电邮这篇文章 Numerical and Experimental Study of a Hybrid Segmented Air Bearing for an Aircraft Gas Turbine Engine
- 作者: Bulat P.V.1,2, Bulat M.P.1,2, Volobuev I.A.2, Levikhin A.A.1
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隶属关系:
- Ustinov Baltic State Technical University “Voenmekh”
- Saint Petersburg State University of Information Technologies, Mechanics and Optics
- 期: 卷 61, 编号 3 (2018)
- 页面: 420-424
- 栏目: 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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详细
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.
作者简介
P. Bulat
Ustinov Baltic State Technical University “Voenmekh”; Saint Petersburg State University of Information Technologies, Mechanics and Optics
Email: volobuev_ig@mail.ru
俄罗斯联邦, ul. 1ya Krasnoarmeiskaya 1, St. Petersburg, 190005; Kronverkskii pr. 49, St. Petersburg, 197101
M. Bulat
Ustinov Baltic State Technical University “Voenmekh”; Saint Petersburg State University of Information Technologies, Mechanics and Optics
Email: volobuev_ig@mail.ru
俄罗斯联邦, ul. 1ya Krasnoarmeiskaya 1, St. Petersburg, 190005; Kronverkskii pr. 49, St. Petersburg, 197101
I. Volobuev
Saint Petersburg State University of Information Technologies, Mechanics and Optics
编辑信件的主要联系方式.
Email: volobuev_ig@mail.ru
俄罗斯联邦, Kronverkskii pr. 49, St. Petersburg, 197101
A. Levikhin
Ustinov Baltic State Technical University “Voenmekh”
Email: volobuev_ig@mail.ru
俄罗斯联邦, ul. 1ya Krasnoarmeiskaya 1, St. Petersburg, 190005
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