The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.
The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.
Patent No.:
Date of Patent:
Dec. 15, 2015
Filed:
Feb. 08, 2012
Applicants:
Edoardo Curti, Chieri, IT;
Ivan Borra, Savigliano, IT;
Marco Cipriani, Turin, IT;
Inventors:
Assignee:
GE AVIO S.p.A., , IT;
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
H02K 7/10 (2006.01); H02K 7/116 (2006.01); F01D 15/10 (2006.01); F02C 7/268 (2006.01); F02C 7/32 (2006.01); H02K 1/30 (2006.01); H02K 7/18 (2006.01); H02K 16/04 (2006.01);
U.S. Cl.
CPC ...
H02K 7/1163 (2013.01); F01D 15/10 (2013.01); F02C 7/268 (2013.01); F02C 7/32 (2013.01); H02K 1/30 (2013.01); F05D 2220/50 (2013.01); H02K 7/1815 (2013.01); H02K 7/1823 (2013.01); H02K 16/04 (2013.01); Y02T 50/671 (2013.01);
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.