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STUDY ON OPTIMUM OF LASER-SHOCKING PARAMETERS FOR IMPROVING FATIGUE LIFE OF AIRCRAFT ALUMINUM ALLOY
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作者 Y.K.Zhang G.R.Hua x.h.lu 《Acta Metallurgica Sinica(English Letters)》 SCIE EI CAS CSCD 1998年第1期61-67,共7页
The aircraft aluminum 2024-T62 is shock-treated by pulsed laser with the same wavelength and different pulse durations. The laser parameters, arrangements of laser optics and strengthening effects are investigated. Th... The aircraft aluminum 2024-T62 is shock-treated by pulsed laser with the same wavelength and different pulse durations. The laser parameters, arrangements of laser optics and strengthening effects are investigated. The optimal laser-shocking parameters, i.e., a pulse durotion (FWHM) of 30ns, shot spot 7 to 10mm in diameter and pulse energy of 15-20J are obtained under the condition that the Q modulation crystal is KD*P and the laser optical system has three amplification stages. Therefore, the fatigue life of aluminum specimens is increased greatly and the maximum increasement is 23. 7 times. 展开更多
关键词 Al-Cu-Mg alloy fatigue life laser treatment
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