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

Autor: M. V. Siluyanova, A. О. Fertikov

Publikováno v: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 18, Iss 2, Pp 75-88 (2019)

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

Externí odkaz: https://doaj.org/article/0d1f3bfa03a84034b762774c3efc6786