TURBINE ASSEMBLY AND METHOD FOR REDUCING FLUID FLOW BETWEEN TURBINE COMPONENTS

PROBLEM TO BE SOLVED: To reduce a flow of fluid between turbine components in order to improve the efficiency and performance of a turbine.SOLUTION: The turbine assembly (100) includes a stator (204) and a rotor (202) adjacent to the stator. The turbine assembly also includes a passage (212) formed...

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Bibliographische Detailangaben
Hauptverfasser:	BABU RAMESH KEMPANNA, SRINIVASAN KARTHIK
Format:	Patent
Sprache:	eng
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:	PROBLEM TO BE SOLVED: To reduce a flow of fluid between turbine components in order to improve the efficiency and performance of a turbine.SOLUTION: The turbine assembly (100) includes a stator (204) and a rotor (202) adjacent to the stator. The turbine assembly also includes a passage (212) formed in a projection (210) from the rotor to form a fluid curtain (308) between the rotor and stator. The fluid curtain reduces a flow of fluid (214) into a hot gas flow path (218).