AIRCRAFT TURBINE ENGINE WITH AT LEAST TWO BODIES AND MEANS FOR DRAWING POWER

Aircraft turbine engine (10), said turbine engine comprising at least a low-pressure body (12a) and a high-pressure body (12b), as well as means (54) for drawing power on said low-pressure body, said means comprising a first shaft (54a) for drawing power, the radially inner end of said first shaft b...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	GUILLOTEL, LOIC PAUL YVES, CHARIER, GILLES ALAIN MARIE, FRANTZ, CAROLINE MARIE, MILLIER, VINCENT FRANCOIS GEORGES
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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