METHOD FOR COOLING A GAS TURBINE AND GAS TURBINE FOR CONDUCTING SAID METHOD

The Invention relates to a method for cooling a gas turbine (10), which comprises a turbine (15), wherein a rotor (11), which rotates about a machine axis, carries a plurality of rotating blades (17), which are mounted on said rotor (11) by means of blade roots and extend with their airfoils into a...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	SIMON-DELGADO, CARLOS, OLMES, SVEN, ROSSI, EUGENIO, TAHENY, OLIVER JOSEPH, SIMONET, CHRISTOPHE, JEMORA, DANIEL, ALBERTI, LUCA, BUSEKROS, ARMIN
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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