Coexisting Attractors and Bifurcation Dynamics in Single-Stage Spur Gears

Spur gear pairs are fundamental components in a vast array of mechanical power transmission systems. Their dynamic performance directly influences the overall efficiency, noise, vibration, and longevity of the machinery. Consequently, the nonlinear dynamics of gear systems, accounting for factors such as time-varying mesh stiffness, static transmission error, and backlash, have been a subject of enduring interest in mechanical engineering. The study of single-degree-of-freedom models is particularly valuable, offering both theoretical insights and practical significance for understanding the complex behavior inherent in spur gears. This article delves into the intricate global dynamics of a single-stage spur gear pair, with a specific focus on the phenomena of coexisting attractors, their stability, bifurcations, and the resulting complex system behaviors like chaotic crises.

The dynamic response of spur gears is inherently nonlinear and non-smooth due to the periodic nature of the mesh stiffness and the piecewise characteristic introduced by gear backlash. Traditional analysis methods, including the incremental harmonic balance method, the A-operator method, and numerical integration, have been extensively employed to study periodic solutions and chaotic motions. However, these approaches often focus on the asymptotic, stable attractors reachable from common initial conditions. This can obscure the full picture of the system’s global dynamics, leaving hidden attractors—both stable and unstable—undiscovered. The coexistence of multiple attractors for the same parameter set means that the final steady-state motion depends critically on the initial conditions, a property with significant implications for system design and operational robustness.

This work aims to comprehensively reveal the global dynamics of a single-stage spur gear system. We construct a Poincaré map to reduce the continuous system to a discrete mapping. To uncover the complete set of periodic attractors, we employ a synergistic approach combining the initial cell mapping method, the continuation shooting method, and direct numerical simulation. This allows us to solve for and track the evolution of coexisting attractors, including unstable periodic orbits that are invisible to standard simulation. The stability of periodic solutions is determined via Floquet theory by calculating the eigenvalues of the Jacobian matrix derived from the Poincaré map. Furthermore, we utilize the cell mapping method to compute the basins of attraction, visually depicting the regions in state space that lead to different final attractors. Our analysis uncovers rich dynamical phenomena, including abundant multi-attractor coexistence, period-doubling cascades, saddle-node bifurcations, and, critically, non-smooth bifurcation events such as saddle-node-type grazing bifurcations and boundary/internal crises of chaotic attractors. These findings provide a deeper, more complete understanding of the dynamic landscape of spur gear pairs, offering valuable guidance for parameter design, optimization, and performance evaluation to ensure reliable and quiet operation.

Dynamic Model of the Spur Gear Pair

The physical model under consideration is a single-stage spur gear transmission system. The system incorporates key nonlinear and non-smooth features that characterize real spur gears: time-varying mesh stiffness, static transmission error, and gear backlash. A schematic representation of the model is considered, where $I_i$, $r_{bi}$, and $\theta_i$ (for $i=1,2$) denote the moment of inertia, base circle radius, and angular displacement of the driving and driven gears, respectively. $C_g$ represents the mesh damping. The nonlinearities are introduced through the periodic mesh stiffness $K(t)$ and the composite static transmission error $e(t)$. The non-smoothness arises from the constant gear backlash of magnitude $2D$.

By applying Newton’s second law and employing a standard normalization procedure, the dimensionless equation of motion for the relative gear mesh displacement $x$ can be derived as:

$$
\ddot{x} + 2\xi\dot{x} + (1 + k \cos(\omega t)) \, g(x, d) = F + \varepsilon \omega^2 \cos(\omega t)
$$

Here, $\xi$ is the damping ratio, $k$ is the amplitude of the time-varying mesh stiffness, $\varepsilon$ is the amplitude of the transmission error fluctuation, $F$ is the dimensionless torque load, and $\omega$ is the dimensionless meshing frequency. The function $g(x, d)$ is the piecewise-linear backlash function. Using the backlash half-width $D$ as the nominal scale ($d=1$), it is defined as:

$$
g(x) =
\begin{cases}
x – 1, & x > 1 \\
0, & |x| \le 1 \\
x + 1, & x < -1
\end{cases}
$$

This function divides the phase space into three distinct regions: $G_1 = \{ (x, \dot{x}): x > 1 \}$ (driving-side contact), $G_2 = \{ (x, \dot{x}): |x| \le 1 \}$ (backlash or no contact), and $G_3 = \{ (x, \dot{x}): x < -1 \}$ (driven-side contact).

Table 1: Key Parameters of the Spur Gear Model
Parameter Symbol Description
Dynamic Transmission Error $x$ Dimensionless relative displacement
Damping Ratio $\xi$ Ratio of mesh damping to critical damping
Stiffness Modulation Amplitude $k$ Amplitude of time-varying mesh stiffness
Error Amplitude $\varepsilon$ Amplitude of static transmission error
Torque Load $F$ Dimensionless mean load
Meshing Frequency $\omega$ Dimensionless excitation frequency
Backlash Half-width $d$ Normalized gear backlash (typically $d=1$)

Analytical and Numerical Methods for Global Dynamics

To analyze the global dynamics of this non-smooth system, we employ a Poincaré map framework combined with advanced numerical techniques for tracking solutions and their stability.

Let $\mathbf{u} := (x, \dot{x})^T \in \mathbb{R}^2$ denote the state vector. The system’s trajectory is $\mathbf{u}(t) = (x(t), \dot{x}(t))^T$. We define the Poincaré section $\Pi_0 = \{ (\mathbf{u}, t) \in \mathbb{R}^2 \times \mathbb{S} \, | \, \text{mod}(t, 2\pi/\omega) = 0 \}$, which samples the state at discrete times corresponding to the period of the parametric excitation. The associated Poincaré map is denoted as $P: \Pi_0 \rightarrow \Pi_0$.

The non-smooth boundaries $\Sigma_1 = \{ \mathbf{u}: x = 1 \}$ and $\Sigma_2 = \{ \mathbf{u}: x = -1 \}$ partition the phase space. We define local maps $P_1: \mathbf{u}_{10} \mapsto \mathbf{u}_{11}$, $P_2: \mathbf{u}_{20} \mapsto \mathbf{u}_{21}$, and $P_3: \mathbf{u}_{30} \mapsto \mathbf{u}_{31}$, where the subscripts $0$ and $1$ indicate initial and final points within a specific region $G_i$. Since the vector field is continuous across boundaries, the Jacobian for a local map describing contact with and release from a boundary is the identity matrix. A full-period Poincaré map is thus a composition of these local maps. For instance, a period-$n$ orbit starting in $G_1$ and traversing $G_1 \rightarrow G_2 \rightarrow G_3 \rightarrow G_2 \rightarrow G_1$ is described by:

$$
P_{\Pi_0 \rightarrow \Pi_0} = P’_1 \circ P’_2 \circ P_3 \circ P_2 \circ P_1
$$

where $P’_i$ are the appropriate return segments. The Jacobian matrix $D\mathbf{P}$ of the full Poincaré map, required for Floquet stability analysis, is the product of the Jacobians of the constituent local maps and identity matrices at crossing events. It can be computed by integrating the matrix differential equation:

$$
\frac{d}{dt}\left( \frac{\partial \mathbf{u}(t)}{\partial \mathbf{u}_0} \right) = \frac{\partial \mathbf{f}}{\partial \mathbf{u}} \cdot \frac{\partial \mathbf{u}(t)}{\partial \mathbf{u}_0}, \quad \text{with} \quad \frac{\partial \mathbf{u}(t_0)}{\partial \mathbf{u}_0} = \mathbf{I}
$$

along the trajectory, where $\mathbf{f}$ is the vector field of the system.

Our methodology for investigating coexisting attractors involves three key steps, considering a bifurcation parameter $v$ (e.g., $\omega$ or $k$):

  1. Initial Cell Mapping & Shooting: For a fixed parameter value $v=v_0$, we discretize a region of interest on the Poincaré section $\Pi_0$ into a grid of cells. Each grid point serves as an initial guess for a periodic point (a fixed point of $P$). We apply a shooting method combined with Newton-Raphson iteration to solve $P(\mathbf{u}_0) – \mathbf{u}_0 = 0$ for each guess. The stability of each found periodic orbit is determined by computing the eigenvalues (Floquet multipliers) $\lambda$ of $D\mathbf{P}$. The orbit is stable if all multipliers lie inside the unit circle ($|\lambda| < 1$). This process reveals all coexisting periodic attractors and repellors within the scanned region.
  2. Numerical Continuation: Starting from each periodic solution found at $v=v_0$, we employ a parameter continuation algorithm (a predictor-corrector scheme) to trace the evolution of the solution branch as $v$ is varied incrementally within an interval $[v_1, v_2]$. This traces out bifurcation diagrams, identifying points where stability changes (bifurcations) occur, such as when a multiplier crosses $+1$ (saddle-node, SN) or $-1$ (period-doubling, PD).
  3. Validation and Chaos Detection: The branches of stable periodic solutions obtained via continuation are validated using direct numerical integration (e.g., 4th/5th order Runge-Kutta). Furthermore, numerical simulation is used to explore regions where periodic solutions lose stability and to detect chaotic attractors, which are visualized by their Poincaré points.
  4. Basin of Attraction Analysis: For parameters where multiple attractors (periodic or chaotic) coexist, we employ the cell mapping method to compute their basins of attraction. The state space region is divided into cells, and the long-term fate of trajectories starting from each cell center is determined via simulation. This graphically reveals the intricate boundaries separating domains of influence for different attractors.

Results: Coexisting Attractors, Bifurcations, and Crises

We present detailed results for two distinct parameter sets to illustrate the rich dynamics of the spur gear system.

Case 1: Frequency Variation ($\omega$)

Set parameters: $k=0.1$, $\varepsilon=0.2$, $\xi=0.04$, $F=0.05$. The bifurcation parameter is the meshing frequency $\omega \in [0.20, 1.20]$. The composite bifurcation diagram, synthesizing results from continuation of all found periodic branches and numerical simulation, reveals an extraordinarily complex landscape with extensive multi-attractor coexistence.

Key observations from the diagram include:

  • Multiple Stable Periodic Orbits: Up to four different stable period-1 orbits (labeled P1, Q1, R1, S1) coexist in narrow windows of $\omega$, alongside higher-period and chaotic attractors. For example, at $\omega=0.3950$, nine distinct periodic orbits coexist: four stable period-1, three unstable period-1, one stable period-4, and one unstable period-4.
  • Bifurcation Mechanisms: Saddle-node (SN) bifurcations are responsible for the birth and annihilation of pairs of periodic orbits (one stable, one unstable). Period-doubling (PD) bifurcations cause a change in stability, often initiating a cascade towards chaos.
  • Non-Smooth Grazing Bifurcation: A critical phenomenon is observed for the P1 branch near $\omega \approx 0.4725$. As $\omega$ increases, the purely in-contact P1 orbit undergoes a grazing bifurcation (GR) where its trajectory becomes tangent to the backlash boundary $\Sigma_1$ ($x=1$). Immediately following this, a saddle-node bifurcation (SN$_1$) occurs. This grazing-induced saddle-node bifurcation is a continuous bifurcation (the grazing point) that triggers a discontinuous jump in the system’s steady-state. It also introduces hysteresis: when decreasing $\omega$ from above the SN point, the system follows a different stable branch (T1) than when increasing $\omega$ from below (P1 branch). The parameter gap $\Delta \omega$ between GR and SN$_1$ is极小 (on the order of $5 \times 10^{-4}$).

The Floquet multiplier criterion confirms bifurcation types. For instance, at a period-doubling point, one multiplier crosses the unit circle at $\lambda = -1$.

Case 2: Stiffness Variation ($k$)

Set parameters: $\omega=0.50$, $\varepsilon=0.2$, $\xi=0.05$, $F=0.10$. The bifurcation parameter is the stiffness variation amplitude $k \in [0.0, 1.80]$.

This case highlights another crucial global phenomenon: chaotic crises. As $k$ increases, a stable period-2 orbit undergoes a period-doubling cascade to chaos. Subsequently, a saddle-node bifurcation (SN$_3$) creates a new pair of period-2 orbits. The unstable period-2 orbit from this pair resides on the boundary of the chaotic attractor’s basin. As $k$ increases further, the chaotic attractor expands until it collides with this unstable periodic orbit on the basin boundary. This collision leads to a boundary crisis, causing the sudden destruction of the chaotic attractor and its basin. The system’s long-term behavior abruptly switches to the coexisting stable period-2 motion.

Later, another chaotic attractor emerges from a different period-doubling route. This attractor undergoes a sudden, discontinuous expansion in size without colliding with a basin boundary orbit. This is characteristic of an internal crisis, which differs from its counterpart in smooth systems as the collision partner is not necessarily a periodic orbit within the attractor’s interior.

Basin of Attraction Structures

The cell-mapping analysis of basins provides profound insight into the system’s global stability and the mechanisms behind crises.

  • Fractal Basins and Sensitivity: When chaotic and periodic attractors coexist, their basins are often intricately interwoven, exhibiting fractal boundaries. This indicates high sensitivity to initial conditions, where minute changes can lead to radically different final states.
  • Crisis Visualization: The evolution of basins leading to a boundary crisis is clear: the chaotic attractor’s basin grows, “eating into” the basin of the periodic attractor, until the chaotic attractor itself touches its basin boundary (marked by the unstable manifold of a saddle periodic orbit). At the crisis parameter, the chaotic basin vanishes.
  • Role of Unstable Orbits: Unstable periodic orbits created by saddle-node bifurcations often lie on basin boundaries. In contrast, those born from period-doubling bifurcations typically reside inside the basin (or attractor). This distinction is critical; collisions with boundary-set unstable orbits cause boundary crises, fundamentally altering the system’s available asymptotic states.

Discussion and Conclusions

The investigation into the nonlinear dynamics of a single-stage spur gear pair reveals a dynamical landscape of remarkable complexity, far richer than what is captured by analyzing only the primary harmonic response or stable attractors found from typical initial conditions. The synergy of the initial cell mapping, continuation, and basin analysis methods has been essential in unveiling this hidden structure.

The primary conclusions of this study are as follows:

  1. Ubiquitous Coexistence of Attractors: Under a wide range of operational parameters, spur gear systems exhibit multi-stability, where several periodic and chaotic attractors coexist. The final operational state is therefore history-dependent and sensitive to initial conditions, such as those induced by startup transients or disturbances. This has direct implications for predicting noise and vibration levels.
  2. Non-Smooth Bifurcations: The piecewise-linear nature of the backlash nonlinearity introduces distinctive bifurcation phenomena. The saddle-node-type grazing bifurcation is a salient feature where a continuous grazing event precipitates a discontinuous saddle-node bifurcation, leading to abrupt jumps in the system response and associated hysteresis loops. This mechanism can trigger sudden transitions between quiet (in-contact) and noisy (impacting) operating regimes in spur gears.
  3. Global Crises: Chaotic motions in gear systems are not merely curiosities but can undergo sudden metamorphoses via crises. Boundary crises, caused by the collision of a chaotic attractor with the stable manifold of a saddle periodic orbit on its basin boundary, can lead to the sudden disappearance of chaos, potentially “suddenly” stabilizing the system or transferring it to another remote attractor. Internal crises cause sudden expansions of chaotic attractors, significantly altering the amplitude and spectral characteristics of vibration.
  4. Design Implications: From a practical standpoint, these findings caution against designs operating in parameter regions with:
    • Extremely fractal or intermingled basins, where performance is unpredictable.
    • Proximity to grazing-induced bifurcations, which are points of high susceptibility to jumps and hysteresis.
    • Proximity to crisis points, where small parameter variations can cause large, discontinuous changes in dynamic response.

    Design should aim for robust, mono-stable operating regions with smooth basins of attraction.

In summary, this comprehensive analysis provides a new perspective for fully revealing the dynamics of spur gear pairs. By accounting for the complete set of coexisting attractors and their global bifurcations, including those stemming from non-smooth interactions, we gain a more predictive understanding of system behavior. This knowledge forms a vital theoretical foundation for the optimal design, parameter selection, and condition monitoring of gear transmissions, ultimately contributing to the development of more reliable, efficient, and quiet mechanical systems.

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