稀有金属
稀有金屬
희유금속
CHINESE JOURNAL OF RARE METALS
2009年
6期
850-854
,共5页
彭可武%马贺利%陈韧%吴文远%涂赣峰
彭可武%馬賀利%陳韌%吳文遠%塗贛峰
팽가무%마하리%진인%오문원%도공봉
B_4C-CeB_6/Al复合材料%无压浸渗法%原位合成%增韧
B_4C-CeB_6/Al複閤材料%無壓浸滲法%原位閤成%增韌
B_4C-CeB_6/Al복합재료%무압침삼법%원위합성%증인
B_4C-CeB_6/Al composites%pressureless infiltration technique%in-situ reaction%toughening
采用无压浸渗法制备了B_4C-CeB_6/Al复合材料, 并对其进行了力学性能测试. B_4C-CeB_6/Al复合材料的密度、抗弯强度、断裂韧性相比单一B4C材料都有很大的提高, 而硬度有所降低. 其抗弯强度值为409.47 Mpa, 比单一碳化硼提高了39.32%; 断裂韧性值6.58 Mpa·m~(1/2), 比单一碳化硼提高了78.80%. B_4C-CeB_6/Al复合材料的抗弯强度和断裂韧性的提高主要有两方面的作用: 一是由于原位生成的CeB_6和B_4C颗粒之间热膨胀系数的不匹配产生残余应力, 从而引起裂纹偏转起到增韧的效果; 二是渗入金属铝的延展性在复合材料中得以体现, 使复合材料韧性增加.
採用無壓浸滲法製備瞭B_4C-CeB_6/Al複閤材料, 併對其進行瞭力學性能測試. B_4C-CeB_6/Al複閤材料的密度、抗彎彊度、斷裂韌性相比單一B4C材料都有很大的提高, 而硬度有所降低. 其抗彎彊度值為409.47 Mpa, 比單一碳化硼提高瞭39.32%; 斷裂韌性值6.58 Mpa·m~(1/2), 比單一碳化硼提高瞭78.80%. B_4C-CeB_6/Al複閤材料的抗彎彊度和斷裂韌性的提高主要有兩方麵的作用: 一是由于原位生成的CeB_6和B_4C顆粒之間熱膨脹繫數的不匹配產生殘餘應力, 從而引起裂紋偏轉起到增韌的效果; 二是滲入金屬鋁的延展性在複閤材料中得以體現, 使複閤材料韌性增加.
채용무압침삼법제비료B_4C-CeB_6/Al복합재료, 병대기진행료역학성능측시. B_4C-CeB_6/Al복합재료적밀도、항만강도、단렬인성상비단일B4C재료도유흔대적제고, 이경도유소강저. 기항만강도치위409.47 Mpa, 비단일탄화붕제고료39.32%; 단렬인성치6.58 Mpa·m~(1/2), 비단일탄화붕제고료78.80%. B_4C-CeB_6/Al복합재료적항만강도화단렬인성적제고주요유량방면적작용: 일시유우원위생성적CeB_6화B_4C과립지간열팽창계수적불필배산생잔여응력, 종이인기렬문편전기도증인적효과; 이시삼입금속려적연전성재복합재료중득이체현, 사복합재료인성증가.
B_4C-CeB_6/Al composites were fabricated by pressureless infiltration technology. The mechanical properties of B_4C-CeB_6/Al composites were tested. The density, the flexibility strength and the fracture toughness of B_4C-CeB_6/Al composites were greatly improved compared with those of monolithic boron carbide, but the hardness decreased. The value of flexibility strength of B_4C-CeB_6/Al composites was 409.47 MPa, which was improved nearly 39.32% compared with that of monolithic boron carbide; the value of fracture toughness was 6.58 MPa·m~(1/2), which was improved nearly 78.80% compared with that of monolithic boron carbide. The flexibility strength and the fracture toughness of B_4C-CeB_6/Al composites were greatly improved for two major reasons. Firstly the crack deflection caused by the residual stress resulted from the difference in thermal expansion coefficient between B_4C and CeB_6 was the main toughening mechanisms. Secondly the ductility of aluminum was manifested in B_4C-CeB_6/Al composites.