1) laser shock processing
激光冲击处理
1.
Application of laser shock processing on turbine engines;
激光冲击处理技术在发动机上的应用
2.
The research state of laser shock processing to improve the mechanical properties of aeronautical materials;
激光冲击处理提高航空材料机械性能的研究现状
3.
Laser Shock Processing of 40Cr Steel and Numerical Simulation of Residual Stress Field Induced by LSP;
激光冲击处理40Cr钢及其残余应力场数值模拟
2) microscale laser shock processing
微尺度激光冲击处理
1.
The development of microscale laser shock processing was presented.
展望了微尺度激光冲击处理技术的发展及应用前景。
3) laser shock
激光冲击
1.
Simulation and Analysis of laser shock forming process of sheet metal;
金属板料激光冲击成形数值模拟及工艺分析
2.
Study of the effect of laser shock processing on titanium alloy;
航空钛合金的激光冲击研究
3.
The basic principle of laser shock forming was described and the influences of some factors on the deformation results of TA2 sheet were simulated by ABAQUS.
通过数值模拟可优化激光冲击的相关参数,预测板料变形。
4) Laser shock processing
激光冲击
1.
Experiment with QT700 crankshaft by laser shock processing;
QT700球墨铸铁曲轴的激光冲击强化试验
2.
Effect of coating on titanium alloy during laser shock processing;
涂层对钛合金激光冲击效果的影响
3.
Fracture characteristic of Al_2O_3 ceramics by strong laser shock processing;
强激光冲击波作用下Al_2O_3陶瓷材料的断裂特征
5) Laser shocking
激光冲击
1.
When power density was 5 ×1012W/m2, the peak stress of the shock wave induced by laser shocking exceeded the dynamic yield strength of the aluminum alloy 2024T62,which caused high density dislocations and stable residual compressive surface stresses in the laser-shock-processed are.
采用小型、调Q、高功率密度的钕玻璃激光装置对2024T62铝合金试件进行双面激光冲击处理。
2.
This paper describes the experimental apParatus of laser shocking,the chemical compositions and mechanical properties of aviation aluminium alloys 7475T761 and 2024T62 and the shapes of laser shocked test pieces.
介绍了用于激光冲击的航空铝合金７４７５Ｔ７６１和２０２４Ｔ６２试件。
6) laser shock wave
激光冲击波
1.
Numerical simulation of 3-D nondestructive marking based on laser shock wave;
基于激光冲击波三维无损打标的数值模拟
2.
A new mode of the tip of the crack was put forth by the theory of fracture dynamics,and then the dynamic stress intensity factor of the crack under the laser shock wave was also obtained.
研究了含有裂纹的金属板料在激光冲击波载荷作用下裂纹尖端应力强度因子和裂纹扩展速度的变化,利用断裂力学理论,对激光冲击加载下裂尖参数计算模型进行优化,采用应力强度因子叠加法,将外加载荷引起的应力强度因子和激光冲击后残留的残余压应力引起的应力强度因子叠加,推导出下裂纹尖端应力场强度因子表达式,由此可精确计算出金属板料的裂纹萌生寿命和裂纹扩展速度,实验验证了航空钛合金Ti6Al4V激光冲击后残余应力对裂纹扩展速度的影响,从而建立了激光冲击作用对板料裂纹扩展的影响的理论模型。
3.
The theoretical minimum movement velocity for the sheet to be punched by laser shock waves was deduced.
为了验证激光冲击波冲孔工艺的可行性,采用Nd玻璃高功率脉冲激光器在0。
补充资料：标准操作冲击电压波形(见冲击电压发生器)
标准操作冲击电压波形(见冲击电压发生器)
standard switching impulse voltage waveform
b .oozhun CooZuo ChongJld，onyo boxlng标准操作冲击电压波形(standard switchingimpulse voltage waveform)见冲击电压发生器。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条