Email this article Numerical and Experimental Study of a Hybrid Segmented Air Bearing for an Aircraft Gas Turbine Engine
- Authors: Bulat P.V.1,2, Bulat M.P.1,2, Volobuev I.A.2, Levikhin A.A.1
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Affiliations:
- Ustinov Baltic State Technical University “Voenmekh”
- Saint Petersburg State University of Information Technologies, Mechanics and Optics
- Issue: Vol 61, No 3 (2018)
- Pages: 420-424
- Section: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/230622
- DOI: https://doi.org/10.3103/S1068799818030157
- ID: 230622
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Abstract
The bearing capacity of hybrid segmented bearings with different groove systems is compared. The research establishes that the system with a crescent groove has the best characteristics.
About the authors
P. V. Bulat
Ustinov Baltic State Technical University “Voenmekh”; Saint Petersburg State University of Information Technologies, Mechanics and Optics
Email: volobuev_ig@mail.ru
Russian Federation, ul. 1ya Krasnoarmeiskaya 1, St. Petersburg, 190005; Kronverkskii pr. 49, St. Petersburg, 197101
M. P. Bulat
Ustinov Baltic State Technical University “Voenmekh”; Saint Petersburg State University of Information Technologies, Mechanics and Optics
Email: volobuev_ig@mail.ru
Russian Federation, ul. 1ya Krasnoarmeiskaya 1, St. Petersburg, 190005; Kronverkskii pr. 49, St. Petersburg, 197101
I. A. Volobuev
Saint Petersburg State University of Information Technologies, Mechanics and Optics
Author for correspondence.
Email: volobuev_ig@mail.ru
Russian Federation, Kronverkskii pr. 49, St. Petersburg, 197101
A. A. Levikhin
Ustinov Baltic State Technical University “Voenmekh”
Email: volobuev_ig@mail.ru
Russian Federation, ul. 1ya Krasnoarmeiskaya 1, St. Petersburg, 190005
