HEAT EXCHANGERS AND COOLING METHODS FOR GAS TURBINES

A gas turbine (10) comprising a compressor (20), a combustor (30) downstream of the compressor, a turbine (40) downstream of the combustor, a heat exchanger (70), a first cooling fluid system (50) and a second cooling fluid system (60) is described. The first cooling fluid system and the second cool...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Simon-Delgado, Carlos, Taheny, Oliver Joseph, Alberti, Luca, Jemora, Daniel, Olmes, Sven
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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