Premixer for a combustor
    72.
    发明授权

    公开(公告)号:US11713881B2

    公开(公告)日:2023-08-01

    申请号:US16737040

    申请日:2020-01-08

    CPC classification number: F23R3/286 F23R3/14 F23C7/004 F23R3/16

    Abstract: A premixer for a combustor includes: a centerbody having a hollow interior cavity; a swirler assembly radially outward of the centerbody; a peripheral wall disposed radially outward of the centerbody and the swirler assembly such that a mixing duct is defined between the peripheral wall and the centerbody, downstream from the swirler assembly; an annular splitter radially inward of the swirler assembly and radially outward of the centerbody such that a radial gap is defined between the splitter and an outer surface of the centerbody, wherein the splitter includes a trailing edge which extends axially aft of the swirler assembly; a fuel gallery disposed inside the interior cavity of the centerbody; and at least one fuel injector extending outward from the fuel gallery and passing through an injector port communicating with the outer surface of the splitter.

    SWIRL STABILIZED HIGH CAPACITY DUCT BURNER
    73.
    发明申请

    公开(公告)号:US20180216814A1

    公开(公告)日:2018-08-02

    申请号:US15505917

    申请日:2015-08-25

    Abstract: The present disclosure includes air spinners for use in duct burners, and duct burners and duct burner kits including a plurality of air spinners. Air spinners may include a plurality of blades extending radially outward from a fuel path and configured to impart rotation to air flowing between the blades, where the air spinner is configured to be coupled to a fuel runner of a duct burner such that the air spinner encircles a fuel outlet of the fuel runner with the axis of the fuel path extending at a non-parallel angle from an axis of the fuel runner. Duct burners can comprise a plurality of air spinners coupled to a plurality of fuel runners. Duct burner kits can comprise a plurality of air spinners configured to be coupled (e.g., without welding) to a plurality of fuel runners.

    Axial swirler
    78.
    发明授权
    Axial swirler 有权
    轴流旋流器

    公开(公告)号:US09557061B2

    公开(公告)日:2017-01-31

    申请号:US14072170

    申请日:2013-11-05

    CPC classification number: F23R3/14 F23C7/004 F23D2900/14021 F23R3/286 F23R3/36

    Abstract: An axial swirler, in particular for premixing of oxidizer and fuel in gas turbines, includes a series of swirl vanes with a streamline cross-section. Each swirl vane has a leading edge, a trailing edge, and a suction side and a pressure side extending each between the leading and trailing edges. The swirl vanes are arranged around a swirler axis, wherein the leading edges extend essentially in radial direction. Flow slots are formed between the suction side of each swirl vane and the pressure side of its nearest neighboring swirl vane. Furthermore, at least one swirl vane has a discharge flow angle between a tangent to its camber line at its trailing edge and the swirler axis that is monotonically increasing with increasing radial distance from the swirler axis. The invention also relates to a burner with such a swirler and a method of operating the burner.

    Abstract translation: 特别是用于燃气轮机中氧化剂和燃料的预混合的轴向旋流器包括一系列具有流线横截面的旋流叶片。 每个旋流叶片具有前缘,后缘以及每个在前缘和后缘之间延伸的吸力侧和压力侧。 涡旋叶片围绕旋流器轴线布置,其中前缘基本上沿径向延伸。 流动槽形成在每个涡流叶片的吸力侧和其最近的相邻旋流叶片的压力侧之间。 此外,至少一个旋流叶片具有在其后缘处的其弯曲线的切线与旋流器轴线之间的排出流动角度,该旋流器轴线随着距旋流器轴线的径向距离的增加而单调增加。 本发明还涉及具有这种旋流器的燃烧器和操作燃烧器的方法。

    COMBUSTOR
    79.
    发明申请
    COMBUSTOR 审中-公开

    公开(公告)号:US20170009994A1

    公开(公告)日:2017-01-12

    申请号:US15113429

    申请日:2015-01-06

    Abstract: A burner includes a pilot burner, a combustion chamber, and a swirler located radially outwardly of the combustion chamber and being adapted to impose a swirling motion on a fuel/air mixture about an axial centerline of the combustion chamber. The pilot burner has a pilot burner face located radially inwardly of the swirler and forms an axially upstream wall of the combustion chamber, the pilot burner face incorporating a pilot fuel injector and an ignitor, both being positioned radially offset from the axial centerline. A recess is positioned radially offset from the axial centerline within the pilot burner face.

    Abstract translation: 燃烧器包括引燃燃烧器,燃烧室和位于燃烧室径向外侧的旋流器,并且适于在燃烧室周围的燃料/空气混合物附近施加涡旋运动。 导向燃烧器具有位于旋流器径向内侧的导向燃烧器表面,并形成燃烧室的轴向上游壁,引燃燃烧器表面包括引燃燃料喷射器和点火器,两者均位于径向偏离轴线中心线的位置。 凹口位于导向燃烧器表面内径向偏离轴向中心线的位置。

    LOW NET-SWIRL CONFIGURATIONS FOR GAS TURBINE ENGINE COMBUSTORS
    80.
    发明申请
    LOW NET-SWIRL CONFIGURATIONS FOR GAS TURBINE ENGINE COMBUSTORS 审中-公开
    用于气体涡轮发动机燃烧器的低网速配置

    公开(公告)号:US20160258627A1

    公开(公告)日:2016-09-08

    申请号:US14636689

    申请日:2015-03-03

    CPC classification number: F23R3/14 F23C7/004 F23R3/06 F23R3/286

    Abstract: The present disclosure relates to gas turbine engines, and in particular to combustor swirlers and swirler configurations. In one embodiment, a swirler includes an inner passage for receiving a fuel injector and a plurality of outer passages concentrically arranged around the inner passage. The plurality of outer passages include an outer vane assembly including a plurality of vane elements arranged at a first angle and a first middle vane assembly include a plurality of vane elements arranged at a second angle, wherein the outer vane assembly is concentrically arranged around the first middle vane assembly, and wherein the outer vane assembly and first middle vane assembly are configured to produce a low net-swirl to control the penetration depth and improve premixing of a fuel air mixture for the fuel injector. According to another embodiment, the swirler includes a second middle vane assembly include a plurality of vane elements arranged at a third angle.

    Abstract translation: 本公开涉及燃气涡轮发动机,特别涉及燃烧器旋流器和旋流器构造。 在一个实施例中,旋流器包括用于接收燃料喷射器的内部通道和围绕内部通道同心地布置的多个外部通道。 多个外部通道包括外部叶片组件,该外部叶片组件包括以第一角度布置的多个叶片元件,第一中间叶片组件包括以第二角度布置的多个叶片元件,其中外部叶片组件围绕第一角度同心地布置 中间叶片组件,并且其中外部叶片组件和第一中间叶片组件构造成产生低的网络涡流以控制穿透深度并改善用于燃料喷射器的燃料空气混合物的预混合。 根据另一个实施例,旋流器包括第二中间叶片组件,其包括以第三角度布置的多个叶片元件。

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