Pregled bibliografske jedinice broj: 260741
Characteristics of Non-stationary Thermal Stresses in Steam Turbine Rotor
Characteristics of Non-stationary Thermal Stresses in Steam Turbine Rotor // Proceedings of the 10th International Research/Expert Conference "Trends in the Development of Machinery and Associated Technology" (TMT 2006) : proceedings / Ekinović, Sabahudin ; Vivancos, J. ; Yalcin, S. (ur.).
Zenica : Barcelona: Faculty of Mechanical Engineering ; Escola Tecnica Superior D'Enginyeria Industrial de Barcelona ; Muhendislik Fakultesi Turkey, 2006. str. 465-468 (predavanje, međunarodna recenzija, cjeloviti rad (in extenso), znanstveni)
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Naslov
Characteristics of Non-stationary Thermal Stresses in Steam Turbine Rotor
Autori
Guzović, Zvonimir ; Matijašević, Branimir ; Mihalić, Tihomir
Vrsta, podvrsta i kategorija rada
Radovi u zbornicima skupova, cjeloviti rad (in extenso), znanstveni
Izvornik
Proceedings of the 10th International Research/Expert Conference "Trends in the Development of Machinery and Associated Technology" (TMT 2006) : proceedings
/ Ekinović, Sabahudin ; Vivancos, J. ; Yalcin, S. - Zenica : Barcelona : Faculty of Mechanical Engineering ; Escola Tecnica Superior D'Enginyeria Industrial de Barcelona ; Muhendislik Fakultesi Turkey, 2006, 465-468
Skup
International Research/Expert Conference "Trends in the Development of Machinery and Associated Technology" (10 ; 2006)
Mjesto i datum
Lloret de Mar, Španjolska; Barcelona, Španjolska, 11.09.2006. - 15.09.2006
Vrsta sudjelovanja
Predavanje
Vrsta recenzije
Međunarodna recenzija
Ključne riječi
steam turbine rotor; non-stationary thermal stresses; numerical modelling
Sažetak
The paper "Modelling Non-stationary Thermal Stresses in Steam Turbine Roto" presented at TMT 2004 shows the algorithm and the results of numerical modelling of non-stationary temperature fields, and the respective thermal deformations and stresses, caused by the steam turbine exit pressure change. From the presented general distributions of temperatures, deformations and stresses along the domain of complete rotor the general image about influence of the change of the exit pressure value on its thermal-stressed state is obtained. Simultaneously, some characteristic regions of rotor thermal-stressed state have been indicated which demand additional analysis: a) the central rotor bore ; b) the rotor low pressure part ; c) the disc of last turbine stage ; d) the rear-end labyrinth gland. It is in this work that the results of detailed analysis by means of parametric curves for cited regions for five values of the exit pressure are presented.
Izvorni jezik
Engleski
Znanstvena područja
Strojarstvo
POVEZANOST RADA
Ustanove:
Fakultet strojarstva i brodogradnje, Zagreb