A Time-Frequency Based Approach for Acoustic Emission Assessment of Sliding Wear
Abstract
1. Introduction
2. Methodology Overview
- –
- –
- –
- –
- the resultant AE at every instant is governed by one or few predominant damage mechanisms, whose scale prevails over others.
3. AE Data Acquisition and Processing
4. Materials and Testing Conditions
- (i)
- the number of AE sources identified, which should be logically connected with the active processes established based on tribological data and metallographic observations;
- (ii)
- the number of signals in specific clusters related to the severity of damage processes identified, indicating the “sensitivity” of AE signal recognition;
- (iii)
- the time of the start and the end of the activity of individual AE sources in relation to the actual damage processes revealed by the behavior of the tribological parameters and metallographic observations.
5. Results and Discussion
-type dominate at this stage (c.f. Figure 2a, and the white region I in Figure 3). With the increasing contact load, the signatures of adhesion and incipient seizure are observed in addition to scratches here and there at the contact surface, and the signals of
-type appear in response to the momentary film breaking and local adhesion (Figure 2b,f,g, and the region II in Figure 3). The number of these signals increases with the increasing load and eventually begins to dominate in the whole AE time series, Figure 2g. With the further increase of load, the adhesive wear mechanism changes from mild to severe, leading to the local seizure events and extensive plastic material transfer, which are observed progressively on the contact surface. With regard to this process, the
-type signals appear in addition to the
-type signals, while the number of
signals reduced. The
signals are always seen if D > [D] that corresponds to seizure according to the ASTM Standards [65,66] (Figure 2c,d,h–j; the region III marks the loads at which seizure is confirmed while surface welding is not, and the region IV corresponds to the observed friction welding). Under the most severe loading conditions with intensive adhesive wear followed by welding of contacted surfaces, the
-type signals prevail, c.f. Figure 2d,e,j. The result is also logical that, if compared to oil, grease results in the earlier onset of seizure. Therefore, it was not possible to observe a wear scar formed by dense scratches without signatures of incipient seizure, scoring or spalling, which is indicated by the distribution of corresponding AE clusters, c.f. Figure 2f–h, and Figure 3b. Based on the similar data obtained for other tribological test schedules described above, it can be argued that the proposed approach is very efficient and sensitive to the dominant wear mechanisms.
corresponds to the scratches on the contact surface as a result of a normal abrasive wear process,
denotes severe adhesive damage and incipient seizure that can be occasionally seen at some local areas of the contact surface due to a momentary breakdown of the lubricating film, and
stands collectively for the most severe wear processes heralding the imminent catastrophic wear failure dominated by scoring, seizure, significant plastic material transfer and welding. It is apparent that the proposed classification scheme is substantially simplified. While capturing the principal features and the severity of the wear damage progress, it does not account for the minute details of the wear mechanisms. This simplification is made intentionally, considering the objective of the on-line AE monitoring, which is set as to identify the wear stage and timely diagnose the symptoms of impending catastrophic failure. For this reason, many features of evolving abrasive wear resulting from ploughing by hard asperities and abrasive particles forced against contacting surfaces or adhesive wear associated with the shear of adhesion bonds generated in friction are not discriminated by the proposed method and can be even compiled into the same group of signals in order to highlight the dominated wear mode and classify the severity of damage associate with it.6. Applications
6.1. Real-Time Monitoring and Control of Friction Conditions
-type signals,) come into the scene, Figure 4, the monitoring system flags the issue, which can be resolved, for example, by extra lubrication of the contact area or by reducing the load on the friction contact. Appropriate, timely measures against scoring and seizing may help to prolong the lifetime of the tribological system significantly. Importantly is that those measures can be implemented in an automated workflow if required. 6.2. Recovery of the Friction Unit Fracture Process Chronology
6.3. Comparative Lubricant Performance Testing
6.4. Accelerated Tribological Tests
-type signals, a judgment can be reliably made whether the seizure has set in or not, and assess the scale of seizure severity. The reduction of the number of tests and the decrease of the test time results in lower consumption of the lubricant and contact elements. Considering the respective energy and labor savings, the using of an AE-based damage assessment program is apparently beneficial for cost-cutting in tribological testing. The results exemplified in Figure 6 were obtained out on the four-ball friction machine under conditions stipulated in the standards [65,66], with the difference that the loading of the same assembly was carried in a step-wise manner with the holding time shown in the figure.7. Conclusions
Author Contributions
Funding
Conflicts of Interest
Appendix A. Filtering Procedures
Appendix B. AE Features
| Time domain | ||
| signal root-mean-square value | âq rms = [Σ âq(t)2 / l ]0.5 | (A9) |
| signal energy | Eq = Σ âq(t)2 | (A10) |
| signal variance | σqâ = [Σ(âq(t) - âq mean)2/(l-1)]0.5 | (A11) |
| signal kurtosis | γqâ = {Σ[(âq(t) - âq mean)/ σqâ]4} – 3 | (A12) |
| signal skewness | sqâ = Σ[(âq(t) - âq mean)/ σqâ]3 | (A13) |
| Spectral domain | ||
| median frequency | fq med at Gqm = 1/2·ΣGq(f) | (A14) |
| signal power | Wq =Σ Gq(f) | (A15) |
| spectrum root-mean- square value | Gq rms = [ΣGq(f)2 / fmax]0.5 | (A16) |
| PSD entropy | Hq = –Σ[ f∙Gq(f)∙log2(f∙Gq(f))] | (A17) |
| PSD variance | σqG = [Σ(Gq(f) - Gq mean)2/(f-1)]0.5 | (A18) |
| PSD kurtosis | γqG = {Σ[(Gq(f) - Gq mean)/ σqG]4} – 3 | (A19) |
| PSD skewness | sqG = Σ[Gq(f) - Gq mean)/ σqG]3 | (A20) |
Appendix C. R2 Clustering Algorithm—K1
Appendix D. Modified k-Means Clustering—K2
Appendix E. Classification by the RMS change rate—K3
Appendix F. Details of Loading Conditions for the Mains Series of Tribological Tests
| Contact Materials 1 | Load, N | Lubricants 2 | PV Factor, N/mm2·m/s | Hertzian Contact Stress Max, P0, MPa3 |
|---|---|---|---|---|
| Four-ball Tester «ChMT-1» (Russia), Testing Standards [65,66] | ||||
| 100Cr6/100Cr6 | 10 | D, L1–L6 | 309 | 944 |
| 59 | D, L1–L6 | 562 | 1716 | |
| 196 | D, L1–L6 | 839 | 2563 | |
| 392 | D, L1–L6 | 1057 | 3229 | |
| 491 | D, L1–L6 | 1139 | 3478 | |
| 530 | D, L3 | 1168 | 3569 | |
| 618 | D, L1–L6 | 1230 | 3757 | |
| 657 | L2, L3, L4 | 1255 | 3835 | |
| 696 | L2, L3, L4, L5 | 1280 | 3910 | |
| 736 | L2, L3, L4, L5 | 1303 | 3982 | |
| 785 | D, L1–L6 | 1332 | 4068 | |
| 824 | L2, L5 | 1353 | 4135 | |
| 883 | D, L2, L5 | 1385 | 4231 | |
| 981 | D, L1–L6 | 1434 | 4383 | |
| 1059 | D, L1 | 1472 | 4496 | |
| 1099 | L1 | 1490 | 4551 | |
| 1148 | L1, L6 | 1512 | 4618 | |
| 1167 | L1, L6 | 1520 | 4644 | |
| 1177 | L1, L6 | 1524 | 4657 | |
| 1236 | L1–L6 | 1549 | 4734 | |
| 1305 | L1, L3, L6 | 1578 | 4820 | |
| 1383 | L1, L3 | 1609 | 4914 | |
| 1570 | L1–L6 | 1678 | 5126 | |
| 1746 | L1, L2, L3 | 1738 | 5311 | |
| 1844 | L1, L2 | 1770 | 5409 | |
| 1962 | L1, L2, L4, L5, L6 | 1807 | 5522 | |
| 2070 | L1, L4, L5 | 1840 | 5621 | |
| 2158 | L4, L5 | 1866 | 5700 | |
| 2197 | L1, L4, L5 | 1877 | 5734 | |
| 2325 | L4, L5 | 1913 | 5843 | |
| 2453 | L1, L5, L6 | 1947 | 5948 | |
| 3090 | L6 | 2103 | 6424 | |
| 3924 | L6 | 2277 | 6957 | |
| 4905 | L6 | 2453 | 7494 | |
| 6082 | L6 | 2635 | 8051 | |
| 6180 | L6 | 2649 | 8094 | |
| 7848 | L6 | 2869 | 8765 | |
| Pin-on-disk, Tribometer Nanovea TRB-50N (USA), Testing Standard [67] | ||||
| 100Cr6/St35 | 25 | D, L3 | 199 | 1776 |
| 35 | D, L3 | 223 | 1987 | |
| 100Cr6/C45 | 25 | D, L3 | 203 | 1809 |
| 35 | D, L3 | 227 | 2024 | |
| 100Cr6/W6Mo5Cr4V2 | 25 | D, L3 | 206 | 1840 |
| 35 | D, L3 | 231 | 2058 | |
| Cylinder-on-ring, Testing Machine UMITI (Russia), Testing Standard [68] | ||||
| 45Cr22Ni4Mo3/Gh190 | 20 | D, L1, L3 | 107 | 610 |
| 40 | D, L1, L3 | 134 | 769 | |
| 60 | D, L1, L3 | 154 | 880 | |
| AlMg3/Gh190 | 20 | D, L1, L3 | 74 | 423 |
| 40 | D, L1, L3 | 93 | 533 | |
| 60 | D, L1, L3 | 107 | 610 | |
Appendix G. Results of Testing Various Combinations of Filtering and Clustering Algorithms
appear as over-clustering of
-class, and
is over-clustering of
-group of signals. Thus, the application of these schemes requires the additional procedure for merging clusters, which is laborious for manual post-processing. Otherwise, it needs additional assumptions for the unsupervised automatic implementation. For the reasons mentioned above, these procedures are also not recommended for immediate application. Favorable results of AE signal discrimination are, however, systematically obtained with the F1.3 + K1, F1.3 + K3 and F2.1 + K1 schemes, Figure A1c, revealing a wealth of occurring processes through the statistically well-separated patterns of signals.
- line) value depending on different signal processing schemes shown in Figure 1 and applied to one and the same dataset obtained in the four-ball testing with mineral oil used as a lubricant: (a) scheme F1.1 + K2, (b) scheme F1.2 + K2, (c) scheme F1.3 + K1, (d) scheme F2.1 + K3, (e) scheme F2.2 + K1, and (f) scheme F1.1 + K1. The categorized AE signals are designated as follows:
-type signals correspond to the sliding wear dominated by abrasive friction;
symbols denote adhesive damage and incipient seizure;
represents the severe wear mode due to progressing seizure, significant plastic material transfer and welding (see the text below for details). The results shown in (d) and (e) illustrate the over-clustering effect:
appears as over-clustering of
, and
is over-clustering of
.
- line) value depending on different signal processing schemes shown in Figure 1 and applied to one and the same dataset obtained in the four-ball testing with mineral oil used as a lubricant: (a) scheme F1.1 + K2, (b) scheme F1.2 + K2, (c) scheme F1.3 + K1, (d) scheme F2.1 + K3, (e) scheme F2.2 + K1, and (f) scheme F1.1 + K1. The categorized AE signals are designated as follows:
-type signals correspond to the sliding wear dominated by abrasive friction;
symbols denote adhesive damage and incipient seizure;
represents the severe wear mode due to progressing seizure, significant plastic material transfer and welding (see the text below for details). The results shown in (d) and (e) illustrate the over-clustering effect:
appears as over-clustering of
, and
is over-clustering of
.
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-type signals correspond to the abrasive-dominated wear;
denote prevailing adhesive damage and incipient seizure;
represents the severe wear mode due to progressing seizure, significant plastic material transfer and welding;
represents AE root-mean-square (RMS) voltage.
-type signals correspond to the abrasive-dominated wear;
denote prevailing adhesive damage and incipient seizure;
represents the severe wear mode due to progressing seizure, significant plastic material transfer and welding;
represents AE root-mean-square (RMS) voltage.
correspond to the average wear scar diameter D as a function of the applied load P, while the dashed red line
represents the critical size [D] tabulated in the standards [65,66].
correspond to the average wear scar diameter D as a function of the applied load P, while the dashed red line
represents the critical size [D] tabulated in the standards [65,66].


-group classified according to the F1.1 + K1 scheme; PcAE denotes the load at which welding is observed. Classified AE signals are color coded in the same way as in Figure 2 (see the caption for details).
-group classified according to the F1.1 + K1 scheme; PcAE denotes the load at which welding is observed. Classified AE signals are color coded in the same way as in Figure 2 (see the caption for details).
© 2020 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (http://creativecommons.org/licenses/by/4.0/).
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Rastegaev, I.; Merson, D.; Rastegaeva, I.; Vinogradov, A. A Time-Frequency Based Approach for Acoustic Emission Assessment of Sliding Wear. Lubricants 2020, 8, 52. https://doi.org/10.3390/lubricants8050052
Rastegaev I, Merson D, Rastegaeva I, Vinogradov A. A Time-Frequency Based Approach for Acoustic Emission Assessment of Sliding Wear. Lubricants. 2020; 8(5):52. https://doi.org/10.3390/lubricants8050052
Chicago/Turabian StyleRastegaev, Igor, Dmitry Merson, Inna Rastegaeva, and Alexei Vinogradov. 2020. "A Time-Frequency Based Approach for Acoustic Emission Assessment of Sliding Wear" Lubricants 8, no. 5: 52. https://doi.org/10.3390/lubricants8050052
APA StyleRastegaev, I., Merson, D., Rastegaeva, I., & Vinogradov, A. (2020). A Time-Frequency Based Approach for Acoustic Emission Assessment of Sliding Wear. Lubricants, 8(5), 52. https://doi.org/10.3390/lubricants8050052

