AIRCRAFT PROPULSION ARCHITECTURE INTEGRATING AN ENERGY RECOVERY SYSTEM
摘要
<p>A drive system of at least one rotor of an aircraft via electrical energy in addition to or as a replacement of a mechanical system. The electrical energy is provided at least in part by at least one device for recovering thermal energy from hot gases of an internal combustion engine of the aircraft.</p>
申请公布号
EP2739530(A1)
申请公布日期
2014.06.11
申请号
EP20120753671
申请日期
2012.08.03
申请人
EUROPEAN AERONAUTIC DEFENCE AND SPACE COMPANY EADS FRANCE;AIRBUS HELICOPTERS
