粉末冶金材料科学与工程
粉末冶金材料科學與工程
분말야금재료과학여공정
POWDER METALLURGY MATERIALS SCIENCE AND ENGINEERING
2014年
1期
147-153
,共7页
游江%刘允中%顾才鑫%李志龙%李元元
遊江%劉允中%顧纔鑫%李誌龍%李元元
유강%류윤중%고재흠%리지룡%리원원
粉末热挤压%铝基复合材料%显微组织%力学性能
粉末熱擠壓%鋁基複閤材料%顯微組織%力學性能
분말열제압%려기복합재료%현미조직%역학성능
powder hot extrusion%aluminum matrix composite%microstructure%mechanical properties
利用粉末热挤压工艺制备 SiCp/2024铝基复合材料,研究所制备复合材料的挤压态和热处理态的显微组织及力学性能,分析复合材料的断口形貌和断裂类型。结果表明:大部分SiC颗粒和析出的大量细小第二相粒子均匀地分布在基体合金中,部分区域的SiC颗粒存在轻微团聚现象,晶粒沿挤压方向被显著拉长,刚性的SiC颗粒长轴平行于挤压方向分布,形成热加工纤维组织。对复合材料进行T6(490℃固溶75 min+170℃时效8 h)热处理后,复合材料的晶粒比较细小,抗拉强度达470 MPa,主要的析出强化相为S′(Al2CuMg)。挤压比的提高有利于提高SiC颗粒和基体合金的界面结合强度。粉末热挤压法制备的SiCp/2024铝基复合材料热处理后的断裂方式主要有3种:SiC颗粒断裂、SiC颗粒与基体合金的剥离和基体合金的韧性断裂,该复合材料的断裂机制为韧性断裂和脆性断裂共存的混合断裂。
利用粉末熱擠壓工藝製備 SiCp/2024鋁基複閤材料,研究所製備複閤材料的擠壓態和熱處理態的顯微組織及力學性能,分析複閤材料的斷口形貌和斷裂類型。結果錶明:大部分SiC顆粒和析齣的大量細小第二相粒子均勻地分佈在基體閤金中,部分區域的SiC顆粒存在輕微糰聚現象,晶粒沿擠壓方嚮被顯著拉長,剛性的SiC顆粒長軸平行于擠壓方嚮分佈,形成熱加工纖維組織。對複閤材料進行T6(490℃固溶75 min+170℃時效8 h)熱處理後,複閤材料的晶粒比較細小,抗拉彊度達470 MPa,主要的析齣彊化相為S′(Al2CuMg)。擠壓比的提高有利于提高SiC顆粒和基體閤金的界麵結閤彊度。粉末熱擠壓法製備的SiCp/2024鋁基複閤材料熱處理後的斷裂方式主要有3種:SiC顆粒斷裂、SiC顆粒與基體閤金的剝離和基體閤金的韌性斷裂,該複閤材料的斷裂機製為韌性斷裂和脆性斷裂共存的混閤斷裂。
이용분말열제압공예제비 SiCp/2024려기복합재료,연구소제비복합재료적제압태화열처리태적현미조직급역학성능,분석복합재료적단구형모화단렬류형。결과표명:대부분SiC과립화석출적대량세소제이상입자균균지분포재기체합금중,부분구역적SiC과립존재경미단취현상,정립연제압방향피현저랍장,강성적SiC과립장축평행우제압방향분포,형성열가공섬유조직。대복합재료진행T6(490℃고용75 min+170℃시효8 h)열처리후,복합재료적정립비교세소,항랍강도체470 MPa,주요적석출강화상위S′(Al2CuMg)。제압비적제고유리우제고SiC과립화기체합금적계면결합강도。분말열제압법제비적SiCp/2024려기복합재료열처리후적단렬방식주요유3충:SiC과립단렬、SiC과립여기체합금적박리화기체합금적인성단렬,해복합재료적단렬궤제위인성단렬화취성단렬공존적혼합단렬。
SiCp/2024 aluminum matrix composites were fabricated by powder hot extrusion. Microstructures and mechanical properties of the composites after hot extrusion and heat treatment were studied. The fracture morphology and mechanism were also analyzed. The results show that SiC particles and the precipitated fine second phase particles disperse in the matrix uniformly and there are only a part of SiC particles clustering in local areas. The grains are elongated significantly along the extrusion direction and the long axis of the rigid SiC particles is paralleled to the extrusion direction as well, which shows a fibrous tissue during hot working. After the T6 heat treatment (490 ℃, 75 min+170℃, 8 h), the grains of the matrix are fine and the tensile strength can reach 470 MPa. The major precipitation strengthening phases is S′(Al2CuMg). The strength of the interface between SiC particles and 2024 matrix increases with increasing hot extrusion ratio. There are three types of fracture of the composite after heat treatment:the crack of SiC particles, the interface stripping between SiC and matrix, and the ductile fracture of the matrix. According to the microstructures, the fracture mechanism of the composite is the coexistence of ductile fracture and brittle fracture, which is a mixed fracture.