Optimization of Meshing Performance in Plane Enveloping Internal Worm Gear Drives through Analysis of the Generating Plane Inclination Angle

In the vast field of power transmission, the worm gear drive stands as a cornerstone technology, renowned for its ability to achieve high reduction ratios within compact spaces while offering significant torque transmission and operational precision. Its applications are critical across numerous sectors, including aerospace, robotics, military equipment, and precision instrumentation. Traditional worm gear drives, primarily of the external meshing type, have served well. However, the evolving demands of modern machinery, particularly the need for compact, high-capacity drives capable of powering multiple outputs from a single input shaft, necessitate innovative architectural solutions. My investigation focuses on a novel variant: the plane enveloping internal meshing worm gear drive. This configuration utilizes a unique geometry where a plane (the generating plane) envelopes the worm thread, and meshing occurs internally with the worm wheel. This fundamental shift enables a single internal worm to drive multiple radially arranged worm wheels simultaneously, a feature with profound implications for multi-output systems in robotics, agricultural machinery, and complex mechanical assemblies.

The performance of any worm gear drive is critically dependent on its geometric design parameters. For the plane enveloping internal type, the angle at which the generating plane is oriented relative to the worm axis—termed the generating plane inclination angle (β)—is a paramount design variable. This angle fundamentally dictates the shape of the worm thread and the consequent contact conditions during meshing. An optimal selection of β is therefore essential to minimize contact stresses, reduce wear, improve load distribution, and ultimately enhance the durability and efficiency of the drive. This work is dedicated to a thorough analytical and numerical exploration of the influence of the generating plane inclination angle on the meshing characteristics of this novel worm gear drive. The primary metric for this assessment is the induced normal curvature at the contact point, a key determinant of contact pressure according to Hertzian theory.

1. Theoretical Foundation of the Internal Meshing Worm Gear Drive

1.1 Coordinate System Establishment

To mathematically describe the kinematics and geometry of the plane enveloping internal worm gear drive, a comprehensive set of coordinate systems is established. Figure 1 illustrates these systems. A fixed global coordinate system Sf (Ofif, jf, kf) serves as the reference frame. The worm is associated with a moving coordinate system S1 (O1i1, j1, k1), which rotates about its axis k1 with an angular velocity ω1. The worm wheel is fixed to another moving coordinate system S2 (O2i2, j2, k2), rotating about k2 with angular velocity ω2. The center distance is denoted by A.

The generating plane Σ, which is the tool surface that forms the worm thread, is defined in an auxiliary coordinate system S0 (O0i0, j0, k0). Its orientation is defined by the key parameter, the generating plane inclination angle β. The origin O0 is located on the base circle of the worm wheel blank with a radius r. A local contact coordinate system Sp (Ope1, e2, e3) is attached to the instantaneous contact point P on plane Σ, where P is defined by coordinates (0, u, v) in S0. The worm wheel is installed with a fixed tilt angle δF relative to the worm axis. The number of worm threads is z1 and the number of worm wheel teeth is z2, giving a transmission ratio ic = z1/z2 during the generation process. The instantaneous rotation angles are φ1 for the worm and φ2 for the worm wheel, related by φ2 = ic φ1.

1.2 Coordinate Transformations and Meshing Equation

The spatial relationship between the worm and worm wheel is governed by coordinate transformation matrices. The transformation from the worm wheel system S2 to the worm system S1 is given by:

$$
\mathbf{M}_{21} =
\begin{bmatrix}
p_1 + l_2 p_2 & l_2 p_4 – p_3 & -l_1 g_2 & A g_1 \\
l_2 p_3 – p_4 & p_2 + l_2 p_1 & -l_1 g_1 & -A g_2 \\
l_1 h_2 & l_1 h_1 & l_2 & 0 \\
0 & 0 & 0 & 1
\end{bmatrix}
$$

where:
$$
g_1 = \cos \phi_1, \quad g_2 = \sin \phi_1, \quad h_1 = \cos \phi_2, \quad h_2 = \sin \phi_2
$$
$$
l_1 = \cos \delta_F, \quad l_2 = \sin \delta_F, \quad p_1 = g_1 h_1, \quad p_2 = g_2 h_2, \quad p_3 = g_1 h_2, \quad p_4 = g_2 h_1
$$

The transformation from the generating plane system S0 to the worm wheel system S2 is:

$$
\mathbf{M}_{02} =
\begin{bmatrix}
0 & 1 & 0 & 0 \\
-\cos \beta & 0 & -\sin \beta & r \\
-\sin \beta & 0 & \cos \beta & 0 \\
0 & 0 & 0 & 1
\end{bmatrix}
$$

The fundamental condition for proper meshing in a worm gear drive is that the common normal vector at the contact point must be perpendicular to the relative velocity vector of the two surfaces at that point. This leads to the meshing equation:

$$
\Phi = \mathbf{v}^{(12)} \cdot \mathbf{n} = 0
$$

For the plane Σ, the unit normal vector in S0 is constant: n = (1, 0, 0). The relative velocity vector v(12) between the worm (1) and worm wheel (2) must be derived in S0. The components (x0v, y0v, z0v) of this vector in S0 are complex functions of the design parameters (A, β, δF, r, ic) and the motion parameters (u, v, φ2). Solving the meshing equation Φ=0 for the coordinate v yields a relation of the form:

$$
v = \frac{B_1(u, \phi_2, A, \beta, \delta_F, i_c, r)}{B_2(\phi_2, \delta_F)}
$$

where B1 and B2 are expressions derived from the velocity components. This equation signifies that for a given point defined by parameter u on the generating line and at a given wheel rotation angle φ2, the v-coordinate of the actual contact point is determined, ensuring conjugacy.

1.3 Tooth Surface Equations

The tooth surfaces of both the worm and the worm wheel are generated as the locus of all contact points. The surface of the worm, Σ1, is found by transforming the contact point from S0 to the worm coordinate system S1:

$$
[\mathbf{r}_1, 1]^T = \mathbf{M}_{21} \cdot \mathbf{M}_{02} \cdot [\mathbf{r}_p, 1]^T
$$

Similarly, the worm wheel tooth surface, Σ2, is found by transforming to the worm wheel system S2:

$$
[\mathbf{r}_2, 1]^T = \mathbf{M}_{02} \cdot [\mathbf{r}_p, 1]^T
$$

Together with the meshing equation v = B1/B2 and defining u as a running parameter (u = c, where c is a constant for a specific contact line) and φ2 = icφ1, these equations fully define the conjugate surfaces of the plane enveloping internal worm gear drive. This mathematical model allows for the generation of 3D CAD models and is the basis for all subsequent performance analysis.

1.4 Induced Normal Curvature

The local contact condition between the two tooth surfaces is critically assessed through the induced normal curvature, k(12). This parameter directly influences the size of the contact ellipse and, according to Hertzian contact theory, the maximum contact stress. A lower absolute value of induced normal curvature generally leads to lower contact stress and better load distribution, which are desirable traits for a durable worm gear drive.

The general formula for the induced normal curvature along a given direction on the contact normal is derived from differential geometry and kinematics of meshing surfaces:

$$
k^{(12)} = \frac{(\boldsymbol{\omega}^{(12)} \times \mathbf{n}) \cdot \mathbf{v}^{(12)} – \mathbf{v}^{(12)} \cdot \left( \frac{d\mathbf{n}}{ds} \right)}{\Psi}
$$

where ω(12) is the relative angular velocity vector, and Ψ is a first-order function related to the derivative of the meshing function. For the specific case of the plane enveloping worm gear drive, after substantial derivation and simplification, the induced normal curvature at a contact point can be expressed as a function of the design and motion parameters:

$$
k^{(12)} = f(u, v, \phi_2, A, \beta, \delta_F, i_c, r)
$$

Given that v itself is determined by the meshing equation, the induced curvature ultimately depends on the choice of u (position along the tooth profile), φ2 (angular position), and the core design parameters: A, β, δF, ic, and r. This establishes the functional link between the generating plane inclination angle β and the meshing performance metric k(12).

2. Analysis of the Generating Plane Inclination Angle’s Influence

2.1 Methodology and Baseline Parameters

To isolate and understand the effect of the generating plane inclination angle β, a systematic numerical analysis is performed. The core of the investigation involves calculating the induced normal curvature k(12) over a wide range of β (0° to 90°) while varying other critical parameters such as the worm wheel tooth number z2 (which changes ic) and the center distance A. The analysis focuses on single-start worms (z1 = 1), as the conclusions can be generalized to multi-start designs. The baseline fixed parameters are chosen to represent a realistic design space:

Parameter Symbol Baseline Value
Center Distance A 80 mm
Worm Wheel Tilt Angle δF 35°
Base Circle Radius r 23 mm
Worm Start Number z1 1

A critical step is selecting a representative contact point for analysis. Investigation reveals that the induced normal curvature varies along the tooth profile. Analysis of a full contact line shows that the curvature is highest near the root of the worm wheel tooth (corresponding to the tip of the worm thread) and decreases linearly towards the worm wheel tip. Since the highest curvature (and thus potentially the highest contact stress) occurs at the root, this region is most critical for durability. Therefore, the parameter u is fixed at its minimum value, umin, corresponding to the worm wheel root diameter, ensuring the analysis targets the worst-case meshing condition. For a worm wheel with addendum diameter da = 67 mm and dedendum diameter df = 62 mm, umin is calculated as:

$$
u_{\text{min}} = \sqrt{(d_f/2)^2 – r^2} \approx 57.6 \text{ mm}
$$

The induced normal curvature k(12) is then computed for different worm wheel rotation angles φ2 across the mesh cycle.

2.2 Influence of Worm Wheel Tooth Number (Transmission Ratio)

First, the center distance A is held constant at 80 mm, and the worm wheel tooth number z2 is varied. This changes the transmission ratio ic = 1/z2. The induced normal curvature is calculated for β ranging from 0° to 90°. The results are summarized in the table below, which shows the value of |k(12)| at a mid-range rotation angle (φ2 = 30°) for different combinations of z2 and β.

β (deg) |k(12)| for z2=30 (1/mm) |k(12)| for z2=40 (1/mm) |k(12)| for z2=50 (1/mm) |k(12)| for z2=60 (1/mm)
0 0.0152 0.0141 0.0134 0.0129
10 0.0128 0.0115 0.0107 0.0101
18 0.0105 0.0092 0.0084 0.0078
24 0.0091 0.0079 0.0071 0.0066
30 0.0083 0.0071 0.0064 0.0059
36 0.0082 0.0070 0.0063 0.0058
42 0.0088 0.0075 0.0068 0.0063
54 0.0121 0.0103 0.0093 0.0086
72 0.0245 0.0208 0.0187 0.0173

The data clearly shows a trend. For any given worm wheel tooth number (z2), the magnitude of the induced normal curvature first decreases as β increases from 0°, reaches a minimum in a specific range, and then increases again as β continues to increase. The region where |k(12)| attains its lowest values consistently lies between approximately β = 18° and β = 36°. Within this band, the curvature values are significantly lower than those at smaller or larger angles. For example, at z2=40, |k(12)| is 0.0092 1/mm at β=18° and 0.0070 1/mm at β=36°, compared to 0.0141 1/mm at β=0° and 0.0208 1/mm at β=72°. This represents a reduction of 35-50% in curvature magnitude within the optimal band, which would translate to a substantial reduction in contact stress according to Hertzian theory, directly benefiting the performance and life of the worm gear drive.

2.3 Influence of Center Distance

To verify the robustness of the observed optimal range for β, the analysis is repeated with the worm wheel tooth number fixed at z2 = 40, while the center distance A is varied. This changes the overall scale of the gear set. The results for |k(12)| at φ2 = 30° are presented in the following table.

β (deg) |k(12)| for A=60mm (1/mm) |k(12)| for A=80mm (1/mm) |k(12)| for A=100mm (1/mm) |k(12)| for A=120mm (1/mm)
0 0.0188 0.0141 0.0113 0.0094
10 0.0153 0.0115 0.0092 0.0077
18 0.0123 0.0092 0.0074 0.0062
24 0.0106 0.0079 0.0064 0.0053
30 0.0095 0.0071 0.0057 0.0048
36 0.0093 0.0070 0.0056 0.0047
42 0.0099 0.0075 0.0060 0.0050
54 0.0137 0.0103 0.0082 0.0069
72 0.0277 0.0208 0.0167 0.0139

The trend observed with varying center distance A strongly corroborates the finding from the transmission ratio study. Regardless of the center distance—whether it is a compact 60 mm design or a larger 120 mm drive—the induced normal curvature is minimized within the same band of generating plane inclination angles, approximately 18° to 36°. While the absolute value of curvature decreases with increasing center distance (due to larger gear dimensions), the relative improvement offered by the optimal β range remains pronounced. For instance, at A=100 mm, selecting β=36° (|k(12)|=0.0056 1/mm) over β=0° (|k(12)|=0.0113 1/mm) reduces the curvature by over 50%. This consistent pattern across different geometric scales confirms that the identified optimal range for β is a fundamental characteristic of this type of worm gear drive, not an artifact of a specific size.

2.4 Physical Interpretation and Link to Contact Stress

The significance of minimizing the induced normal curvature is directly linked to the contact mechanics of the worm gear drive. According to the classical Hertz theory for contact between elastic bodies, the maximum contact stress σH for a line contact (closely approximated by gear teeth) is given by:

$$
\sigma_H = \sqrt{ \frac{F_n E^* |k^{(12)}|}{\pi l} }
$$

where Fn is the normal load per unit length, l is the length of the contact line, and E* is the effective elastic modulus of the worm and wheel materials. The equation clearly shows that the contact stress is proportional to the square root of the induced normal curvature:

$$
\sigma_H \propto \sqrt{|k^{(12)}|}
$$

Therefore, reducing |k(12)| has a direct and favorable impact on reducing the peak contact stress. A reduction in |k(12)| by a factor of 2, as commonly observed when choosing an optimal β, would lead to a reduction in contact stress by a factor of √2, or about 29%. This can dramatically increase the load-carrying capacity and the fatigue life (pitting resistance) of the gear set. The analysis conclusively demonstrates that selecting the generating plane inclination angle within the 18° to 36° range is a highly effective strategy for optimizing the meshing conditions and enhancing the structural performance of the plane enveloping internal worm gear drive.

3. Conclusions and Implications for Worm Gear Drive Design

Through a rigorous application of gear meshing theory and numerical analysis, this investigation has elucidated the critical role of the generating plane inclination angle in determining the meshing performance of the novel plane enveloping internal worm gear drive. The primary conclusions are as follows:

1. The induced normal curvature, a key indicator of contact pressure, varies significantly along the tooth profile in this worm gear drive. It is highest at the root of the worm wheel (tip of the worm) and decreases towards the tip of the worm wheel. This establishes the worm wheel root/worm tip region as the most critically loaded zone.

2. The generating plane inclination angle β has a profound and systematic effect on the induced normal curvature. For a wide range of design parameters—specifically, varying worm wheel tooth numbers (z2 from 30 to 60) and center distances (A from 60 mm to 120 mm)—the curvature exhibits a clear minimum within a specific range of β.

3. The optimal range for the generating plane inclination angle is identified to be between 18° and 36°. Within this interval, the plane enveloping internal worm gear drive operates with minimized induced normal curvature compared to designs with smaller or larger angles. This optimal range appears to be a fundamental characteristic of this gear geometry, largely independent of the specific transmission ratio or scale defined by the center distance.

4. The reduction in induced normal curvature achieved by selecting β within the optimal 18°-36° range directly translates to lower Hertzian contact stresses according to the proportionality σH ∝ √|k(12)|. This leads to several performance benefits for the worm gear drive: increased load-carrying capacity, improved resistance to surface fatigue (pitting), and potentially longer operational life.

The findings of this study provide a solid theoretical foundation and a practical guideline for the design and optimization of plane enveloping internal worm gear drives. By constraining the generating plane inclination angle to the identified optimal band, designers can proactively enhance the meshing performance and durability of this innovative transmission system. This knowledge is particularly valuable as this type of worm gear drive, with its inherent capability for multi-output configuration, finds expanding applications in advanced mechanical systems requiring compact, robust, and efficient power transmission solutions. Future work should explore the interaction of the generating plane inclination angle with other parameters, such as the worm wheel tilt angle δF and pressure angle, to develop a comprehensive multi-parameter optimization strategy for this promising class of worm gear drive.

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