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.

Date of Patent:
Jul. 16, 2019

Filed:

Sep. 26, 2016
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Pierre-Alain Jean Philippe Reigner, Moissy-Cramayel, FR;

Antoine Jean-Philippe Beaujard, Moissy-Cramayel, FR;

Augustin Marc Michel Curlier, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 35/06 (2006.01); B64D 27/14 (2006.01); B64C 11/48 (2006.01); F02K 3/072 (2006.01); F02C 7/36 (2006.01); B64D 33/02 (2006.01); B64D 35/08 (2006.01); F16H 48/05 (2012.01); F16H 48/08 (2006.01); F16H 48/10 (2012.01);
U.S. Cl.
CPC ...
B64D 27/14 (2013.01); B64C 11/48 (2013.01); B64D 33/02 (2013.01); B64D 35/06 (2013.01); B64D 35/08 (2013.01); F02C 7/36 (2013.01); F02K 3/072 (2013.01); F16H 48/05 (2013.01); F16H 48/08 (2013.01); F16H 48/10 (2013.01); F05D 2220/323 (2013.01); F05D 2260/40311 (2013.01);
Abstract

The present invention relates to an aircraft comprising a fuselage (), a propulsion unit () at the rear tip of the fuselage and at least two engines () each driving an engine shaft (), the propulsion unit including at least one propeller () driven mechanically by the engine shafts (), characterized in that the propulsion unit () includes two propellers (), each of the propellers being driven by a propeller shaft (), the two propeller shafts being driven by the engine shafts () via a first differential epicyclic gear train (). Specifically, the input of the first differential gear train () is connected to the output of a second differential epicyclic gear train (), the second differential gear train () including two inputs (), each of said two inputs being connected mechanically to one of said engine shafts ().


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