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The aircraft has engines (5-8) whose speed is controlled by throttles (11-14). The inner engines (5, 6) have thrust reversers (9, 10) passing from inactive folded position to an active deployed position, and vice versa. A detector (33) detects the deployment of the reversers and controls locking dev...

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Bibliographische Detailangaben
Hauptverfasser:	ANDRIEU, LAURENT, ANDRE, JOAN
Format:	Patent
Sprache:	ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	The aircraft has engines (5-8) whose speed is controlled by throttles (11-14). The inner engines (5, 6) have thrust reversers (9, 10) passing from inactive folded position to an active deployed position, and vice versa. A detector (33) detects the deployment of the reversers and controls locking devices (36, 37) to lock the throttles (13, 14) related to outer engines (7, 8), when the reversers pass from folded to deployed positions.