功能材料
功能材料
공능재료
JOURNAL OF FUNCTIONAL MATERIALS
2014年
19期
19128-19133
,共6页
曾一达%赵玉涛%焦雷%田康乐
曾一達%趙玉濤%焦雷%田康樂
증일체%조옥도%초뢰%전강악
铝基复合材料%热挤压%热处理%正交试验
鋁基複閤材料%熱擠壓%熱處理%正交試驗
려기복합재료%열제압%열처리%정교시험
aluminum matrix composite%hot extrusion%heat treatment%orthogonal test
采用 Al-KBF4-K2 ZrF6剂体系,通过熔体反应法成功制备(Al3 Zr+ZrB2)p/6063Al 复合材料.对复合材料进行热挤压和热处理,并利用正交试验的方法综合分析挤压和热处理参数(固溶温度、时效时间、时效温度)对铝基复合材料的抗拉强度的影响,采用SEM 等分析方法于各阶段分析了复合材料的相组成,探讨了热处理对复合材料拉伸性能的影响的微观机制.结果表明,热挤压和热处理均对复合材料的微观形貌和抗拉强度有较大影响,分别提升了6%和20%.正交试验计算所得热处理参数对抗拉强度影响的大小顺序为固溶温度、时效温度、时效时间.优选出最大抗拉强度热处理工艺为固溶温度723 K,固溶时间4 h;时效温度423 K,时效时间4 h.
採用 Al-KBF4-K2 ZrF6劑體繫,通過鎔體反應法成功製備(Al3 Zr+ZrB2)p/6063Al 複閤材料.對複閤材料進行熱擠壓和熱處理,併利用正交試驗的方法綜閤分析擠壓和熱處理參數(固溶溫度、時效時間、時效溫度)對鋁基複閤材料的抗拉彊度的影響,採用SEM 等分析方法于各階段分析瞭複閤材料的相組成,探討瞭熱處理對複閤材料拉伸性能的影響的微觀機製.結果錶明,熱擠壓和熱處理均對複閤材料的微觀形貌和抗拉彊度有較大影響,分彆提升瞭6%和20%.正交試驗計算所得熱處理參數對抗拉彊度影響的大小順序為固溶溫度、時效溫度、時效時間.優選齣最大抗拉彊度熱處理工藝為固溶溫度723 K,固溶時間4 h;時效溫度423 K,時效時間4 h.
채용 Al-KBF4-K2 ZrF6제체계,통과용체반응법성공제비(Al3 Zr+ZrB2)p/6063Al 복합재료.대복합재료진행열제압화열처리,병이용정교시험적방법종합분석제압화열처리삼수(고용온도、시효시간、시효온도)대려기복합재료적항랍강도적영향,채용SEM 등분석방법우각계단분석료복합재료적상조성,탐토료열처리대복합재료랍신성능적영향적미관궤제.결과표명,열제압화열처리균대복합재료적미관형모화항랍강도유교대영향,분별제승료6%화20%.정교시험계산소득열처리삼수대항랍강도영향적대소순서위고용온도、시효온도、시효시간.우선출최대항랍강도열처리공예위고용온도723 K,고용시간4 h;시효온도423 K,시효시간4 h.
Aluminum matrix composites reinforced by in-situ Al3 Zr and ZrB2 particles were successfully fabrica-ted from Al-KBF4-K2 ZrF6 system via direct melt reaction.Extrusion processing and heat treatment were per-formed to find the effect of hot extrusion and heat treatment solution for the highestfigure of the tensile strength to the composite.The morphologies of the in-situ particles and mechanical properties of the composite were investigated by SEM,EDS,XRD,OM and tensile tests.The results show that both extrusion and heat treatment has a positive influence on the microstructure and tensile strength of the composite,which increases 6% and 20% respectively.And the influencing sequence of the heat treatment parameters on the tensile strength was:solution treatment temperature,aging temperature and aging time.The specimen with solution treatment for 4hat 723 K and aging temperature for 4 h at 423 K reaches the highest figure of tensile strength with moder-ate extensibility loss.