The invention relates to a hybrid drive system for aircraft, in particular helicopters, comprising at least one energy-generating module having an internal combustion engine (10) and a generator (24) that can be driven by the same for generating electric energy, and comprising at least one electric motor (30) for driving a drive means of the aircraft.
申请公布号
WO2011144692(A3)
申请公布日期
2012.05.24
申请号
WO2011EP58125
申请日期
2011.05.19
申请人
EADS DEUTSCHLAND GMBH;BOTTI, JEAN;STUHLBERGER, JOHANNES;JAENKER, PETER;KLOEPPEL, VALENTIN;NIESL, GEORG
发明人
BOTTI, JEAN;STUHLBERGER, JOHANNES;JAENKER, PETER;KLOEPPEL, VALENTIN;NIESL, GEORG