Fuel injection assembly for a gas turbine

A gas turbine comprises a combustion unit (8), a flow sleeve (2) surrounding the combustion unit (8), wherein the flow sleeve (2) is positioned radially outward from the combustion unit (8). Further, the gas turbine includes a fuel injection assembly which is integrated with a flange means (4) which...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	SINGH, RAM BAHADUR, SINGH, MANOJ, GUPTA, GAURAV, PFADLER, SEBASTIAN
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING BURNERS 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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