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7055铝合金的TTP曲线及其应用 被引量:37

TTP curve of 7055 aluminum alloy and its application
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摘要 采用分级淬火的方法测定了7055铝合金的温度-时间-性能(TTP)曲线,并结合合金实际淬火冷却曲线通过淬火因子分析方法预测了合金的硬度。结果表明,合金TTP曲线的“鼻尖”温度大约为355℃,淬火敏感温度区间为210-420℃。淬火因子分析方法预测的合金硬度值和实测值吻合较好,淬火敏感温度区间的冷却速率对合金硬度有决定性影响。根据理论计算认为,要获得最大硬度,淬火敏感温度区间的平均冷却速率需大于500℃/s。 The temperature--time--property (TTP) curve of 7055 aluminum alloy was evaluated by interrupted quenching method. The results show that the critical temperature range is 210 - 420 ℃ with the nose temperature of about 355 ℃. Combined with measured cooling curves, the TTP curve was used to predict the influence of quenching rate on the hardness of 7055 aluminum alloy by quench factor analysis method. And the predicted results agree reasonably well with the measured values. The quenching rate through the critical temperature range has great influence on the hardness of the alloy, and that must be larger than 500 ℃/s in order to attain the highest hardness.
出处 《中国有色金属学报》 EI CAS CSCD 北大核心 2006年第12期2034-2039,共6页 The Chinese Journal of Nonferrous Metals
基金 国家重点基础研究发展规划资助项目(2005CB623700) 国家教育部博士点基金资助项目(2004053304)
关键词 7055铝合金 温度-时间 性能曲线 淬火因子分析方法 淬火速率 硬度 7055 aluminum alloy temperature--time--property (TTP) curve quench factor analysis method quenching rate hardness
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  • 1Starke E A,Staley J T.Application of modern aluminum alloys to aircraft[J].Progress in Aerospace Sciences,1996,32(2/3):131-172.
  • 2李成功 巫世杰 等.先进铝合金在航空航天工业中的应用与发展[J].中国有色金属学报,2002,12(1):14-21.
  • 3张茁 陈康华 黄兰萍 等.高温预析出对7055铝合金组织和力学性能的影响.中国有色金属学报,2003,13(6):1477-1482.
  • 4Williams J C,Starke E A Jr.Progress in structural materials for aerospace systems[J].Acta Materialia,2003,51(19):5775-5799.
  • 5Fridlyander I N.Laws of variation of properties of aluminum alloys during aging[J].Metal Science and Heat Treatment,2003,45(9/10):337-340.
  • 6Iskandar M,Reyes D,Gaxiola Y,et al.On identifying the most critical step in the sequence of heat treating operations in 7249 aluminum alloy[J].Engineering Failure Analysis,2003,10:199-207.
  • 7Robinson J S,Cudd R L,Tanner D A,et al.Quench sensitivity and tensile property inhomogeneity in 7010 forgings[J].Journal of Materials Processing Technology,2001,119(1-3):261-267.
  • 8Lim S T,Yun S J,Nam S W.Improved quench sensitivity in modified aluminum alloy 7175 for thick forging applications[J].Mater Sci Eng A,2004,A371(1/2):82-90.
  • 9Bates C E,Totten G E.Procedure for quenching media selection to maximize tensile properties and minimize distortion in aluminium-alloy parts[J],Heat Treatment of Metals,1988,15(4):89-97.
  • 10MacKenzies D S.Quench Rate and Ageing Effects in Aluminum AlZnMgCu Alloys[D].Rolla:University of Missouri-Rolla,2002.

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