MEMBRANE THRUST INVERTER FOR AN AIRCRAFT PROPULSION UNIT

An improved thrust reverser for an aircraft propulsion assembly includes redirection of the air flow for performing the thrust reversal by one or more closure membranes, i.e. by thin and flexible structures deployed across the propulsion assembly. The improved thrust reverser includes at least one c...

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Bibliographische Detailangaben
Hauptverfasser:	RAMI, Jean-Paul, CARLES-ESPITEAU, Arnaud, TIREL, STEPHANE, GOULARD, Jean-Baptiste, GONIDEC, Patrick, KERBLER, Olivier, PHI, Alexandre, VANDERLINDEN, Matthieu
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS
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