AFTERBODY FOR A TURBOJET ENGINE COMPRISING A NOZZLE PROVIDED WITH A THRUST REVERSER SYSTEM THAT INCORPORATES A CROWN OF NOISE-REDUCING CHEVRONS

The invention concerns an afterbody for a turbojet engine having a central axis (XX'), provided with a nozzle (1) comprising two doors (3, 4) mounted facing each other between two lateral beams (5, 6) pivoting around axes (15, 16, 17, 18) defining a pivot direction, between a retracted position...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	KERNEMP, IRWIN, CLERE, GÉRARD, PASCAL, SÉBASTIEN, LANGRIDGE, JONATHAN, GUILLOIS, DENIS, CHAPELAIN, LOIC
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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