US 11,692,512 B2
Fan module equipped with an electrical machine for an aircraft turbine engine
Loic Paul Yves Guillotel, Moissy-Cramayel (FR); Tewfik Boudebiza, Moissy-Cramayel (FR); Gilles Alain Marie Charier, Moissy-Cramayel (FR); Caroline Marie Frantz, Moissy-Cramayel (FR); and Vincent Francois Georges Millier, Moissy-Cramayel (FR)
Assigned to SAFRAN AIRCRAFT ENGINES, Paris (FR)
Appl. No. 17/287,857
Filed by SAFRAN AIRCRAFT ENGINES, Paris (FR)
PCT Filed Oct. 16, 2019, PCT No. PCT/FR2019/052457
§ 371(c)(1), (2) Date Apr. 22, 2021,
PCT Pub. No. WO2020/084225, PCT Pub. Date Apr. 30, 2020.
Claims priority of application No. 1859943 (FR), filed on Oct. 26, 2018.
Prior Publication US 2021/0396193 A1, Dec. 23, 2021
Int. Cl. F02K 3/00 (2006.01); F01D 15/10 (2006.01); F02C 7/12 (2006.01)
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
OG exemplary drawing
 
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.