Air-blast fuel-injector with shield-cone upstream of fuel orifices
    2.
    发明授权
    Air-blast fuel-injector with shield-cone upstream of fuel orifices 有权
    燃油喷射器具有屏蔽锥体,在燃油孔的上游

    公开(公告)号:US08347630B2

    公开(公告)日:2013-01-08

    申请号:US12203383

    申请日:2008-09-03

    IPC分类号: F02C1/00

    摘要: An air-blast fuel nozzle assembly includes a housing having an inner surface defining an interior chamber around a central axis. The inner surface terminates in an exit aperture. An air swirler pneumatically communicates with the interior chamber and has vanes operative to impart a swirling motion to air passing across the vanes and into the interior chamber. A fuel injection assembly includes a nozzle portion extending along the central axis and having a plurality of outlets circumferentially-arranged around the central axis that are directed into the interior chamber toward the inner surface of the housing. A shield extends radially outwardly from the nozzle portion upstream of the plurality of outlets. The shield extends between a base at the nozzle section and a free tip end such that the shield extends partially across the interior chamber toward the inner surface.

    摘要翻译: 鼓风燃料喷嘴组件包括壳体,壳体具有限定围绕中心轴线的内部腔室的内表面。 内表面终止于出口孔。 空气旋流器与内部室气动地连通并且具有可操作的叶片,以使空气通过叶片并进入内部空间。 燃料喷射组件包括沿着中心轴线延伸的喷嘴部分,并且具有围绕中心轴线周向布置的多个出口,这些出口朝向壳体的内表面引导进入内部腔室。 护罩从多个出口上游的喷嘴部分径向向外延伸。 护罩在喷嘴部分的基部和自由尖端之间延伸,使得护罩部分地穿过内部腔室朝向内表面延伸。

    Systems and Methods Involving Reduced Thermo-Acoustic Coupling of Gas Turbine Engine Augmentors
    3.
    发明申请
    Systems and Methods Involving Reduced Thermo-Acoustic Coupling of Gas Turbine Engine Augmentors 有权
    涉及燃气轮机发动机减速机热耦合的系统和方法

    公开(公告)号:US20100101208A1

    公开(公告)日:2010-04-29

    申请号:US12260436

    申请日:2008-10-29

    IPC分类号: F23R3/20

    摘要: Systems and methods reducing thermo-acoustic coupling of a gas turbine engine augmentors are provided. In this regard, a representative method includes: determining acoustic resonances and heat release phase relationships associated with the augmentor; and determining relative axial positions of a fuel injector and a flame holder of the augmentor that result in reduced thermo-acoustic coupling of the augmentor during operation.

    摘要翻译: 提供了减少燃气涡轮发动机增压器的热声耦合的系统和方法。 在这方面,代表性的方法包括:确定与增强器相关联的声共振和放热相位关系; 并且确定燃料喷射器和增压器的火焰保持器的相对轴向位置,其导致在操作期间增强器的热声耦合的减小。

    Phase resolved sampling system
    6.
    发明授权
    Phase resolved sampling system 失效
    相位解析抽样系统

    公开(公告)号:US5616870A

    公开(公告)日:1997-04-01

    申请号:US533591

    申请日:1995-09-25

    IPC分类号: G01N1/22 G01N1/24

    CPC分类号: G01N1/2247 G01N2001/2297

    摘要: A system and method periodically sample a fluid stream in a conduit for undergoing analysis thereof. A sampling tube having a probe is joined to the conduit for removing samples from the stream flowing therethrough. An analyzer is joined to the sampling tube for analyzing the removed samples. A solenoid valve is disposed in the tube for controlling flow of the samples to the analyzer. A dynamic pressure transducer is joined to the conduit so that a specific dynamic pressure reference frequency of the stream in the conduit may be locked-on to and used for periodically switching the solenoid valve open and closed for intermittently removing stream samples from the conduit at the reference frequency for channeling to the analyzer periodic stream samples at a sampling frequency corresponding to the reference frequency. In a preferred embodiment, the solenoid valve is switched open at a specific sampling phase in the sampling frequency, which phase may be indexed for obtaining different periodic samples at the sampling frequency for measuring periodic and short duration concentration fluctuations.

    摘要翻译: 系统和方法周期性地对管道中的流体流进行采样以进行分析。 具有探针的采样管被连接到导管,用于从流过其中的流中去除样品。 分析仪连接到采样管上,用于分析去除的样品。 电磁阀设置在管中,用于控制样品流向分析仪。 动态压力传感器连接到管道,使得管道中的流的特定动态压力参考频率可以被锁定并且用于周期性地切换电磁阀的打开和关闭,以间歇地从管道中去除流样品 以与参考频率相对应的采样频率向分析仪周期性流采样的参考频率。 在优选实施例中,电磁阀以采样频率的特定采样相位开关,该相位可以被索引,以便在采样频率处获得用于测量周期性和短持续时间浓度波动的不同周期性采样。

    Augmentor
    9.
    发明授权
    Augmentor 有权
    增强器

    公开(公告)号:US07093442B2

    公开(公告)日:2006-08-22

    申请号:US10426671

    申请日:2003-04-30

    申请人: Jeffery A. Lovett

    发明人: Jeffery A. Lovett

    IPC分类号: F02K3/10

    CPC分类号: F23R3/20 F02K3/10 F23R3/343

    摘要: A turbine engine augmentor has a centerbody within a gas flowpath. A flameholder is positioned in the flowpath outboard of the centerbody. A burner within the centerbody has an outlet for expelling combustion products of a first pilot fuel. A pilot fuel conduit has an outlet positioned to introduce a supplemental pilot fuel to the expelled combustion products.

    摘要翻译: 涡轮发动机增压器在气体流路内具有中心体。 火焰稳定器位于中心体外侧的流路中。 中心体内的燃烧器具有用于排出第一引燃燃料的燃烧产物的出口。 导向燃料导管具有出口,其定位成将补充的先导燃料引入排出的燃烧产物。