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. 04, 2018
Filed:
Jul. 21, 2016
Applicant:
Airbus Helicopters, Marignane, FR;
Inventors:
Christian Mercier, La Fare les Oliviers, FR;
Pierre-Julien Hubert, Igny, FR;
Pierre Gavanier, Croissy sur Seine, FR;
Yann Balastrier, Saint-Cloud, FR;
Assignee:
AIRBUS HELICOPTERS P.C., Marignane, FR;
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16D 1/076 (2006.01); F16H 57/025 (2012.01); B60K 3/02 (2006.01); B60K 5/02 (2006.01); B64C 27/12 (2006.01); B64D 27/04 (2006.01); F16D 1/06 (2006.01); F16D 3/06 (2006.01); F16H 57/00 (2012.01); B64D 27/26 (2006.01); B64D 35/00 (2006.01); F02B 61/00 (2006.01); F16C 3/12 (2006.01);
U.S. Cl.
CPC ...
F16D 1/076 (2013.01); B60K 3/02 (2013.01); B60K 5/02 (2013.01); B64C 27/12 (2013.01); B64D 27/04 (2013.01); F16D 1/06 (2013.01); F16D 3/06 (2013.01); F16H 57/0025 (2013.01); F16H 57/025 (2013.01); B64D 27/26 (2013.01); B64D 35/00 (2013.01); F02B 61/00 (2013.01); F16C 3/12 (2013.01);
Abstract
The present invention relates to a combustion engine which includes at least one crankshaft rotating about a first rotation shaft; at least one output shaft outputting an engine torque, said output shaft rotating about a second rotation shaft separate from said first rotation shaft; at least one transmission assembly rotating about said first rotation shaft and being rotated by said crankshaft in order to transmit said engine torque to said output shaft.