TURBINE ENGINE PROVIDED WITH MEANS FOR ABSORBING STRESSES FROM THE THRUST OF THE ENGINE THEREOF

Turbine engine, comprising two structural annular casings (16, 22) which are interconnected by connecting rods (54), characterized in that the turbine engine further has at least one accessory gearbox (40) which is fixed to a first of the casings (16) and which is connected by the connecting rods to...

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Bibliographische Detailangaben
Hauptverfasser:	FERT, JÉRÉMY, EDMOND, ANCUTA, CARMEN
Format:	Patent
Sprache:	eng ; fre ; 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 LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	Turbine engine, comprising two structural annular casings (16, 22) which are interconnected by connecting rods (54), characterized in that the turbine engine further has at least one accessory gearbox (40) which is fixed to a first of the casings (16) and which is connected by the connecting rods to the other of the casings (22).