TURBINE ENGINE COMPRISING AN ELECTRICALLY ACTIVATED FUEL SUPPLY PUMP, AND TURBINE ENGINE FUEL SUPPLY METHOD

摘要

Aircraft turbomachine comprising a turbomachine shaft and a pumping module (100) comprising a structural housing (9), a pumping shaft (11), connected to the turbomachine shaft, a fuel supply pump (3) of the turbomachine, mounted on said pumping shaft (11), mounted inside the structural housing and an electrical device (5), mounted on said pumping shaft (11), adapted to drive said pumping shaft (11) in rotation for actuate the feed pump (3) or to be driven in rotation by said pumping shaft (11) for electrically supplying equipment (8) of the turbomachine, the electrical device comprising rotor elements (51) mounted on the outer periphery of a movable part (32) of the feed pump and stator elements (52) mounted on the inner periphery of the structural housing.