Detecting flashback by monitoring engine-dynamic spikes
    2.
    发明授权
    Detecting flashback by monitoring engine-dynamic spikes 有权
    通过监视引擎动态尖峰来检测闪回

    公开(公告)号:US09376963B2

    公开(公告)日:2016-06-28

    申请号:US13742401

    申请日:2013-01-16

    Abstract: A tuning process is provided for dynamically tuning a gas-turbine (GT) engine to correct for flashback events without directly measuring occurrences of the flashback events at the GT engine. Initially, readings are taken that measure low-frequency dynamics at the GT engine. A determination of whether flashback criteria are met by an instantaneous signal that quantifies a detected spike within the measured low-frequency dynamics is carried out, where the flashback criteria include the following: identifying the spike overcomes a multiple of an average of the low-frequency dynamics measured over a predefined period of time; and identifying the spike overcomes a preestablished minimum amplitude. Upon the spike meeting the flashback criteria, a count is added to a running record of spikes, which is compared to an alarm limit. If the alarm limit is triggered, action(s) are invoked to address the flashback events, such as adjusting fuel-flow splits of the GT engine.

    Abstract translation: 提供了一种调节过程,用于动态调整燃气轮机(GT)发动机,以校正闪回事件,而不直接测量GT发动机的闪回事件的发生。 最初,采用测量GT发动机低频动力学的读数。 执行闪光标准是否通过在所测量的低频动态中量化检测到的尖峰的瞬时信号来满足闪回标准,其中闪回标准包括以下:识别尖峰克服了低频的平均值的倍数 动态测量在预定义的时间段内; 并且识别尖峰克服了预先建立的最小幅度。 当峰值满足闪回标准时,会将一个计数添加到运行中的尖峰记录,与报警限制进行比较。 如果触发报警限制,则调用动作来解决闪回事件,例如调整GT引擎的燃油流量分配。

    SEQUENTIAL COMBUSTION WITH DILUTION GAS MIXER
    3.
    发明申请
    SEQUENTIAL COMBUSTION WITH DILUTION GAS MIXER 有权
    与稀释气体混合器连续燃烧

    公开(公告)号:US20150159876A1

    公开(公告)日:2015-06-11

    申请号:US14626003

    申请日:2015-02-19

    Abstract: The invention refers to a sequential combustor arrangement comprising a first burner, a first combustion chamber, a mixer for admixing a dilution gas via a dilution gas inlet to the hot gases leaving the first combustion chamber during operation, a second burner, and a second combustion chamber arranged sequentially in a fluid flow connection. The sequential combustor arrangement further includes four cooling zones with a cooling channel. During operation a cooling gas flows through the cooling channels. The disclosure further refers to a method for operating a gas turbine with such a sequential combustor arrangement.

    Abstract translation: 本发明涉及连续的燃烧器装置,其包括第一燃烧器,第一燃烧室,用于将稀释气体经由稀释气体入口混合到在运行期间离开第一燃烧室的热气体的混合器,第二燃烧器和第二燃烧器 腔室依次布置在流体流动连接中。 顺序燃烧器装置还包括具有冷却通道的四个冷却区。 在运行期间,冷却气体流过冷却通道。 本发明还涉及一种用这种连续燃烧器装置操作燃气轮机的方法。

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