航空学报 > 1986, Vol. 7 Issue (3): 319-324

形变热处理LC4铝合金强度及应力腐蚀性能的研究

洪班德1, 蒋大鸣1, 孙泰国2, 赵常英2   

  1. 1. 哈尔滨工业大学;2. 哈尔滨伟建机器厂
  • 收稿日期:1985-04-04 修回日期:1900-01-01 出版日期:1986-06-25 发布日期:1986-06-25

AN INVESTIGATION OF THE STRENGTH AND STRESS-CORROSION CRACKING PROPERTIES OF A THERMOMECHANICALLY TREATED ALUMINUM ALLOY LC4

Hong Bande1, Jiang Daming1, Sun Taiguo Zhao Changying2   

  1. 1. Harbin Institute of Technology;2. Harbin Aircraft Manufactory
  • Received:1985-04-04 Revised:1900-01-01 Online:1986-06-25 Published:1986-06-25

摘要:

一、引言 应力腐蚀开裂敏感及疲劳强度较低,是高强度铝合金应用中面临的两个主要问题。应力腐蚀造成的低应力破断,常常引起灾难性后果。虽然过时效处理可以显著改善应力腐蚀敏感性,但同时也使合金的强度比时效峰状态有所降低,因此,不能充分发挥材料的性能潜力。形变热处理可以提高高强铝合金的强度,但对该类合金应力腐蚀及疲劳强度的影响,尚缺乏深入研究。

Abstract:

The material used in this investigation was LC4 aluminum alloy (e-quivalent to 7075 in ASTM) in sheet form with thickness 2.4mm. It contains 6.03% Zn, 2.70% Mg. 1.54% Cu, 0.30%Mn, 0.48% Fe, 0.23% Si and 0.13% Cr. Specimens were solution treated for 30 min in salt bath at 470±2℃, quenched in water at room temperature, pre-aged at 100℃ for 4 h, rolled at room temperature with a reduction of 0, 5, 10 and 20%, then aged at 120, 140 or 160℃ for different times. The standard T6 and T73 tempers were also performed for comparison. The hardness, tensile strength, fatigue properties and resistance to SCC of the material were measured. The microstructures in different states were investigated with optical metallography, SEM and TEM.The results show that the tensile and yield strengths of the material are increased by TMT, and the higher the reduction, the larger the strengthening effect. After TMT with 10-20% reduction, the T. S. and Y. S. are 10% higher than that of the T6 temper. TMT gives the alloy higher resistance to SCC. For example, in the aqueous medium of 3.5% NaCl+ 0.5% H2O2, the critical fracture stress for 200 h of TMT specimens is 85% higher than that of the T6 temper and comes near to the level for the T73 temper. However, the tensile strength of TMT specimens is 20% higher than that of the T73 temper. This indicates that the advantages of T6 and T73 tempers are combined in TMT.There is no apparent difference in fatigue properties after different processes. The observation of microstructure and fracture finds that the deformation during TMT makes inclusion particles crack and the fatigue origins are often located at the cracked particles near surface or on the clad layer which is not affected by TMT. The transmission electron micrographs show that there are chain precipitates distributed along grain boundaries and a PFZ in the T6 temper, whereas there is only separated intergranular precipitates and no PFZ in the TMT specimens. Furthermore, the dislocation density in the substructure of TMT specimens is much higher than that of the T6 temper. Such beneficial changes in microstructure alter the slip characteristics, eliminate the intergranular fracture tendency and lead to the increase in tensile strength and resistance to SCC of the alloy.