Table 1.
ML/DL methods used for PdM.
| Goal | Learning Task | ML/DL Method | Data Source | Equipment/Process | Ref. |
|---|---|---|---|---|---|
| Failure Prediction (FP) | Anomaly Detection | Hierarchical Clustering | General faults | Time and Frequency | [81] |
| Classification | RF, SVM and LR | Physical faults | Track geometry | [82] | |
| AE | General faults | Rolling bearing | [35,36] | ||
| Spacecraft | [32] | ||||
| Transformers | [34] | ||||
| Rotor bearing systems | [37] | ||||
| Vibration | Tidal turbine | [33] | |||
| Bearings | [29] | ||||
| Acoustic signals Sensor data | Motors | [83] | |||
| DNN | Vibration | Bearings | [84] | ||
| Gasoline engines | [54] | ||||
| Engines | [63] | ||||
| Vibration, pressure and speed | Diesel engines | [55] | |||
| Optical and visual | Laser welding | [56] | |||
| CNN | Vibration | Planetary gearbox | [65,68] | ||
| Grinding faults | Abrasive belt wear | [66] | |||
| General faults | Rotor bearing systems | [37] | |||
| Vibration and images | Rotating machinery | [67] | |||
| RNN | General faults | Rolling bearing | [70] | ||
| Air compressor | [71] | ||||
| Air compressor in buses | [73] | ||||
| Sensor data | Turbofan engine degradation | [72] | |||
| Time-frequencies | Cantilever beams | [75] | |||
| GAN | Sensor data | Turbofan engine degradation | [79] | ||
| Vibration | Induction motor | [78] | |||
| Remaining Useful Life (RUL) | Regression | Online-SVR | Vibration | Rolling Bearing | [85] |
| PSO+SVM | Vibration | Rolling Bearing | [41] | ||
| Bi-directional LSTM | Sensor data | Turbofan engine degradation | [42] | ||
| AE | Acoustic signal Sensor data | Turbofan engine degradation | [38] | ||
| CNN | Sensor data | Turbofan engine degradation | [10,69,86] | ||
| RNN | Sensor data | Turbofan engine degradation | [74] |