[1] 张荣霞,曾元松.铝锂合金的发展、工艺特性及国外应用现状.航空制造技术,2007(增刊): 438-441.
[2] 尹登峰,郑子樵.铝锂合金的研究开发的历史现状．材料导报，2003(2)：19-23.
[3] 邱惠中.铝锂合金的发展概况及其应用．宇航材料工艺，1993(4)：38-45.
[4] 刘斌，陈铮铮．铝锂合金的发展与应用．现代机械,2001(4)：7l-75.
[5] 潘肃．铝锂合金的发展及其工艺特性．航天工艺,1994(5)：40-45.
[6] 霍红庆，郝维新，耿桂宏,等．航天轻型结构材料-铝锂合金的发展. 真空与低温,2005(6):63-69.
[7] Lyttle M T, Weft J A. The plastic anlsotropy of an Al-Li-Cu-Zr alloy extrusion in unidirectionai deformation . Metall Mater Trans A, 1996, 27 (11): 3503-3511．
[8] Li Hongying, Yi Tanga, Zeng Zaide, et al. Effect of aging time on strength and microstructures of an Al-Cu-Li-Zn-Mg-Mn-Zr alloy. Materials Science and Engineering A, 2008 (498): 314-320.
[9] Huang J C, Ardell A J, Addition rules and the contributlon of δ′ precipitates to strengthening of aged Al-Li-Cu alloys . Acta Metall，1988, 36(11): 2995-3006．
[10] Huang J C, Ardell A J. Precipitation strengthening of binary Al-Li alloys by δ′ prec ipitates．Mater Sci Eng A,1988, 104: 149-156.
[11] 马高山. 复杂铝锂合金零件热成形技术. 北京:化学工业出版社，2011.
[12] Gupta R K, Nayan N, Sharma S C. Development and characterization of Al-Li alloys.Materials Science and Engineering A, 2006, 420:228-234.
[13] 钟利萍. 1420 Al-Li合金热处理工艺及组织性能的研究[D]. 长沙: 中南林学院, 2003.
[14] John W, Marcia D, Eric H. Recent advances in near-net-shape fabrication of Al-Li alloy 2195 for launch vehicles, NASA Research Report, 2007.
[15] Rainer K, Tamara V, Thomas S. Laserstrahlschweiβen im flugzeugbau: stand und künftige anwendungen. Bremen: Laser-Anwenderforum, 2006:13-14.
[16] Chen P S, Bhat B N. Time-temperature-precipitation behavior in Al-Li Alloy 2195, NASA Research Report,2002.
2012, 
