An aircraft propulsion system (10) comprises first and second co-axial propulsors (13a, 13b), one of the first and second propulsor (13a, 13b) being positioned forward of the other propulsor (13a, 13b). A first electric motor (30a) is configured to drive the first propulsor (13a), and a second electric motor (30b) is configured to drive the second propulsor (13b). The first electric motor (30a) comprising a rotor (32a) radially inwardly of the stator (42a), and the second electric motor (30b) comprises a rotor (32b) radially outwardly of the stator (42b). The stator (42a) of the first electric motor (30a) is mounted to the stator (42b) of the second electric motor (30b).


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    Title :

    Aircraft Propulsion System


    Publication date :

    2018-10-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English



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