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Calculation of aircraft high-speed rolling-element bearing rings fit
- Authors: Makarchuk V.V.1, Zhilnikov E.P.2
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Affiliations:
- OJSC "Aviation bearing plant", Samara
- Samara State Aerospace University named after academician S.P. Korolyov (National Research University)
- Issue: Vol 10, No 3-3 (2011): Special Issue
- Pages: 370-376
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/6911
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-3(27)-370-376
- ID: 6911
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Abstract
Hereunder are recommendations for calculation of aircraft rolling bearing rings fitting pull and screw nut tightening efforts considering thermal expansion and deformation due to high-speed centrifugal force.
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About the authors
V. V. Makarchuk
OJSC "Aviation bearing plant", Samara
Author for correspondence.
Email: okm@ssau.ru
Candidate of Engineering science
Russian FederationE. P. Zhilnikov
Samara State Aerospace University named after academician S.P. Korolyov (National Research University)
Email: okm@ssau.ru
Candidate of Engineering science, professor
Russian FederationReferences
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