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.
Type:
Grant
Filed:
July 21, 2016
Date of Patent:
December 4, 2018
Assignee:
AIRBUS HELICOPTERS P.C.
Inventors:
Christian Mercier, Pierre-Julien Hubert, Pierre Gavanier, Yann Balastrier