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1)  fillet weld
角焊缝
1.
Researches on the coming into being mechanism for fillet weld's angular distortion;
角焊缝角变形产生机制的研究
2.
Nondestructive test for fillet welds in nozzle stubs of HP utility boilers;
电站高压锅炉管座角焊缝的无损检测
3.
Inspection of fillet weld shape dimension based on laser vision sensing;
基于激光视觉传感的角焊缝外形尺寸检测
2)  fillet [英]['fɪlɪt]  [美][fɪ'le]
角焊缝
1.
Ultrasonic Testing for Fillet Weld of Thermocouple in Coal-Fired Power Plant
火力发电厂测温热电偶套管角焊缝的超声波检测
2.
This article discusses the method and accuracy for header differential steel nozzle fillet magnetic particle inspection, and shows the actual dissection result that the author did on products.
对集箱异种钢管接头角焊缝磁粉探伤的方法和准确性进行了探讨 ,并在产品上进行了实物解剖验证。
3.
The fillet ray insqection technique for plate and tube of active service waste boiler has been introduced in details,as well as its reliability.
对在役废热锅炉管板角焊缝的射线检验技术进行了详细介绍,并对检验可靠性进行了讨论。
3)  fillet welding
角焊缝
1.
Single Chip Microcomputer Control System for Fillet Welding Seam Tracking on Robot with Rotating Arc Welding Sensor;
机器人旋转电弧传感角焊缝跟踪单片机控制系统
2.
According to fatigue destructive characteristic of welded joints,this paper carries out researches in- to the constant amplitude fatigue behaviour of 16Mn steel fillet welding joints,and analyzes the fatigue life of fillet welding with different rates of weld legs,preparation and non—preparation.
本文根据焊接接头的疲劳破坏特性,通过研究16Mn 钢角焊缝的常幅疲劳行为,比较和分析了具有不同焊脚比,开坡口与不开坡口情况下角焊缝的疲劳寿命;同时对试验数据进行了统计处理。
4)  fillet weld
角焊[缝];贴角焊;填角焊缝
5)  fillet weld seam
角焊缝焊接
6)  leg of fillet weld
角焊缝焊脚
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