Abstract
The analysis concerns the strength state of a gas turbine rotor under unsteady conditions of operation. A four-stage gas turbine is described. The analysis includes its performance during start-ups and shut-downs as well as off-design operation for a modified fuel composition, Thermal boundary conditions at the rotor surface have been determined. Exemplary variations of maximal stresses for a normal and fast start-up as well as for emergency shut-down are given.
| Translated title of the contribution | Analysis of rotor stresses in a gas turbine under unsteady operational conditions |
|---|---|
| Original language | Polish |
| Pages (from-to) | 875-887 |
| Number of pages | 13 |
| Journal | Chemical and Process Engineering - Inzynieria Chemiczna i Procesowa |
| Volume | 26 |
| Issue number | 4 |
| Publication status | Published - 2005 |
ASJC Scopus subject areas
- General Chemistry
- General Chemical Engineering
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