Combustion chamber for gas turbine

The combustion chamber arrangement has a combustion chamber wall (1) encompassing the combustion chamber, which encloses a flow channel in the area of the combustion chamber outlet for hot gases formed inside the combustion chamber. A combustion chamber wall edge (4) is constructed in profiled manne...

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Bibliographische Detailangaben
Hauptverfasser:	Magni, Fulvio, Poyyapakkam, Madhavan Narasimhan, Ince, Nadir
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES ENGINE PLANTS IN GENERAL GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	The combustion chamber arrangement has a combustion chamber wall (1) encompassing the combustion chamber, which encloses a flow channel in the area of the combustion chamber outlet for hot gases formed inside the combustion chamber. A combustion chamber wall edge (4) is constructed in profiled manner, such that by this a profile (17), with an overflow of the combustion chamber wall edge by a cooling air in the annular space region (13) is guided axially through the flow channels (12), where an inhibitory diffuser effect arises.