Abstract
We present the architecture of a conceptual, multifactor model of a high-speed rolling-contact bearing for aircraft engines that operates in the working liquid. We show the solutions for this model that is obtained on the basis of the comprehensive system approach by its decomposition on the second level model.
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Original Russian Text © B.M. Silaev, P.A. Danilenko, 2014, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2014, No. 4, pp. 61–63.
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Silaev, B.M., Danilenko, P.A. Architecture of a multifactor conceptual model of high-speed rolling-contact bearing for aircraft engines and research guidelines. Russ. Aeronaut. 57, 416–420 (2014). https://doi.org/10.3103/S1068799814040175
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DOI: https://doi.org/10.3103/S1068799814040175