Gear Shaving Technology for Spiroid Face Gears: Theory and Experimental Research

Spiroid face gear drives constitute a novel spatial crossed-axis transmission system comprising an involute spiroid pinion and a spiroid face gear. These systems offer advantages including high contact ratios (often exceeding 2.0), compact structure, high transmission ratios (ranging 10:1–400:1), low noise, and robust load-bearing capacity. Spiroid face gears are typically manufactured via die-casting for applications like fishing reels. However, mold precision limitations and thermal distortions result in poor surface quality (Ra ≈ 0.8 μm), accelerating wear and degrading transmission performance. This research introduces precision gear shaving as a post-casting solution.

Mathematical Foundation of Spiroid Face Gear Tooth Surfaces

The tooth surface of the spiroid face gear (Σ₂) is generated through the envelope of an imaginary pinion cutter (Σ_c). The pinion cutter’s involute helicoid surface equations in coordinate system $S_c$ are:

$$ \mathbf{r}_c^{(k)} = \begin{bmatrix}
r_b \cos(\theta_c \pm \mu_c \sin\lambda_b) \\
r_b \sin(\theta_c \mp \mu_c \cos\lambda_b) \\
p_c \mu_c \\
1
\end{bmatrix} $$
$$ \mathbf{n}_c^{(k)} = \begin{bmatrix}
\sin\lambda_b \sin\theta_c \\
-\sin\lambda_b \cos\theta_c \\
\mp \cos\lambda_b
\end{bmatrix} \quad (k=I, II) $$

where $r_b$ is base radius, $\lambda_b$ is base helix angle, $p_c$ is helix parameter, $\mu_c$ and $\theta_c$ are surface parameters. Coordinate systems for generation (Fig. 1) define the spatial relationship between cutter and gear. The meshing equation is derived from the orthogonality condition between the relative velocity $\mathbf{v}_c^{(c2)}$ and surface normal $\mathbf{n}_c$:

$$ f_c^{(k)} = \mathbf{n}_c^{(k)} \cdot \mathbf{v}_c^{(c2)} = 0 $$
$$ \mathbf{v}_c^{(c2)} = \mathbf{v}_c^{(c)} – \mathbf{v}_c^{(2)} = (\boldsymbol{\omega}_c – \boldsymbol{\omega}_2) \times \mathbf{r}_c – \boldsymbol{\omega}_2 \times \mathbf{R} $$

The gear tooth surface Σ₂ is then expressed parametrically:

$$ \mathbf{r}_2 = \mathbf{M}_{2c}(\phi_c) \mathbf{r}_c, \quad f_c^{(k)}(\mu_c, \theta_c, \phi_c) = 0 $$

Tooth geometry is constrained by undercutting and pointing avoidance. The minimum inner radius $L_1$ preventing undercutting solves:

$$ F(\mu_c, \theta_c, \phi_c) = \begin{vmatrix}
\frac{\partial f}{\partial \mu_c} & \frac{\partial f}{\partial \theta_c} & \frac{\partial f}{\partial \phi_c} \\
\frac{\partial x_c}{\partial \mu_c} & \frac{\partial x_c}{\partial \theta_c} & \frac{\partial x_c}{\partial \phi_c} \\
\frac{\partial y_c}{\partial \mu_c} & \frac{\partial y_c}{\partial \theta_c} & \frac{\partial y_c}{\partial \phi_c}
\end{vmatrix} = 0 \quad \text{at} \quad \theta_c^* = \sqrt{\frac{r_{ac}^2 – r_{bc}^2}{r_{bc}}} $$

The maximum outer radius $L_2$ preventing pointing is determined by solving:

$$ \mathbf{r}_2^{(I)} = \mathbf{r}_2^{(II)}, \quad z_2 = -r_{fc} $$

Design Parameter Symbol Value
Pinion Teeth $N_c$ 7
Normal Module $m_n$ 0.65 mm
Min Inner Radius $L_1$ 11.7 mm
Max Outer Radius $L_2$ 14.5 mm

Gear Shaving Principle and Kinematic Model

Gear shaving utilizes a modified involute spiroid pinion as a shaving cutter. The cutter features axial slots creating cutting edges at the intersection with the tooth flank. The kinematic model (Fig. 2) involves three motions:

  1. Cutter rotation ($\omega_s$) about axis $z_s$
  2. Workpiece rotation ($\omega_g^*$) driven by the cutter
  3. Radial feed ($v_{s0}$) along the gear’s radius

The corrected workpiece angular velocity accounts for radial feed:

$$ \omega_g^* = m_{gs} \omega_s – \frac{N_s}{N_g p_s} v_{s0} \quad \text{where} \quad m_{gs} = \frac{N_g}{N_s} $$

The relative velocity $\mathbf{v}_{sg}$ in coordinate system $S_s$ is:

$$ \mathbf{v}_{sg} = \begin{bmatrix}
\omega_s y_s – \omega_g^* \cos\phi_s (z_s + l_0 + \Delta l) – \omega_g^* \sin\phi_s E \\
-\omega_s x_s + \omega_g^* \sin\phi_s (z_s + l_0 + \Delta l) – \omega_g^* \cos\phi_s E \\
v_{s0} + \omega_g^* (\cos\phi_s x_s – \sin\phi_s y_s)
\end{bmatrix} $$

The meshing equation for gear shaving becomes:

$$ f_{sg}^{(k)} = \mathbf{n}_s^{(k)} \cdot \mathbf{v}_{sg} = 0 \quad (k=I, II) $$

The generated gear surface during gear shaving is:

$$ \mathbf{r}_g^{(k)} = \mathbf{M}_{gs}(\phi_s) \mathbf{r}_s^{(k)}, \quad f_{sg}^{(k)}(\mu_s, \theta_s, \phi_s) = 0 $$

Shaving Cutter Design and Manufacturing

The cutter material is W6Mo5Cr4V2 high-speed steel (HRC 63-66). Key geometric parameters calculated via helical gear formulas are:

Parameter Symbol Value
Normal Module $m_n$ 0.65 mm
Teeth Number $N_s$ 7
Pressure Angle $\alpha_n$ 20°
Helix Angle $\beta$ 52° (LH)
Tip Diameter $d_{as}$ 6.25 mm
Root Diameter $d_{fs}$ 4.46 mm
Slot Width $B_s$ 1.0 mm
Slot Depth $H_s$ 2.0 mm

Axial rectangular slots were machined (Fig. 3). Manufacturing tolerances adhered to AGMA 12 standards:

$$ \Delta f_h \leq 0.004 \text{mm}, \quad \Delta F_{\beta} = \pm 0.006 \text{mm}, \quad \Delta f_{pb} = \pm 0.003 \text{mm} $$

Numerical Control Simulation of Gear Shaving

A 5-axis CNC machine model (X, Y, Z, A, C) was built in VERICUT. The simulation workflow comprised:

  1. Machine modeling: Defined kinematics chain $$ \text{Base} \rightarrow \text{Y} \rightarrow \text{X} \rightarrow \text{A} \rightarrow \text{Fixture} \rightarrow \text{Workpiece} $$
    $$ \text{Base} \rightarrow \text{Z} \rightarrow \text{C} \rightarrow \text{Spindle} \rightarrow \text{Cutter} $$
  2. Tool/Workpiece Import: STEP models of cutter and blank
  3. G-code generation for synchronized motion:
N6 R1=0 R2=0 R3=44.2872535 R4=0 
N7 A=R1 C=R2 Z=R3 
N8 MARK: R1=11.07653*R4 R2=57.29578*R4 R3=R3-0.0001 R4=R4+0.006 
      A=R1 C=R2 Z=R3 
N9 IF R3>=38.287 GOTOB MARK

Simulation results (Fig. 4) confirmed the theoretical tooth form. Deviation analysis showed:

$$ \Delta_{\text{max}}^{\text{working flank}} = 9.8 \mu\text{m}, \quad \Delta_{\text{root}} \approx 25 \mu\text{m} \text{(non-contact)} $$

Experimental Validation and Surface Analysis

Gear shaving experiments used a CNC machining center with parameters:

Parameter Value
Spindle Speed 2000 rpm
Radial Feed ($v_{s0}$) 50 mm/min
Axis Angle ($\gamma_m$) 90°
Offset ($E$) 7 mm

Surface roughness was measured using InfiniteFocus G5 optical profilometer:

Surface Ra Before Shaving (μm) Ra After Shaving (μm) Reduction
Concave Flank 0.8365 0.6311 24.6%
Convex Flank 0.8527 0.6419 24.7%

The significant Ra reduction validated gear shaving effectiveness for die-cast spiroid gears.

Conclusions and Future Work

This research established a complete methodology for gear shaving of spiroid face gears:

  1. Mathematical models for tooth generation and gear shaving kinematics were derived
  2. Axial-slot shaving cutters were designed/manufactured
  3. VERICUT simulations verified CNC toolpaths (deviation < 9.8μm)
  4. Experiments demonstrated 24.6% surface roughness reduction

Future work will focus on:

  • Cutter flank modification for localized bearing contact
  • Dynamics analysis under gear shaving-modified surface topography
  • Groove optimization on concave flanks for vibration suppression
  • Extended durability testing of shaved gear pairs

The proposed gear shaving technique enables high-quality finishing of die-cast spiroid gears using standard CNC equipment, enhancing performance in precision transmission systems.

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