THRUST REVERSER FOR AN AIRCRAFT BYPASS TURBOJET ENGINE NACELLE

A thrust reverser for an aircraft bypass turbojet engine nacelle has a generally annular shape around an axis and includes an annular frame for securing deflection grids. The frame has a first frusto-conical wall widening in the downstream direction and including an upstream peripheral edge configur...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	PASCAL, Sébastien Laurent Marie, CAZUC, Xavier, JORET, Jean-Philippe, PEYRON, Vincent Jean-François
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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