feat: 2nd wing segment with spacer

nhf/materials.py

@@ -33,6 +33,7 @@ class Material(Enum):
     PLASTIC_PLA = 0.5, _color('azure3', 0.6)
     RESIN_TRANSPARENT = 1.1, _color('cadetblue2', 0.6)
     ACRYLIC_BLACK = 0.5, _color('gray50', 0.6)
+    ACRYLIC_TRANSPARENT = 0.5, _color('ghostwhite', 0.5)
 
     def __init__(self, density: float, color: Cq.Color):
         self.density = density

nhf/parts/joints.py

@@ -332,6 +332,7 @@ class TorsionJoint:
         )
 
     def track(self):
+        # TODO: Cover outer part of track only. Can we do this?
         groove_profile = (
             Cq.Sketch()
             .circle(self.radius)

nhf/touhou/houjuu_nue/__init__.py

@@ -104,12 +104,16 @@ class Parameters(Model):
     shoulder_attach_diam: float = 8
 
     """
-    Heights for various wing joints, where the numbers start from the first joint.
+    Heights for various wing joints, where the numbers start from the first
+    joint.
     """
     wing_s0_thickness: float = 40
     wing_s0_height: float = 100
-    wing_r1_height: float = 100
+
-    wing_r1_width: float = 400
+    # Length of the spacer
+    wing_s1_thickness: float = 20
+    wing_s1_spacer_thickness: float = 25.4 / 8
+    wing_s1_spacer_width: float = 20
 
     trident_handle: Handle = field(default_factory=lambda: Handle(
         diam=38,
@@ -121,6 +125,9 @@ class Parameters(Model):
         simplify_geometry=False,
     ))
 
+    material_panel: Material = Material.ACRYLIC_TRANSPARENT
+    material_bracket: Material = Material.ACRYLIC_TRANSPARENT
+
     def __post_init__(self):
         super().__init__(name="houjuu-nue")
         assert self.wing_root_radius > self.hs_hirth_joint.radius,\
@@ -258,6 +265,10 @@ class Parameters(Model):
         result.faces("<Z").tag("base")
         return result
 
+    #@target(name="wing/joining-plate", kind=TargetKind.DXF)
+    #def joining_plate(self) -> Cq.Workplane:
+    #    return self.wing_joining_plate.plate()
+
     @target(name="wing_root")
     def wing_root(self) -> Cq.Assembly:
         """
@@ -312,43 +323,42 @@ class Parameters(Model):
         )
         return result
 
-    def wing_r1_profile(self) -> Cq.Sketch:
+    @target(name="wing/s1-spacer", kind=TargetKind.DXF)
-        """
+    def wing_s1_spacer(self) -> Cq.Workplane:
-        Generates the first wing segment profile, with the wing root pointing in
-        the positive x axis.
-        """
-        # Depression of the wing middle
-        bend = 200
-        factor = 0.7
         result = (
-            Cq.Sketch()
+            Cq.Workplane('XZ')
-            .segment((0, 0), (0, self.wing_r1_height))
+            .sketch()
-            .spline([
+            .rect(self.wing_s1_spacer_width, self.wing_s1_thickness)
-                (0, self.wing_r1_height),
+            .finalize()
-                (0.5 * self.wing_r1_width, self.wing_r1_height - factor * bend),
+            .extrude(self.wing_s1_spacer_thickness)
-                (self.wing_r1_width, self.wing_r1_height - bend),
-            ])
-            .segment(
-                (self.wing_r1_width, self.wing_r1_height - bend),
-                (self.wing_r1_width, -bend),
-            )
-            .spline([
-                (self.wing_r1_width, - bend),
-                (0.5 * self.wing_r1_width, - factor * bend),
-                (0, 0),
-            ])
-            .assemble()
         )
+        result.faces("<Z").tag("mate1")
+        result.faces(">Z").tag("mate2")
+        result.faces(">Y").tag("dir")
         return result
 
-    def wing_r1(self) -> Cq.Solid:
+    @target(name="wing/r1s1", kind=TargetKind.DXF)
-        profile = self.wing_r1_profile()
+    def wing_r1s1_profile(self) -> Cq.Sketch:
+        return MW.wing_r1s1_profile()
+
+    def wing_r1s1_panel(self, front=True) -> Cq.Workplane:
+        profile = self.wing_r1s1_profile()
+        anchors = [
+            ("shoulder_bot", 10, 10),
+            ("middle", 50, -20),
+            ("tip", 390, -150),
+        ]
         result = (
             Cq.Workplane("XY")
             .placeSketch(profile)
             .extrude(self.panel_thickness)
-            .val()
         )
+        plane = result.faces(">Z" if front else "<Z").workplane()
+        sign = 1 if front else -1
+        tag_direction = "+Y" if front else "-Y"
+        for name, px, py in anchors:
+            plane.moveTo(px, sign * py).tagPlane(name)
+            #plane.moveTo(px, sign * py).tagPlane(f"{name}_dir", direction=tag_direction)
         return result
 
     ######################
@@ -405,6 +415,29 @@ class Parameters(Model):
         )
         return result
 
+    def wing_r1s1_assembly(self) -> Cq.Assembly:
+        result = (
+            Cq.Assembly()
+            .add(self.wing_r1s1_panel(front=True), name="panel_front",
+                 color=self.material_panel.color)
+            .add(self.wing_r1s1_panel(front=False), name="panel_back",
+                 color=self.material_panel.color)
+            .constrain("panel_front@faces@>Z", "panel_back@faces@<Z", "Point",
+                       param=self.wing_s1_thickness)
+        )
+        for tag in ["shoulder_bot", "middle", "tip"]:
+            (
+                result
+                .add(self.wing_s1_spacer(), name=f"{tag}_spacer",
+                     color=self.material_bracket.color)
+                .constrain(f"panel_front?{tag}", f"{tag}_spacer?mate1", "Plane")
+                .constrain(f"panel_back?{tag}", f"{tag}_spacer?mate2", "Plane")
+            )
+
+        result.solve()
+        return result
+
+
     def wing_r1_assembly(self) -> Cq.Assembly:
         result = (
             Cq.Assembly()

nhf/touhou/houjuu_nue/wing.py

@@ -226,3 +226,34 @@ def wing_root(joint: HirthJoint,
              loc=Cq.Location((0, 0, -joint.total_height)))
     )
     return result
+
+def wing_r1s1_profile() -> Cq.Sketch:
+    """
+       Generates the first wing segment profile, with the wing root pointing in
+       the positive x axis.
+       """
+    # Depression of the wing middle
+    h = 100
+    w = 400
+    bend = 200
+    factor = 0.7
+    result = (
+        Cq.Sketch()
+        .segment((0, 0), (0, h))
+        .spline([
+            (0, h),
+            (0.5 * w, h - factor * bend),
+            (w, h - bend),
+        ])
+        .segment(
+            (w, h - bend),
+            (w, -bend),
+        )
+        .spline([
+            (w, - bend),
+            (0.5 * w, - factor * bend),
+            (0, 0),
+        ])
+        .assemble()
+    )
+    return result

nhf/utils.py

@@ -6,6 +6,7 @@ Adds the functions to `Cq.Workplane`:
 2. `tagPlane`
 """
 import cadquery as Cq
+from typing import Union, Tuple
 
 
 def tagPoint(self, tag: str):
@@ -18,12 +19,16 @@ def tagPoint(self, tag: str):
 Cq.Workplane.tagPoint = tagPoint
 
 
-def tagPlane(self, tag: str, axis='Z'):
+def tagPlane(self, tag: str,
+             direction: Union[str, Cq.Vector, Tuple[float, float, float]] = '+Z'):
     """
     Adds a phantom `Cq.Edge` in the given location which can be referenced in a
     `Axis`, `Point`, or `Plane` constraint.
     """
+    if isinstance(direction, str):
         x, y, z = 0, 0, 0
+        assert len(direction) == 2
+        sign, axis = direction
         if axis in ('z', 'Z'):
             z = 1
         elif axis in ('y', 'Y'):
@@ -32,7 +37,16 @@ def tagPlane(self, tag: str, axis='Z'):
             x = 1
         else:
             assert False, "Axis must be one of x,y,z"
-    edge = Cq.Edge.makeLine((-x, -y, -z), (x, y, z))
+        if sign == '+':
+            sign = 1
+        elif sign == '-':
+            sign = -1
+        else:
+            assert False, "Sign must be one of +/-"
+        v = Cq.Vector(x, y, z) * sign
+    else:
+        v = Cq.Vector(direction)
+    edge = Cq.Edge.makeLine(v * (-1), v)
     self.eachpoint(edge.moved, useLocalCoordinates=True).tag(tag)
 
 Cq.Workplane.tagPlane = tagPlane