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Periodic Report Summary 4 - FACTOR (Full Aero-thermal Combustor-Turbine interactiOn Research)
Project Context and Objectives: To reduce fuel consumption and CO2 / NOx emissions, modern turbo-machineries operate at high velocities and high temperature conditions. The lack of confidence in the prediction of combustor-turbine interaction leads to apply extra safety...
Programme: FP7-TRANSPORT
Record Number: 199796
Last updated on: 2017-06-21
Periodic Report Summary 2 - FACTOR (Full Aero-thermal Combustor-Turbine interactiOn Research)
Project Context and Objectives:To reduce fuel consumption and CO2 / NOx emissions, modern turbo-machineries operate at high velocities and high temperature conditions. The lack of confidence in the prediction of combustor-turbine interaction leads to apply extra safety margins...
Programme: FP7-TRANSPORT
Record Number: 153809
Last updated on: 2014-12-12
Periodic Report Summary 3 - FACTOR (Full Aero-thermal Combustor-Turbine interactiOn Research)
Project Context and Objectives:To reduce fuel consumption and CO2 / NOx emissions, modern turbo-machineries operate at high velocities and high temperature conditions. The lack of confidence in the prediction of combustor-turbine interaction leads to apply extra safety margins...
Programme: FP7-TRANSPORT
Record Number: 176887
Last updated on: 2016-02-02
Full Aero-thermal Combustor-Turbine interactiOn Research
ID: 265985
Data di inizio: 2010-12-01, Termine: 2017-08-31
To achieve lower Specific Fuel Consumption (SFC) and CO2/NOx emissions, modern turbomachineries operate at high velocities and high temperature conditions. The lack of confidence in the prediction of combustor-turbine interactions leads to apply extra safety margins on compon...
Programme: FP7-TRANSPORT
Record Number: 96395
Last updated on: 2017-05-29
Periodic Report Summary - FACTOR (Full aero-thermal combustor-turbine interaction research)
Project context and objectives: To reduce fuel consumption and CO2 / NOx emissions, modern turbo-machineries operate at high velocities and high temperature conditions. The lack of confidence in the prediction of combustor-turbine interaction leads to apply extra safety margin...
Programme: FP7-TRANSPORT
Record Number: 53921
Last updated on: 2014-05-29
Evolutionäres Design für Triebwerke
Die Gasturbinenleistung hängt stark von der Strömungsfeld innerhalb der Brennkammer ab. EU-finanzierte Wissenschaftler haben das Triebwerksdesign weiterentwickelt, indem Brennkammer und Turbine als ein System betrachtet wurden, anstatt jede einzelne Komponente getrennt zu opti...
Programme: FP7-TRANSPORT
Record Number: 90413
Last updated on: 2013-02-15
Available languages: DE, EN, ES, FR, IT, PL
Un concept de moteur d'avion évolutif
La performance des turbines à gaz dépend fortement du champ d'écoulement dans la chambre de combustion. Des scientifiques financés par l'UE ont fait progresser le concept en considérant la turbine et la chambre de combustion comme un seul système, au lieu de les optimiser sépa...
Programme: FP7-TRANSPORT
Record Number: 90413
Last updated on: 2013-02-15
Available languages: DE, EN, ES, FR, IT, PL
Aero engine evolutionary design
[RISULTATO IN BREVE] Aero engine evolutionary design
Gas turbine performance strongly depends on the flow field inside the combustor. EU-funded scientists advanced aero engine design by treating the combustor and turbine as a system instead of optimising each component separately.
Programme: FP7-TRANSPORT
Record Number: 90413
Last updated on: 2013-02-15
Available languages: DE, EN, ES, FR, IT, PL
Diseño evolutivo de motores para aeronaves
El rendimiento de las turbinas de gases depende fuertemente del campo de flujo dentro del combustor. Un grupo de científicos de la Unión Europea ha avanzado en el diseño de motores para aeronaves tratando el combustor y la turbina como un solo sistema en lugar de optimizar cad...
Programme: FP7-TRANSPORT
Record Number: 90413
Last updated on: 2013-02-15
Available languages: DE, EN, ES, FR, IT, PL
Design evolutivo dei motori aeronautici
Le prestazioni delle turbine a gas dipendono fortemente dal campo di flusso all’interno del combustore. I ricercatori finanziati dall’UE hanno apportato avanzamenti al design dei motori aeronautici trattando il combustore e la turbina come un sistema anziché ottimizzare separa...
Programme: FP7-TRANSPORT
Record Number: 90413
Last updated on: 2013-02-15
Available languages: DE, EN, ES, FR, IT, PL
12 3 4 5 6 7 8 9 10 > >| 
List retrieved on: 2017-09-26