AIRCRAFT TURBOMACHINE COMPRISING AN ELECTRIC MACHINE

The invention relates to a turbomachine (10) for an aircraft comprising a stator (16), a turbine shaft (17) and an electric machine (18) arranged to the rear of the turbine shaft, and comprising an electric machine stator (22) and an electric machine rotor (24), a rotationally fixed coupling carriag...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	BARET, Emmanuel Fabrice Marie, TAILLANT, Jean-Claude Christian, BECOULET, Julien Fabien Patrick, BOUDEBIZA, Tewfik, REIGNER, Pierre-Alain Jean Philippe
Format:	Patent
Sprache:	eng ; fre ; ger
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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