Dynamic Response Analysis of Spur Gears with Multi-Faults Considering Tooth Root Transition Curve

In the field of mechanical engineering, spur gears are widely used in various transmission systems due to their simplicity and efficiency. However, these gear systems are prone to failures such as cracks, pitting, and missing teeth, which can lead to significant dynamic responses and operational issues. Traditional dynamic models often overlook the precise geometry of the tooth root transition curve, leading to inaccuracies in calculating time-varying meshing stiffness. In this study, I propose an enhanced dynamic modeling approach that integrates tooth deformation, gear matrix deformation, contact deformation, and the actual tooth root transition curve. This method aims to improve the accuracy and efficiency of time-varying meshing stiffness calculations for spur gears under multiple fault conditions. By establishing a coupled vibration analysis model and deriving stiffness computation methods, I simulate the dynamic responses of gears with various faults and validate the results through experimental comparisons. The findings demonstrate that the proposed model reliably captures fault-induced vibrations in both time and frequency domains, offering valuable insights for fault diagnosis and system integrity in spur gear applications.

The dynamic behavior of spur gears is primarily influenced by time-varying meshing stiffness, which arises from the alternating single and double tooth engagement during operation. Numerous studies have focused on stiffness calculation and vibration analysis. For instance, early research introduced energy-based methods to compute meshing stiffness, while subsequent works incorporated additional factors like shear potential energy and gear matrix deformation. However, many of these approaches simplified the tooth root transition curve, potentially compromising accuracy. Recent advancements by researchers have addressed this by refining stiffness calculations to account for realistic tooth geometries and fault conditions. In this work, I build upon these developments by explicitly considering the tooth root transition curve in the stiffness model, enabling a more precise representation of spur gear dynamics under faults like cracks, pitting, and missing teeth. This comprehensive approach not only enhances computational efficiency but also provides a robust framework for analyzing multi-fault scenarios in spur gear systems.

To model the dynamic response of spur gears, I developed a coupled vibration analysis model that accounts for translational and rotational motions. The governing equations are derived using a lumped parameter approach, considering factors such as mesh stiffness, damping, and support conditions. The dynamic equations for the gear pair can be expressed as follows:

$$m_p \ddot{x}_p + c_{px} \dot{x}_p + k_{px} x_p = F_f$$
$$m_g \ddot{x}_g + c_{gx} \dot{x}_g + k_{gx} x_g = F_f$$
$$m_p \ddot{y}_p + c_{py} \dot{y}_p + k_{py} y_p = F_p$$
$$m_g \ddot{y}_g + c_{gy} \dot{y}_g + k_{gy} y_g = F_g$$
$$I_p \ddot{\theta}_p = T_p + M_p – F_p R_p$$
$$I_g \ddot{\theta}_g = -T_g + M_g + F_g R_g$$

Here, \(m_p\) and \(m_g\) represent the masses of the driving and driven spur gears, respectively, while \(I_p\) and \(I_g\) denote their moments of inertia. The terms \(R_p\) and \(R_g\) are the base circle radii, and \(k_m\) and \(c_m\) are the time-varying meshing stiffness and damping. The support stiffness and damping in the x and y directions are given by \(k_{px}\), \(k_{gx}\), \(k_{py}\), \(k_{gy}\), \(c_{px}\), \(c_{gx}\), \(c_{py}\), and \(c_{gy}\). The external torques are \(T_p\) and \(T_g\), and \(F_f\) is the friction force at the mesh interface. The dynamic mesh forces \(F_p\) and \(F_g\) are calculated as:

$$F_p = -F_g = c_m \dot{y} + k_m y$$

Solving these equations allows for the analysis of the dynamic response of spur gears under various operating conditions. The accuracy of this model heavily relies on the precise computation of time-varying meshing stiffness, which I will elaborate on in the following sections.

The time-varying meshing stiffness of spur gears is a critical parameter that significantly influences their dynamic behavior. I employ an energy method to compute this stiffness, considering the gear tooth as a non-uniform cantilever beam. The total deformation at the meshing point comprises three main components: tooth deformation, gear matrix deformation, and contact deformation. The tooth deformation itself includes bending, shear, and axial compression deformations. For a meshing force \(F\) applied at a point on the tooth, the bending deformation \(\delta_b\) is given by:

$$\delta_b = F \int_0^l \frac{[(l – x) \cos \alpha_p – h \sin \alpha_p]^2}{E I_x} dx$$

The shear deformation \(\delta_s\) and axial compression deformation \(\delta_a\) are expressed as:

$$\delta_s = F \int_0^l \frac{1.2 \cos^2 \alpha_p}{G A_x} dx$$
$$\delta_a = F \int_0^l \frac{\sin^2 \alpha_p}{E A_x} dx$$

In these equations, \(E\) is the elastic modulus, \(G\) is the shear modulus, \(I_x\) is the area moment of inertia at distance \(x\) from the tooth root, and \(A_x\) is the cross-sectional area. The geometric parameters \(l\), \(\alpha_p\), and \(h\) define the tooth profile and engagement conditions. For spur gears, the tooth root transition curve is particularly important, as it affects the stress distribution and deformation. I model this curve using parametric equations that describe the transition from the involute profile to the root fillet. For a standard spur gear, the transition curve can be represented as:

$$x = r \cos \phi – \left( \frac{a_1}{\sin \gamma} + r_p \right) \sin(\gamma – \phi)$$
$$y = r \sin \phi – \left( \frac{a_1}{\sin \gamma} + r_p \right) \cos(\gamma – \phi)$$

Here, \(r\) is the pitch radius, \(r_p\) is the tip radius of the cutting tool, \(a_1\) is the distance from the tool tip to the midline, and \(\gamma\) and \(\phi\) are angular parameters. This detailed representation allows for a more accurate calculation of \(I_x\) and \(A_x\) along the tooth height, which is essential for precise stiffness evaluation in spur gears.

Additionally, the deformation due to the gear matrix \(\delta_f\) is calculated using empirical formulas derived from previous studies:

$$\delta_f = \frac{F \cos^2 \alpha_p}{W E} \left[ L^* \left( \frac{u_f}{s_f} \right)^2 + M^* \left( \frac{u_f}{s_f} \right) + P^* (1 + Q^* \tan^2 \alpha_p) \right]$$

where \(W\) is the tooth width, and \(L^*\), \(M^*\), \(P^*\), and \(Q^*\) are coefficients that depend on the gear geometry. The contact deformation \(\delta_h\), based on Hertzian theory, is:

$$\delta_h = \frac{4 F (1 – \nu^2)}{\pi E W}$$

where \(\nu\) is Poisson’s ratio. The total deformation \(\delta\) at the meshing point is the sum of these components:

$$\delta = \delta_b + \delta_s + \delta_a + \delta_f + \delta_h$$

Thus, the equivalent meshing stiffness \(K_j^i\) for a tooth pair \(i\) at contact point \(j\) is:

$$K_j^i = \frac{F}{\delta} = \frac{F}{\delta_{t1} + \delta_{f1} + \delta_{t2} + \delta_{f2} + \delta_h}$$

where subscripts 1 and 2 refer to the driving and driven spur gears, respectively. This formulation ensures that the time-varying meshing stiffness accurately reflects the actual gear geometry, which is crucial for dynamic analysis.

When faults are present in spur gears, the meshing stiffness undergoes significant changes. For crack faults, which often initiate at the tooth root, the area moment of inertia \(I_x\) and cross-sectional area \(A_x\) are modified. In the case of a through-root crack, these parameters are adjusted as follows:

$$I_x = \begin{cases}
\frac{1}{12} (h_x + h_x)^3 W & \text{if } h_x \leq h_q \\
\frac{1}{12} (h_x + h_q)^3 W & \text{if } h_x > h_q
\end{cases}$$
$$A_x = \begin{cases}
(h_x + h_x) W & \text{if } h_x \leq h_q \\
(h_x + h_q) W & \text{if } h_x > h_q
\end{cases}$$

Here, \(h_q = h_c – q_0 \sin \alpha_c\), where \(q_0\) is the crack length, \(\alpha_c\) is the crack angle, and \(h_c\) is the distance from the crack start point to the tooth centerline. These modifications capture the reduction in stiffness due to cracking, which is essential for accurate dynamic modeling of faulty spur gears.

For pitting faults, which involve surface damage, the changes in cross-sectional area \(\Delta A_x\) and moment of inertia \(\Delta I_x\) are defined based on the pit dimensions. If a pit has length \(a_s\), width \(W_s\), and height \(h_s\), and is centered at a distance \(\mu\) from the tooth root, then:

$$\Delta W_x = \begin{cases}
W_s & \text{if } x \in \left[ \mu – \frac{a_s}{2}, \mu + \frac{a_s}{2} \right] \\
0 & \text{otherwise}
\end{cases}$$
$$\Delta A_x = \begin{cases}
\Delta W_x h & \text{if } x \in \left[ \mu – \frac{a_s}{2}, \mu + \frac{a_s}{2} \right] \\
0 & \text{otherwise}
\end{cases}$$
$$\Delta I_x = \begin{cases}
\frac{1}{12} \Delta W_x h^3 + \frac{A_x \Delta A_x (h_x – \frac{h}{2})^2}{A_x – \Delta A_x} & \text{if } x \in \left[ \mu – \frac{a_s}{2}, \mu + \frac{a_s}{2} \right] \\
0 & \text{otherwise}
\end{cases}$$

The updated parameters are \(I’_x = I_x – \Delta I_x\), \(A’_x = A_x – \Delta A_x\), and \(W’_x = W – \Delta W_x\). These adjustments allow the model to account for the localized stiffness reduction caused by pitting in spur gears.

In the case of missing teeth, the meshing stiffness is altered by removing the contribution of the affected tooth from the engagement cycle. This transforms double-tooth contact regions into single-tooth contact and single-tooth regions into no contact, leading to abrupt changes in stiffness and increased dynamic impacts. By incorporating these fault-specific modifications, the proposed method enables a comprehensive analysis of multi-fault scenarios in spur gears.

To validate the dynamic model, I conducted simulations and experiments on a parallel spur gearbox. The gear parameters are summarized in Table 1, which includes details such as tooth numbers, module, pressure angle, and inertial properties. The driving gear operates at 1800 rpm, resulting in a meshing frequency of 690 Hz. The support stiffness and damping values were identified through model updating and are used in the simulations.

Table 1: Key Parameters of the Spur Gears Used in the Study
Parameter Driving Gear Driven Gear
Number of Teeth 23 84
Module (mm) 2 2
Pressure Angle (°) 20 20
Tooth Width (mm) 20 20
Mass (kg) 0.22 1.9
Moment of Inertia (kg·m²) 4.858 × 10⁻⁵ 3.509 × 10⁻³
Rotational Speed (rpm) 1800 493

For crack fault analysis, I simulated a gear with a root crack of depth 1 mm and angle 45°. The dynamic responses, including acceleration signals, were obtained and compared to experimental data. In the time domain, the simulation results show periodic impacts corresponding to the fault, while frequency domain analysis reveals increased amplitudes at shaft-related frequencies and sidebands around the meshing frequency harmonics. These characteristics align with experimental observations, confirming the model’s accuracy in capturing crack-induced vibrations in spur gears.

For pitting faults, I modeled a surface pit with dimensions 1 mm length, 10 mm width, and 0.5 mm depth located at the pitch point. The simulation outputs indicate minor vibrations in the time domain, with frequency spectra dominated by meshing frequency harmonics and minimal sidebands. This subtle response is consistent with experimental data, where pitting causes less severe impacts compared to other faults. However, the model successfully identifies the fault presence, demonstrating its sensitivity for early-stage damage detection in spur gears.

Missing tooth faults result in significant dynamic changes, as evidenced by large impacts in the time domain simulations. The frequency spectra show numerous sidebands around the meshing frequency, often overshadowing the harmonic components. Experimental validations corroborate these findings, with audible impacts and broad sideband distributions. This agreement underscores the model’s capability to handle severe fault conditions in spur gears.

To further illustrate the fault effects, Table 2 compares the key dynamic characteristics observed in simulations and experiments for different fault types. This summary highlights how each fault influences the vibration response of spur gears, providing a reference for fault diagnosis.

Table 2: Dynamic Response Characteristics of Spur Gears Under Various Faults
Fault Type Time Domain Features Frequency Domain Features Simulation-Experiment Consistency
Crack Periodic impacts Prominent shaft frequency components and sidebands High
Pitting Minor amplitude fluctuations Meshing harmonics with low-amplitude sidebands Moderate
Missing Tooth Large impulsive peaks Extensive sidebands masking harmonics High

In conclusion, the proposed dynamic modeling approach for spur gears, which incorporates the tooth root transition curve, offers significant improvements in calculating time-varying meshing stiffness and analyzing multi-fault responses. The method accounts for various deformation mechanisms and fault conditions, enabling accurate simulations that align with experimental results. For crack and missing tooth faults, the model clearly captures the fault-induced vibrations in both time and frequency domains. Although pitting faults produce subtler effects, the model still identifies them reliably. This work underscores the importance of precise geometry representation in spur gear dynamics and provides a foundation for developing comprehensive fault databases. Future research could focus on enhancing the model for very slight pitting faults and extending it to other gear types, further advancing the reliability of gear transmission systems.

The mathematical formulations and computational techniques presented here are grounded in energy principles and dynamic theory. For instance, the total energy potential in the spur gear system can be expressed as the sum of elastic and kinetic components. Using Hamilton’s principle, the equations of motion are derived, ensuring consistency with the dynamic model. The time-varying stiffness \(k_m(t)\) is periodic and can be expanded into Fourier series to analyze its harmonic effects on the system response. For a spur gear with \(N\) teeth, the fundamental frequency of stiffness variation is \(N\) times the rotational frequency, which directly influences the vibration spectrum. By integrating these analytical insights with numerical simulations, I achieve a robust framework for spur gear fault diagnosis, contributing to the broader goal of improving mechanical system durability and performance.

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