Enviar artigo por via de e-mail Numerical and Experimental Study of a Hybrid Segmented Air Bearing for an Aircraft Gas Turbine Engine
- Autores: Bulat P.1,2, Bulat M.1,2, Volobuev I.2, Levikhin A.1
-
Afiliações:
- Ustinov Baltic State Technical University “Voenmekh”
- Saint Petersburg State University of Information Technologies, Mechanics and Optics
- Edição: Volume 61, Nº 3 (2018)
- Páginas: 420-424
- Seção: 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
Citar
Acesso aberto
Acesso está concedido
Somente assinantes
Resumo
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.
Sobre autores
P. Bulat
Ustinov Baltic State Technical University “Voenmekh”; Saint Petersburg State University of Information Technologies, Mechanics and Optics
Email: volobuev_ig@mail.ru
Rússia, 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
Rússia, 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
Autor responsável pela correspondência
Email: volobuev_ig@mail.ru
Rússia, Kronverkskii pr. 49, St. Petersburg, 197101
A. Levikhin
Ustinov Baltic State Technical University “Voenmekh”
Email: volobuev_ig@mail.ru
Rússia, ul. 1ya Krasnoarmeiskaya 1, St. Petersburg, 190005
