DEVELOPMENT CONTRACT — GE AVIO SRL — RESEARCH (Q2017689): Difference between revisions
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(Created claim: summary (P836): THE RESEARCH AND DEVELOPMENT PROJECT INCLUDES THE TECHNOLOGICAL DEVELOPMENT OF A JET FUEL AND GAS TURBINE COMPONENTS FOR AERONAUTICI.NAUTICAL ENGINES, THE Ê CONSISTING OF THE FOLLOWING OBJECTIVES: 1 TECHNOLOGICAL DEVELOPMENT OF A FULL ANNULAR REVERSE FLOW COMBUSTOR OF A NEW GENERATION AIR ENGINE, 2 TECHNOLOGICAL DEVELOPMENT OF THE EXHAUST PIPE AND MIXING A TURBOFAN ENGINE, 3 TECHNOLOGICAL DEVELOPMENT OF HSM (HIGH SPEED AND MILLS) WORKING ON TUR...) |
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| Property / summary | |||
THE RESEARCH AND DEVELOPMENT PROJECT INCLUDES THE TECHNOLOGICAL DEVELOPMENT OF A JET FUEL AND GAS TURBINE COMPONENTS FOR AERONAUTICI.NAUTICAL ENGINES, THE Ê CONSISTING OF THE FOLLOWING OBJECTIVES: 1 TECHNOLOGICAL DEVELOPMENT OF A FULL ANNULAR REVERSE FLOW COMBUSTOR OF A NEW GENERATION AIR ENGINE, 2 TECHNOLOGICAL DEVELOPMENT OF THE EXHAUST PIPE AND MIXING A TURBOFAN ENGINE, 3 TECHNOLOGICAL DEVELOPMENT OF HSM (HIGH SPEED AND MILLS) WORKING ON TURBINE BLADES, 4 OPTIMISATION OF INDUSTRIAL TECHNOLOGIES FOR THE PRODUCTION OF TURBINE COMPONENTS, 5 OPTIMISATION OF INDUSTRIAL TECHNOLOGIES FOR THE PRODUCTION OF TURBINE COMPONENTS, OPTIMISATION OF INDUSTRIAL TECHNOLOGIES FOR THE MAINTENANCE OF TURBINE COMPONENTS. (English) | |||
| Property / summary: THE RESEARCH AND DEVELOPMENT PROJECT INCLUDES THE TECHNOLOGICAL DEVELOPMENT OF A JET FUEL AND GAS TURBINE COMPONENTS FOR AERONAUTICI.NAUTICAL ENGINES, THE Ê CONSISTING OF THE FOLLOWING OBJECTIVES: 1 TECHNOLOGICAL DEVELOPMENT OF A FULL ANNULAR REVERSE FLOW COMBUSTOR OF A NEW GENERATION AIR ENGINE, 2 TECHNOLOGICAL DEVELOPMENT OF THE EXHAUST PIPE AND MIXING A TURBOFAN ENGINE, 3 TECHNOLOGICAL DEVELOPMENT OF HSM (HIGH SPEED AND MILLS) WORKING ON TURBINE BLADES, 4 OPTIMISATION OF INDUSTRIAL TECHNOLOGIES FOR THE PRODUCTION OF TURBINE COMPONENTS, 5 OPTIMISATION OF INDUSTRIAL TECHNOLOGIES FOR THE PRODUCTION OF TURBINE COMPONENTS, OPTIMISATION OF INDUSTRIAL TECHNOLOGIES FOR THE MAINTENANCE OF TURBINE COMPONENTS. (English) / rank | |||
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Revision as of 08:52, 23 March 2020
Project in Italy financed by DG Regio
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | DEVELOPMENT CONTRACT — GE AVIO SRL — RESEARCH |
Project in Italy financed by DG Regio |
Statements
2,110,808.07 Euro
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6,074,000.0 Euro
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34.75 percent
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22 December 2016
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31 December 2019
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GE AVIO SRL
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40°54'28.48"N, 14°23'10.43"E
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IL PROGETTO DI RICERCA E SVILUPPO PREVEDE LO SVILUPPO TECNOLOGICO DI UN COMBUSTORE E DEI COMPONENTI DI TURBINA A GAS PER MOTORI AERONAUTICI.NELLO SPECIFICO, IL PROGETTO Ê ARTICOLATO SUI SEGUENTI OBIETTIVI:1 SVILUPPO TECNOLOGICO DI UN COMBUSTORE FULL ANNULAR REVERSE FLOW DI UN MOTORE AERONAUTICO TURBOPROP DI NUOVA GENERAZIONE,2 SVILUPPO TECNOLOGICO DEL CONDOTTO DI SCARICO E MISCELAMENTO DI UN MOTORE TURBOFAN,3 SVILUPPO TECNOLOGICO DELLE LAVORAZIONI DI HSM (HIGH SPEED MILLING) ED ECM (ELECTRO- CHEMICAL MILLING) SULLE PALE ROTORICHE TURBINA,4 OTTIMIZZAZIONE DELLE TECNOLOGIE INDUSTRIALI PER LA PRODUZIONE DI COMPONENTI TURBINA,5 OTTIMIZZAZIONE DELLE TECNOLOGIE INDUSTRIALI PER LA MANUTENZIONE DI COMPONENTI TURBINA. (Italian)
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THE RESEARCH AND DEVELOPMENT PROJECT INCLUDES THE TECHNOLOGICAL DEVELOPMENT OF A JET FUEL AND GAS TURBINE COMPONENTS FOR AERONAUTICI.NAUTICAL ENGINES, THE Ê CONSISTING OF THE FOLLOWING OBJECTIVES: 1 TECHNOLOGICAL DEVELOPMENT OF A FULL ANNULAR REVERSE FLOW COMBUSTOR OF A NEW GENERATION AIR ENGINE, 2 TECHNOLOGICAL DEVELOPMENT OF THE EXHAUST PIPE AND MIXING A TURBOFAN ENGINE, 3 TECHNOLOGICAL DEVELOPMENT OF HSM (HIGH SPEED AND MILLS) WORKING ON TURBINE BLADES, 4 OPTIMISATION OF INDUSTRIAL TECHNOLOGIES FOR THE PRODUCTION OF TURBINE COMPONENTS, 5 OPTIMISATION OF INDUSTRIAL TECHNOLOGIES FOR THE PRODUCTION OF TURBINE COMPONENTS, OPTIMISATION OF INDUSTRIAL TECHNOLOGIES FOR THE MAINTENANCE OF TURBINE COMPONENTS. (English)
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Identifiers
C53D16000770004
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