发明名称 Improvement for rotorcraft equipped with turboshaft engines
摘要 <p>The rotocraft has a main transmission mechanism connected to a forward lifting rotor and a turbo-shaft engine to allow driving of the rotor and the turbo-shaft engine. The engine includes a free turbine (132) connected to the transmission mechanism in a shaft (15). An external compressor (19) at the engine is arranged for being driven by the free turbine or by an electric motor via the transmission mechanism. An air transmitting conduit (21) connects the external compressor to the engine to deliver the air compressed by the compressor to an inlet (22) of the engine.</p>
申请公布号 EP2052967(B1) 申请公布日期 2010.05.05
申请号 EP20080017873 申请日期 2008.10.13
申请人 EUROCOPTER 发明人 CERTAIN, BERNARD
分类号 B64C27/04;B64C27/10;B64C27/12;B64D33/02;B64D35/02;F02C3/10 主分类号 B64C27/04
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