发明名称 Auxiliary Drive System for a Helicopter
摘要 A drive system for a helicopter includes a main drive for driving a rotor the helicopter, a flywheel mass battery including at least one flywheel, a first transmission coupling the flywheel mass battery with the main drive such that, during operation of the main drive, output can be transferred from the main drive to the flywheel mass battery, and a second, variable transmission connecting the flywheel mass battery to the rotor of the helicopter such that a predetermined output can be transferred to the rotor through adjustment of a transmission ratio of the variable transmission.
申请公布号 US2015197343(A1) 申请公布日期 2015.07.16
申请号 US201314416764 申请日期 2013.07.19
申请人 Airbus Defence and Space GmbH 发明人 Jaenker Peter
分类号 B64D35/02;B64C27/12;B64D41/00 主分类号 B64D35/02
代理机构 代理人
主权项
地址 Ottobrunn DE