Turbomachine comprising a rear integrated electrical machine
AssigneeSafran Aircraft Engines
InventorsGilles Alain Marie Charier, Romain Truco, Julien Fabien Patrick Becoulet
Life of this patent
Estimating the term…
Loading patent…
AssigneeSafran Aircraft Engines
InventorsGilles Alain Marie Charier, Romain Truco, Julien Fabien Patrick Becoulet
Estimating the term…
A turbomachine including a low-pressure shaft; a stator supporting the low-pressure shaft by bearings including a rear bearing; an electrical machine located at a rear portion of the turbomachine and including a rotor disconnectably driven by the low-pressure shaft and a stator surrounding the rotor and attached to the stator of the turbomachine; the turbomachine includes a journal for supporting the rotor of the electrical machine, the journal including a shaft segment releasably attached to a rear end of the low-pressure shaft by extending the low-pressure shaft, a frame to which the rotor of the electrical machine is attached and which surrounds the shaft segment, and at least one bearing mounted between the frame and the shaft segment; and a sleeve that is axially movable about the low-pressure shaft and/or the shaft segment that is rotationally connected to the low-pressure shaft and the shaft segment.
A turbomachine comprising:
Dependencies are inferred from the claim text.