Literature Review on Fault Mechanism Analysis and Diagnosis Methods for Main Pump Systems
Abstract
1. Introduction
2. Main Pump Systems and Analysis of Typical Failure Mechanisms
2.1. Analysis of Structural Composition and Functions of the Main Pump
2.2. Analysis of Typical Failure Mechanism
2.2.1. Failure Mechanism of Bearing System
- Rolling bearing failure: Rolling bearing failure primarily manifests as pitting, spalling, and cage fracture, primarily caused by contact fatigue under alternating stress [37,38]. The underlying mechanisms are as follows: Lei et al. [39,40] confirmed that cooling water intrusion into lubricants leads to oil film rupture, causing direct metal-to-metal wear; the generated wear particles further exacerbate surface spalling. Under elevated temperatures (>120 °C), bearing steel underwent annealing-induced softening, with a 20–30% decrease in hardness, thereby accelerating fatigue crack propagation. Chen et al. [41] developed a nonlinear dynamic model that revealed the sensitivity of whirl trajectory to slip: a 15% increase in the amplitude in the X-direction resulted in more than a 40% increase in the roller-raceway slip ratio. This whirl effect leads to oscillations of the minimum oil film thickness and micropitting under boundary lubrication conditions. Li et al. [42] further reported that the coupling of centrifugal force and gyroscopic moment triggered atypical spalling of aeroengine main shaft bearings under high-speed, light-load conditions. This spalling was characterized by axially distributed fish-scale cracks, distinct from the radial spalling typical of traditional Hertzian contact fatigue. Patil et al. [43] established a theoretical model that quantified the relationship between pitting size and harmonic components of the vibration spectrum, although multi-defect coupling was not taken into account. Cao et al. [26] extended the model and demonstrated through a five-degree-of-freedom rotor-bearing system simulation that multi-point damage can excite a 2–5 kHz high-frequency resonance band. However, the requirement of preset defect locations limited its engineering applicability. Recent research has focused on the optimization of fatigue life models and slip dynamics. Zhai et al. [44] proposed a performance degradation assessment model based on cluster migration distance, enabling early fatigue failure warning through vibration signal feature extraction. Xia et al. [45] combined machine learning algorithms, such as SVM and cluster analysis, to improve fault classification accuracy; however, reliance on high-quality labeled data constrains its engineering generalization ability. Lee et al. [46] verified that insufficient lubrication and misalignment are the primary causes of overheating failure and verified that abnormal temperature rises can be monitored in real time using infrared thermal imaging.
- Failure mechanism of sliding bearing: The failure mechanisms of sliding bearings, which rely on hydrodynamic lubrication to form a load-bearing oil film, primarily include oil film rupture, vortex instability, and material adhesion [47,48,49]. Wang et al. [50] identified rotor eccentricity as a factor causing uneven lubricant flow, which in turn induces half-speed whirl and self-excited vibration. Antunović et al. [51] reported that solid particles embedded in the babbitt bushing can initiate scratching and plastic deformation. McKee et al. [52] demonstrated that local overheating softens the bearing alloy, leading to micro-welding with the journal. Recent research has further advanced the understanding of wear mechanisms, abrasive wear thermal runaway, and eddy instability. Traditional theory predicts a vortex frequency at half the power frequency; however, Wang et al. [50], using CFD simulation, found that turbulence in water-lubricated bearings at 15.4 MPa reduces the frequency to 0.48 times the power frequency, attributing the discrepancy to previously neglected fluid inertia effects. König et al. [53] demonstrated through acoustic emission signal analysis that particles larger than 5 μm can penetrate the oil film and embed into the soft liner, with embedding depth increasing under higher loads. This particle embedding can elevate the wear rate by 300%. Wang et al. [50] attributed wear primarily to fluid inertia forces, while Chen et al. [41] argued that the flexible deformation of the bearing housing plays a more predominant role. Current microscopic models address a single adhesion mechanism but fail to predict macroscopic lifetimes, whereas phenomenological models like the Archard equation rely heavily on empirical coefficients and therefore lack universality [53,54].
- Failure mechanism of mating interface: The failure of mating interfaces primarily manifests as interference-fit loosening, fretting wear, and interfacial debonding, typically caused by preload imbalance [55]. These failures can significantly reduce structural stiffness, trigger abnormal vibrations, and accelerate fatigue crack propagation. Li et al. [56] confirmed through residual stress analysis that concentrated interfacial shear stress during thermal cycling is the dominant cause of package module cracking. Needleman’s [57] continuum model identified two debonding modes: ductile matrix and brittle interface. Dong et al. [58] showed through simulations that wear at the interference-fit edge of a hollow shaft was 150% greater than that of a solid shaft, due to uneven contact stress distribution resulting from the lower stiffness of the hollow structure. Additionally, wear depth predicted by the Archard equation indicated a shift in the crack initiation site from the fit edge to the interior, leading to a 40% reduction in the fatigue life for hollow shafts compared with solid ones. Recent studies on molecular and medium dynamics have focused on understanding the mechanisms of interface failure. Zhou et al. [59] argued that atomic bond fracture energy is the dominant factor, whereas Needleman [57] maintained that stress triaxiality T is the key parameter. The core challenge remains the absence of cross-scale correlation models, hindering the integration of micro-parameters into engineering criteria. Nonetheless, consensus exists that debonding is governed by intrinsic strength and stress state, fretting wear results from the interaction of kinematics and material response, preload must be dynamically aligned with interference, and insights from molecular dynamics regarding bond fracture should be incorporated into continuum-scale models.
2.2.2. Failure Mechanism of Sealing System
- Mechanical seal failure: The mechanical seal is a critical component that forms a dynamic seal through contact between the rotating and stationary ring faces. Its failure primarily manifests as end-face wear, thermal cracking, and auxiliary system malfunction [63,64]. The predominant cause is dry running, where insufficient lubrication leads to a sudden increase in frictional heat at the sealing surfaces, resulting in thermoelastic instability, surface deformation, and the initiation of microcracks [52,61]. Shaft vibration further exacerbates the misalignment of the sealing surfaces, leading to localized contact stresses that exceed the material’s yield limit and accelerate fatigue failure [46,65]. Antunović et al. [51] and Chittora [61] reported that the leakage from seal face clearances originates from the transmission of bearing vibration to the seal assemblies. Additionally, long-term operation can generate microcracks in sealing materials due to cyclic fatigue stress, leading to grease loss and a reduction in interface compression force, as observed by Berezhansky et al. [33]. Seal performance is particularly vulnerable under extreme conditions compared with conventional conditions. Lee et al. [46] demonstrated that during low-temperature start-up, the increased viscosity of sealing grease can result in dry friction at the seal interface, raising the wear rate by 40% compared with standard operating conditions.
- Packing seal failure mechanism: The sealing performance of packed glands relies on the axial compression force to induce radial expansion of the soft packing material, thereby filling the gap between the shaft and sleeve. However, the failure of such seals is often attributed to a combination of packing wear, thermal hardening, and stress relaxation [66]. Continuous friction between the packing and sleeve causes progressive material wear, enlarging the clearance and ultimately leading to leakage. Microscopic analysis by Bistriceanu et al. [65] revealed that aramid fiber packing subjected to cyclic loading experienced fiber fracture, resulting in a 12% reduction in sealing pressure. Furthermore, high-temperature conditions promote thermal hardening of the filler resin matrix, reducing its elastic deformability. Makay et al. [67] reported a 40% decrease in compression resilience in braided fillers above 120 °C, whereas metal foil fillers exhibited high-temperature resistance but caused increased journal wear. Additionally, relaxation of the bolt preload can cause uneven gland pressure, thereby inducing medium leakage along preferential paths within the packing layer. The nuclear main pump experiences thermal shock during a loss-of-coolant accident. Azarm et al. [68] demonstrated through a probabilistic model that vulcanized rubber hardens when the seal ring material’s temperature gradient exceeds 200 °C/min, tripling the probability of elastic failure compared with normal conditions. Under high-pressure scenarios, Taylor [69] found that the Octagonal Gasket Flange relaxes due to the bolt temperature hysteresis, reducing the sealing compression force by 15–20%. Additionally, extreme pressure fluctuations expand the plastic deformation area of the gasket.
2.2.3. Failure Mechanism of Hydraulic Components
- Impeller damage: The impeller’s high-speed rotation propels the fluid, with its structural integrity crucial for maintaining head and efficiency. Common failures include blade fracture, cavitation, and wear. Bennekom et al. [75,76] identified casting defects as the primary cause of blade fractures. Zaman et al. [77] attributed cavitation mainly to bubble collapse in low-pressure regions impacting the blade surface. Zhou et al. [78] demonstrated that cavitation leads to impeller surface erosion and induces high-frequency impact vibrations, as revealed by vibration signal analysis. Numerical simulations by Gong et al. [79] indicated that the distribution of low-pressure regions is directly related to the geometry of the impeller inlet. Wang et al. [80] observed that during temperature transients, the cavitation erosion rate of PWR main pumps increases significantly, elevating the risk of seal failure. Tao and Li [81,82] highlighted that off-design operations, such as low load, can easily trigger flow separation and secondary flows, exacerbating hydraulic losses. For instance, under low-flow conditions, centrifugal pump outlet flow exhibits marked asymmetry, leading to head drop and the formation of a hump characteristic. Concurrently, Przybyla et al. [83] demonstrated that leading-edge wear results from foreign body impact or erosion by solid–liquid two-phase flow, as evidenced by aviation compressor impeller notch analysis. A central debate concerns the universality of cavitation prediction models. Wu et al. [84] argued that existing models lack adaptability to multiphase flow conditions and fail to capture the microscopic fatigue characteristics of materials.
- Guide vane failure: Guide vanes are essential fluid machinery components, serving to rectify flow and reduce vortex losses. The adjustment of their opening significantly affects pump efficiency and stability. Common issues associated with guide vanes include wear, deformation, and flow-induced vibration [85,86]. Wear is primarily caused by particle-laden fluid scouring [87], while deformation mainly results from fatigue accumulation [50] under high-frequency eddy loading. Visual experiments conducted by Song et al. [87] demonstrated that the wear rate of guide vanes increased with greater opening, and the maximum wear area is located on the blade pressure surface, showing a positive correlation with fluid sediment concentration. Wang et al. [50] highlighted that high-frequency whirl in water-lubricated guide bearings can be transmitted to the guide vanes, inducing resonance and accelerating structural fatigue. Two-dimensional holography has demonstrated that the vertical rotation axis of a vertical Reactor Coolant Pump is lubricated by high-pressure water, which can lead to water film whirl faults. The characteristic frequency of this whirl is 0.48 times the power frequency, and the whirl amplitude can exceed 50%. Under normal conditions, the water film vortex can be suppressed by damping forces [88,89], but in extreme environments, the coupling of random fluid disturbance forces with the system’s natural frequency can readily induce resonance instability [89,90,91].
- Wear of the mouth ring: Wear leads to increased clearance, diminishing efficiency and amplifying vibration [92]. Primary causes of wear include material mismatch in friction pairs and particle invasion [84]. Wu et al. [84,93] demonstrated via experiments and simulations that increasing front ring wear clearance from 0.2 mm to 0.5 mm results in a 12% decrease in pump head and a 150% increase in vibration velocity. DEM–CFD coupling simulations indicated a significant rise in flow field turbulence post-wear. Li et al. [94] noted that the uneven distribution of the self-lubricating phase in 1Cr13 MoS steel rings causes abrupt local friction coefficient changes, accelerating wear. Bonet-Jara et al. [95] developed a dynamic model of end-ring wear, employing the Runge-Kutta method to solve the rotor circuit equation, enabling real-time simulation of wear resistance changes for the first time. They observed that clearance enlargement exponentially decreases efficiency while linearly increasing vibration. Front ring wear reduces lift, whereas rear ring wear exacerbates vibration. Controversies exist in material selection: high-hardness alloys resist wear but are susceptible to stress corrosion cracking, while self-lubricating composites are expensive and last under 10,000 h [44,96]. Maintenance priorities also vary; for instance, FMEA analysis ranks ring wear as low risk, yet experimental evidence indicates it can lead to interlocking bearing failures [97,98].
2.2.4. Rotor Dynamic Fault
- Critical speed: The natural frequency of the rotor system and its rotation frequency can coincide at a specific speed, leading to resonance upon even minor excitation and resulting in a surge in amplitude [104,105]. The classical theory developed by Jeffcott [100] elucidates the abrupt changes in amplitude exhibited by rotors near the critical speed. The Jeffcott rotor model is a single-disk symmetric rotor, and its motion can be described by the following differential equations:where is the rotor mass, is the damping coefficient, is the bearing stiffness, is the mass eccentricity, and ω is the rotational angular velocity. The solution shows that resonance occurs when , and at the critical speed, the theoretical amplitude approaches infinity. Over the past decade, research has focused on the correction of complex boundary conditions. Furthermore, Zhang [106] demonstrated through a multi-field coupling model that thermal expansion of materials under high-temperature and high-pressure conditions can reduce the critical speed, while nonlinear variations in bearing stiffness can broaden the critical speed range. Comparative findings by Pennacchi et al. [107] focused on experimental validation, capturing bifurcation phenomena of axis trajectories through high-speed cameras. In contrast, research [106] preferred finite element method (FEM) simulations, which are computationally efficient but neglect turbulence effects. Controversies remain regarding damping quantification. The Muszynska model [108] assumed linear damping, whereas Wilkening [3], based on the case of nuclear power main pumps, demonstrated that fluid damping exhibits strong velocity dependence, necessitating the introduction of a nonlinear term correction. The limitation of current models lies in their inability to accurately characterize the transient over-critical process, along with the neglect of material creep effect under high-temperature environments, as highlighted in the separation margin design criterion [97,106] of the international standard API 610 [109]. Accurate prediction of critical velocity requires consideration of geometric nonlinearity, sealing effects, and thermal deformation, but the computational cost of high-fidelity models restricts real-time application.
- Unbalance response: Rotor mass eccentricity is a common source of excitation, and the corresponding response amplitude increases nonlinearly with rotational speed [110]. Lee et al. [111] demonstrated through a rotor–ball bearing system model that angular misalignment amplifies the unbalanced force, leading to a degeneration of the axis trajectory from an ellipse to a straight line. Recent progress in the field is reflected in the analysis of multi-fault coupling. Wang et al. [112] established a rotor model for a turbocharger, revealing that when imbalance and friction are coupled, the spectrum is dominated by the first-order harmonic (1×, corresponding to the rotation frequency), and the axis track exhibits a “0” pattern. Conversely, if the superposition is not centered, second-order harmonics (2×) are excited, and the track distortion resembles an “8” pattern. Methodologically, there are significant differences among approaches. The lumped parameter method employed by Lee et al. [111] is computationally straightforward but limited in accuracy, while the method by Marscher et al. [97] extracts parameters from field vibration data, which is more representative of engineering practice but constrained by sensor layout. Active balancing devices offer superior efficiency compared to passive dampers, though they require precise installation. While laser dynamic balancing is cost-effective, it has a dynamic error margin of ±15% [112]. Ma et al. [113] introduced a flexible coupling–rotor system model that first quantifies the fluid inertia effect due to misalignment, yet it fails to address force transfer lag in multiphase flow media. Typically, unbalance diagnosis relies on vibration signals; however, the enclosed structure of the main pump restricts sensor placement, and fluid noise often masks power-frequency components, complicating accurate fault detection.
- Fluid-induced instability: Fluid-induced instability is primarily characterized by self-excited vibrations resulting from the interaction between fluid excitation forces and rotor motion, often manifesting as half-frequency whirl or whip. This phenomenon arises from a positive feedback loop caused by the phase difference between the fluid dynamic pressure field and rotor displacement. Instability occurs when high-pressure fluid generates an asymmetric pressure distribution within the bearing clearance or impeller seal, aligning the resultant force with the rotor’s whirl direction [114,115]. Wang et al. [50] demonstrated, in the context of a nuclear main pump, that a 15.4 MPa high-pressure water flow induces a radial pressure gradient in the bearing gap. Changes in vortex displacement alter the clearance geometry, causing the fluid dynamic pressure field to amplify vortex amplitude, thus perpetuating a cycle of self-excited vibration. This effect is particularly pronounced in water-lubricated bearings, where water’s low viscosity results in insufficient damping and ability to suppress the accumulation of eddy energy. Additionally, research has increasingly examined turbulence nonlinearity and the instability threshold. The classical half-speed vortex theory, which assumes a constant vortex ratio of 0.5, is notably weakened by turbulence effects. Zhai et al. [116] demonstrated via vertical rotor tests that turbulence in slotted bearings reduces the swirl ratio to 0.42–0.48, consistent with the 0.48 frequency-doubling characteristic measured in nuclear main pumps. This occurs because turbulence increases the fluid’s equivalent mass, thereby altering the system’s natural frequency. Additionally, Pennacchi et al. [107] found that misalignment decreases the instability threshold by 30% due to exacerbated pressure field inhomogeneities from geometric deviations. A central debate in fluid-induced instability concerns fluid excitation forces: the traditional Reynolds equation neglects inertia forces, leading to significant errors at high speeds [3]. In contrast, the CFD full model by Gao et al. [117] offers high accuracy but requires over 100 times the computational resources of the simplified model, severely limiting its applicability for real-time monitoring.
3. Fault Diagnosis Methods for Main Pump Systems
3.1. Methods Based on Signal Processing
3.1.1. Time–Frequency Domain Analysis Techniques
3.1.2. Signal Decomposition and Reconstruction Methods
3.1.3. Nonlinear Signal Processing Methods
3.1.4. Physical Feature Demodulation Method
3.1.5. Special Consideration for Signal Processing Methods in the Fault Diagnosis of Main Pumps
3.2. Model-Based Approach
3.2.1. Fault Diagnosis Methods Based on Physical Models
3.2.2. Model Methods Based on Signal Processing and Feature Extraction
3.2.3. Model Comparison Methods Based on Analytical Redundancy
3.2.4. Special Consideration for Model Methods in the Fault Diagnosis of Main Pumps
3.3. Data-Driven Approach
3.3.1. Traditional Machine Learning Intelligent Diagnosis Methods
3.3.2. Deep Learning-Based Intelligent Diagnosis Method
3.3.3. Transfer Learning-Based Intelligent Diagnosis Method
3.3.4. Special Considerations for Data-Driven Methods in Main Pump Fault Diagnosis
3.4. Fusion-Based Approach
3.4.1. Data Level Fusion
3.4.2. Feature-Level Fusion
3.4.3. Decision-Level Fusion
3.4.4. Special Consideration for Fusion Methods in the Fault Diagnosis of Main Pumps
3.5. Diagnostic Methods
4. Analysis of the Development of Fault Diagnosis Methods for Main Pumps
5. Core Challenges and Future Research Directions
5.1. Core Challenge 1: Failure Mechanism Coupling and Evolution Law Under Extreme Working Conditions Are Unclear
5.2. Core Challenge 2: Insufficient Generalization and Reliability of Diagnostic Models in Complex Environments
5.3. Core Challenge 3: Leap from Fault Diagnosis to Predictive Maintenance and Proactive Health Management
6. Conclusions
6.1. Study Summary
6.2. Comparison with Existing Reviews and Innovation
6.3. Future Expectations
Author Contributions
Funding
Data Availability Statement
Conflicts of Interest
References
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| Component Category | Specific Component | Fault Causes | Impact | Severity Level |
|---|---|---|---|---|
| Bearing System | Rolling Bearings | Lubrication contamination (water/particles in oil), overheating (improper oil level/poor oil quality), misalignment, and fatigue wear. | Increased vibration, elevated noise levels, and temperature rise, leading to shaft damage or seizure. | High |
| Plain Bearings | Oil whirl, journal/bearing friction, and insufficient lubrication. | Oil film failure and direct metal contact, causing high temperature and vibration. | High | |
| Fitted Interfaces | Shaft wear (corrosion/imbalance) and installation stress. | Increased clearance, exacerbating vibration and seal failure. | Medium | |
| Sealing System | Mechanical Seals | Dry running, vibration, seal face wear, shaft vibration, and insufficient lubrication. | Medium leakage (e.g., glue solution), flushing phenomena, and pressure/flow reduction. | High |
| Packed Seals | Vibration, foreign material blockage, and wear. | Reduced rotational speed, increased leakage, and decreased pump efficiency. | Medium | |
| Hydraulic Components | Impeller | Cavitation (inlet pressure < saturation vapor pressure), wear (impurities/prolonged operation), blockage, and reverse installation. | Efficiency reduction, increased vibration/noise, unstable flow, and blade fracture. | High |
| Guide Vanes | Wear and corrosion. | Hydraulic imbalance and flow channel blockage, exacerbating vibration. | Medium | |
| Wear Rings | Improper clearance (misalignment/wear) and dirty medium. | Increased internal leakage and reduced volumetric efficiency. | Medium | |
| Rotor Dynamics | Critical Speed | Rotor resonance (design defects/deposits) and loose baseplate. | Sudden increase in amplitude, causing bearing/seal damage. | High |
| Unbalance Response | Impeller imbalance, shaft bending, coupling wear, and piping stress. | Periodic vibration, inducing mechanical fatigue and component loosening. | High | |
| Fluid-Induced Instability | Cavitation, vortex shedding, and hydraulic excitation. | Low-frequency vibration and flow pulsation, potentially triggering structural resonance. | Medium |
| Fusion Level | Description | Advantages | Disadvantages | Typical Methods | Applicable Scenarios |
|---|---|---|---|---|---|
| Data-level Fusion | Direct alignment, filtering, and fusion of raw sensor data. | Minimal information loss and theoretically highest accuracy. | Large data volume and high computational cost; requires precise sensor synchronization; sensitive to noise. | Wavelet transform and CNN directly processing multi-source signals. | Offline precision analysis and in-depth study of failure mechanisms. |
| Feature-level Fusion | First extracts features from each sensor signal, and then fuses the feature vectors. | Significantly compresses data volume; retains key information; high flexibility and strong robustness. | Quality of feature extraction directly affects the final result; complex fusion algorithm selection. | Feature concatenation, weighted fusion, and principal component analysis (PCA). | Most commonly used in online real-time or quasi-real-time diagnostic systems. |
| Decision-level Fusion | Each sensor or method first independently performs preliminary diagnosis, and then fuses the multiple diagnostic results. | Best fault tolerance; modular design and easy to expand; friendly to asynchronous sensors. | Maximum information loss; relies on the preliminary diagnosis performance of each sub-module. | Voting methods, D-S evidence theory, and Bayesian inference. | High reliability requirements, fault-tolerant control, and distributed monitoring systems. |
| Comparison Dimension | Signal Processing Methods | Model-Driven Methods | Data-Driven Methods | Information Fusion Methods |
|---|---|---|---|---|
| Core Principle | Direct feature extraction from signals (vibration and pressure) | Residual-based diagnosis using system | ML-based learning of fault-state mappings from historical data | Integration of multi-sensor/multi-method information |
| Optimal Scenario | Periodic impact faults in rotating components | Parametric faults (sensors, actuators, and leaks) | Complex systems with ample data but no precise models | High-reliability systems with unreliable single sources |
| Main Advantage | Clear physical interpretation; minimal fault data needed | Strong explainability; reasoning and early warning capabilities | Powerful feature extraction; high accuracy for complex faults | Enhanced accuracy and robustness; good fault tolerance |
| Main Limitation | Expert-dependent; low intelligence; insensitive to unknown faults | Complex modeling; sensitive to parameter variations | Data quality/quantity dependent; “black box” models | Complex implementation; high computational/communication costs |
| Diagnostic Paradigm | Signal Processing | |||
|---|---|---|---|---|
| Specific Methods | Time–domain analysis. | Signal decomposition and reconstruction. | Nonlinear signal processing. | Physical feature extraction. |
| Advantages | Simultaneously captures time-frequency characteristics; suitable for non-stationary signal analysis. | Can separate fault feature components; effectively suppresses background noise. | Can reveal nonlinear characteristics of systems; detects weak nonlinear faults. | Directly extracts physical fault features (e.g., characteristic frequencies); strong engineering interpretability. |
| Disadvantages | Basis function selection depends on experience; requires parameter tuning. | Endpoint effects exist; high computational complexity. | Parameter optimization is difficult; requires high sampling rate data support. | Relies on prior knowledge for demodulation strategy design; insensitive to compound faults. |
| Signal Type | Vibration and noise. | Vibration and pressure. | Vibration and pressure. | Vibration. |
| Real-time Capability | Medium. | Medium. | Medium. | High. |
| Typical Applicable Faults | Bearing pitting, gear tooth breakage, and cavitation | Early bearing wear, pulley loosening, and valve plate failure | Rotor wear, misalignment, and nonlinear damage | Bearing spalling, ball damage, and gear local defects |
| Application Scenarios | Transient fault diagnosis in rotating machinery. | Early weak fault extraction in strong noise environments. | Fault diagnosis in complex dynamic systems. | Quantitative diagnosis of characteristic faults in rotating components like bearings/gears. |
| Diagnostic Paradigm | Model-Driven | ||
|---|---|---|---|
| Specific Methods | Physical Model. | Signal Processing and Feature Extraction Model. | Analytical Redundancy Model Comparison. |
| Advantages | Provides accurate and precise diagnostic estimates; strong fault isolation capability. | Improves diagnostic robustness; can handle certain noise and instability. | Robust to unknown disturbances; suitable for real-time systems with fast fault detection. |
| Disadvantages | High model complexity; not easily adaptable to system changes or new fault types. | Complex model training; improper feature selection may cause overfitting. | Model errors may cause false alarms; not suitable for strongly nonlinear or time-varying systems. |
| Signal Type | Pressure, flow, and speed. | Vibration and pressure. | Pressure, flow, and temperature. |
| Real-time Capability | High. | Medium. | High. |
| Typical Applicable Faults | System leakage, efficiency decline, and parametric faults. | Pulley wear, plunger sticking, and performance degradation. | Sensor faults, actuator faults, and control anomalies. |
| Application Scenarios | Efficiency decline or leakage fault diagnosis in hydraulic systems, suitable for internal system mechanisms. | Fault classification and early warning, suitable for nonlinear systems. | Detection of sensor faults or control system abnormalities, suitable for linear time-invariant systems. |
| Diagnostic Paradigm | Data-Driven | ||
|---|---|---|---|
| Specific Methods | Traditional machine learning. | Deep learning. | Transfer learning. |
| Advantages | Simple architecture, high classification performance, and strong noise immunity; can handle multivariate data. | Automatically extracts features, avoiding manual interference; excellent capability for processing high-dimensional data. | Can adapt to new scenarios or small data, reducing training requirements and data dependency. |
| Disadvantages | High computational complexity, requires large training data; parameter selection is ambiguous; decision process is opaque. | “Black box” nature leads to unclear decisions; long training time; stability affected by gradient issues. | Transfer effect depends on similarity between source and target; accuracy may be unstable in new environments. |
| Signal Type | Vibration and feature values. | Vibration images, time-series signals, and multi-source data. | Vibration, images, and multi-source. |
| Real-time Capability | High. | Low (training)/Medium (application). | Medium. |
| Typical Applicable Faults | Bearing wear, misalignment, and impeller imbalance. | Compound faults, deep-seated faults, and unknown faults. | Cross-condition faults and small-sample faults. |
| Application Scenarios | Fan fault diagnosis in ventilation systems, suitable for situations with labeled historical data. | End-to-end intelligent diagnosis and prediction in industrial systems, suitable for big data scenarios. | Cross-condition diagnosis in industrial systems, solving small-sample and zero-shot problems. |
| Diagnostic Paradigm | Information Fusion | ||
|---|---|---|---|
| Specific Methods | Data-level fusion. | Feature-level fusion. | Decision-level fusion. |
| Advantages | Fuses raw data, complete information retention, and theoretically highest accuracy. | Reduces data dimensionality; strong robustness, can handle partial information loss. | Highest fault tolerance, can handle uncertainty; friendly to asynchronous sensors. |
| Disadvantages | Large data volume and complex processing; susceptible to noise and synchronization issues; high computational overhead. | Improper feature extraction may cause information loss; complex fusion algorithm selection. | Maximum information loss; decision delay may affect real-time performance. |
| Signal Type | Multi-source heterogeneous (Vibration + Pressure + Current). | Multi-source features. | Multi-source decisions. |
| Real-time Capability | Low. | Medium. | High. |
| Typical Applicable Faults | Multiple faults. | Compound faults. | System faults. |
| Application Scenarios | Offline precision analysis and in-depth study of failure mechanisms. | Most commonly used in online monitoring and diagnostic systems, balancing performance and efficiency. | Final decision-making in high-reliability requirements and fault-tolerant control systems. |
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Ma, W.; Ma, S.; Zou, Z.; Fu, B.; Ma, J.; Liu, J.; Zhang, Q. Literature Review on Fault Mechanism Analysis and Diagnosis Methods for Main Pump Systems. Machines 2025, 13, 1000. https://doi.org/10.3390/machines13111000
Ma W, Ma S, Zou Z, Fu B, Ma J, Liu J, Zhang Q. Literature Review on Fault Mechanism Analysis and Diagnosis Methods for Main Pump Systems. Machines. 2025; 13(11):1000. https://doi.org/10.3390/machines13111000
Chicago/Turabian StyleMa, Wensheng, Shoutao Ma, Zheng Zou, Benyuan Fu, Jinghua Ma, Junjiang Liu, and Qi Zhang. 2025. "Literature Review on Fault Mechanism Analysis and Diagnosis Methods for Main Pump Systems" Machines 13, no. 11: 1000. https://doi.org/10.3390/machines13111000
APA StyleMa, W., Ma, S., Zou, Z., Fu, B., Ma, J., Liu, J., & Zhang, Q. (2025). Literature Review on Fault Mechanism Analysis and Diagnosis Methods for Main Pump Systems. Machines, 13(11), 1000. https://doi.org/10.3390/machines13111000

