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Journal of Chinese Society for Corrosion and protection  2014, Vol. 34 Issue (5): 419-425    DOI: 10.11902/1005.4537.2014.017
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Correlation Between Intergranular Corrosion Behavior and Aging Treatment of 2099 Al-Li Alloy
XU Long1, YAO Xi1, LI Jingfeng1(), CAI Chao2
1. School of Materials Science and Engineering, Central South University, Changsha 410083, China
2. School of Chemistry and Chemical Engineering, Ningxia University, Yinchuan 750001, China
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Abstract  

The correlation between the intergranular corrosion (IGC) behavior and the aging temper (including T6 aging at 150 and 175 ℃, T8 aging at 150 ℃) of 2099 Al-Li alloy was investigated. Then a diagram was established to describe the relation of IGC with the aging procedure. According to the aging resulted corrosion morphology of the alloy, the aging process might be divided into four stages: i.e. stage I is the initial aging stage, stage II the under-aging stage, stage III the near-optimal aging stage and stage IV the over-aging stage. The aged alloy showed different modes corrosion after aged by different stages: i.e. pitting corrosion or local intergranular corrosion (LIGC) for stage I; general intergranular corrosion (GIGC) for stage II; LIGC for stage III; and pitting corrosion without IGC for stage IV. In the under-aged alloy, a great number of very fine precipitates preferentially deposited along grain boundaries, which seem like a continuous chain, hence resulting in the highest susceptibility to IGC for the alloy. In the over-aged alloy, the precipitates were coarsened and the inter-precipitate spacing became larger, so that the susceptibility to IGC may be suppressed. In general, with the rising of aging temperature, the grain boundary precipitates grew coarse and the spacing between the precipitates became larger, while a proper pre-deformation of the alloy might facilitate the uniform nucleation of precipitates and suppress the formation of precipitate-free zone (PFZ) along grain boundary. These two factors shortened or even eliminated the Stage II and Stage III, therewith increasing the resistance to IGC of the alloy.

Key words:  2099 Al-Li alloy      intergranular corrosion      corrosion-aging diagram     
ZTFLH:  TG166  
  TG178  

Cite this article: 

XU Long, YAO Xi, LI Jingfeng, CAI Chao. Correlation Between Intergranular Corrosion Behavior and Aging Treatment of 2099 Al-Li Alloy. Journal of Chinese Society for Corrosion and protection, 2014, 34(5): 419-425.

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https://www.jcscp.org/EN/10.11902/1005.4537.2014.017     OR     https://www.jcscp.org/EN/Y2014/V34/I5/419

Aging temper Temperature / ℃ Time / h
T6 150 0.5, 3, 6, 18, 42, 66, 120, 150, 195
T6 175 0.5, 3, 6, 18, 48, 72, 96
T8 150 0.5, 3, 6, 18, 48, 72, 96
Table 1  Aging temperature and aging time of three tempers
Fig.1  Representative sectional corrosion morphologies of 2099 Al-Li alloy with T6 aging at 150 ℃ for 0.5 h (a), 3 h (b), 18 h (c), 120 h (d) and 150 h (e)
Fig.2  Representative sectional corrosion morphologies of 2099 Al-Li alloy with T6 aging at 175 ℃ for 0.5 h (a), 3 h (b), 18 h (c) and 48 h (d)
Fig.3  Representative sectional corrosion morphologies of the 2099 Al-Li alloy with T8 treatment at 150 ℃ for 0.5 h (a), 3 h (b) and 6 h (c)
Fig.4  Micro-hardness curves of 2099 Al-Li alloys as a function of aging time
Temper Aging time / h Dominating corrosion mode Maximum IGC depth / μm
T6 at 150 ℃ 0.5 Pitting None
3 LIGC+ 51.54
6 LIGC++ 242.87
18 GIGC 191.02
42 GIGC 196.58
66 GIGC 191.14
120 LIGC++ 198.63
150 Pitting None
195 Pitting None
0.5 LIGC 108.04
T6 at 175 ℃ 3 GIGC 209.96
6 GIGC 170.64
18 LIGC+ 140.63
48 Pitting None
72 Pitting None
96 Pitting None
0.5 Pitting None
T8 at 150 ℃ 3 LIGC+ 92.31
6 Pitting None
18 Pitting None
48 Pitting None
72 Pitting None
96 Pitting None
Table 2  Corrosion modes of 2099 Al-Li alloy with various aging-treatments and corresponding measured maximum IGC depth
Fig.5  Corrosion diagram of the studied Al-Li alloy treated in different aging conditions
Fig.6  TEM images of the local region adjacent to the grain boundary for 2099 Al-Li alloy with T6 aging at 150 ℃ for 48 h (a) and 195 h (b)
Fig.7  TEM images of the local region around grain boundary for 2099 Al-Li alloy after T6 aging at 175 ℃ (a) and T8 aging at 150 ℃ (b) for 48 h
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