journal article·2016-12-28

Effect of pre-corrosion and corrosion/fatigue alternation frequency on the fatigue life of 7B04-T6 aluminum alloy

Tengfei Cui, Daoxin Liu, Jian Cai, Xiaohua Zhang

Journal of Materials Research· Volume 31· Issue 24
Publisher page

Abstract

Influence of corrosion/fatigue factors on the fatigue life of 7B04-T6 aluminum alloys were studied in this paper. Different kinds of alternating corrosion-fatigue tests were carried out. Three factors influencing fatigue life were investigated: pre-corrosion time, corrosion/fatigue alternation frequency, and specimen’s size. The results show that: with the extension of pre-corrosion time, fatigue lives decreased; although the total corrosion time was the same (192 h), as the corrosion/fatigue alternation frequency increased, the total fatigue lives increased. The total fatigue lives of specimens subjected to two, four, and six corrosion/fatigue cycles (n= 2, 4, 6), in which specimens underwent pre-corrosion for 96 h per cycle (n= 2), 48 h per cycle (n= 4), and 32 h per cycle (n= 6), respectively, was measured. It was found that the fatigue lives increased by 56.4, 84.4, 136%, as the number of cycles increased, compared to tests in which no alternation took place (192 h of continuous corrosion). When exposed to the same corrosion times, different sized specimens demonstrated different fatigue lives. The fatigue lives of small specimens were shorter than the larger specimens. These results are all due to the specific properties of corrosion/fatigue factors.
Source: expertdata · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Fatigue and fracture mechanics · Material Properties and Failure Mechanisms · Aluminum Alloy Microstructure Properties

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (19)

Show source-provided references
1. On fatigue crack initiation from corrosion pits in 7075-T7351 aluminum alloy
2. 10.1016/j.ijfatigue.2004.04.00410.1016/j.ijfatigue.2004.04.004 ↗
3. 10.1016/j.ijfatigue.2013.10.01710.1016/j.ijfatigue.2013.10.017 ↗
4. 10.1016/j.corsci.2011.10.03210.1016/j.corsci.2011.10.032 ↗
5. 10.1016/j.engfracmech.2013.10.01210.1016/j.engfracmech.2013.10.012 ↗
6. Influence of cyclic action of corrosion and alternate load on fatigue life of 2A12-T4 aluminum alloy
7. Liu · 2004 · 187
8. 10.1016/j.ijfatigue.2015.10.02310.1016/j.ijfatigue.2015.10.023 ↗
9. 10.1016/j.jmatprotec.2010.03.00410.1016/j.jmatprotec.2010.03.004 ↗
10. Effect of pre corrosion on the fatigue behavior of AA7B04 and life forecast
11. Li · 2005 · 274
12. 10.1016/j.engfailanal.2014.01.02010.1016/j.engfailanal.2014.01.020 ↗
13. Effect of prior corrosion state on the fatigue small cracking behavior of 6151-T6 aluminum alloy10.1016/j.corsci.2011.09.025 ↗
14. Jiang · 2012 · 413
15. 10.1016/j.corsci.2009.10.00610.1016/j.corsci.2009.10.006 ↗
16. 10.1016/S0010-938X(03)00050-710.1016/S0010-938X(03)00050-7 ↗
17. 10.1016/j.corsci.2011.12.03810.1016/j.corsci.2011.12.038 ↗
18. Predicting service life of aircraft coating in various environments
19. 10.1016/j.corsci.2008.06.03910.1016/j.corsci.2008.06.039 ↗