Author:
Smirnov N I,Smirnov N N,Prozhega M V,Matveev S A,Shirobokov O V,Gorbunov A V,Zheltyshev O V
Abstract
Abstract
This paper presents the methodology and test results of rolling bearings of low-flow electric pump units used to ensure circulation of the thermal liquid in the active thermal control system of spacecraft. A multi-position stand has been developed for testing bearings within 40 days in a thermal liquid at a speed of 6000 rpm with the possibility of registering the separator rate speed. As a performance criterion, the clearance in the bearing is used. The conditions of the onset of pitting are investigated.
Reference14 articles.
1. Tribology of machine parts in low-viscous lubricant environments;Silaev,2008
2. Research of possibility of an assessment of the technical conditions of rolling bearings of aircraft engines through vibrodiagnostic criteria;Silaev;Procedia Engineering,2015
3. Microscip Mechanism in Raceways and Rolling Elements of Roller Bearings;Korolev;Int. Conf. on Industrial Engineering ICIE 2016 Procedia Engineering,2016
4. Evaluation of contact stress during rolling process, by three dimensional analytical inverse method;Ehrlacher;Int. J. of Solids and Structures,2013
5. A new roughness parameter to evaluate the near-surface deformation in dry rolling/sliding contact;Daves;Tribology Int.,2013
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