feat: Electronic board assembly
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07fb43cd01
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@ -34,6 +34,11 @@ class Hole:
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diam: Optional[float] = None
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tag: Optional[str] = None
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@property
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def rev_tag(self) -> str:
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assert self.tag is not None
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return self.tag + "_rev"
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@dataclass
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class MountingBox(Model):
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"""
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@ -56,6 +61,11 @@ class MountingBox(Model):
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# Determines the position of side tags
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flip_y: bool = False
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def __post_init__(self):
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for i, hole in enumerate(self.holes):
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if hole.tag is None:
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hole.tag = f"conn{i}"
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@target(kind=TargetKind.DXF)
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def profile(self) -> Cq.Sketch:
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bx, by = 0, 0
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@ -84,12 +94,11 @@ class MountingBox(Model):
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)
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plane = result.copyWorkplane(Cq.Workplane('XY')).workplane(offset=self.thickness)
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reverse_plane = result.copyWorkplane(Cq.Workplane('XY'))
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for i, hole in enumerate(self.holes):
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tag = hole.tag if hole.tag else f"conn{i}"
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plane.moveTo(hole.x, hole.y).tagPlane(tag)
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for hole in self.holes:
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assert hole.tag
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plane.moveTo(hole.x, hole.y).tagPlane(hole.tag)
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if self.generate_reverse_tags:
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rev_tag = hole.tag + "_rev" if hole.tag else f"conn{i}_rev"
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reverse_plane.moveTo(hole.x, hole.y).tagPlane(rev_tag, '-Z')
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reverse_plane.moveTo(hole.x, hole.y).tagPlane(hole.rev_tag, '-Z')
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if self.generate_side_tags:
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result.faces("<Y").workplane(origin=result.vertices("<X and <Y and >Z").val().Center()).tagPlane("left")
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@ -106,10 +115,10 @@ class MountingBox(Model):
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Cq.Assembly()
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.add(self.generate(), name="box")
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)
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for i in range(len(self.holes)):
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result.markPlane(f"box?conn{i}")
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for hole in self.holes:
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result.markPlane(f"box?{hole.tag}")
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if self.generate_reverse_tags:
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result.markPlane(f"box?conn{i}_rev")
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result.markPlane(f"box?{hole.rev_tag}")
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if self.generate_side_tags:
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(
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result
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@ -0,0 +1,18 @@
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from nhf.parts.fasteners import FlatHeadBolt, HexNut, ThreaddedKnob
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NUT_COMMON = HexNut(
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# FIXME: measure
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mass=0.0,
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diam_thread=4.0,
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pitch=0.7,
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thickness=3.2,
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width=7.0,
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)
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BOLT_COMMON = FlatHeadBolt(
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# FIXME: measure
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mass=0.0,
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diam_head=8.0,
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height_head=2.0,
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diam_thread=4.0,
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height_thread=20.0,
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)
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@ -1,13 +1,16 @@
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"""
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Electronic components
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"""
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from dataclasses import dataclass
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from dataclasses import dataclass, field
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from typing import Optional, Tuple
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import math
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import cadquery as Cq
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from nhf.materials import Role
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from nhf.build import Model, TargetKind, target, assembly, submodel
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from nhf.materials import Role, Material
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from nhf.parts.box import MountingBox, Hole
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from nhf.parts.item import Item
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from nhf.parts.fasteners import FlatHeadBolt, HexNut
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from nhf.touhou.houjuu_nue.common import NUT_COMMON, BOLT_COMMON
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import nhf.utils
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@dataclass(frozen=True)
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@ -268,8 +271,6 @@ class BatteryBox18650(Item):
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)
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LINEAR_ACTUATOR_50 = LinearActuator(
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mass=34.0,
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stroke_length=50,
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@ -427,6 +428,65 @@ class Flexor:
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@dataclass
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class ElectronicBoard:
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class ElectronicBoard(Model):
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hole_diam: float = 4.0
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name: str = "electronic-board"
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nut: HexNut = NUT_COMMON
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bolt: FlatHeadBolt = BOLT_COMMON
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length: float = 70.0
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width: float = 170.0
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mount_holes: list[Hole] = field(default_factory=lambda: [
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Hole(x=30, y=80),
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Hole(x=30, y=-80),
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Hole(x=-30, y=80),
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Hole(x=-30, y=-80),
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])
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panel_thickness: float = 25.4 / 16
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mount_panel_thickness: float = 25.4 / 4
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material: Material = Material.WOOD_BIRCH
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@property
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def mount_hole_diam(self) -> float:
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return self.bolt.diam_thread
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def __post_init__(self):
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super().__init__(name=self.name)
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@submodel(name="panel")
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def panel(self) -> MountingBox:
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return MountingBox(
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holes=self.mount_holes,
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hole_diam=self.mount_hole_diam,
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length=self.length,
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width=self.width,
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centred=(True, True),
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thickness=self.panel_thickness,
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generate_reverse_tags=True,
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)
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def assembly(self) -> Cq.Assembly:
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panel = self.panel()
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result = (
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Cq.Assembly()
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.addS(panel.generate(), name="panel",
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role=Role.STRUCTURE, material=self.material)
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)
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for hole in panel.holes:
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spacer_name = f"{hole.tag}_spacer"
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bolt_name = f"{hole.tag}_bolt"
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(
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result
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.add(self.nut.assembly(), name=spacer_name)
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.add(self.bolt.assembly(), name=bolt_name)
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.constrain(
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f"{spacer_name}?top",
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f"panel?{hole.rev_tag}",
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"Plane"
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)
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.constrain(
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f"{bolt_name}?root",
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f"panel?{hole.tag}",
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"Plane", param=0
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)
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)
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return result.solve()
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@ -90,7 +90,7 @@ class WingProfile(Model):
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elbow_rotate: float = -5.0
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wrist_rotate: float = -30.0
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# Position of the elbow axle with 0 being bottom and 1 being top (flipped on the left side)
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elbow_axle_pos: float = 0.3
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elbow_axle_pos: float = 0.5
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wrist_axle_pos: float = 0.0
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# False for the right side, True for the left side
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@ -99,6 +99,8 @@ class WingProfile(Model):
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def __post_init__(self):
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super().__init__(name=self.name)
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assert self.electronic_board.length == self.shoulder_height
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self.elbow_top_loc = self.elbow_bot_loc * Cq.Location.from2d(0, self.elbow_height)
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self.wrist_top_loc = self.wrist_bot_loc * Cq.Location.from2d(0, self.wrist_height)
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if self.flip:
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@ -114,6 +116,7 @@ class WingProfile(Model):
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self.shoulder_joint.angle_neutral = -self.shoulder_angle_neutral - self.shoulder_angle_bias
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self.shoulder_axle_loc = Cq.Location.from2d(self.shoulder_tip_x, self.shoulder_tip_y - self.shoulder_width / 2, self.shoulder_angle_bias)
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self.shoulder_joint.child_guard_width = self.s1_thickness + self.panel_thickness * 2
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assert self.spacer_thickness == self.root_joint.child_mount_thickness
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@property
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@ -278,21 +281,16 @@ class WingProfile(Model):
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flip_y=self.flip,
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)
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@submodel(name="spacer-s0-electronic")
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def spacer_s0_electronic(self) -> MountingBox:
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holes = [
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Hole(x=30, y=80),
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Hole(x=30, y=-80),
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Hole(x=-30, y=80),
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Hole(x=-30, y=-80),
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]
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def spacer_s0_electronic_mount(self) -> MountingBox:
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return MountingBox(
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holes=holes,
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hole_diam=self.electronic_board.hole_diam,
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holes=self.electronic_board.mount_holes,
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hole_diam=self.electronic_board.mount_hole_diam,
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length=self.root_height,
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width=170,
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width=self.electronic_board.width,
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centred=(True, True),
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thickness=self.spacer_thickness,
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flip_y=self.flip
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flip_y=self.flip,
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generate_reverse_tags=True,
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)
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def surface_s0(self, top: bool = False) -> Cq.Workplane:
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@ -310,7 +308,7 @@ class WingProfile(Model):
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self.shoulder_joint.parent_arm_loc() *
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loc_tip),
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("base", Cq.Location.from2d(base_dx, base_dy, 90)),
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("electronic", Cq.Location.from2d(-55, 75, 64)),
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("electronic_mount", Cq.Location.from2d(-55, 75, 64)),
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]
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result = extrude_with_markers(
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self.profile_s0(top=top),
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@ -323,7 +321,7 @@ class WingProfile(Model):
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return result
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@assembly()
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def assembly_s0(self) -> Cq.Assembly:
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def assembly_s0(self, ignore_detail: bool=False) -> Cq.Assembly:
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result = (
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Cq.Assembly()
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.addS(self.surface_s0(top=True), name="bot",
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@ -343,7 +341,7 @@ class WingProfile(Model):
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for o, tag in [
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(self.spacer_s0_shoulder().generate(), "shoulder"),
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(self.spacer_s0_base().generate(), "base"),
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(self.spacer_s0_electronic().generate(), "electronic"),
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(self.spacer_s0_electronic_mount().generate(), "electronic_mount"),
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]:
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top_tag, bot_tag = "top", "bot"
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if self.flip:
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@ -357,6 +355,27 @@ class WingProfile(Model):
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.constrain(f"{tag}?{top_tag}", f"top?{tag}", "Plane")
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.constrain(f"{tag}?dir", f"top?{tag}_dir", "Axis")
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)
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if not ignore_detail:
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result.add(self.electronic_board.assembly(), name="electronic_board")
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for hole in self.electronic_board.mount_holes:
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assert hole.tag
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nut_name = f"electronic_board_{hole.tag}_nut"
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(
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result
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.addS(
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self.electronic_board.nut.assembly(),
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name=nut_name)
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.constrain(
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f"electronic_mount?{hole.rev_tag}",
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f'{nut_name}?top',
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"Plane"
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)
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.constrain(
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f"electronic_mount?{hole.tag}",
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f'electronic_board/{hole.tag}_spacer?bot',
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"Plane"
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)
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)
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return result.solve()
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@ -804,6 +823,7 @@ class WingProfile(Model):
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elbow_wrist_deflection: float = 0.0,
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root_offset: int = 5,
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fastener_pos: float = 0.0,
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ignore_detail: bool = False,
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) -> Cq.Assembly():
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if parts is None:
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parts = [
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@ -824,7 +844,7 @@ class WingProfile(Model):
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tag_top, tag_bot = tag_bot, tag_top
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if "s0" in parts:
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result.add(self.assembly_s0(), name="s0")
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result.add(self.assembly_s0(ignore_detail=ignore_detail), name="s0")
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if "root" in parts:
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result.addS(self.root_joint.assembly(
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offset=root_offset,
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