航空材料学报
航空材料學報
항공재료학보
JOURNAL OF AERONAUTICAL MATERIALS
2010年
1期
36-40
,共5页
胡燕辉%李建国%谭敦强%曹凑先
鬍燕輝%李建國%譚敦彊%曹湊先
호연휘%리건국%담돈강%조주선
AZ31镁合金%细化%本构方程%再结晶
AZ31鎂閤金%細化%本構方程%再結晶
AZ31미합금%세화%본구방정%재결정
AZ31 magnesium alloy%refine%constitutive equation%recrystallization
通过Gleeble-1500试验机对坯料预先经过晶粒细化处理的AZ31镁合金圆柱体试样进行单向热压缩试验,压缩温度为300~450℃,应变速率ε·为0.01s~(-1),0.1s~(-1),1.0s~(-1),根据试样结果分析计算了本构方程中的各参数,获得了完整的镁合金高温本构方程,进一步分析了压缩试样的显微组织.结果表明:在本试验条件下,AZ31镁合金的热变形应力指数n为6.24,热变形激活能为177.2kJ/mol.压缩试样心部组织变形程度明显高于边缘;随着温度的升高,心部压缩组织发生明显的再结晶,新晶粒在晶界处形核并长大.
通過Gleeble-1500試驗機對坯料預先經過晶粒細化處理的AZ31鎂閤金圓柱體試樣進行單嚮熱壓縮試驗,壓縮溫度為300~450℃,應變速率ε·為0.01s~(-1),0.1s~(-1),1.0s~(-1),根據試樣結果分析計算瞭本構方程中的各參數,穫得瞭完整的鎂閤金高溫本構方程,進一步分析瞭壓縮試樣的顯微組織.結果錶明:在本試驗條件下,AZ31鎂閤金的熱變形應力指數n為6.24,熱變形激活能為177.2kJ/mol.壓縮試樣心部組織變形程度明顯高于邊緣;隨著溫度的升高,心部壓縮組織髮生明顯的再結晶,新晶粒在晶界處形覈併長大.
통과Gleeble-1500시험궤대배료예선경과정립세화처리적AZ31미합금원주체시양진행단향열압축시험,압축온도위300~450℃,응변속솔ε·위0.01s~(-1),0.1s~(-1),1.0s~(-1),근거시양결과분석계산료본구방정중적각삼수,획득료완정적미합금고온본구방정,진일보분석료압축시양적현미조직.결과표명:재본시험조건하,AZ31미합금적열변형응력지수n위6.24,열변형격활능위177.2kJ/mol.압축시양심부조직변형정도명현고우변연;수착온도적승고,심부압축조직발생명현적재결정,신정립재정계처형핵병장대.
Unidirectional hot compressive tests of AZ31 magnesium alloy after grain refinement were performed by Gleeble-1500 machine at strain rates changed among 0.01~1s~(-1) and deformation temperature varied among 300~450℃. Each parameter of the constitutive equation was gained by analyzing and calculating the results of samples, and a complete constitutive equation of AZ31 magnesium alloy for high temperature was fabricated, furthermore, the microstructures of compressive samples were studied. The results show that the hot deformation activation energy Q is 177.181 kJ/mol and the stress exponent n is 6.24. Compared with the edge of the compressive samples, the center has more intense degeneration. With the temperature increasing, obvious recrystallization is observed in the compressive organization. The new grain forms toward the crystal boundary and then grows up.