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97 lines
3.4 KiB
Python
97 lines
3.4 KiB
Python
"""
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Creation of a complex sheet metal part
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name: ttt_sm_hanger.py
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by: Gumyr
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date: July 17, 2023
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desc:
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This example implements the sheet metal part described in Too Tall Toby's
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sm_hanger CAD challenge.
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Notably, a BuildLine/Curve object is filleted by providing all the vertices
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and allowing the fillet operation filter out the end vertices. The
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make_brake_formed operation is used both in Algebra and Builder mode to
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create a sheet metal part from just an outline and some dimensions.
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license:
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Copyright 2023 Gumyr
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Licensed under the Apache License, Version 2.0 (the "License");
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you may not use this file except in compliance with the License.
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You may obtain a copy of the License at
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http://www.apache.org/licenses/LICENSE-2.0
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Unless required by applicable law or agreed to in writing, software
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distributed under the License is distributed on an "AS IS" BASIS,
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WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
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See the License for the specific language governing permissions and
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limitations under the License.
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"""
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from build123d import *
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from ocp_vscode import *
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sheet_thickness = 4 * MM
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# Create the main body from a side profile
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with BuildPart() as side:
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d = Vector(1, 0, 0).rotate(Axis.Y, 60)
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with BuildLine(Plane.XZ) as side_line:
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l1 = Line((0, 65), (170 / 2, 65))
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l2 = PolarLine(l1 @ 1, length=65, direction=d, length_mode=LengthMode.VERTICAL)
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l3 = Line(l2 @ 1, (170 / 2, 0))
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fillet(side_line.vertices(), 7)
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make_brake_formed(
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thickness=sheet_thickness,
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station_widths=[40, 40, 40, 112.52 / 2, 112.52 / 2, 112.52 / 2],
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side=Side.RIGHT,
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)
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fe = side.edges().filter_by(Axis.Z).group_by(Axis.Z)[0].sort_by(Axis.Y)[-1]
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fillet(fe, radius=7)
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# Create the "wings" at the top
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with BuildPart() as wing:
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with BuildLine(Plane.YZ) as wing_line:
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l1 = Line((0, 65), (80 / 2 + 1.526 * sheet_thickness, 65))
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PolarLine(l1 @ 1, 20.371288916, direction=Vector(0, 1, 0).rotate(Axis.X, -75))
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fillet(wing_line.vertices(), 7)
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make_brake_formed(
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thickness=sheet_thickness,
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station_widths=110 / 2,
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side=Side.RIGHT,
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)
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bottom_edge = wing.edges().group_by(Axis.X)[-1].sort_by(Axis.Z)[0]
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fillet(bottom_edge, radius=7)
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# Create the tab at the top in Algebra mode
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tab_line = Plane.XZ * Polyline(
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(20, 65 - sheet_thickness), (56 / 2, 65 - sheet_thickness), (56 / 2, 88)
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)
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tab_line = fillet(tab_line.vertices(), 7)
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tab = make_brake_formed(sheet_thickness, 8, tab_line, Side.RIGHT)
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tab = fillet(tab.edges().filter_by(Axis.X).group_by(Axis.Z)[-1].sort_by(Axis.Y)[-1], 5)
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tab -= Pos((0, 0, 80)) * Rot(0, 90, 0) * Hole(5, 100)
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# Combine the parts together
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with BuildPart() as sm_hanger:
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add([side.part, wing.part])
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mirror(about=Plane.XZ)
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with BuildSketch(Plane.XY.offset(65)) as h1:
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with Locations((20, 0)):
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Rectangle(30, 30, align=(Align.MIN, Align.CENTER))
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fillet(h1.vertices().group_by(Axis.X)[-1], 7)
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SlotCenterPoint((154, 0), (154 / 2, 0), 20)
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extrude(amount=-40, mode=Mode.SUBTRACT)
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with BuildSketch() as h2:
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SlotCenterPoint((206, 0), (206 / 2, 0), 20)
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extrude(amount=40, mode=Mode.SUBTRACT)
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add(tab)
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mirror(about=Plane.YZ)
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mirror(about=Plane.XZ)
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# Target 1028g +/- 10g
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print(f"Mass: {sm_hanger.part.volume*7800*1e-6:0.1f} g") # 1027.7g
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show(sm_hanger)
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