TURBINE ENGINE COMBUSTION CHAMBER

An annular combustion chamber for a turbine engine, the chamber including an inner wall and an outer wall forming surfaces of revolution, the walls being connected together by a chamber end wall fitted with a fuel injection mechanism, each of the inner and outer walls including primary holes and dil...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: CAZALENS MICHEL PIERRE, RULLAUD MATTHIEU FRANCOIS
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:An annular combustion chamber for a turbine engine, the chamber including an inner wall and an outer wall forming surfaces of revolution, the walls being connected together by a chamber end wall fitted with a fuel injection mechanism, each of the inner and outer walls including primary holes and dilution holes situated downstream from the primary holes in a gas flow direction, the primary and dilution holes being regularly distributed around the circumference of the inner and outer walls. The outer wall has a greater number of dilution holes than the inner wall.