Characterization of TC17 Titanium Alloy Treated by Square-Spot Laser Shock Peening

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Abstract:

Laser shock peening (LSP) is widely known as a cold-worked surface treatment, and this technology has been to greatly improve the fatigue life of many metallic components. Our works focused on laser shock peening with Nd: glass laser system (pulse duration 30ns) and square laser spot size of 4mm×4mm for TC17 titanium alloy. Surface morphology, residual stresses and fatigue performance had been studied for TC17 alloy specimens and blades processed by LSP treatment. The results show that plastic strains in shocked dents become more homogeneous than ones produced by original circle spot with gaussian energy distribution. Surface residual stresses which measured using x-ray diffraction method showed different characteristic as varying specimen thickness, and LSP with overlapping ratio of 8% provided uniform residual stresses on peened surface. Low fluence peening which was implemented at borderline of peened surface was effective to diminish the stress gradient. Compared with mechanical shot peening, LSP attained smoother surface, lower microhardness and better fatigue performance. In a word, Square-spot LSP is an excellent way to improve fatigue life of titanium blade.

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Advanced Materials Research (Volumes 652-654)

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2378-2383

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January 2013

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© 2013 Trans Tech Publications Ltd. All Rights Reserved

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[1] B. N Mordyuk, Yu.V. Milman etc. Characterization of ultrasonically peened and laser-shock peened surface layers of AISI 321 stainless steel. Surface & Coating Technology 202 (2008) 4875-4883.

DOI: 10.1016/j.surfcoat.2008.04.080

Google Scholar

[2] R.K. Nalla, I. Altenberger etc. On the influence of mechanical surface treatments-deep rolling and laser shock peening-on the fatigue behavior of Ti-6Al-4V at ambient and elevated temperatures. Materials Science and Engineering A 335 (2003).

DOI: 10.1016/s0921-5093(03)00069-8

Google Scholar

[3] Graham Hammersley, Lloyd A. hackle, Fritz harris. Surface prestressing to improve fatigue strength of components by laser shot Peening. Optics and Lasers in Engineering 34 (2000) 327-337.

DOI: 10.1016/s0143-8166(00)00083-x

Google Scholar

[4] C. Rubio-Gonzalez, J.L. Ocana etc. Effect of laser shock processing on fatigue crack growth and fracture toughness of 6061-T6 aluminum alloy. Materials Science and Engineering A 386 (2004) 291-295.

DOI: 10.1016/s0921-5093(04)00937-2

Google Scholar

[5] Zou Shikun, Gong Shuili, Guo Enming, Li Bin. Laser Peening of Turbine Engine Integrally Blade Rotor. CHINESE JOURNAL OF LASERS. 2011 38(6):101-104.

DOI: 10.3788/cjl201138.0601009

Google Scholar

[6] CAO Zi-wen, CHE Zhi-gang, ZOU Shi-kun, FEI Qun-xing. Numerical simulation of residual stress field induced by laser shock processing with square spot. J shanghai Univ (Engl Ed), 2011, 15(6): 553-556.

DOI: 10.1007/s11741-011-0785-1

Google Scholar

[7] Cao Ziwen, Zou Shikun, Gong Shuili. The Latest Movement and Development Trend of Laser Shock Processing. Aeronautical Manufacturing Technology, 2010(5): 40-42.

Google Scholar

[8] L. Berthe, R. Fabbro, P. Peyre. Experimental study of the transmission of breakdown plasma generated during laser shock processing. The European Physical Journal Applied Physics, 1998 (3): 215-218.

DOI: 10.1051/epjap:1998222

Google Scholar

[9] A. Chahardehi, F.P. Brennan, A. Steuwer. The effect of residual stresses arising from laser shock peening on fatigue crack growth. Engineering Fracture Mechanics. 77 (2010) 2033-(2039).

DOI: 10.1016/j.engfracmech.2010.03.033

Google Scholar

[10] B J.Z. Lu, K.Y. Luo, Y.K. Zhang. Grain refinement mechanism of multiple laser shock processing impacts on ANSI 304 Stainless steel. Acta Materialia, 58 (2010) 5354-5362.

DOI: 10.1016/j.actamat.2010.06.010

Google Scholar