COMBUSTOR FRONT ASSEMBLY FOR A GAS TURBINE

A combustor front assembly for a gas turbine power plant, wherein the combustor front assembly is provided with at least a through hole for allowing the gas flow to come into a combustion chamber, the combustor front assembly comprising: - a combustor front plate having at least a through hole and p...

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Bibliographische Detailangaben
Hauptverfasser:	BEG, Marijan, SIEWERT, Piotr, BENZ, Urs, BELINA, Ivo, CVITAK, Branko
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	A combustor front assembly for a gas turbine power plant, wherein the combustor front assembly is provided with at least a through hole for allowing the gas flow to come into a combustion chamber, the combustor front assembly comprising: - a combustor front plate having at least a through hole and provided with an outer surface outside the combustor chamber; - at least a combustor front segment having a through hole and coupled with the outer surface of the combustor front plate so that the through hole of the front segment is aligned with the through hole of the front plate; wherein the combustor front segment is clamped in position and forced against the outer surface of the combustor front plate.