CONE ARRIERE DE TURBOREACTEUR TOURNANT A MICRO-JETS

The invention relates to a rear casing for a turbine engine comprising a primary body generating a primary flow (10) to be ejected through a primary nozzle (6), said rear casing (7) being shaped so as to be positioned downstream from the primary body and to define, on the inside of the turbine engin...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	VUILLEMIN ALEXANDRE, ALFRED, GASTON, GERVAIS YVES, JORDAN PETER, KOENIG MAXIME, COMTE PIERRE
Format:	Patent
Sprache:	fre
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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