AERODERIVATIVE GAS TURBINE WITH IMPROVED THERMAL MANAGEMENT

An aeroderivative gas turbine provided with a casing 13, a compressor having a rotor 14 mounted on a generator shaft 16 supported for rotation in the casing 13, a high pressure turbine 19 arranged in the casing and with a rotor mounted on the generator shaft 16 for co-rotation with the compressor ro...

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Bibliographische Detailangaben
1. Verfasser:	CARATELLI, Francesco
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:	An aeroderivative gas turbine provided with a casing 13, a compressor having a rotor 14 mounted on a generator shaft 16 supported for rotation in the casing 13, a high pressure turbine 19 arranged in the casing and with a rotor mounted on the generator shaft 16 for co-rotation with the compressor rotor 14, a combustor 17, a power turbine 21 arranged in the casing 13 and having a rotor mounted on a turbine shaft 22 to drive a load, wherein a thermal insulation coating is present to reduce heat dispersion through the casing 13.