管节点焊缝,tubular joint weld,音标,读音,翻译,英文例句,英语词典

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1) tubular joint weld 点击朗读

管节点焊缝

Ultrasonic phased array inspection technology of offshore platform structure tubular joint welds;

海洋平台结构管节点焊缝超声相控阵检测技术

2) welded joint 点击朗读

焊接缝焊接节点

3) seamless pipe joint 点击朗读

无缝钢管节点

4) non-load-bearing fillet weld joint 点击朗读

不承载角焊缝节点

In order to research the damage evolution rules of three typical details of bolt and weld steel bridges(lap joints,non-load-bearing fillet weld joints and high-strength bolted friction-type joints),the relations between damage degree and cycle ratio of the three details were investigated by MTS(mechanical testing and simulation)fatigue testing machines with sinusoidal loadings.

为了研究搭接节点、不承载角焊缝节点、摩擦型高强螺栓连接节点这3种典型栓焊钢桥细节的疲劳损伤演化规律,采用MTS疲劳试验机和正弦波加载的方法研究了这3种细节的损伤程度与循环比之间的关系,共进行了4个单面盖板搭接节点、2个不承载角焊缝节点和2个摩擦型高强螺栓连接节点的疲劳试验,建立了这3种典型细节基于Chaboche疲劳损伤模型的损伤演化方程:单面盖板搭接节点细节:D=1-[1-(n/Nf)0。

5) resistance spot and seam welding 点击朗读

点、缝焊

Nondestructive inspection methods applied in resistance spot and seam welding; 点击朗读

点、缝焊质量的无损检测技术现状

6) spot weld 点击朗读

点焊缝

例句>>

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

焊缝管焊缝接管对缝焊管

紧缝焊点焊接缝[点] 直缝焊管管座焊缝管板焊缝管道焊缝

说明：双击或选中下面任意单词，将显示该词的音标、读音、翻译等；选中中文或多个词，将显示翻译。
	您的位置：首页 -> 词典 -> 管节点焊缝 1) tubular joint weld 管节点焊缝 1. Ultrasonic phased array inspection technology of offshore platform structure tubular joint welds; 海洋平台结构管节点焊缝超声相控阵检测技术 2) welded joint 焊接缝焊接节点 3) seamless pipe joint 无缝钢管节点 4) non-load-bearing fillet weld joint 不承载角焊缝节点 1. In order to research the damage evolution rules of three typical details of bolt and weld steel bridges(lap joints,non-load-bearing fillet weld joints and high-strength bolted friction-type joints),the relations between damage degree and cycle ratio of the three details were investigated by MTS(mechanical testing and simulation)fatigue testing machines with sinusoidal loadings. 为了研究搭接节点、不承载角焊缝节点、摩擦型高强螺栓连接节点这3种典型栓焊钢桥细节的疲劳损伤演化规律,采用MTS疲劳试验机和正弦波加载的方法研究了这3种细节的损伤程度与循环比之间的关系,共进行了4个单面盖板搭接节点、2个不承载角焊缝节点和2个摩擦型高强螺栓连接节点的疲劳试验,建立了这3种典型细节基于Chaboche疲劳损伤模型的损伤演化方程:单面盖板搭接节点细节:D=1-[1-(n/Nf)0。 5) resistance spot and seam welding 点、缝焊 1. Nondestructive inspection methods applied in resistance spot and seam welding; 点、缝焊质量的无损检测技术现状 6) spot weld 点焊缝例句>> 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)=-20fyEleCenter(I,3,1)2+0.3fy endif IF,EleCenter(I,2,1),LT,0.0,THEN !下翼缘初始应力 EleIS(I,1,1)=-20fyEleCenter(I,3,1)*2+0.3fy 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)=4.076fy(EleCenter(I,2,1)-0.5)2 EleIS(I,1,1)=EleIS(I,1,1)-0.719fy IF,EleIS(I,1,1),LT,-0.3fy,THEN ELeIS(I,1,1)=-0.3fy 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。参考词条焊缝管焊缝接管对缝焊管

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