Cosplay/nhf/touhou/houjuu_nue/__init__.py

from dataclasses import dataclass
import unittest
import cadquery as Cq

@dataclass(frozen=True)
class Parameters:

    """
    Thickness of the exoskeleton panel in millimetres
    """
    panel_thickness: float = 25.4 / 16

    # Wing root properties
    """
    Radius of the mounting mechanism of the wing root. This is constrained by
    the size of the harness.
    """
    root_radius: float = 60

    """
    Heights for various wing joints, where the numbers start from the first joint.
    """
    wing_r1_height = 100
    wing_r1_width = 400
    wing_r2_height = 100
    wing_r3_height = 100

    def wing_r1_profile(self) -> Cq.Sketch:
        """
        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()
            .segment((0, 0), (0, self.wing_r1_height))
            .spline([
                (0, self.wing_r1_height),
                (0.5 * self.wing_r1_width, self.wing_r1_height - factor * bend),
                (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()
        )
        return result

    def wing_root(self,
                  side_width=30,
                  side_height=100) -> Cq.Shape:
        """
        Generate the wing root which contains a Hirth joint at its base and a
        rectangular opening on its side, with the necessary interfaces.
        """
        result = (
            Cq.Workplane("XY")
            .circle(self.root_radius)
            .transformed(offset=Cq.Vector(80, 0, 80),
                         rotate=Cq.Vector(0, 45, 0))
            .rect(side_width, side_height)
            .loft()
            .val()
        )
        return result