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1)  microweld ['maikrəuweld]
微型焊缝
2)  Micro weld
微焊缝
3)  weld formation
焊缝成型
1.
Study on the effect of the ZA alloy TIG flux on the weld formation and welding arc;
ChinZA合金TIG焊剂对焊接电弧及焊缝成型的影响
4)  weld shaping
焊缝成型
1.
The influence of welding parameters on the weld shaping was studied,the microstructures of joint without flaws was observed by useing OM and field emission scanning electron microscope.
利用MEF3光学显微镜和JSM-6700F场发射扫描电镜分析不同焊接参数下焊缝成型特点及无缺陷致密焊接接头的微观组织变化。
5)  T-type welding seam
T型焊缝
1.
Supersonic fault localization of T-type welding seam of crane girder;
吊车梁T型焊缝的超声波探伤
2.
Briefly introduced the pretreatment prior to supersonic detection of the T-type welding seam between crane beam side plate and bottom plate,the selection of supersonic detection method,the operation key points,evaluation as well as recording.
简要介绍了吊车梁翼板与腹板焊接T型焊缝超声波探伤前的预处理,超声波探伤方法的选择及操作要点,评定与记录。
6)  X type welded joint
X型焊缝
1.
Stress concentration due to a possible tree dimensional weld defect of a X type welded joint is computed via FEM.
用有限元法计算了X型焊缝接头处一种可能的三维焊接缺陷所导致的应力集中 ,定量分析了缺陷尺寸的变化对应力集中系数的影响 ,结果表明缺陷高度和宽度的增加将导致应力集中系数的增大 ,但其增大趋势逐渐变缓 ;而缺陷厚度的增加则使应力集中系数减小。
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