Aeroengine starter/generator arrangement
    1.
    发明申请
    Aeroengine starter/generator arrangement 有权
    航空发动机启动器/发电机装置

    公开(公告)号:US20100133832A1

    公开(公告)日:2010-06-03

    申请号:US12588810

    申请日:2009-10-28

    申请人: David C. Butt

    发明人: David C. Butt

    摘要: An open-rotor gas turbine engine comprising a starter/generator, a first spool and a second spool, the second spool is of a lower pressure than the first spool; wherein the starter/generator is connected to the first and second spools via first and second clutches respectively. The method of operating the open-rotor engine comprises the step of supplying power to the starter/generator to drive the first spool via the first clutch to start the engine and, once the engine is self-propelling, a step of driving the starter/generator from the second spool via the second clutch to generate electricity.

    摘要翻译: 一种包括起动器/发电机,第一阀芯和第二阀芯的开式转子燃气涡轮发动机,所述第二阀芯的压力低于所述第一阀芯; 其中起动器/发电机分别经由第一离合器和第二离合器连接到第一和第二线轴。 操作开式转子发动机的方法包括:向起动器/发电机供电以通过第一离合器驱动第一线轴起动发动机的步骤,一旦发动机是自行推进的,则驱动起动器/ 发电机通过第二离合器从第二线轴产生电力。

    Power transmission arrangement
    2.
    发明授权
    Power transmission arrangement 有权
    动力传动装置

    公开(公告)号:US07698884B2

    公开(公告)日:2010-04-20

    申请号:US12222551

    申请日:2008-08-12

    IPC分类号: F02C3/107 F02C7/36 F02C7/32

    摘要: A power transmission arrangement comprises a first power transmission member connectable to a first main shaft of an engine. The arrangement also includes a second power transmission member connectable to a second main shaft of the engine and to a third power transmission member. A coupling assembly is provided which has a selectable coupling condition to couple the first power transmission member to the second power transmission member to allow power to be transmitted from the third power transmission member to the first main shaft of the engine via the first power transmission member. The coupling assembly has a decoupling condition to decouple the first power transmission member from the second power transmission member to allow power to be transmitted from the main shaft of the engine to the third power transmission member via the second power transmission member.

    摘要翻译: 动力传递装置包括可连接到发动机的第一主轴的第一动力传递构件。 该装置还包括可连接到发动机的第二主轴和第三动力传递构件的第二动力传递构件。 提供了一种联接组件,其具有可选择的联接状态,以将第一动力传递构件联接到第二动力传递构件,以允许动力经由第一动力传递构件从第三动力传递构件传递到发动机的第一主轴 。 联接组件具有去耦条件,以将第一动力传递构件与第二动力传递构件分离,以允许动力经由第二动力传递构件从发动机的主轴传递到第三动力传递构件。

    Generator assembly
    3.
    发明授权
    Generator assembly 有权
    发电机总成

    公开(公告)号:US07543439B2

    公开(公告)日:2009-06-09

    申请号:US11167383

    申请日:2005-06-28

    IPC分类号: F02C7/32

    CPC分类号: F02C7/36 F02C7/32 H02K7/108

    摘要: A generator assembly for a gas turbine engine. The assembly includes an electrical generator connected via a first sprag clutch to an accessory gearbox driven by the engine. The generator is also connected by a second sprag clutch to an air turbine connected to engine bleed valves which are selectively open when the engine speed falls below a predetermined level. The clutches are arranged such that the generator is driven at any time by the fastest rotating of the gearbox and turbine.

    摘要翻译: 一种用于燃气涡轮发动机的发电机组件。 组件包括通过第一楔形离合器连接到由发动机驱动的附件齿轮箱的发电机。 发电机还通过第二起落架离合器连接到连接到发动机放气阀的空气涡轮机,当发动机转速低于预定水平时,发动机排气阀选择性地打开。 离合器被布置成使得发电机随时通过齿轮箱和涡轮机的最快旋转被驱动。

    Aircraft gas turbine engines
    4.
    发明授权
    Aircraft gas turbine engines 失效
    飞机燃气涡轮发动机

    公开(公告)号:US07418821B2

    公开(公告)日:2008-09-02

    申请号:US11049748

    申请日:2005-02-04

    申请人: David C. Butt

    发明人: David C. Butt

    IPC分类号: F02C7/22 F02C7/26

    CPC分类号: F02C7/275 F01D25/20 F02C7/32

    摘要: An aircraft gas turbine engine including a first hydraulic pump connected to a starter motor and a second hydraulic pump connected to the high-pressure compressor. The engine being arranged such that during starting the starter motor drives the first pump, to pump hydraulic fluid to operate the second pump as a motor to drive the high pressure compressor. During running the first and second pumps are connected to the aircraft hydraulic system.

    摘要翻译: 一种飞机燃气涡轮发动机,包括连接到起动马达的第一液压泵和连接到高压压缩机的第二液压泵。 发动机被布置成使得在起动时起动马达驱动第一泵,泵送液压流体以使第二泵作为电动机驱动高压压缩机。 在运行期间,第一和第二泵连接到飞行器液压系统。

    Aeroengine starter/generator arrangement
    5.
    发明授权
    Aeroengine starter/generator arrangement 有权
    航空发动机启动器/发电机装置

    公开(公告)号:US08350398B2

    公开(公告)日:2013-01-08

    申请号:US12588810

    申请日:2009-10-28

    申请人: David C. Butt

    发明人: David C. Butt

    IPC分类号: F02C3/107 F02C7/32

    摘要: An open-rotor gas turbine engine comprising a starter/generator, a first spool and a second spool, the second spool is of a lower pressure than the first spool; wherein the starter/generator is connected to the first and second spools via first and second clutches respectively. The method of operating the open-rotor engine comprises the step of supplying power to the starter/generator to drive the first spool via the first clutch to start the engine and, once the engine is self-propelling, a step of driving the starter/generator from the second spool via the second clutch to generate electricity.

    摘要翻译: 一种包括起动器/发电机,第一阀芯和第二阀芯的开式转子燃气涡轮发动机,所述第二阀芯的压力低于所述第一阀芯; 其中起动器/发电机分别经由第一离合器和第二离合器连接到第一和第二线轴。 操作开式转子发动机的方法包括:向起动器/发电机供电以通过第一离合器驱动第一线轴起动发动机的步骤,一旦发动机是自行推进的,则启动/ 发电机通过第二离合器从第二线轴产生电力。

    Rotor assembly and annulus filler for gas turbine engine compressor
    6.
    发明授权
    Rotor assembly and annulus filler for gas turbine engine compressor 有权
    用于燃气涡轮发动机压缩机的转子组件和环形填料

    公开(公告)号:US07527476B2

    公开(公告)日:2009-05-05

    申请号:US11107927

    申请日:2005-04-18

    IPC分类号: F01D5/22

    摘要: A rotor assembly for a gas turbine engine compressor includes a rotor disc for mounting a plurality of radially extending rotor blades for rotation thereon, an annulus filler for securing to the disc to provide a radially inner airflow surface for air passing through the rotor assembly and a securing arrangement for securing the annulus filler to the rotor disc, the annulus filler being configured such that it is biased into a condition in which the securing arrangement mechanically retains the annulus filler on the disc, but is movable against its bias to allow the annulus filler to be removed from the disc.

    摘要翻译: 用于燃气涡轮发动机压缩机的转子组件包括用于安装多个径向延伸的转子叶片以用于旋转的转子盘,用于固定到盘的环形填料,以提供通过转子组件的空气的径向内部气流表面,以及 用于将环形填料固定到转子盘的固定装置,环形填料被构造成使得其被偏压到固定装置将环形填料机械地保持在盘上但可抵靠其偏压运动的状态,以允许环形填料 从光盘中删除。

    Power transmission arrangement
    7.
    发明申请
    Power transmission arrangement 有权
    动力传动装置

    公开(公告)号:US20080302082A1

    公开(公告)日:2008-12-11

    申请号:US12222551

    申请日:2008-08-12

    IPC分类号: F02C3/10

    摘要: A power transmission arrangement comprises a first power transmission member connectable to a first main shaft of an engine. The arrangement also includes a second power transmission member connectable to a second main shaft of the engine and to a third power transmission member. A coupling assembly is provided which has a selectable coupling condition to couple the first power transmission member to the second power transmission member to allow power to be transmitted from the third power transmission member to the first main shaft of the engine via the first power transmission member. The coupling assembly has a decoupling condition to decouple the first power transmission member from the second power transmission member to allow power to be transmitted from the main shaft of the engine to the third power transmission member via the second power transmission member.

    摘要翻译: 动力传递装置包括可连接到发动机的第一主轴的第一动力传递构件。 该装置还包括可连接到发动机的第二主轴和第三动力传递构件的第二动力传递构件。 提供了一种联接组件,其具有可选择的联接状态,以将第一动力传递构件联接到第二动力传递构件,以允许动力经由第一动力传递构件从第三动力传递构件传递到发动机的第一主轴 。 联接组件具有去耦条件,以将第一动力传递构件与第二动力传递构件分离,以允许动力经由第二动力传递构件从发动机的主轴传递到第三动力传递构件。