MODIFIED ACOUSTIC SECONDARY NOZZLE

An assembly for the rear of a bypass turbomachine (10) comprises a primary nozzle (11) comprising a trailing edge defining a primary flow path portion and a secondary nozzle (110) defining a secondary flow path portion, defined about a longitudinal axis (X), said secondary nozzle being configured to...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	JODET, Norman Bruno André, MARDJONO, Jacky Novi, GONZALEZ, Jérémy Paul Francisco, BODARD, Guillaume
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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