HIGH EFFICIENCY POWER PRODUCTION METHODS, ASSEMBLIES, AND SYSTEMS

The present disclosure provides a turbine assembly, comprising a plurality of components including a casing defining an inlet configured to receive a combustion product stream, and an outlet, a rotor positioned in the casing, and a plurality of blades extending from the rotor, wherein a ratio of a l...

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Bibliographische Detailangaben
Hauptverfasser:	Allam, Rodney John, Fetvedt, Jeremy Eron, Palmer, Miles R
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS 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:	The present disclosure provides a turbine assembly, comprising a plurality of components including a casing defining an inlet configured to receive a combustion product stream, and an outlet, a rotor positioned in the casing, and a plurality of blades extending from the rotor, wherein a ratio of a length of the turbine assembly to an average diameter of the blades is greater than about 3.5, and wherein the length of the turbine assembly is a distance within the casing from the turbine blade immediately adjacent the inlet to the turbine blade immediately adjacent the outlet.