LOW EMISSIONS COMBUSTOR ASSEMBLY FOR GAS TURBINE ENGINE

    公开(公告)号:US20190032559A1

    公开(公告)日:2019-01-31

    申请号:US15658464

    申请日:2017-07-25

    摘要: A combustor assembly for a gas turbine engine according to an example of the present disclosure includes, among other things, a combustion chamber, and a fuel injector assembly in communication with the combustion chamber that has a swirler body situated about a nozzle to define an injector passage that converges to a throat. The throat is defined at a distance from the combustion chamber. The nozzle includes a primary fuel injector along a first fuel injector axis and at least one secondary plain jet fuel injector axially forward of the primary fuel injector.

    Multiple-excitation multiple-receiving (MEMR) capacitance tomography
    7.
    发明授权
    Multiple-excitation multiple-receiving (MEMR) capacitance tomography 有权
    多激发多重接收(MEMR)电容层析成像

    公开(公告)号:US09581560B2

    公开(公告)日:2017-02-28

    申请号:US14813925

    申请日:2015-07-30

    摘要: A method for operating a sensor, including simultaneously exciting a first set of electrodes and sensing an output of each electrode of a second set of electrodes, storing output data corresponding to the output of each electrode of the second set of electrodes in a memory storage device, shifting at least one electrode from the first set of electrodes to the second set of electrodes and at least one electrode from the second set of electrodes to the first set of electrodes, and repeating the simultaneously exciting and sensing, the storing, and the shifting until an output data has been stored for each possible pair of electrodes in the first and second set of electrodes.

    摘要翻译: 一种用于操作传感器的方法,包括同时激励第一组电极并感测第二组电极的每个电极的输出,将与第二组电极的每个电极的输出相对应的输出数据存储在存储器存储装置 将至少一个电极从第一组电极移动到第二组电极,以及将至少一个电极从第二组电极移动到第一组电极,并重复同时激发和感测,存储和移位 直到在第一和第二组电极中的每对可能的电极存储输出数据。

    MIXER ASSEMBLY FOR A GAS TURBINE ENGINE
    8.
    发明申请
    MIXER ASSEMBLY FOR A GAS TURBINE ENGINE 有权
    燃气轮机发动机混合器总成

    公开(公告)号:US20150121882A1

    公开(公告)日:2015-05-07

    申请号:US14593877

    申请日:2015-01-09

    IPC分类号: F23R3/28

    摘要: A mixer assembly for a gas turbine engine is provided, including a main mixer with fuel injection holes located between at least one radial swirler and at least one axial swirler, wherein the fuel injected into the main mixer is atomized and dispersed by the air flowing through the radial swirler and the axial swirler.

    摘要翻译: 提供了一种用于燃气涡轮发动机的混合器组件,包括具有位于至少一个径向旋流器和至少一个轴向旋流器之间的燃料喷射孔的主混合器,其中喷射到主混合器中的燃料被流过的空气雾化和分散 径向旋流器和轴向旋流器。

    MAIN MIXER FOR A GAS TURBINE ENGINE COMBUSTOR

    公开(公告)号:US20180156463A1

    公开(公告)日:2018-06-07

    申请号:US15371615

    申请日:2016-12-07

    IPC分类号: F23R3/28 F23R3/14

    摘要: A main mixer including a swirler along an axis, the swirler including an outer swirler with a multiple of outer vanes, and a center swirler with a multiple of center vanes and a swirler hub along the axis, the swirler hub including a fuel manifold and an inner swirler with a multiple of inner vanes that support a centerbody, the multiple of inner vanes interconnect the fuel manifold and the centerbody.