Steuerungsverfahren einer Gasturbine

A gas turbine apparatus has a gas turbine (2) and a plurality of burners (3) for providing combustion gas to drive the turbine. A flow control means (28) of each burner (3) for fuel or combustion air is adjusted by control means (42) to control each said burner individually in dependence on a predet...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	SHIMURA, AKIRA, HITACHI-SHI, IBARAKI 319-12, JP, KOMATSU, YASUTAKA, HITACHI-SHI, IBARAKI 317, JP, IKEDA, HIRAKU, KATSUTA-SHI, IBARAKI 312, JP, IWAMIYA, TAKESHI, KATSUTA-SHI, IBARAKI 312, JP, ISHIDA, TAKESHI, AYUKAWADAI APT 13-202, HITACHI-SHI, IBARAKI 316, JP, OTAWARA, YASUHIKO, KATSUTA-SHI, IBARAKI 312, JP, TAKABA, MINORU, HITACHI-SHI, IBARAKI 319-14, JP, IWATA, NAOHIKO, HITACHI-SHI, IBARAKI 317, JP, IIZUKA, NOBUYUKI, HITACHI-SHI, IBARAKI 316, JP, SATO, ISAO, HITACHI-SHI, IBARAKI 316, JP, HIROSE, FUMIYUKI, HITACHI-SHI, IBARAKI 317, JP
Format:	Patent
Sprache:	ger
Schlagworte:	AIR AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING METHODSOR APPARATUS FOR COMBUSTION USING FLUID FUELOR SOLID FUEL SUSPENDED IN WEAPONS
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