Transactions of Nonferrous Metals Society of China The Chinese Journal of Nonferrous Metals

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中国有色金属学报

ZHONGGUO YOUSEJINSHU XUEBAO

第18卷    第10期    总第115期    2008年10月

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文章编号:1004-0609(2008)10-1781-07
热暴露对7475-T7351铝合金组织与性能的影响
彭小芒1,尹志民1,陈 军1,沈 凯2,郭加林1,王 华1

(1. 中南大学 材料科学与工程学院,长沙 410083;
2. 南京航空航天大学 材料科学与工程学院,南京 210016
)

摘 要:

通过对不同热暴露制度下合金的常温拉伸力学性能测试和微观组织演变的观察,分析热暴露制度对7475-T7351铝合金微观组织和性能的影响。结果表明, 热暴露温度和时间不同,对合金力学性能的影响也不同。当热暴露温度超过7475-T7351合金末级时效温度163 ℃时, 合金强度明显下降而塑性明显提高, 175 ℃热暴露100和500 h后, 合金强度分别下降29.7%和40.4%;当热暴露温度低于末级时效温度时,如果热暴露时间比较短,合金力学性能变化不大,但是如果热暴露时间很长,合金强度也下降而塑性也有所上升。125 ℃热暴露100和500 h后合金强度分别下降0.9%和3.2%,150 ℃热暴露100和500 h后合金强度分别下降11.4%和19.0%。热暴露条件下7475-T7351合金力学性能衰退的主要原因是晶内主要强化相η′ (MgZn2)粗化以及晶界附近的无沉淀析出带(PFZ)的宽化。

 

关键字: 7475铝合金;热暴露;力学性能;显微组织

Influences of thermal exposure on properties and microstructures of 7475-T7351 aluminum alloy
PENG Xiao-mang1, YIN Zhi-min1, CHEN Jun1, SHEN Kai2, GUO Jia-lin1, WANG Hua1

1. School of Materials Science and Engineering, Central South University, Changsha 410083, China;
2. College of Materials Science and Technology, Nanjing University of Aeronautics and Astronautics,Nanjing 210016, China

Abstract:The microstructures and tensile properties at different thermal exposure condition of 7475-T7351 alloy were studied by means of tensile test, OM and TEM analysis. The results show that when the thermal exposure temperature is higher than the second aging temperature of 7475-T7351 alloy, the strength drops dramatically and the elongation increases. When the alloy is thermal-exposed at 175 ℃ for 100 and 500 h, the strength decreases 29.7% and 40.4%, respectively. When the thermal exposure temperature is lower than the second aging temperature of the alloy and thermal exposure time is not so long, the tensile properties of the alloy have no change, but if the thermal exposure time is long, the tensile properties of the alloy will also decrease and the ductility also increase. For example, when 7475-T7351 alloy is thermal-exposed at 125 ℃ for 100 and 500 h, the strength decreases 0.9% and 3.2%, respectively, but when it is exposed at 150 ℃ for 100 and 500 h, the strength drops 11.4% and 19.0%, respectively. Coarsening of η′ (MgZn2) precipitates and widening of precipitate-free-zones (PFZ) should be responsible for the decay of 7475-T7351 alloy during thermal exposure condition.

 

Key words: 7475 aluminium alloy; thermal exposure; mechanical property; microstructure

ISSN 1004-0609
CN 43-1238/TG
CODEN: ZYJXFK

ISSN 1003-6326
CN 43-1239/TG
CODEN: TNMCEW

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