OUTLET NOZZLE PROVIDED WITH CHEVRONS FOR AERONAUTICAL THRUSTER

The invention relates to an outlet nozzle (12') for an aeronautical thruster arranged downstream of at least one stator vane (32) of the thruster, a trailing edge (122') of the outlet nozzle comprising a plurality of chevrons (4) distributed circumferentially around a central axis, said tr...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	GEA AGUILERA, Fernando, BODARD, Guillaume, Michel, Marcel, BOITEUX, Jean-Michel, Daniel, Paul
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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