|
|
1) Bead Shape Dimension
焊缝参数
2) weld shape parameters
焊缝形状参数
1.
Effects of pulsing parameters on weld shape parameters during pulsed Nd-YAG laser welding of aluminum alloys;
铝合金脉冲YAG激光焊脉冲调制参数对焊缝形状参数的影响
3) bead geometry parameter
焊缝几何参数
1.
The effects of arc voltage and welding speed on bead geometry parameters were discussed,and the microstructure and mechanical properties of joint were studied.
对8mm厚2A12铝合金板进行CO2激光-MIG(metal intergas)复合焊接,讨论了焊接电压和焊接速度对焊缝几何参数的影响,并研究接头显微组织和力学性能。
4) weld geometry parameters
焊缝成形参数
1.
In order to improve the welding efficiency,tripleelectrode high-speed CO2 fillet welding process was adopted based on the twin-electrode CO2 welding,and the effect of welding conditions on weld geometry parameters was analyzed.
在传统双电极角焊焊接工艺基础上,为了进一步提高焊接效率,采用三电极高速CO2双边角焊工艺,分析不同焊接工艺参数对焊缝成形参数的影响。
5) welded joint efficiency
焊缝系数
6) fracture parameter
裂缝参数
1.
The method of confirming fracture parameter and development degree in carbonate reservoir;
碳酸盐岩储层裂缝参数和发育程度的确定方法
2.
According to the effects of volcanics fractured reservoir to the production, the tectonic stress field numerical modeling have been used to study the space distribution characteristic of the fracture parameter.
针对闵桥火山岩油藏裂缝对开发效果的影响,在对闵桥地区开展构造演化史和裂缝观察研究的同时,采用构造应力场数值模拟的方法,运用ANSYS软件进行裂缝参数预测,研究了裂缝参数在空间的分布特征。
3.
Studied are fracture identification and parameters extraction from micro resistivity images as well as seismic high resolution inversion of fracture parameters.
开展了微电阻率扫描成像的裂缝识别、参数提取以及裂缝参数的地震高分辨率反演研究。
补充资料：ANSYS工字梁焊缝初应力例子
建立好模型
…..
/SOLU
!*
ANTYPE,0
/INPUT,'input','txt',
/INPUT,'output1','txt',
!*
ISFILE,READ,1,txt, ,0
SOLVE
=====================
!定义残余应力矩阵
I=1
fy=310e6
!定义单元中心坐标数组，初应力数组
*DIM,EleCenter,ARRAY,NumNode,3,1, , ,
*DIM,EleIS,ARRAY,NumNode,1,1, , ,
*DO,I, 1, NumNode,1
!得到单元中心坐标
*GET,EleCenter(I,1,1),ELEM,I,CENT,X
*GET,EleCenter(I,2,1),ELEM,I,CENT,Y
*GET,EleCenter(I,3,1),ELEM,I,CENT,Z
!焊缝位置在X=1.0 到1.05 之间
*IF,EleCenter(I,1,1),GT,1,THEN
*IF,EleCenter(I,1,1),LT,1.05,THEN
*IF,EleCenter(I,2,1),GT,0.5,THEN
!上翼缘初始应力
EleIS(I,1,1)=-20*fy*EleCenter(I,3,1)**2+0.3*fy
*endif
*IF,EleCenter(I,2,1),LT,0.0,THEN
!下翼缘初始应力
EleIS(I,1,1)=-20*fy*EleCenter(I,3,1)**2+0.3*fy
*endif
!腹板初始应力
*if,EleCenter(I,2,1),GE,0.0,THEN
*IF,ELECENTER(I,2,1),LE,0.5,THEN
EleIS(I,1,1)=4.076*fy*(EleCenter(I,2,1)-0.5)**2
EleIS(I,1,1)=EleIS(I,1,1)-0.719*fy
*IF,EleIS(I,1,1),LT,-0.3*fy,THEN
ELeIS(I,1,1)=-0.3*fy
*ENDIF *ENDIF
*ENDIF
*ENDIF
*ENDIF
*ENDDO
===============
!输出应力数值
*CFOPEN,'1','txt',' '
*DO,I,1,3840
!*IF,EleIS(I,1,1),ne,0.,then
*VWRITE,'!'
(A)
*VWRITE,'! Stress for element',
(A,F)
*VWRITE,'!'
(A)
*VWRITE,'eis,',I
(A,F)
P=EleIS(I,1,1)
*VWRITE,P,0.,0.,0.,0.,0.
(E,E,E,E,E,E)
!*ENDIF
*ENDDO
*CFCLOS
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
|