摘要
使用连续固-液复合的方法制备了锡青铜(Tin bronze,TB)/10号钢(1010 steel)双金属层状复合材料。通过金相显微镜、电子探针显微镜和透射电镜分析了复合材料的微观组织和界面结合机制。使用硬度和拉伸-剪切测试的方法分别研究了锡青铜/10号钢复合板的力学性能和界面结合强度。结果表明,复合板中锡青铜微观组织均匀,而钢由于冷却过程中复杂的温度场,形成了铁素体+珠光体+贝氏体的复杂微观组织。复合材料具有优异的界面结合性能,实现了界面的全冶金结合。TEM结果表明,在锡青铜和10号钢之间形成了牢固的原子间结合界面。拉伸-剪切测试结果表明,最终的断裂发生在锡青铜侧,界面的结合强度大于锡青铜的。
Tin bronze(TB)/1010 steel bimetal laminated composites were prepared using continuous solid-liquid bonding method.Microstructure and interfacial bonding mechanism of the composites were analyzed by optical micro⁃structure(OM),electron probe microanalysis(EPMA)and transmission electron microscope(TEM).The mechani⁃cal properties and interfacial bonding strength of composites were investigated by hardness and tensile-shear tests,respectively.The results indicate that microstructure of the tin-bronze is homogeneous,while a complex microstruc⁃ture of ferrite+pearlite+bainite are formed in steel due to the complex temperature field during the cooling process.The composites exhibit excellent interfacial bonding properties,realizing the completely metallurgical bonding.TEM results reveal that a strong interatomic bonding interface is generated between tin bronze and 1010 steel.The tensileshear test results demonstrate that the final fracture occurs on the tin-bronze side,and the bonding strength of the inter⁃face is higher than that of tin-bronze.
作者
彭博
于凤云
邓佳男
接金川
李廷举
PENG Bo;YU Fengyun;DENG Jia'nan;JIE Jinchuan;LI Tingju(School of Materials Science and Engineering,Dalian University of Technology,Dalian 116024;China Avia-tion Development Shenyang Liming Aero Engine Co.,Ltd.,Shenyang 110043;Ningbo Institute of Dalian Uni-versity of Technology,Ningbo 315000)
出处
《特种铸造及有色合金》
CAS
北大核心
2024年第10期1307-1312,共6页
Special Casting & Nonferrous Alloys
基金
国家自然科学基金资助项目(52071050)
国家重点研发计划资助项目(2018YFE0306103)。
关键词
固/液复合
锡青铜
双金属复合板
界面
拉伸-剪切
Solid-liquid Bonding
Tin Bronze
Bimetal Composite Plate
Interface
Tensile-shear