Design features of the axial pump bearings for thermoregulation systems of aircraft

Space technics and technology


Аuthors

Khaustov A. I.*, Shashkin I. N., Malgichev V. A., Nevzorov . M.

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: sinna8@post.ru

Abstract

The results of the design of axial pump bearings for thermoregulation systems of aircraft with a view to minimizing the size and the high requirements for reliability. The paper considers the approaches to the selection of materials of friction bearings. Showing the results of designed bearing unit tests in the experimental samples of axial pumps.

Keywords:

bearings of axial pump, thermoregulation system


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