summaryrefslogtreecommitdiff
path: root/Connections/Shear/Finplate/drawing_2D.py
diff options
context:
space:
mode:
authordeepa-chaudhari2015-09-02 10:54:07 +0530
committerdeepa-chaudhari2015-09-02 10:54:07 +0530
commit4a239fb5ce4710f9005466c2b8577b35273827ab (patch)
treefc0bb6f34f00a9616e085a0dda3074f15ffcf1b9 /Connections/Shear/Finplate/drawing_2D.py
parentb47147e28d492740f7a6dc3ccb1f768faf8840f9 (diff)
downloadOsdagLive-4a239fb5ce4710f9005466c2b8577b35273827ab.tar.gz
OsdagLive-4a239fb5ce4710f9005466c2b8577b35273827ab.tar.bz2
OsdagLive-4a239fb5ce4710f9005466c2b8577b35273827ab.zip
2D drawing2D_Drawing
Diffstat (limited to 'Connections/Shear/Finplate/drawing_2D.py')
-rw-r--r--Connections/Shear/Finplate/drawing_2D.py160
1 files changed, 160 insertions, 0 deletions
diff --git a/Connections/Shear/Finplate/drawing_2D.py b/Connections/Shear/Finplate/drawing_2D.py
new file mode 100644
index 0000000..0b1ee80
--- /dev/null
+++ b/Connections/Shear/Finplate/drawing_2D.py
@@ -0,0 +1,160 @@
+'''
+Created on 24-Aug-2015
+
+@author: deepa
+'''
+import svgwrite
+from svgwrite import mm
+from PyQt4.QtCore import QString
+import numpy as np
+
+class Fin2DCreatorFront(object):
+
+ def __init__(self, inputObj,ouputObj,dictBeamdata,dictColumndata):
+
+ beam_T = float(dictBeamdata[QString("T")])
+ D = int (dictBeamdata[QString("D")])
+ col_B = int(dictColumndata[QString("B")])
+ col_tw = float(dictColumndata[QString("tw")])
+ col_R1 = float(dictColumndata[QString("R1")])
+ plate_ht= ouputObj['Plate']['height']
+ plate_width = ouputObj['Plate']['width']
+ weld_len = ouputObj['Plate']['height']
+ weld_thick = ouputObj['Weld']['thickness']
+ self.bolt_dia = inputObj["Bolt"]["Diameter (mm)"]
+ self.pitch = ouputObj['Bolt']["pitch"]
+ self.gauge = ouputObj['Bolt']["gauge"]
+ self.end_dist = ouputObj['Bolt']["enddist"]
+ self.edge_dist = ouputObj['Bolt']["edge"]
+ self.no_of_rows = ouputObj['Bolt']["numofrow"]
+ self.no_of_col = ouputObj['Bolt']["numofcol"]
+ self.col_L = 1000
+ self.beam_L = 500
+
+
+ self.A2 =(col_B,(self.col_L-D)/2)
+ self.B = (col_B,0)
+ self.A = (0,0)
+ self.D = (0,self.col_L)
+ self.C = (col_B,self.col_L)
+ self.B2 = (col_B,(D + self.col_L)/2)
+
+ ptEx = (col_B-col_tw)/2
+ ptEy = 0.0
+ self.E = (ptEx,ptEy)
+ ptHx = (col_B-col_tw)/2
+ ptHy = self.col_L
+ self.H = (ptHx,ptHy)
+ ptFx = (col_B + col_tw)/2
+ ptFy = 0
+ self.F = (ptFx,ptFy)
+ ptGx = (col_B + col_tw)/2
+ ptGy = self.col_L
+ self.G = (ptGx,ptGy)
+
+ #Draw rectangle for finPlate PRSU
+ ptPx = (col_B + col_tw)/2
+ ptPy = ((self.col_L - D)/2) + (beam_T + col_R1 + 3)
+ self.P = (ptPx,ptPy)
+ self.ptP = np.array([ptPx,ptPy])
+
+ self.plate_ht = plate_ht
+ self.plate_width = plate_width
+ self.weld_thick = weld_thick
+ self.weld_len = weld_len
+ # Draw Rectangle for weld
+ ptCx1 = ((col_B + col_tw)/2 + 20)
+ ptCy1 = ((self.col_L - D)/2) + (beam_T + col_R1 + 3)
+ self.C1 =(ptCx1,ptCy1)
+
+ ptAx1 = ptCx1
+ ptAy1 = ((self.col_L - D)/2)
+ self.A1 = (ptAx1,ptAy1)
+
+ ptAx3 = ptCx1 + self.beam_L
+ ptAy3 = ptAy1
+ self.A3 = (ptAx3,ptAy3)
+
+ ptBx3 = ptAx3
+ ptBy3 = ((self.col_L + D)/2 )
+ self.B3 = (ptBx3,ptBy3)
+
+ ptBx1 = ptCx1
+ ptBy1 = ptBy3
+ self.B1 = (ptBx1,ptBy1)
+
+ ptC2x= ptCx1
+ ptC2y = ptCy1 + plate_ht
+ self.C2 = (ptC2x,ptC2y)
+
+ ptAx5 = ptAx1
+ ptAy5 = ptAy1 + beam_T
+ self.A5 = ptAx5,ptAy5
+
+ ptAx4 = ptAx3
+ ptAy4 = ptAy3 + beam_T
+ self.A4 = (ptAx4,ptAy4)
+
+ ptBx4 = ptBx3
+ ptBy4 = ptBy3 - beam_T
+ self.B4 = (ptBx4,ptBy4)
+
+ ptBx5 = ((col_B + col_tw)/2) + 20
+ ptBy5 = ptBy3 - beam_T
+ self.B5 = (ptBx5,ptBy5)
+
+ ptP1x = ((col_B + col_tw)/2 + self.edge_dist)
+ ptP1y = ((self.col_L - D)/2 +(col_tw + col_R1 + 3)+ self.end_dist)
+ self.P1 = (ptP1x,ptP1y)
+
+ ptP2x = ptP1x
+ ptP2y = ptP1y + self.pitch
+ self.P2 = (ptP1x,ptP1y)
+
+ ptP3x = ptP1x
+ ptP3y = ptP2y + self.pitch
+ self.P3 = (ptP1x,ptP1y)
+ # points for diamension
+
+
+ def saveToSvg(self):
+ dwg = svgwrite.Drawing('finfront.svg', profile='tiny')
+ dwg.add(dwg.polyline(points=[(self.A2),(self.B),(self.A),(self.D),(self.C) ,(self.B2)], stroke='blue', fill='none', stroke_width=2.5))
+ dwg.add(dwg.line((self.E),(self.H)).stroke('blue',width = 2.5,linecap = 'square'))
+ dwg.add(dwg.line((self.F),(self.G)).stroke('blue',width = 2.5,linecap = 'square'))
+ dwg.add(dwg.rect(insert=(self.P), size=(self.plate_width, self.plate_ht),fill = 'none', stroke='blue', stroke_width=2.5))
+ dwg.add(dwg.rect(insert=(self.P), size=(self.weld_thick, self.plate_ht),fill = 'none', stroke='blue', stroke_width=2.0))
+ #C1,A1,A3,B3,B1,C2
+ dwg.add(dwg.polyline(points=[(self.C1),(self.A1),(self.A3),(self.B3),(self.B1),(self.C2)],stroke = 'blue',fill= 'none',stroke_width =2.5))
+ #C1,C2
+ dwg.add(dwg.line((self.C1),(self.C2)).stroke('red',width = 2.5,linecap = 'square').dasharray(dasharray = ([5,5])))
+ #A2,B2
+ dwg.add(dwg.line((self.A2),(self.B2)).stroke('red',width = 2.5,linecap = 'square').dasharray(dasharray = ([5,5])))
+ dwg.add(dwg.line((self.A5),(self.A4)).stroke('blue',width = 2.5,linecap = 'square'))
+ dwg.add(dwg.line((self.B5),(self.B4)).stroke('blue',width = 2.5,linecap = 'square'))
+ nr = self.no_of_rows
+ nc = self.no_of_col
+ bolt_r = self.bolt_dia/2
+ for i in range(1,(nr+1)):
+ for j in range (1,(nc+1)):
+ pt = self.ptP + self.edge_dist * np.array([1,0]) + self.end_dist * np.array ([0,1]) + \
+ (i-1) * self.pitch * np.array([0,1]) + (j-1) * self.gauge * np.array([1,0])
+ dwg.add(dwg.circle(center=(pt), r = bolt_r, stroke='blue',fill ='black',stroke_width=1.5))
+ ptA = pt - (bolt_r + 4) * np.array([0,1])
+ ptB = pt + (bolt_r + 4) * np.array([0,1])
+ #dwg.add(dwg.line((ptA),(ptB)).stroke('blue',width = 2.0,linecap = 'square'))
+ ptC = pt - (bolt_r + 4) * np.array([1,0])
+ PtD = pt + (bolt_r + 4) * np.array([1,0])
+ dwg.add(dwg.line((ptC),(PtD)).stroke('blue',width = 2.0,linecap = 'square'))
+ ptE = self.ptP + self.edge_dist * np.array([1,0]) +(j-1) * self.gauge * np.array([1,0])
+ ptF = ptE + self.plate_ht * np.array([0,1])
+ dwg.add(dwg.line((ptE),(ptF)).stroke('blue',width = 1.5,linecap = 'square').dasharray(dasharray = ([20, 5, 1, 5])))
+
+ dwg.save()
+ print"Saved"
+
+
+
+
+
+ \ No newline at end of file