Dynamic Modeling, Correction, and Experimental Verification of Spur Gears with Faults

Spur gears is a critical aspect of gear system performance, particularly when faults such as cracks and pitting occur. Understanding the dynamics under such conditions is essential for fault diagnosis and system reliability. In this article, we explore the process of modeling the dynamics of spur gears, correcting these models with real-world experimental data, and verifying their accuracy. The study focuses on the influence of different failure modes—such as cracks and pitting—on the meshing stiffness and vibration responses of spur gears.

1. Introduction

Spur gears are essential components in many mechanical systems, and their performance directly influences the efficiency and stability of these systems. However, when faults such as cracks or pitting occur, the dynamic behavior of the gears changes, leading to increased vibrations and potential system failure. The challenge lies in accurately modeling these dynamic changes, particularly in systems with multiple failure modes. This study proposes a comprehensive approach to model and correct the dynamics of spur gears, incorporating time-varying meshing stiffness and real-world experimental data for validation.

2. Modeling Spur Gear Dynamics

To analyze the dynamic behavior of spur gears, we start by establishing a coupled vibration model that considers bending and torsional vibrations. This model uses lumped parameters to describe the system and incorporates the elasticity of the transmission shaft and supporting bearings. The system is modeled as a six-degree-of-freedom (DOF) planar vibration system, where the four translational DOFs and two rotational DOFs are crucial for understanding gear behavior during operation.

2.1 Generalized Displacement Vector

The generalized displacement vector for the spur gear system is represented as:{δ}={xp,yp,θp,xg,yg,θg}T\{ \delta \} = \{ x_p, y_p, \theta_p, x_g, y_g, \theta_g \}^T{δ}={xp​,yp​,θp​,xg​,yg​,θg​}T

Where:

  • xp,ypx_p, y_pxp​,yp​ represent the displacements of the driving gear.
  • xg,ygx_g, y_gxg​,yg​ represent the displacements of the driven gear.
  • θp,θg\theta_p, \theta_gθp​,θg​ are the angular displacements of the driving and driven gears, respectively.

2.2 Dynamic Meshing Forces

The dynamic meshing force between the two gears is influenced by the time-varying meshing stiffness, which is calculated based on the relative displacement between the gears at the meshing point. The forces acting on the gears are given by:Fp=cmy˙+kmyF_p = c_m \dot{y} + k_m yFp​=cm​y˙​+km​y Fg=−Fp=−cmy˙−kmyF_g = -F_p = -c_m \dot{y} – k_m yFg​=−Fp​=−cm​y˙​−km​y

Where cmc_mcm​ is the meshing damping coefficient, and kmk_mkm​ is the time-varying meshing stiffness.

3. Time-Varying Meshing Stiffness Calculation

The time-varying meshing stiffness of spur gears depends on various factors, including gear tooth deformation, base body deformation, and contact deformation. The calculation of meshing stiffness involves several energy components, including:

  • Bending energy UbU_bUb​
  • Shear energy UsU_sUs​
  • Axial compression energy UaU_aUa​
  • Hertzian contact energy UhU_hUh​
  • Base body deformation energy UfU_fUf​

Each energy component is associated with its respective stiffness value, which is calculated using material and geometric properties of the gear teeth. For example, the bending stiffness KbK_bKb​ is calculated as:Kb=∫0l[(l−x)cos⁡αp−hsin⁡αp]2EIxdxK_b = \int_0^l \left[ (l-x) \cos \alpha_p – h \sin \alpha_p \right]^2 \frac{E I_x}{dx}Kb​=∫0l​[(l−x)cosαp​−hsinαp​]2dxEIx​​

Where lll is the length of the gear tooth, αp\alpha_pαp​ is the pressure angle, and IxI_xIx​ is the inertia moment.

3.1 Crack-Induced Stiffness Variation

Cracks in gears typically initiate at the root of the tooth, leading to stress concentration and changes in the gear’s meshing stiffness. The crack’s effect is modeled by simplifying its shape as a line and adjusting the inertia moment and cross-sectional area based on the crack’s position and depth.

3.2 Pitting-Induced Stiffness Variation

Pitting, which occurs due to surface fatigue, causes small indentations on the gear teeth. This failure mode results in changes to the effective contact area and meshing stiffness, particularly near the pitch circle. Pitting damage is modeled as rectangular indentations, and its effect on meshing stiffness is calculated by adjusting the effective contact width and area.

4. Simulation and Analysis

Using the aforementioned dynamic model and time-varying meshing stiffness values, simulations were carried out for spur gears under different fault conditions, including normal gears, cracked gears, and pitted gears. The simulation results were then compared with experimental data to validate the model’s accuracy.

4.1 Normal Gear Response

For normal gears, the meshing stiffness remains relatively consistent, with no significant deviations. The vibration response in both the time domain and frequency domain shows smooth, regular patterns, with the primary frequencies being the mesh frequency and its harmonics.

4.2 Cracked Gear Response

When cracks are introduced into the gear, the meshing stiffness decreases in the affected regions, leading to a periodic decrease in vibration amplitude. The simulation results show that the crack depth directly affects the degree of stiffness reduction, with deeper cracks causing more pronounced changes in the vibration signal.

4.3 Pitted Gear Response

Pitting also alters the meshing stiffness, although the effects are less pronounced compared to cracks. The simulation shows that the meshing stiffness decreases in the regions affected by pitting, leading to minor fluctuations in the vibration response. However, these changes are subtle and require careful analysis to detect.

5. Model Correction and Experimental Verification

To improve the accuracy of the dynamic model, we employed a model correction technique using experimental vibration data. The experimental setup involved a gear test rig where vibration signals were collected from gears with different failure types. The system’s stiffness and damping parameters were adjusted based on the frequency response functions obtained from the experimental data.

5.1 Experimental Setup

The test rig was equipped with a high-precision accelerometer to measure vibrations along the radial direction. Vibration signals were collected under different operating conditions and failure types, including normal, cracked, and pitted gears. The data was processed using time-synchronous averaging (TSA) to eliminate noise and enhance the signal clarity.

5.2 Comparison of Simulation and Experimental Data

The corrected model showed a good agreement with the experimental results. In the time domain, the vibration amplitude matched closely, with both the simulation and experimental data exhibiting similar trends. In the frequency domain, the mesh frequency and its harmonics were consistently present, and the frequencies corresponding to failure modes (such as crack-induced modulation) were also detected.

6. Conclusion

This study successfully demonstrated a dynamic modeling approach for spur gears with faults, incorporating time-varying meshing stiffness and real-world experimental validation. The results showed that the model could accurately simulate the dynamic behavior of spur gears under different failure conditions, providing valuable insights for fault diagnosis and system monitoring.

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