Calculation of lubricant flow in the slide bearing of the aviation engine reducer

A method has been developed for calculating the pressure distribution in a cylindrical slide bearing. We present the process of designing a heavy-duty slide bearing as a component of the reduction gearbox of a bypass turbojet engine as the object of our investigation. The process comprises the follo...

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Bibliographic Details
Main Authors: M. V. Siluyanova, A. О. Fertikov
Format: Article
Language:English
Published: Samara National Research University 2019-07-01
Series:Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
Subjects:
Online Access:https://journals.ssau.ru/index.php/vestnik/article/view/6746