Micromixer Heat Shield

Methods and systems are provided for operating a turbine engine. The combustor includes a combustor wall defining a combustion zone (210) and a fuel nozzle (200). The fuel nozzle includes a forward face (220), an aft face (230) downstream from the forward face and adjacent to the combustion zone, a...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Barker, Carl Robert, Johnson, Thomas Edward
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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