Effect of Rolling Process on Fatigue Property of 2A66 Aluminum-Lithium Alloy Sheet

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Abstract:

The effect of rolling process on the mechanical property and microstructure of 2A66 Al-Li alloy sheet was investigated. Three different rolling processes for 2A66 AL-Li Alloy Sheet were picked for fatigue crack growth test in T3. The results showed that enhancing the amount of deformation in the range of moderate or reducing the rolling step of rolling process will increase the fatigue crack growth rate.

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706-709

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March 2016

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© 2016 Trans Tech Publications Ltd. All Rights Reserved

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[1] YIN D F,ZHENG Z Q.History and current status of aluminum—lithium alloys research and development[J].Materials Review. 2003; 17(2): 18.

Google Scholar

[2] Yang S J, Lu Z, Su B, Dai S L, Liu B C, Yan M G. Development of Aluminum-Lithium Alloys. Journal of Materials Engineering. 2001; 5: 44.

Google Scholar

[3] Zhang R X, Zeng Y S. Development, Technical Properties and Applications Abroad of Al-Li Alloy. Aeronautical Manufacturing technology. 2007(Z1): 438.

Google Scholar

[4] Zheng Z Q, Li J F, Chen G Z, Li H Y, Li S C, T C Y. Alloying and microstructure evolution of Al-Li alloys. The Chinese Journal of Nonferrous Metals. 2011; 10(21): 2337.

Google Scholar

[5] Li J F, Zheng Z Q, Chen Y L, Zhang X H. Al-Li Alloys and Their Application in Aerospace Industry. Aerospace Materials & Technology. 2012; 1(42): 13.

Google Scholar

[6] Zhou C R, Pan L Q, Zhu Z M, He Y B, Yin Z M. Development and Study of New Types Aluminum-Lithium Alloys. Materials Review. 2004; 5(18): 30.

Google Scholar

[7] Xue Z, Ma Y P, Li X L, Li S, Yu Y. Effect of heat treatment on microstructure and mechanical properties of Al-Li-Cu Alloy. Heat Treatment of Metals. 2013; 5(38).

Google Scholar

[8] Xiang S G, Jiang N, Wang B. Study on Rolling Process of 2195 Al-Li Alloy. Aluminum Fabrication. 2003; 3: 34.

Google Scholar

[9] Wu X L, Yuan Z S, Xie Y H,Dai S L. Effects of Solution Treatment on Microstructures and Properties of AL-Cu-Li-X Alloy. Aeronautical Manufacturing technology. 2009; 3(29): 1.

Google Scholar

[10] Yuan Z S,WU X L,LU Z. et a1.The aging behavior of aluminum—lithium alloy 2A97[J].Rare Metal Materials and Engineering,2008; 37(1I):1898.

Google Scholar

[11] Li H Y, Wang X F, Zhao Y K, Zeng C T, Zhang J F. Transactions of Materials And Heat Treatment. 2010; 31(4): 114.

Google Scholar

[12] Li H Y,Ou L,Zheng Z Q. Study on the Anisotropy of 2195 AL-Li Alloy. Journal of Materials Engineering. 2005; 10: 31.

Google Scholar

[13] Yuan Z S, Lu Z, Xie Y H, Dai S L, Liu C S. Study On Microstructure and Properties of a novel high strength aluminum Lithium alloy 2A97. Transactions of Materials and Heat Treatment. 2008; 5(29): 44.

Google Scholar

[14] Wang Y W. Study on Microstructure and Properties of Al-Cu-Li-X Alloy During Early Aging Process. Hot Working Technology. 2013; 10(43).

Google Scholar

[15] Wang Y X, Chen Z, Xu L, Liu B. The Study of the Tensile Fracture Process of Al-Li Alloys. Rare Metal Materials and Engineering. 2005; 7(34): 1025.

Google Scholar