FIELD: mechanical engineering. SUBSTANCE: proposed one-shaft gas-turbine plant with three-support rotor on antifriction bearings has shaft made as solid piece or consisting of relatively fixed parts. At least two supports of rotor are made elastically damping. Ratio of distance between support bearings to diameter of rotor shaft is 0.2 - 8. EFFECT: improved reliability of plant owing to compensation for alternating bending loads at assembling and operation of engine. 5 dwg
Title | Year | Author | Number |
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GAS TURBINE ENGINE COMPRESSOR | 2000 |
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RU2386831C1 |
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RU2190110C2 |
ELASTIC-DAMPING SUPPORT | 1999 |
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SUPPORT FOR TURBO-COMPRESSOR ROTOR | 1999 |
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RU2211936C2 |
Authors
Dates
2002-02-20—Published
2000-01-10—Filed