| Literature DB >> 29522443 |
Abstract
Machining of titanium alloys is characterised by extremely rapid tool wear due to the high cutting temperature and the strong adhesion at the tool-chip and tool-workpiece interface, caused by the low thermal conductivity and high chemical reactivity of Ti alloys. With the aim to monitor the tool conditions during dry turning of Ti-6Al-4V alloy, a machine learning procedure based on the acquisition and processing of cutting force, acoustic emission and vibration sensor signals during turning is implemented. A number of sensorial features are extracted from the acquired sensor signals in order to feed machine learning paradigms based on artificial neural networks. To reduce the large dimensionality of the sensorial features, an advanced feature extraction methodology based on Principal Component Analysis (PCA) is proposed. PCA allowed to identify a smaller number of features (k = 2 features), the principal component scores, obtained through linear projection of the original d features into a new space with reduced dimensionality k = 2, sufficient to describe the variance of the data. By feeding artificial neural networks with the PCA features, an accurate diagnosis of tool flank wear (VBmax) was achieved, with predicted values very close to the measured tool wear values.Entities:
Keywords: artificial neural network; dimensionality reduction; machine learning; principal component analysis; sensor fusion; titanium alloy; tool condition monitoring; turning
Year: 2018 PMID: 29522443 PMCID: PMC5876750 DOI: 10.3390/s18030823
Source DB: PubMed Journal: Sensors (Basel) ISSN: 1424-8220 Impact factor: 3.576
Cutting conditions and number of passes for each experimental turning test.
| Test ID | Cutting Speed (m/min) | Feed Rate (mm/rev) | Depth of Cut (mm) | No. of Passes |
|---|---|---|---|---|
| Test 1 | 60 | 0.20 | 0.5 | 24 |
| Test 2 | 60 | 0.20 | 1.0 | 10 |
| Test 3 | 60 | 0.20 | 1.5 | 12 |
| Test 4 | 60 | 0.25 | 0.5 | 30 |
| Test 5 | 60 | 0.25 | 1.0 | 8 |
| Test 6 | 60 | 0.25 | 1.5 | 12 |
| Test 7 | 60 | 0.30 | 0.5 | 20 |
| Test 8 | 60 | 0.30 | 1.0 | 14 |
| Test 9 | 60 | 0.30 | 1.5 | 11 |
Figure 1Sensor monitoring system mounted on the tool holder.
Figure 2Portable digital microscope and measurement of maximum flank wear land, VB. Cutting parameters: v = 60 m/min, f = 0.2 mm/rev, d = 1 mm (pass no. 4).
Figure 3Measured maximum tool flank wear values vs. machining time for all the cutting conditions.
Figure 4Example of cutting force signals, F, F, F and segmented signal portions.
Figure 5Example of acoustic emission RMS signal, AE and segmented signal portions.
Figure 6Example of vibration acceleration signals, A, A, A and segmented signal portions.
Extracted statistical sensor signal features for each turning pass.
| Sensor Signal | |||||||
|---|---|---|---|---|---|---|---|
| Extracted features per pass |
Figure 7Scree plot reporting the variance explained as a function of the principal components for test 8 (v = 60 m/min, f = 0.3 mm/rev, d = 1 mm).
Figure 8Scores of the first two principal components, PC1 and PC2 and measured tool wear values, VB, vs. number of turning passes for test 4 (v = 60 m/min, f = 0.25 mm/rev, d = 0.5 mm).
Overall Mean Square Error (MSE) obtained by ANN tool wear estimation for all the turning tests.
| MSE | |||
|---|---|---|---|
| 3 Hidden Nodes | 6 Hidden Nodes | 9 Hidden Nodes | |
| Test 1 | 5.31 × 10−3 | 2.51 × 10−2 | |
| Test 2 | 5.22 × 10−3 | 8.66 × 10−3 | |
| Test 3 | 5.48 × 10−3 | 1.31 × 10−2 | |
| Test 4 | 1.95 × 10−3 | 1.87 × 10−3 | |
| Test 5 | 2.23 × 10−3 | 6.56 × 10−3 | |
| Test 6 | 3.69 × 10−2 | 5.17 × 10−2 | |
| Test 7 | 8.67 × 10−3 | 3.71 × 10−2 | |
| Test 8 | 1.22 × 10−3 | 3.20 × 10−3 | |
| Test 9 | 3.48 × 10−3 | 3.02 × 10−3 |
Figure 9Regression plot between ANN predicted and measured VB for turning test 1 at v = 60 m/min, f = 0.20 mm/rev, d = 0.5 mm. ANN configuration: 3-6-1. MSE = 2.48 × 10.
Figure 10Regression plot between ANN predicted and measured VB for turning test 4 at v = 60 m/min, f = 0.25 mm/rev, d = 0.5 mm. ANN configuration: 3-3-1. MSE = 8.12 × 10.
Figure 11Regression plot between ANN predicted and measured VB for turning test 8 at v = 60 m/min, f = 0.30 mm/rev, d = 1.0 mm. ANN configuration: 3-6-1. MSE = 2.54 × 10.