1) SiC/Al Alloy
SiC/Al合金
1.
Mechanical Properties and Damage Behaviors of SiC/Al Alloy Multilayered Composite Materials;
SiC／Al合金层状复合材料的机械性能及损伤行为
2) SiC/Al alloy composite
SiC/Al合金复合材料
4) Fe-Al/SiC composite coating
Fe-Al/SiC复合涂层
1.
Fe-Al/SiC composite coating was made by HVFS.
利用高速火焰喷涂技术制备出Fe-Al/SiC复合涂层,在MM-A1立式磨损试验机上对涂层常温下的摩擦磨损特性进行研究。
2.
It indicated that the matrix of Fe-Al/SiC composite coating was Fe-Al phase (Fe3Al,FeAl) and SiC hard phase distributed all over the coating, and the coating displayed the typical layers structure characteristics.
采用高速火焰喷涂技术制备了Fe-Al/SiC复合涂层,对涂层在650℃下的热腐蚀动力学规律进行了研究,并利用扫描电镜(SEM)、能谱仪(EDS)和X射线衍射仪(XRD)对涂层及腐蚀产物的成分和形貌进行分析。
3.
In order to solve the hot corrosion problem on the water-wall tubes in thermal power plants, HVFS technology was used to prepare the Fe-Al/SiC composite coating, and the bonding strength, micro hardness, thermal shock and hot corrosive resistance performance of the coating were studied.
为解决火电厂锅炉水冷壁热腐蚀问题,采用高速火焰喷涂技术首次制备出Fe-Al/SiC复合涂层,并对涂层的结合强度、显微硬度、抗热震性能和耐热腐蚀性能进行了研究。
5) SiC/Al composites
SiC/Al复合材料
1.
Effect of pore-forming agents content on bending strength of SiC/Al composites;
造孔剂含量对SiC/Al复合材料抗弯强度的影响
2.
SiC/Al composites were fabricated by pressureless infiltration technique.
采用无压浸渗法制备了SiC含量较高的SiC/Al复合材料,分析了造孔剂添加量对多孔预制体孔隙率的影响,利用铝液浸渗多孔体理论分析了多孔预制体孔隙结构对复合材料孔隙率的影响。
3.
SiC/Al composites reinforced with high volume fraction of low cost SiC powder have excellent properties of high specific strength, specific elastic modulus, improved wear resistance, low thermal expansion and high thermal conductivity.
高增强体含量SiC/Al复合材料不仅具有高的比强度、比弹性模量和耐磨损等力学性能，还拥有低膨胀、高导热的热学性能，而且原材料价格低廉、性能可任意剪裁，无论用作结构件、还是功能构件，都有很大的发展潜力。
6) SiC/Al composite
SiC/Al复合材料
1.
High volume fraction SiC/Al composites for space-based optomechanical structures;
制备空间光机结构件的高体份SiC/Al复合材料
2.
Application of high volume fraction SiC/Al composites to unmanned airborne photoelectric platforms
高体份SiC/Al复合材料在无人机载光电稳定平台中的应用
3.
SiC/Al composite were prepared by hot pressing,variations in friction and wear were studied related to heat treatment.
载荷超过5 N后,高SiC(20wt%以上)含量的复合材料热处理后的磨损率大幅降低,7 N时,30wt%SiC/Al复合材料的磨损率可达到1。
补充资料：Al-Li合金构件——歼7-II飞机舱口盖及副翼扰流片
Al-Li合金构件——歼7-II飞机舱口盖及副翼扰流片
Al—Ll合金构件——歼7一I 1机舱口盖及副翼扰流片 张自供稿
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条