Abstract: An aircraft power generating assembly having a mechanical gear transmission, and an electric machine integrated in the mechanical transmission; the electric machine having a stator connected directly to a fixed frame of the mechanical transmission, and a rotor surrounding and rotated by a rotary shaft of the mechanical transmission; and the opposite ends of the rotary shaft being connected to respective further rotary input/output shafts.
Type:
Grant
Filed:
February 8, 2012
Date of Patent:
December 15, 2015
Assignee:
GE AVIO S.p.A.
Inventors:
Edoardo Curti, Ivan Borra, Marco Cipriani