ansys apdl板的冲压成形仿真

2017-03-02  by:CAE仿真在线  来源:互联网

ANSYS环境下全参数化建模分析,通过调整上下模参数使成型过程中不出现空隙.分三工步:上模快速下降,板料接触下模后缓慢压延,拔模回弹.

!!!!!!!!!板的冲压仿真
FINISH
/CLEAR
*AFUN,DEG

X0=0
Y0=0
Z0=0

HBL=8
HXBL1=7.5
HXBL2=7.5
HYBL1=7.5
HYBL2=7

XBL1=25
XBL2=40
YBL1=28
YBL2=80

CE0=0.2

X1=XBL1
X101=X1+6
X201=X1+XBL2-11
X2=X1+XBL2
X4=200
X5=220

XCT1=X1+HXBL1
XCT101=XCT1+3
XCT2=X201-HXBL2+3
XCT201=XCT2+7
XCT3=XCT201+50


Y1=YBL1
Y2=Y1+10
Y3=YBL2
Y4=Y3+HBL+CE0+5
Y5=Y4+YBL1-(HBL*2-HYBL1-HYBL2)
Y6=Y4+YBL1+6
Y7=Y6+58


R01=10
R02=8
R03=10
R04=10
R05=13
SIT=50

RCT1=18
RCT2=5
RCT3=5
RCT4=20
X3=X2+(Y3-Y2)*COS(50)/SIN(50)


DY1=Y4-HBL
DY2=DY1+(HBL-HYBL2)+1
DY3=DY2-5


/PREP7
ET,1,182
KEYOPT,1,3,3

ET,2,169
ET,3,172
ET,4,169
ET,5,172
ET,6,169
ET,7,172


MP,EX,1,17000
MP,PRXY,1,0.3
TB,BKIN,1,1,2,1
TBTEMP,0.0
TBDATA,,30,0

MP,MU,2,0.2
MP,MU,3,0.2
MP,MU,4,0.2


R,1,2
R,2
R,2,,,0.3,0.1,0,
RMORE,,,1.0E20,0.0,1.0,
RMORE,0.0,0,1.0,,1.0,0.5
RMORE,0,1.0,1.0,0.0,,1.0
NROPT,UNSYM
KEYOPT,3,10,1

R,3
R,3,,,0.3,0.1,0,
RMORE,,,1.0E20,0.0,1.0,
RMORE,0.0,0,1.0,,1.0,0.5
RMORE,0,1.0,1.0,0.0,,1.0
NROPT,UNSYM
KEYOPT,3,10,1

R,4
R,4,,,0.3,0.1,0,
RMORE,,,1.0E20,0.0,1.0,
RMORE,0.0,0,1.0,,1.0,0.5
RMORE,0,1.0,1.0,0.0,,1.0
NROPT,UNSYM
KEYOPT,3,10,1


K,1,X0,Y1,Z0
K,2,X1,Y1,Z0
K,3,X101,Y0,Z0
K,4,X201,Y0,Z0
K,5,X2,Y2,Z0
K,6,X3,Y3,Z0
K,7,X5,Y3,Z0

L,1,2
L,2,3
L,3,4
L,4,5
L,5,6
L,6,7

LFILLT,1,2,R01
LFILLT,2,3,R05
LFILLT,3,4,R02
LFILLT,4,5,R03
LFILLT,5,6,R04

CM,TARBOT,LINE
NUMCMP,KP
LSEL,NONE

K,100,X3,Y3+HBL+CE0,Z0
K,101,X5,Y3+HBL+CE0,Z0
L,100,101
CM,TARTOP,LINE

NUMCMP,KP
NUMCMP,LINE
*GET,LMAXN,LINE,0,NUM,MAX

LSEL,NONE
K,100,X0,Y5,Z0
K,101,XCT1,Y5,Z0
K,102,XCT101,Y4,Z0
K,103,XCT2,Y4,Z0
K,104,XCT201,Y6,Z0
K,105,XCT3,Y7,Z0

L,100,101
L,101,102
L,102,103
L,103,104
L,104,105

LFILLT,LMAXN+1,LMAXN+2,RCT1
LFILLT,LMAXN+2,LMAXN+3,RCT2
LFILLT,LMAXN+3,LMAXN+4,RCT3
LFILLT,LMAXN+4,LMAXN+5,RCT4

CM,TARCT,LINE

NUMCMP,KP
K,100,100,150,Z0
K,101,100,160,Z0
K,102,100,170,Z0

LSEL,NONE
RECTNG,X0,X4,Y3,Y3+HBL
APLO
CM,ACONT,AREA
LSEL,S,LOC,Y,Y3
CM,LCONBOT,LINE
LSEL,S,LOC,Y,Y3+HBL
CM,LCONTOP,LINE

ALLSEL
LPLO


ESIZE,3,0,
MSHAPE,0,2D
MSHKEY,0
AMESH,ALL
NUMCMP,NODE

CMSEL,S,TARCT
TYPE,2
REAL,2
MAT,2
LMESH,ALL
KMESH,102
*GET,NCT,NODE,0,NUM,MAX


CMSEL,S,LCONTOP
NSLL,S,1
ESLN,S,0
TYPE,3
REAL,2
MAT,2
ESURF

CMSEL,S,TARTOP
TYPE,4
REAL,3
MAT,3
LMESH,ALL
KMESH,101
*GET,NTOP,NODE,0,NUM,MAX


CMSEL,S,LCONTOP
NSLL,S,1
ESLN,S,0
TYPE,5
REAL,3
MAT,3
ESURF


CMSEL,S,TARBOT
TYPE,6
REAL,4
MAT,4
LMESH,ALL
KMESH,100
*GET,NBOT,NODE,0,NUM,MAX

CMSEL,S,LCONBOT
NSLL,S,1
ESLN,S,0
TYPE,7
REAL,4
MAT,4
ESURF


CMSEL,S,TARBOT
NSLL,S,1
ESLN,S,1
ESURF,,REVERSE

ALLSEL
FINISH


/SOLU
ANTYPE,STATIC
NLGEOM,ON
RESCON,DEFINE,NONE
OUTRES,ALL,ALL
NSUBST,300,500,100
TIME,1

LSEL,S,LOC,X,X0
DL,ALL,,SYMM
D,NBOT,ALL
D,NTOP,ALL
D,NCT,,-DY1,,,,UY
ALLSEL
NPLO
EPLO
SOLVE

TIME,2
NSUBST,200,400,50
D,NCT,,-DY2,,,,UY
ALLSEL
SOLVE

TIME,3
NSUBST,200,400,50
D,NCT,,-DY3,,,,UY
ALLSEL
SOLVE
FINISH

2010年06月15日 - 林子 - 林子清风 CAE/CFD工作室


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