ANTRIEB FÜR EINE TURBINE NEBST ANTRIEBSVERFAHREN
    1.
    发明公开
    ANTRIEB FÜR EINE TURBINE NEBST ANTRIEBSVERFAHREN 审中-公开
    DRIVE用于涡轮连同驱动方法

    公开(公告)号:EP2440852A1

    公开(公告)日:2012-04-18

    申请号:EP10722135.0

    申请日:2010-06-09

    申请人: Air-lng GmbH

    IPC分类号: F23R3/32 F23R3/34

    CPC分类号: F02C7/22 F23R3/32 F23R3/343

    摘要: The invention relates to a drive for a turbine, in particular an aircraft turbine, and a method for operating such a turbine. According to the invention, a drive for a turbine is provided with a compressor (1) for compressing air, a nozzle (14) for injecting a first fuel into the compressed air, and a combustion chamber (16) for igniting the air-fuel mixture. The drive also comprises a further nozzle (7) for injecting a second fuel. The nozzle for injecting a first fuel is used to start the drive. Therefore, the first fuel is a conventional fuel, in particular kerosene. The second nozzle is used to inject a novel fuel, which at least initially is a liquefied gas. In particular, a mixture and bio-LNG having a high calorific value is used as the liquefied gas.