TUBULAR COMBUSTION CHAMBER SYSTEM AND GAS TURBINE UNIT HAVING A TUBULAR COMBUSTION CHAMBER SYSTEM OF THIS TYPE

A tubular combustion chamber system for a gas turbine unit includes a plurality of annularly arranged transition lines, which are designed to be connected at the upstream ends thereof to respective burners and to conduct hot gas produced by the burners to a turbine. The tubular combustion chamber sy...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Schmidt, Daniel, Gralki, Matthias, Krusch, Claus
Format:	Patent
Sprache:	eng
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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