def final_example(self):
from hotwing_core import Profile
from hotwing_core import Rib
from hotwing_core import Machine
from hotwing_core import Panel
from hotwing_core import Coordinate
## Setup Rib
r1 = Rib(
"http://airfoiltools.com/airfoil/seligdatfile?airfoil=s6063-il",
scale=10,
xy_offset=None,
top_sheet=0.0625,
bottom_sheet=0.0625,
front_stock=0.5,
tail_stock=1.25)
r2 = Rib(
"http://airfoiltools.com/airfoil/seligdatfile?airfoil=rg14-il",
scale=10,
xy_offset=Coordinate(0, 0),
top_sheet=0.0625,
bottom_sheet=0.0625,
front_stock=0.5,
tail_stock=1.25)
# Setup Panel
p = Panel(r1, r2, 24)
# Trim Panel
p1 = Panel.trim(p, 0, 12)
# Setup Machine
m = Machine(24, kerf=0.075, profile_points=200)
# Load panel into machine
m.load_panel(panel=p1, left_offset=6)
# Generate GCode
gcode = m.generate_gcode(safe_height=5)
def test_create_machine(self):
from hotwing_core import Coordinate
from hotwing_core import Profile
from hotwing_core import Rib
from hotwing_core import Panel
## Create Root Rib
r1 = Rib(
"http://airfoiltools.com/airfoil/seligdatfile?airfoil=s6063-il",
scale=10,
xy_offset=None,
top_sheet=0.0625,
bottom_sheet=0.0625,
front_stock=0.5,
tail_stock=1.25)
## Create Tip Rib
r2 = Rib(
"http://airfoiltools.com/airfoil/seligdatfile?airfoil=rg14-il",
scale=10,
xy_offset=Coordinate(0, 0),
top_sheet=0.0625,
bottom_sheet=0.0625,
front_stock=0.5,
tail_stock=1.25)
# Setup Panel - takes the two ribs, at a specified distance of 24 units (inches or centimeters)
p = Panel(r1, r2, 24)
# A Panel can be trimmed. Say for example, the machine you will be using to cut your wing will
# only cut wings up to 12 units. We can use the Panel.trim classmethod to create a new,
# Panel. The trim will handle the interpolation and creation of a new Rib and Panel.
p1 = Panel.trim(
p, 0, 12
) # cut at 0 (no cut will occur) and at 12 - new panel is 12 units long.
p2 = Panel.trim(
p, 12, 24
) # cut at 12 and at 24 (no cut will occur) - new panel is 12 units long.
from hotwing_core import Machine
# Setup Machine
m = Machine(
24, # Width between pillars of machine
kerf=0.075, # Allowance for wire size and melted foam
profile_points=
200, # number of points to use for each surface when iterpolating
)
# Load panel into machine (p1 is the panel created in the previous step)
# The offset is the distance the left of the panel will be from the left of the machine --
# If you want it centered, for this example use an offset of 6 --
# (24-12[machine width-panel width]) -> 12/2(equal amount on each side)
m.load_panel(panel=p1, left_offset=6)
# Generate GCode
# safe_height is where the machine can move without hitting anything
gcode = m.generate_gcode(safe_height=5)
def test_cutting_strategies(self):
from hotwing_core import Profile
from hotwing_core import Rib
from hotwing_core import Machine
from hotwing_core import Panel
from hotwing_core import Coordinate
## Setup Rib
r1 = Rib("http://m-selig.ae.illinois.edu/ads/coord/ah83159.dat",
scale=10,
xy_offset=None,
top_sheet=0.0625,
bottom_sheet=0.0625,
front_stock=0.5,
tail_stock=1.25 )
r2 = Rib("http://m-selig.ae.illinois.edu/ads/coord/rg14.dat",
scale=10,
xy_offset=Coordinate(0, 0),
top_sheet=0.0625,
bottom_sheet=0.0625,
front_stock=0.5,
tail_stock=1.25 )
# Setup Panel
p = Panel(r1, r2, 24)
cutting_strategy_names=["CuttingStrategy1","CuttingStrategy2"]
for csn in cutting_strategy_names:
# Setup Machine
m = Machine(24, kerf=0.075, units="inches", cutting_strategy_name=csn, profile_points=300)
# Load panel into machine
m.load_panel(p)
# Generate GCode
gcode = m.generate_gcode(safe_height=3)
# test default
m = Machine(24, kerf=0.075, units="inches", cutting_strategy_name="default", profile_points=300)
# Load panel into machine
m.load_panel(p)
# Generate GCode
gcode = m.generate_gcode(safe_height=3)
# test invalid
m = Machine(24, kerf=0.075, units="inches", cutting_strategy_name="bad name", profile_points=300)
# Load panel into machine
m.load_panel(p)
# Generate GCode
gcode = m.generate_gcode(safe_height=3)
def test_create_rib(self):
from hotwing_core import Rib
## Create Rib
r1 = Rib(
"http://m-selig.ae.illinois.edu/ads/coord/e374.dat", # Dat file to use - File or URL
scale=10, # Width of the Rib - Scales the dat file profile
xy_offset=None, # Offset
top_sheet=
0.0625, # Sheeting allowance top - this will make the foil smaller by this
# amount
bottom_sheet=0.0625, # Sheeting allowance bottom
front_stock=
0.5, # Trims the front of the airfoil by this amount. You would glue
# wooden stock here and shape it
tail_stock=
1.25, # Trims the trailing edge of the foil. You would put tail stock
# here and shape to the foil.
rotation=
0, # The angle to rotate the rib in degrees - positive number points
# the nose upward
rotation_pos=0.5
) # Where the rotation point should occur. 0.25 = 25% along the
# chord (starting from the front)
# you can get the manipulated profile
r1.profile
# you can get the manipulated profile (pre-sheeting)
r1.airfoil_profile
def test_gcode_formatters(self):
from hotwing_core import Profile
from hotwing_core import Rib
from hotwing_core import Machine
from hotwing_core import Panel
from hotwing_core import Coordinate
## Setup Rib
r1 = Rib("http://m-selig.ae.illinois.edu/ads/coord/ah83159.dat",
scale=10,
xy_offset=None,
top_sheet=0.0625,
bottom_sheet=0.0625,
front_stock=0.5,
tail_stock=1.25)
r2 = Rib("http://m-selig.ae.illinois.edu/ads/coord/rg14.dat",
scale=10,
xy_offset=Coordinate(0, 0),
top_sheet=0.0625,
bottom_sheet=0.0625,
front_stock=0.5,
tail_stock=1.25)
# Setup Panel
p = Panel(r1, r2, 24)
gcode_formatter_names = [
"GenericGcodeFormatter", "DebugGcodeFormatter", "default"
]
for gfn in gcode_formatter_names:
# Setup Machine
m = Machine(24,
kerf=0.075,
units="inches",
gcode_formatter_name=gfn,
profile_points=300)
# Load panel into machine
m.load_panel(p)
# Generate GCode
gcode = m.generate_gcode(safe_height=3)
def test_create_panel(self):
from hotwing_core import Coordinate
from hotwing_core import Profile
from hotwing_core import Rib
from hotwing_core import Panel
## Create Root Rib
r1 = Rib(
"http://airfoiltools.com/airfoil/seligdatfile?airfoil=s6063-il",
scale=10,
xy_offset=None,
top_sheet=0.0625,
bottom_sheet=0.0625,
front_stock=0.5,
tail_stock=1.25)
## Create Tip Rib
r2 = Rib(
"http://airfoiltools.com/airfoil/seligdatfile?airfoil=rg14-il",
scale=10,
xy_offset=Coordinate(0, 0),
top_sheet=0.0625,
bottom_sheet=0.0625,
front_stock=0.5,
tail_stock=1.25)
# Setup Panel - takes the two ribs, at a specified distance of 24 units (inches or centimeters)
p = Panel(r1, r2, 24)
# A Panel can be trimmed. Say for example, the machine you will be using to cut your wing will
# only cut wings up to 12 units. We can use the Panel.trim_panel classmethod to create a new,
# Panel. The trim_panel will handle the interpolation and creation of a new Rib and Panel.
p1 = Panel.trim(
p, 0, 12
) # cut at 0 (no cut will occur) and at 12 - new panel is 12 units long.
p2 = Panel.trim(
p, 12, 24
) # cut at 12 and at 24 (no cut will occur) - new panel is 12 units long.
from hotwing_core import Profile
from hotwing_core import Rib
from hotwing_core import Machine
from hotwing_core import Panel
from hotwing_core import Coordinate
## Setup Rib
r1 = Rib("http://m-selig.ae.illinois.edu/ads/coord/ah83159.dat",
scale=10,
xy_offset=None,
top_sheet=0.0625,
bottom_sheet=0.0625,
front_stock=0.5,
tail_stock=1.25)
r2 = Rib("http://m-selig.ae.illinois.edu/ads/coord/rg14.dat",
scale=10,
xy_offset=Coordinate(0, 0),
top_sheet=0.0625,
bottom_sheet=0.0625,
front_stock=0.5,
tail_stock=1.25)
# Setup Panel
p = Panel(r1, r2, 24)
# Trim Panel
p = Panel.trim(p, 0, 12)
# Setup Machine
m = Machine(24, kerf=0.075, units="inches", profile_points=300)