FLOW DEFLECTOR HAVING CHANNELS WITH DOUBLE EJECTION ANGLES

The invention relates to a flow deflector (21) for a compressor of a ducted-fan turbine engine (1) having a longitudinal axis, the flow deflector comprising a wall (25) provided with a plurality of ejection channels (29) capable of discharging a discharge air flow into a flow path of the turbine eng...

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Bibliographische Detailangaben
Hauptverfasser:	VERDON, Valentin, BALLAND, Morgan
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS STEAM ENGINES WEAPONS
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