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1)  main welding seam
主焊缝
1.
This paper made a stress state analysis of main welding seam of fin stabilizer controlled by force, and presented some noticeable problemes about design of fin stabilizer and technological methods for ensuring welding tension of it.
对力控式减摇鳍箱体主焊缝的应力状态进行了分析 ,提出了箱体设计中应注意的问题。
2)  backing run (before making main weld); backing weld
底层焊接(焊主焊缝前)
3)  welding seam
焊缝
1.
Study of nondestructive magnetic inspection of pressure vessel welding seam on neural network;
基于神经网络的压力容器焊缝磁性无损检测的研究
2.
The expert system of X-ray welding seam defects digtinguishing;
射线焊缝缺陷识别的专家系统
4)  seam welding
缝焊
1.
Research on seam welding principle and technology for minitype thin shell cylinder welding assemblies;
小型薄壁缸筒焊接组合的缝焊原理和工艺分析
2.
Electric Capacity Percussion Seam Welding for Thin Filter Basket of Stainless Steel;
不锈钢薄滤网的电容储能缝焊
3.
The Application of AC Servo Control System in Seam Welding Equipment
交流伺服系统在平行缝焊机中的应用
5)  weld seam
焊缝
1.
Real time detecting technology for weld seam position based on DSP;
基于DSP的焊缝位置实时检测技术
2.
Initial study on ballistic performance and stress corrosion resistance property of weld seam of 2519-T87 armor plate;
2519-T87装甲板焊缝抗弹规律及抗应力腐蚀性能初探
3.
Control of the Weld Seam Sizes of a 400m~3 Spherical Tank;
400m~3球罐焊缝组对几何尺寸控制
6)  weld [英][weld]  [美][wɛld]
焊缝
1.
Analysis for toughness of 2205 duplex stainless steel pipe welds;
2205双相不锈钢管焊缝韧度分析
2.
Research on metal magnetic memory testing in weld inspection;
磁记忆检测在焊缝检验中的应用研究
3.
Second Phase Particles in CGHAZ and Weld of Ti-V-Nb Microalloyed Pipeline Steel;
Ti-V-Nb微合金管线钢焊缝及热影响区中第二相粒子
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