CPC F02K 3/00 (2013.01) [F01D 15/10 (2013.01); F02C 7/12 (2013.01); F05D 2220/323 (2013.01); F05D 2230/61 (2013.01)] | 13 Claims |
1. A fan module for an aircraft turbine engine, this module comprising a fan and an electrical machine, characterised in that the electrical machine is coaxially mounted downstream of the fan and comprises a rotor coupled to rotate with the fan and an annular member with generally C-shaped axial cross-section, the opening of which is axially facing and receives said rotor, the annular member comprising a radially outer portion forming a stator, and a radially inner portion forming a support for bearings guiding the rotor, said rotor disposed radially between said radially outer portion and said radially inner portion.
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