Мақаланы E-mail арқылы жіберу Numerical and Experimental Study of a Hybrid Segmented Air Bearing for an Aircraft Gas Turbine Engine
- Авторлар: Bulat P.V.1,2, Bulat M.P.1,2, Volobuev I.A.2, Levikhin A.A.1
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Мекемелер:
- Ustinov Baltic State Technical University “Voenmekh”
- Saint Petersburg State University of Information Technologies, Mechanics and Optics
- Шығарылым: Том 61, № 3 (2018)
- Беттер: 420-424
- Бөлім: 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
Дәйексөз келтіру
Ашық рұқсат
Рұқсат берілді
Тек жазылушылар үшін
Аннотация
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.
Авторлар туралы
P. Bulat
Ustinov Baltic State Technical University “Voenmekh”; Saint Petersburg State University of Information Technologies, Mechanics and Optics
Email: volobuev_ig@mail.ru
Ресей, 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
Ресей, 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
Хат алмасуға жауапты Автор.
Email: volobuev_ig@mail.ru
Ресей, Kronverkskii pr. 49, St. Petersburg, 197101
A. Levikhin
Ustinov Baltic State Technical University “Voenmekh”
Email: volobuev_ig@mail.ru
Ресей, ul. 1ya Krasnoarmeiskaya 1, St. Petersburg, 190005
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