COMBUSTION CHAMBER FOR TURBINE ENGINE COMPRISING MEANS FOR IMPROVING THE COOLING OF AN ANNULAR WALL IN THE WAKE OF AN OBSTACLE

The invention relates to a combustion chamber (40) for a turbine engine which comprises an annular wall (12) defining an inner space (11) of the chamber, a film of wall-cooling air (28) along the annular wall (12) in the inner space, coming from air-inlet openings (26) formed in the annular wall (12...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	LENFANT, Nils, DUCHAINE, Patrick, BERAT, Claude, LAMAISON, Olivier, HERNANDEZ, Lorenzo, Huacan, LABEAUNE, Sylvain
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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