ANNULAR DEFLECTION WALL FOR A TURBOMACHINE COMBUSTION CHAMBER INJECTION SYSTEM PROVIDING A WIDE FUEL ATOMIZATION ZONE

ANNULAR DEFLECTION WALL FOR A TURBOMACHINE COMBUSTION CHAMBER INJECTION SYSTEM PROVIDING A WIDE FUEL ATOMIZATION ZONE

A deflection wall known as is disclosed to improve the air fuel mix within an injection system installed in a turbomachine combustion chamber, having a downstream edge formed by the repetition of a pattern extending on each side of a virtual circle and formed from a plurality of bosses each of whic...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: MERY YOANN, CAYRE ALAIN
Format: Patent
Sprache:eng
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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Beschreibung
Zusammenfassung:A deflection wall known as is disclosed to improve the air fuel mix within an injection system installed in a turbomachine combustion chamber, having a downstream edge formed by the repetition of a pattern extending on each side of a virtual circle and formed from a plurality of bosses each of which is centred relative to a corresponding plane inclined by an angle α from a corresponding median axial plane of the annular deflection wall passing through a corresponding end of the downstream edge of the annular deflection wall at the boss considered.