SYSTEM FOR DELIVERING AIR FROM A MULTI-STAGE COMPRESSOR TO A TURBINE PORTION OF A GAS TURBINE ENGINE
    1.
    发明申请
    SYSTEM FOR DELIVERING AIR FROM A MULTI-STAGE COMPRESSOR TO A TURBINE PORTION OF A GAS TURBINE ENGINE 有权
    将空气从多级压缩机输送到气体涡轮发动机的涡轮机部分的系统

    公开(公告)号:US20090104020A1

    公开(公告)日:2009-04-23

    申请号:US11876277

    申请日:2007-10-22

    IPC分类号: F01B25/22

    CPC分类号: F02C6/08 F01D25/12

    摘要: A system for providing air from a multi-stage to a turbine includes a turbine having a high pressure input port and a low pressure input port. The system also includes a compressor having at least one high pressure extraction air output and at least one low pressure extraction air output. A valve is fluidly connected to the at least one high pressure extraction air output, at least one low pressure extraction air output and low pressure input port of the turbine. The valve is selectively operated to fluidly connect the at least one low pressure extraction air output with the low pressure input port during normal operating conditions and fluidly connect the at least one high pressure extraction air output and the low pressure input port during a turn down condition or below design temperature operation to enhance turbine engine performance.

    摘要翻译: 用于从多级到涡轮提供空气的系统包括具有高压输入端口和低压输入端口的涡轮机。 该系统还包括具有至少一个高压抽取空气输出和至少一个低压抽出空气输出的压缩机。 阀与流体连接至至少一个高压抽取空气输出,涡轮的至少一个低压抽取空气输出和低压输入端口。 选择性地操作阀,以在正常操作条件期间将至少一个低压抽取空气输出与低压输入端口流体连接,并且在转向状态期间流体连接至少一个高压抽取空气输出和低压输入端口 或低于设计温度运行,以提高涡轮发动机性能。

    Methods and systems for detecting gas turbine engine fuel leaks
    2.
    发明授权
    Methods and systems for detecting gas turbine engine fuel leaks 有权
    用于检测燃气涡轮发动机燃油泄漏的方法和系统

    公开(公告)号:US06761629B1

    公开(公告)日:2004-07-13

    申请号:US10680633

    申请日:2003-10-07

    IPC分类号: F02C700

    CPC分类号: F01D11/00 F02C9/00

    摘要: A method for detecting a fuel leak in a compartment is provided. The compartment includes at least one inlet and an exhaust outlet that is coupled in flow communication with the compartment and in flow communication with a fan. The method includes determining a fan speed, measuring a fuel leak gas concentration value, determining a fuel leak gas concentration limit value within the compartment based on the determined fan speed, comparing the measured fuel leak gas concentration value with the determined fuel leak gas concentration limit value, and generating at least one of an alarm signal and a trip signal based on the comparison.

    摘要翻译: 提供了一种用于检测隔室中的燃料泄漏的方法。 隔室包括至少一个入口和排气出口,其与隔室流动连通并与风扇流动连通。 该方法包括确定风扇速度,测量燃料泄漏气体浓度值,基于确定的风扇速度确定隔室内的燃料泄漏气体浓度极限值,将测量的燃料泄漏气体浓度值与确定的燃料泄漏气体浓度极限进行比较 值,并且基于该比较生成报警信号和跳闸信号中的至少一个。

    System for delivering air from a multi-stage compressor to a turbine portion of a gas turbine engine
    4.
    发明授权
    System for delivering air from a multi-stage compressor to a turbine portion of a gas turbine engine 有权
    用于将空气从多级压缩机输送到燃气涡轮发动机的涡轮机部分的系统

    公开(公告)号:US08057157B2

    公开(公告)日:2011-11-15

    申请号:US11876277

    申请日:2007-10-22

    CPC分类号: F02C6/08 F01D25/12

    摘要: A system for providing air from a multi-stage to a turbine includes a turbine having a high pressure input port and a low pressure input port. The system also includes a compressor having at least one high pressure extraction air output and at least one low pressure extraction air output. A valve is fluidly connected to the at least one high pressure extraction air output, at least one low pressure extraction air output and low pressure input port of the turbine. The valve is selectively operated to fluidly connect the at least one low pressure extraction air output with the low pressure input port during normal operating conditions and fluidly connect the at least one high pressure extraction air output and the low pressure input port during a turn down condition or below design temperature operation to enhance turbine engine performance.

    摘要翻译: 用于从多级到涡轮提供空气的系统包括具有高压输入端口和低压输入端口的涡轮机。 该系统还包括具有至少一个高压抽取空气输出和至少一个低压抽出空气输出的压缩机。 阀与流体连接至至少一个高压抽取空气输出,涡轮的至少一个低压抽取空气输出和低压输入端口。 选择性地操作阀,以在正常操作条件期间将至少一个低压抽取空气输出与低压输入端口流体连接,并且在转向状态期间流体连接至少一个高压抽取空气输出和低压输入端口 或低于设计温度运行,以提高涡轮发动机性能。