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Rotor in gas bearings dynamics experiment-calculated investigation
- Authors: Temis Y.M.1, Temis M.Y.1, Egorov A.M.1, Gavrilov V.V.1, Ogorodov V.N.1
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Affiliations:
- Central Institute of Aviation Motors
- Issue: Vol 10, No 3-1 (2011): Special Issue
- Pages: 174-182
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/1745
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-1(27)-174-182
- ID: 1745
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Abstract
Mathematical model of rotor dynamics and test rig with rotor in gas bearings are developed for developing of experiment calculated model of high-speed rotor in gas bearings. Rotor mathematical model includes shaft model and nonlinear support with gasdynamic foil bearing model considering four body contact: shaft-gas film-foils-bearing race. Test rig with rotor in gas bearing for verification of numerical simulation results and for adjustment of small gas turbine units (GTU) shafting performance are developed. First stage of numerical simulations and experimental research are done for investigation of simulator rotor rotation in gas supports. Rotor orbits in supports are received for numerical model and experimental investigation and their comparative spectrum analysis are carried out.
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About the authors
Yu. M. Temis
Central Institute of Aviation Motors
Author for correspondence.
Email: tejoum@ciam.ru
Doctor of Technical Sciences
Professor
Head of Mathematical Simulating Department
Russian FederationM. Yu. Temis
Central Institute of Aviation Motors
Email: tejoum@ciam.ru
PhD
Head of Department Sector
Russian FederationA. M. Egorov
Central Institute of Aviation Motors
Email: tejoum@ciam.ru
Engine
Russian FederationV. V. Gavrilov
Central Institute of Aviation Motors
Email: tejoum@ciam.ru
Head of Department Sector
Russian FederationV. N. Ogorodov
Central Institute of Aviation Motors
Email: tejoum@ciam.ru
Engineer
Russian FederationReferences
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