HIGH PRESSURE TURBINE INLET DUCT AND ENGINE

A duct for connection between an exhaust manifold and a high-pressure turbine inlet includes a cylindrical duct body defining a longitudinal axis. A frustoconical outlet nozzle connected at one end of the duct body and extending at about eighty-five degrees from the longitudinal axis. The duct furth...

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Bibliographische Detailangaben
Hauptverfasser:	PIOTROWSKI CAIN, PHANEUF EDWARD, DOWELL JOHN PATRICK, SHITOLE PRATAP SUBHASH, BHIDE SHIRISH V, WARALE ABHIJEET, LARSON TRENT, JAYAKAR VIJAYASELVAN, ATZ CHARLES BERNARD
Format:	Patent
Sprache:	eng ; kor
Schlagworte:	BLASTING COMBUSTION ENGINES COMBUSTION ENGINES IN GENERAL ENGINE PLANTS IN GENERAL HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INTERNAL-COMBUSTION PISTON ENGINES LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	A duct for connection between an exhaust manifold and a high-pressure turbine inlet includes a cylindrical duct body defining a longitudinal axis. A frustoconical outlet nozzle connected at one end of the duct body and extending at about eighty-five degrees from the longitudinal axis. The duct further includes an inlet bell connected at the other end of the duct body and extending at about fifty degrees from the longitudinal axis.