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:
Apr. 02, 2019
Filed:
Oct. 03, 2016
Applicant:
Safran Aircraft Engines, Paris, FR;
Inventors:
Augustin Marc Michel Curlier, Boissise la Bertrand, FR;
Sebastien Courtois, Evry, FR;
Assignee:
SAFRAN AIRCRAFT ENGINES, Paris, FR;
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/36 (2006.01); F16H 48/08 (2006.01); F01D 5/02 (2006.01); F02C 3/04 (2006.01); F04D 29/053 (2006.01); F04D 29/32 (2006.01); F02C 3/107 (2006.01); F02C 3/113 (2006.01);
U.S. Cl.
CPC ...
F02C 7/36 (2013.01); F01D 5/02 (2013.01); F02C 3/04 (2013.01); F02C 3/107 (2013.01); F02C 3/113 (2013.01); F04D 29/053 (2013.01); F04D 29/325 (2013.01); F16H 48/08 (2013.01); F05D 2220/323 (2013.01); F05D 2240/35 (2013.01); F05D 2240/60 (2013.01); F05D 2250/312 (2013.01); F05D 2260/40311 (2013.01);
Abstract
A propulsion unit of an aircraft including a turbine (), at least one fan () with an axis offset relative to the axis of the turbine and a power transmission mechanism between the turbine and the fan. The power transmission mechanism includes a speed reducing gear () with an input and a movement output, the input being in the extension of the axis () of the turbine and the output connected to the fan.