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pro vyhledávání: '"E. Go¨ttlich"'
Publikováno v:
Journal of Turbomachinery. 126:297-305
The current paper presents steady and unsteady flow data of a transonic test turbine stage operating under flow conditions similar to modern highly loaded gas turbines. Measurements were performed between stator and rotor as well as downstream of the
Akademický článek
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Publikováno v:
Volume 7: Turbomachinery, Parts A and B.
The demand of a further increased bypass ratio of aero engines will lead to low pressure turbines with larger diameters which rotate at lower speed. Therefore, it is necessary to guide the flow leaving the high pressure turbine to the low pressure tu
Publikováno v:
Volume 2: Controls, Diagnostics and Instrumentation; Cycle Innovations; Electric Power.
The high power highest efficiency zero-emission Graz Cycle plant of 400 MW was presented at ASME IGTI conference 2006 and at CIMAC conference 2007. In continuation of these works a raise of power output to 600 MW is presented and important design det
Publikováno v:
Volume 6: Turbomachinery, Parts A and B.
The current paper presents experimental clocking investigations of the flow field in midspan in a high-pressure transonic turbine with a downstream vane row (1.5 stage machine). Laser-Doppler-Velocimetry measurements were carried out in order to reco
Autor:
L. Innocenti, Wolfgang Sanz, E. Go¨ttlich, J. Woisetschla¨ger, Herbert Jericha, Andrea Vacca, E. Rossi, Bruno Facchini
Publikováno v:
Scopus-Elsevier
Gas turbine design technology requires the development of transonic turbine stages capable of carrying high stage load and of handling hot gas temperatures at turbine inlet. A reliable cooling system is necessary to cope with shocks emanating from pr
Publikováno v:
Volume 6: Turbo Expo 2003, Parts A and B.
The current paper presents steady and unsteady flow data of a transonic test turbine stage operating under flow conditions similar to modern highly loaded gas turbines. Measurements were performed between stator and rotor as well as downstream of the
Autor:
E. Go¨ttlich, Herbert Jericha
Publikováno v:
Volume 2: Turbo Expo 2002, Parts A and B.
The gas turbine system GRAZ CYCLE has been thoroughly studied in terms of thermodynamics and turbomachinery layout. What is to be presented here is a prototype design for an industrial size plant, suited for NG-fuel and coal and heavy fuel oil gasifi
Publikováno v:
Volume 5: Turbo Expo 2002, Parts A and B.
Gas turbine design technology requires the development of transonic turbine stages capable of carrying high stage load and of handling hot gas temperatures at turbine inlet. A reliable cooling system is necessary to cope with the shock system in the