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    DEVICE AND A METHOD FOR STARTING A TURBINE ENGINE FITTED TO A HELICOPTER, MAKING USE OF AN ELECTRICAL ENERGY SOURCE THAT INCLUDES DISCHARGE BOOSTER MEMBERS
    1.
    发明申请
    DEVICE AND A METHOD FOR STARTING A TURBINE ENGINE FITTED TO A HELICOPTER, MAKING USE OF AN ELECTRICAL ENERGY SOURCE THAT INCLUDES DISCHARGE BOOSTER MEMBERS 有权
    装置和用于启动直升机的涡轮发动机的方法，使用包括放电增压器构件的电能源

    公开(公告)号：US20100319357A1

    公开(公告)日：2010-12-23

    申请号：US12816608

    申请日：2010-06-16

    申请人： Marc Gazzino ,  Pierre Bertrand Lancelevee

    发明人： Marc Gazzino ,  Pierre Bertrand Lancelevee

    IPC分类号： F02C7/26

    CPC分类号： F02C7/26 ,  F02C7/268 ,  F05D2220/329 ,  F05D2260/85 ,  Y02T50/671

    摘要： The invention provides a device and a method for starting at least one turbine engine (1) fitted to a helicopter. A starter (6) is fed with electrical energy from an electricity network (8) including at least one battery (9) and/or an electrical energy generator member. Discharge members (10) suitable for providing the starter (6) with a short-term boost of electrical energy in the form of a high-power pulse are incorporated in the network (8). The current pulse is delivered at a determined instant T starting from when the starter (6) is itself started, and/or from a determined threshold S for the speed and/or the variation in the speed with which the compressor (2) of the turbine engine (1) is driven, and/or from detecting D the ignition stage of the turbine engine (1), and/or from a manual control.

    摘要翻译： 本发明提供一种用于启动装配到直升机的至少一个涡轮发动机（1）的装置和方法。 起动器（6）从包括至少一个电池（9）和/或电能发生器构件的电网（8）馈送电能。 适于提供起动器（6）的大功率脉冲形式的电能的短期升压的放电构件（10）被并入网络（8）中。 当起动器（6）自身起动时，从起动器（6）起动的确定时刻T和/或来自确定的速度和/或速度的变化的确定的阈值S来传送当前脉冲。 涡轮发动机（1）被驱动，和/或从涡轮发动机（1）的点火级检测D和/或来自手动控制。

    Device and a method for starting a turbine engine fitted to a helicopter, making use of an electrical energy source that includes discharge booster members
    2.
    发明授权
    Device and a method for starting a turbine engine fitted to a helicopter, making use of an electrical energy source that includes discharge booster members 有权
    装置和一种用于起动安装在直升机上的涡轮发动机的方法，利用包括放电增压部件的电能源

    公开(公告)号：US08752392B2

    公开(公告)日：2014-06-17

    申请号：US12816608

    申请日：2010-06-16

    申请人： Marc Gazzino ,  Pierre Bertrand Lancelevee

    发明人： Marc Gazzino ,  Pierre Bertrand Lancelevee

    IPC分类号： F02C7/268

    CPC分类号： F02C7/26 ,  F02C7/268 ,  F05D2220/329 ,  F05D2260/85 ,  Y02T50/671

    摘要： The invention provides a device and a method for starting at least one turbine engine (1) fitted to a helicopter. A starter (6) is fed with electrical energy from an electricity network (8) including at least one battery (9) and/or an electrical energy generator member. Discharge members (10) suitable for providing the starter (6) with a short-term boost of electrical energy in the form of a high-power pulse are incorporated in the network (8). The current pulse is delivered at a determined instant T starting from when the starter (6) is itself started, and/or from a determined threshold S for the speed and/or the variation in the speed with which the compressor (2) of the turbine engine (1) is driven, and/or from detecting D the ignition stage of the turbine engine (1), and/or from a manual control.

    摘要翻译： 本发明提供一种用于启动装配到直升机的至少一个涡轮发动机（1）的装置和方法。 起动器（6）从包括至少一个电池（9）和/或电能发生器构件的电网（8）馈送电能。 适于提供起动器（6）的大功率脉冲形式的电能的短期升压的放电构件（10）被并入网络（8）中。 当起动器（6）自身起动时，从起动器（6）起动的确定时刻T和/或来自确定的速度和/或速度的变化的确定的阈值S来传送当前脉冲。 涡轮发动机（1）被驱动，和/或从涡轮发动机（1）的点火级检测D和/或来自手动控制。