镇江高专学报
鎮江高專學報
진강고전학보
JOURNAL OF ZHENJIANG COLLEGE
2014年
4期
61-63
,共3页
钱绍祥%殷晓中%王琦%刘波%冷承业
錢紹祥%慇曉中%王琦%劉波%冷承業
전소상%은효중%왕기%류파%랭승업
激光冲击处理%小孔构件%LY12CZ 铝合金%残余应力
激光遲擊處理%小孔構件%LY12CZ 鋁閤金%殘餘應力
격광충격처리%소공구건%LY12CZ 려합금%잔여응력
laser shock processing(LSP)%hole components%LY12CZ aluminum alloy%residual stress
采用高功率 Nd:glass 激光器对 LY12CZ 铝合金小孔构件表面进行激光冲击强化处理,并对冲击区域进行残余应力场的测试与分析。结果显示,在激光功率密度为1.75 GW/cm2和光斑直径为6 mm 的强激光冲击作用下,冲击区域产生了残余压应力场,层深约1.2 mm,表面最大残余应力为-57 MPa,厚度方向上最大残余应力为-36 MPa。优化后的激光冲击处理工艺参数能够获得较好的残余应力场。
採用高功率 Nd:glass 激光器對 LY12CZ 鋁閤金小孔構件錶麵進行激光遲擊彊化處理,併對遲擊區域進行殘餘應力場的測試與分析。結果顯示,在激光功率密度為1.75 GW/cm2和光斑直徑為6 mm 的彊激光遲擊作用下,遲擊區域產生瞭殘餘壓應力場,層深約1.2 mm,錶麵最大殘餘應力為-57 MPa,厚度方嚮上最大殘餘應力為-36 MPa。優化後的激光遲擊處理工藝參數能夠穫得較好的殘餘應力場。
채용고공솔 Nd:glass 격광기대 LY12CZ 려합금소공구건표면진행격광충격강화처리,병대충격구역진행잔여응력장적측시여분석。결과현시,재격광공솔밀도위1.75 GW/cm2화광반직경위6 mm 적강격광충격작용하,충격구역산생료잔여압응력장,층심약1.2 mm,표면최대잔여응력위-57 MPa,후도방향상최대잔여응력위-36 MPa。우화후적격광충격처리공예삼수능구획득교호적잔여응력장。
The surface of LY12CZ aluminum alloy hole component was treated with Nd:glasss laser,and its residu-al stress was tested and analyzed.In the impact of laser shock processing using the laser power density of 1.75 GW/cm2 and spot diameter of 6mm,the shocked area produced compressive residual stress with its deepness about 1.2mm.The maximum surface residual stress is -57MPa and the maximum residual stress in the thickness direc-tion is -36MPa.The optimization of LSP technological parameters can obtain good residual stress field.