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:
Jun. 04, 2019
Filed:
Oct. 12, 2016
Applicant:
Codrin-gruie Cantemir, Columbus, OH (US);
Inventor:
Codrin-Gruie Cantemir, Columbus, OH (US);
Assignee:
Codrin-Gruie (CG) Cantemir, Columbus, OH (US);
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 6/00 (2006.01); F02K 3/06 (2006.01); F02K 3/00 (2006.01); F02C 7/32 (2006.01); F02K 5/00 (2006.01); F04F 5/20 (2006.01); B64D 27/16 (2006.01); F04D 19/02 (2006.01); F04D 27/00 (2006.01); F04D 29/053 (2006.01); B64D 27/24 (2006.01); H02K 11/33 (2016.01); H02K 3/28 (2006.01); H02K 9/06 (2006.01); H02K 21/22 (2006.01); H02K 1/14 (2006.01); H02K 3/12 (2006.01); H02K 3/18 (2006.01); H02K 3/50 (2006.01); H02K 3/52 (2006.01); H02K 7/14 (2006.01); F01D 15/10 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64D 27/16 (2013.01); B64D 27/24 (2013.01); F01D 15/10 (2013.01); F02C 6/00 (2013.01); F02C 7/32 (2013.01); F02K 3/00 (2013.01); F02K 3/06 (2013.01); F02K 5/00 (2013.01); F04D 19/02 (2013.01); F04D 27/009 (2013.01); F04D 29/053 (2013.01); F04F 5/20 (2013.01); H02K 1/146 (2013.01); H02K 3/12 (2013.01); H02K 3/18 (2013.01); H02K 3/28 (2013.01); H02K 3/50 (2013.01); H02K 3/524 (2013.01); H02K 7/14 (2013.01); H02K 9/06 (2013.01); H02K 11/33 (2016.01); H02K 21/225 (2013.01); B64D 2027/026 (2013.01); F05D 2220/76 (2013.01); Y02T 50/672 (2013.01);
Abstract
Disclosed is a high-power electric motor and its fabrication technology. The motor and its distributed power electronics are all being fully integrated in a conventional turbofan engine. The rotor drives directly (with no gears) the LP shaft of the jet engine while requiring minimal modification to a basic jet engine and without distortion to the nacelle geometry. In principle such a configuration should be suitable for a power level of 10 to 50 MW, which makes it fully capable of providing a standard flight envelope by only using electric energy.