In order to optimize the design of the thermodynamic cycle of a turbine (Brayton cycle) for using modern common rail as an “active” combustion chamber, it was intended to write the present paper. About the present case, the “active” combustion chamber produces a large amount of the mechanical energy that drives the fan. The incoming air is compressed by the compressor, then it is refrigerated and inputted in the diesel engine. A high pressure common rail system optimizes the combustion in the diesel combustion chamber and the expansion begins inside the diesel engine. At the exhaust of the combustion chamber, a turbine completes the expansion of the hot gases. A nozzle accelerates the exhaust from the turbine to increase the overall thrust

Frizziero, L., Rocchi, I., Donnici, G., Pezzuti, E. (2015). Aircraft diesel engine turbocompound optimized. JP JOURNAL OF HEAT AND MASS TRANSFER, 11(2), 133-150 [10.17654/JPHMTMay2015_133_150].

Aircraft diesel engine turbocompound optimized

PEZZUTI, EUGENIO
2015-05-01

Abstract

In order to optimize the design of the thermodynamic cycle of a turbine (Brayton cycle) for using modern common rail as an “active” combustion chamber, it was intended to write the present paper. About the present case, the “active” combustion chamber produces a large amount of the mechanical energy that drives the fan. The incoming air is compressed by the compressor, then it is refrigerated and inputted in the diesel engine. A high pressure common rail system optimizes the combustion in the diesel combustion chamber and the expansion begins inside the diesel engine. At the exhaust of the combustion chamber, a turbine completes the expansion of the hot gases. A nozzle accelerates the exhaust from the turbine to increase the overall thrust
1-mag-2015
Pubblicato
Rilevanza internazionale
Articolo
Esperti anonimi
Settore ING-IND/15 - DISEGNO E METODI DELL'INGEGNERIA INDUSTRIALE
English
Con Impact Factor ISI
Aircraft, Diesel, Engines
Frizziero, L., Rocchi, I., Donnici, G., Pezzuti, E. (2015). Aircraft diesel engine turbocompound optimized. JP JOURNAL OF HEAT AND MASS TRANSFER, 11(2), 133-150 [10.17654/JPHMTMay2015_133_150].
Frizziero, L; Rocchi, I; Donnici, G; Pezzuti, E
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/2108/116762
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