def run(self):
path = geom.path(
geom.XYZ(0.0, 0.0, 0.0),
geom.XYZ(0.0, 1.0, 0.0),
geom.XYZ(1.0, 0.0, 0.0),
geom.XYZ(0.0, 0.0, 100.0),
geom.XYZ(0.0, 0.0, 1.0),
geom.XYZ(1.0, 0.0, 0.0),
)
#geom.plot(path.position)
print path.get_length()
print path.find(90.0)
print path.get_point(90.0)
l = path.get_length()
prof = profile.make_profile([(0.0, 20.0), (l, 0.0)])
tentacle = shape.path_extrusion(path, shape.circle, prof)
self.save(tentacle, 'tentacle')
def run(self):
path = geom.path(
geom.XYZ(0.0,0.0,0.0),
geom.XYZ(0.0,1.0,0.0),
geom.XYZ(1.0,0.0,0.0),
geom.XYZ(0.0,0.0,100.0),
geom.XYZ(0.0,0.0,1.0),
geom.XYZ(1.0,0.0,0.0),
)
#geom.plot(path.position)
print path.get_length()
print path.find(90.0)
print path.get_point(90.0)
l = path.get_length()
prof = profile.make_profile([(0.0,20.0),(l,0.0)])
tentacle = shape.path_extrusion(path,shape.circle,prof)
self.save(tentacle, 'tentacle')
def construct(self):
bore = self.bore
outside = self.outside
#outside = bore * 1.4
bore_length = bore * 1.5 #*2.0
gap_length = bore * self.gap_length
windcutter_length = bore * 1.0
airway_length = bore*1.5
z_min = -bore_length
z_gap_0 = z_min + bore_length - gap_length
z_gap_1 = z_min + bore_length
z_windcutter_0 = z_gap_0 - windcutter_length
z_windcutter_1 = z_gap_0
z_airway_0 = z_gap_1
z_airway_1 = z_airway_0 + airway_length
z_max = z_airway_1
#airway_xsize = bore * 0.15
#airway_xsize = (outside-bore) * 0.4
airway_xsize = 2.0 #Constant!
airway_ysize = bore * self.gap_width
#print 'Note mill bit diameter must be less than: %.1fmm' % (airway_xsize*2.0)
windcutter_rounding = bore * 0.1
windcutter_ysize = airway_ysize + windcutter_rounding
windcutter_lip = bore * 0.02
airway_x_low = bore*0.5-airway_xsize*0.5+windcutter_lip*0.5
airway_x_high = bore*0.5+airway_xsize*0.5+windcutter_lip*0.5
airway_line_0 = profile.make_profile(
[(z_airway_0, airway_x_low),
(z_airway_1, airway_x_low)])
airway_line_1 = profile.make_profile(
[(z_airway_0, airway_x_high),
(z_airway_1, airway_x_high)])
windcutter_line = profile.make_profile(
[(z_windcutter_0, outside*0.5),
(z_windcutter_1, bore*0.5+windcutter_lip)])
undercutter_line = profile.make_profile(
[(z_windcutter_0, bore*0.35),
(z_windcutter_1, bore*0.5)])
body = shape.extrude_profile(
profile.make_profile([(z_min,outside),(z_max,outside)]),
)
bore_space = shape.extrude_profile(
profile.make_profile([(z_min,bore),(z_gap_1,bore)]),
)
#body.remove(bore_space)
space = bore_space.copy()
windcutter_space = shape.extrude_profile(
windcutter_line.clipped(z_windcutter_0-1.0,z_gap_1),
cross_section = lambda x:
shape.rounded_rectangle(
x, x+bore,
windcutter_ysize*-0.5,windcutter_ysize*0.5,
windcutter_rounding)
)
body.remove(windcutter_space)
#space.add(windcutter_space)
undercutter_space = shape.extrude_profile(
undercutter_line.clipped(z_windcutter_0,z_gap_1),
cross_section = lambda x:
# shape.halfrounded_rectangle(
shape.rectangle(
x-airway_xsize, x,
airway_ysize*-0.5,airway_ysize*0.5)
)
#body.remove(undercutter_space)
space.add(undercutter_space)
airway_space = shape.extrude_profile(
airway_line_0.clipped(z_gap_0,z_airway_1+ airway_xsize*2), #Make longer, for milling inside
airway_line_1.clipped(z_gap_0,z_airway_1+ airway_xsize*2),
cross_section = lambda x0, x1:
shape.rectangle(
x0, x1,
airway_ysize*-0.5,airway_ysize*0.5)
)
body.remove(airway_space)
space.add(airway_space)
gap_space = shape.block(
0.0, bore,
airway_ysize*-0.5,airway_ysize*0.5,
z_gap_0,z_gap_1
)
body.remove(gap_space)
#space.add(gap_space)
cutaway_diameter = outside*1.5
cutaway_space = shape.extrude_profile(
profile.make_profile([(-outside*0.51, cutaway_diameter),(outside*0.51,cutaway_diameter)]))
cutaway_space.rotate(1,0,0, 90)
cutaway_space.move(-cutaway_diameter*0.5+bore*0.5-(outside*0.5-bore*0.5),0,z_max)
#cutaway_space.clip(shape.block(-outside*0.51,outside*0.51,-outside*0.51,outside*0.51,z_min,z_max))
body.remove(cutaway_space)
space.add(cutaway_space)
#self.save(body, 'whistle')
#assert airway_xsize_0 == airway_xsize_1
#jaw_clipper = shape.extrude_profile(
# profile.make_profile([(-outside,0),(outside,0)]),
# cross_section=lambda foo: shape.rounded_rectangle(
# z_gap_0, z_max+gap_length,
# -outside, airway_line_0(z_airway_0),
# gap_length*2.0)
# )
#jaw_clipper.rotate(1,0,0,90)
#jaw_clipper.rotate(0,1,0,-90)
#jaw_clipper.rotate(0,0,1,180)
#jaw_clipper = shape.extrude_profile(
# airway_line_0.clipped(z_airway_0,z_airway_1+1.0),
# airway_line_1.clipped(z_airway_0,z_airway_1+1.0),
# cross_section = lambda x0, x1:
# shape.rounded_rectangle(
# -x0*0.8, #(Can't be larger than bore)
# x1 * 0.995, #So as to not leave a little fuzz
# airway_ysize*-0.5,airway_ysize*0.5,
# (x1-x0)*2.0)
# )
d = airway_x_low*2
jaw_clipper = shape.extrude_profile(
profile.make_profile([(-outside*0.5-10, d),(outside*0.5+10, d)]),
cross_section = lambda d:
shape.halfrounded_rectangle(
-0.001, airway_x_low*1.001,
z_airway_0-d*0.5,z_max+d*0.5)
)
jaw_clipper.rotate(1,0,0, 90)
#jaw = jaw_clipper.copy()
#jaw.remove(space)
#jaw.clip(body)
#self.save(jaw, 'jaw')
#head = body.copy()
#head.remove(jaw)
#self.save(head, 'head')
return body, space, jaw_clipper
def construct(self):
bore = self.bore
outside = self.outside
#outside = bore * 1.4
bore_length = bore * 1.5 #*2.0
gap_length = bore * self.gap_length
windcutter_length = bore * 1.0
airway_length = bore * 1.5
z_min = -bore_length
z_gap_0 = z_min + bore_length - gap_length
z_gap_1 = z_min + bore_length
z_windcutter_0 = z_gap_0 - windcutter_length
z_windcutter_1 = z_gap_0
z_airway_0 = z_gap_1
z_airway_1 = z_airway_0 + airway_length
z_max = z_airway_1
#airway_xsize = bore * 0.15
#airway_xsize = (outside-bore) * 0.4
airway_xsize = 2.0 #Constant!
airway_ysize = bore * self.gap_width
#print 'Note mill bit diameter must be less than: %.1fmm' % (airway_xsize*2.0)
windcutter_rounding = bore * 0.1
windcutter_ysize = airway_ysize + windcutter_rounding
windcutter_lip = bore * 0.02
airway_x_low = bore * 0.5 - airway_xsize * 0.5 + windcutter_lip * 0.5
airway_x_high = bore * 0.5 + airway_xsize * 0.5 + windcutter_lip * 0.5
airway_line_0 = profile.make_profile([(z_airway_0, airway_x_low),
(z_airway_1, airway_x_low)])
airway_line_1 = profile.make_profile([(z_airway_0, airway_x_high),
(z_airway_1, airway_x_high)])
windcutter_line = profile.make_profile([
(z_windcutter_0, outside * 0.5),
(z_windcutter_1, bore * 0.5 + windcutter_lip)
])
undercutter_line = profile.make_profile([(z_windcutter_0, bore * 0.35),
(z_windcutter_1, bore * 0.5)])
body = shape.extrude_profile(
profile.make_profile([(z_min, outside), (z_max, outside)]), )
bore_space = shape.extrude_profile(
profile.make_profile([(z_min, bore), (z_gap_1, bore)]), )
#body.remove(bore_space)
space = bore_space.copy()
windcutter_space = shape.extrude_profile(
windcutter_line.clipped(z_windcutter_0 - 1.0, z_gap_1),
cross_section=lambda x: shape.rounded_rectangle(
x, x + bore, windcutter_ysize * -0.5, windcutter_ysize * 0.5,
windcutter_rounding))
body.remove(windcutter_space)
#space.add(windcutter_space)
undercutter_space = shape.extrude_profile(
undercutter_line.clipped(z_windcutter_0, z_gap_1),
cross_section=lambda x:
# shape.halfrounded_rectangle(
shape.rectangle(x - airway_xsize, x, airway_ysize * -0.5,
airway_ysize * 0.5))
#body.remove(undercutter_space)
space.add(undercutter_space)
airway_space = shape.extrude_profile(
airway_line_0.clipped(
z_gap_0, z_airway_1 +
airway_xsize * 2), #Make longer, for milling inside
airway_line_1.clipped(z_gap_0, z_airway_1 + airway_xsize * 2),
cross_section=lambda x0, x1: shape.rectangle(
x0, x1, airway_ysize * -0.5, airway_ysize * 0.5))
body.remove(airway_space)
space.add(airway_space)
gap_space = shape.block(0.0, bore, airway_ysize * -0.5,
airway_ysize * 0.5, z_gap_0, z_gap_1)
body.remove(gap_space)
#space.add(gap_space)
cutaway_diameter = outside * 1.5
cutaway_space = shape.extrude_profile(
profile.make_profile([(-outside * 0.51, cutaway_diameter),
(outside * 0.51, cutaway_diameter)]))
cutaway_space.rotate(1, 0, 0, 90)
cutaway_space.move(
-cutaway_diameter * 0.5 + bore * 0.5 -
(outside * 0.5 - bore * 0.5), 0, z_max)
#cutaway_space.clip(shape.block(-outside*0.51,outside*0.51,-outside*0.51,outside*0.51,z_min,z_max))
body.remove(cutaway_space)
space.add(cutaway_space)
#self.save(body, 'whistle')
#assert airway_xsize_0 == airway_xsize_1
#jaw_clipper = shape.extrude_profile(
# profile.make_profile([(-outside,0),(outside,0)]),
# cross_section=lambda foo: shape.rounded_rectangle(
# z_gap_0, z_max+gap_length,
# -outside, airway_line_0(z_airway_0),
# gap_length*2.0)
# )
#jaw_clipper.rotate(1,0,0,90)
#jaw_clipper.rotate(0,1,0,-90)
#jaw_clipper.rotate(0,0,1,180)
#jaw_clipper = shape.extrude_profile(
# airway_line_0.clipped(z_airway_0,z_airway_1+1.0),
# airway_line_1.clipped(z_airway_0,z_airway_1+1.0),
# cross_section = lambda x0, x1:
# shape.rounded_rectangle(
# -x0*0.8, #(Can't be larger than bore)
# x1 * 0.995, #So as to not leave a little fuzz
# airway_ysize*-0.5,airway_ysize*0.5,
# (x1-x0)*2.0)
# )
d = airway_x_low * 2
jaw_clipper = shape.extrude_profile(
profile.make_profile([(-outside * 0.5 - 10, d),
(outside * 0.5 + 10, d)]),
cross_section=lambda d: shape.halfrounded_rectangle(
-0.001, airway_x_low * 1.001, z_airway_0 - d * 0.5, z_max + d *
0.5))
jaw_clipper.rotate(1, 0, 0, 90)
#jaw = jaw_clipper.copy()
#jaw.remove(space)
#jaw.clip(body)
#self.save(jaw, 'jaw')
#head = body.copy()
#head.remove(jaw)
#self.save(head, 'head')
return body, space, jaw_clipper
