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Diagnostics of the units of aviation gas turbine engines washed with lube lubricant according to the results of the flush sample analysis of the diagnostic layer of filter elements

https://doi.org/10.26896/1028-6861-2018-84-8-39-43

Abstract

Fine mesh disposable oil filters with a service life of 600 hours and more are used in aviation engines to increase the degree of oil purification. A diagnostic layer in form of a non-woven tape attached to the filter can be removed from the filter to keep up the filter in service. Information on the wear particles accumulated on the filter can be obtained each 200 h. Technique and device used for extracting wear particles from the diagnostic layer of a filter element of the type QA-07930-01 was developed. It is shown that the first flushing from the tape by the number and composition of particles is most indicative for a reliable assessment of the technical state of the engine by the parameters of the wear particles. The total time spent for analysis, including flushing, sedimentation, and treatment in an ultrasonic bath is 90 minutes. The results of assessing the technical condition of the oil system of PS-90A engines equipped with a filter element with and without a diagnostic layer are presented. The obtained data indicate that the filter element QA-07930-01 significantly improves the convenience of servicing the aircraft engines and reduces the costs of diagnostic tests.

About the Authors

V. G. Drokov
Irkutsk State University
Russian Federation

Viktor G. Drokov 

Applied Physics Institute

Irkutsk



V. V. Drokov
Irkutsk State University
Russian Federation

Viktor V. Drokov 

Applied Physics Institute

Irkutsk



V. V. Muryshchenko
Irkutsk State University
Russian Federation

Vladimir V. Muryshchenko 

Applied Physics Institute

Irkutsk



F. I. Muhutdinov
JSC ODK-Aviadvigatel
Russian Federation

Farit I. Muhutdinov

Perm



Yu. D. Skudaev
Irkutsk State University
Russian Federation

Yury D. Skudaev 

Applied Physics Institute

Irkutsk



V. F. Khalioullin
JSC ODK-Aviadvigatel
Russian Federation

Vitaly F. Khalioullin 

Perm



References

1. RF Pat. 2251674, 7G01 M15/00, G01 N3/56, Technique for aircraft engines transmission bearings technical condition evaluation / Gaidai M. S. et al.; applicant and owner NPO «Saturn», JSC «Diagnosticheskie tekhnologii». — № 2002132524; appl. 03.12.2002; publ. 10.05.2005. Byull. N 13 [in Russian].

2. RF Pat. 2164344, 7G01 M15/00, G01 N3/56, Method for monitoring and forecasting the state of gas turbine engines, mainly engines with inter-shaft bearings / Zaritskii S. P. et al.; applicant and owner Letno-issledovatel’skii institut im. M. M. Gromova. — N 98121374/06; appl. 24.11.1998; publ. 20.09.2000. Byull. N 13 [in Russian].

3. Inozemtsev A. A., Drokov V. G., Drokov V. V. et al. Condition and prospects of the spectral methods for the diagnostics of aircraft gas turbine engines. Part 4. Diagnostic parameters and oil sampling points in evaluating of the technical condition of gas turbine engines via spectral measurements / Kontrol’. Diagn. 2012. N 9(159). P. 20 – 28 [in Russian].


Review

For citations:


Drokov V.G., Drokov V.V., Muryshchenko V.V., Muhutdinov F.I., Skudaev Yu.D., Khalioullin V.F. Diagnostics of the units of aviation gas turbine engines washed with lube lubricant according to the results of the flush sample analysis of the diagnostic layer of filter elements. Industrial laboratory. Diagnostics of materials. 2018;84(8):39-43. (In Russ.) https://doi.org/10.26896/1028-6861-2018-84-8-39-43

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ISSN 1028-6861 (Print)
ISSN 2588-0187 (Online)