volume fraction and annealing temperatures to crack opening force and propagation energy are systematically studied by three point bending tests and by SEM investigations. The bending test data show that for the same reinforcement volume fraction, 2618 and 7075 Al composites require much higher force to open the cracks than 6061 matrix. This relates to the much higher levels of solute elements which causes matrix hardening. Studies reveal that the energy absorption level of the materials during crack propagation depends on both matrix strength and ductility which relates to the reinforcement volume fraction, composition and heat treatment conditions. Large deformation zones are found in front of the crack tip before crack propagation which indicate a ductile failure mode for the composites. Studies also reveal that cracks initiate generally at the particle/matrix interfaces for the low volume fraction reinforced composites. However, for the high volume fraction reinforced composites, crack initiation has been found from both reinforcement/matrix interfaces and broken particles. This indicates that increasing reinforcement volume fraction and matrix strengthening tend to change the fracture mode from interface debonding to particle cleavage cracking.  相似文献   

19.
碳化硅增强铝基复合材料连接技术研究进展   总被引:5,自引:1,他引:5  
综述了SiC增强铝基复合材料(包括SiCp/AlMMC和SiCw/AlMMC)连接技术的研究现状,分析了连接中存在的问题。简单介绍了用于该复合材料连接的传统焊接方法,如熔化焊、固相连接、钎焊等。重点介绍了SiC颗粒及SiC纤维增强铝基复合材料的一些新型连接技术,并展望了SiC增强铝基复合材料连接技术的发展方向。  相似文献   

20.
Herein, it is concerned with the use of profilometry-based indentation plastometry (PIP) to obtain mechanical property information for particulate metal matrix composites (MMCs). This type of test, together with conventional uniaxial testing, has been applied to four different MMCs (produced with various particulate contents and processing conditions). It is shown that reliable stress–strain curves can be obtained using PIP, although the possibility of premature (prenecking) fracture should be noted. Close attention is paid to scale effects. As a consequence of variations in local spatial distributions of particulate, the “representative volume” of these materials can be relatively large. This can lead to a certain amount of scatter in PIP profiles and it is advisable to carry out a number of repeat PIP tests in order to obtain macroscopic properties. Nevertheless, it is shown that PIP testing can reliably detect the relatively minor (macroscopic) anisotropy exhibited by forged materials of this type.  相似文献   

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