VARIABLE AREA NOZZLE FOR A TURBO REACTOR, AND AIRCRAFT COMPRISING SUCH AN EQUIPMENT

The invention relates to a variable area nozzle for a turbo-jet engine. This nozzle comprises a convergent portion, formed by a fixed semi-shell (2) and a semi-shell (3) pivotal about a diametral axis (4a-4b); the fluid-tightness of the convergent portion is ensured by a substantially semi-circular...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	SOLIGNY, MARCEL ROBERT, BOUILLER, JEAN GEORGES, BUISSON, MARC FRANCOIS BERNARD, BAYLE-LABOURE, GERARD JOSEPH PASCAL
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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