GAS TURBINE ASSEMBLIES AND METHODS
    21.
    发明申请

    公开(公告)号:US20190093891A1

    公开(公告)日:2019-03-28

    申请号:US15714118

    申请日:2017-09-25

    Abstract: The systems and methods described herein relate to a dome of a gas turbine assembly configured to suppress pressure pulsations. The systems and methods provide a dome having an aperture configured to surround an injector assembly of a combustor. The dome having a front panel extending radially from the aperture. The systems and methods couple a first cavity to the front panel. The first cavity includes a series of ducts. A first duct of the series of ducts is configured to receive airflow into the first cavity from a compressor and a second set of ducts of the series of ducts and a third duct of the series of ducts are configured to direct airflow to the combustor from the first cavity, wherein the third duct has a larger diameter than the second set of ducts.

    Systems and methods for measuring temperature in a gas turbine using acoustic interference

    公开(公告)号:US09989423B2

    公开(公告)日:2018-06-05

    申请号:US14611639

    申请日:2015-02-02

    CPC classification number: G01K11/22 G01K13/02 G01K2013/024

    Abstract: Systems and methods for measuring temperature in a gas turbine are disclosed. The method can include directing a first acoustic signal towards a gas path in a turbine; directing a second acoustic signal towards the gas path in the turbine; receiving the first acoustic signal and the second acoustic signal at a downstream gas path location; combining the first acoustic signal and the second acoustic signal to create a combined acoustic signal, where a portion of the first acoustic signal cancels out a portion of the second acoustic signal; and determining a temperature of the gas path based at least in part on the combined acoustic signal.

    Systems and Methods for Measuring Temperature in a Gas Turbine Using Acoustic Interference
    23.
    发明申请
    Systems and Methods for Measuring Temperature in a Gas Turbine Using Acoustic Interference 审中-公开
    使用声学干涉测量燃气轮机温度的系统和方法

    公开(公告)号:US20160341606A1

    公开(公告)日:2016-11-24

    申请号:US15229613

    申请日:2016-08-05

    CPC classification number: G01K11/22 G01K13/02 G01K2013/024 G01M15/14

    Abstract: Systems and methods for measuring temperature in a gas turbine are disclosed. The method can include directing a first acoustic signal and a second acoustic signal towards a gas path in a turbine; receiving the first acoustic signal and the second acoustic signal at a downstream gas path location; combining the first acoustic signal and the second acoustic signal to create a combined acoustic signal, wherein the combined acoustic signal forms at least one of either a signal maxima or a signal minima; and based at least in part on the combined acoustic signal, determining a temperature of the gas path.

    Abstract translation: 公开了一种用于测量燃气轮机温度的系统和方法。 该方法可以包括将第一声信号和第二声信号引向涡轮机中的气体路径; 在下游气体路径位置处接收第一声信号和第二声信号; 组合所述第一声信号和所述第二声信号以产生组合声信号,其中所述组合声信号形成信号最大值或信号最小值中的至少一个; 并且至少部分地基于组合的声信号,确定气体路径的温度。

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