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1) standard weld
标准焊缝
2) criteria of ultrasonic examination of welded seam
焊缝超声波探伤标准
3) marking the welding line
焊缝标注
1.
In this paper, the author introduces the method of developing AutoCAD with the ActiveX automation,and creates the new function of marking the welding line.
采用ActiveX自动化技术对AutoCAD进行二次开发的模式,利用AutoCAD提供的Application对象,以客户机/服务器的工作方式从内部控制AutoCAD,从而为AutoCAD添加了焊缝标注的新功能。
4) welding standard
焊接标准
1.
This paper introduces the difference between the welding part of ASME code, an extensively used standard for imported boilers and pressure vessels, and welding standard of China power industry.
文章介绍了进口锅炉压力容器广泛采用的ASME规范中焊接部分和我国电力行业焊接标准在体系和内容等方面的差别 ,为理解规范、标准有很大帮
5) standard side seam line
标准侧缝线
1.
On the basis of dress aesthetics and the principle of garments construction, the paper presents the concept of side seam line of woman's clothes, it can obtain the design by correcting standard side seam line.
论文在服饰美学、服装结构基本原理的基础上,提出了女装标准侧缝线的概念,通过对标准侧缝线的修正,得到设计需要的实际侧缝线。
6) weld coordinate
焊缝特征坐标系
1.
The conception of weld coordinate is presented in the paper,which is adopted to describe various weld positions of complicated weld joint and space weld.
提出了焊缝特征坐标系的概念 ,采用焊缝特征坐标系来描述各种焊接接头复杂空间焊缝的焊接位置 ,并将复杂空间焊缝分解为“立坡焊”和“横坡焊”两种简单焊接位置的组合。
2.
The conception of weld coordinate is put forward in this paper,which is adopted to describe various weld position of complicated weld joint and space weld.
提出了焊缝特征坐标系的概念 ,采用焊缝特征坐标系来描述各种焊接接头复杂空间焊缝的焊接位置 ,并将复杂空间焊缝分解为“立坡焊”和“横坡焊”二种简单焊接位置的组合。
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
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