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    Tangential entry fuel nozzle
    11.
    发明公开
    Tangential entry fuel nozzle 失效
    TangentialeBrennstoffeintrittsdüse

    公开(公告)号：EP0849529A2

    公开(公告)日：1998-06-24

    申请号：EP97310463.1

    申请日：1997-12-22

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Snyder, Timothy S. ,  Sowa, William A. ,  Kramer, Stephen K.

    IPC: F23C7/00 ,  F23D17/00

    CPC classification number: F23D17/002 ,  F05B2250/322 ,  F23C7/002 ,  F23C2900/07002

    Abstract: A method of reducing the tendency of the combustion flame to attach to the centerbody of a tangential entry nozzle 10 is disclosed which comprises mixing fuel and air in a mixing zone 28 within a fuel nozzle assembly, thereby producing a first fuel/air mixture, which is isolated from the combustion products by maintaining sufficiently high axial velocities throughout the mixing zone.
    The nozzle has a longitudinal axis 26 and two cylindrical-arc scrolls 22,24 with the centerline of each offset from that of the other. Overlapping ends of these scrolls form an air inlet slot therebetween for the introduction of an air/fuel mixture into the fuel nozzle. A combustor-end endplate 18 has a central opening 20 to permit air and fuel to exit into a combustor, while at the opposite end another endplate 16 blocks the nozzle flow area. The scrolls are secured between these endplates. A centerbody 12 is located between the scrolls coaxial with the axis. The centerbody 12 has a base 58 which includes at least one air supply port extending therethrough, and an internal passageway 64. It includes a frustum portion (54) and aerodynamic ramps theat prevent flow reversal and flame stabilisation between the endplates 16,18.

    Abstract translation: 公开了一种降低燃烧火焰附着到切向入口喷嘴10的中心体的趋势的方法，其包括将燃料和空气混合在燃料喷嘴组件内的混合区28中，从而产生第一燃料/空气混合物， 通过在整个混合区域保持足够高的轴向速度与燃烧产物隔离。 喷嘴具有纵向轴线26和两个圆柱形涡卷22,24，其中心线各自偏离另一个。 这些涡卷的重叠端部在其间形成空气入口槽，用于将空气/燃料混合物引入燃料喷嘴。 燃烧器端端板18具有中心开口20，以允许空气和燃料排出到燃烧器中，而在相对端，另一端板16阻挡喷嘴流动区域。 涡卷固定在这些端板之间。 中心体12位于与轴线同轴的涡卷之间。 中心体12具有基部58，其包括延伸穿过其中的至少一个空气供应端口和内部通道64.其包括平截头体部分（54）和空气动力学斜坡，以防止端板16,18之间的流动反转和火焰稳定。

    Fuel nozzles and centerbodies therefor
    16.
    发明公开
    Fuel nozzles and centerbodies therefor 失效
    BrennstoffdüsenundZentralkörperdafür

    公开(公告)号：EP0849530A2

    公开(公告)日：1998-06-24

    申请号：EP97310464.9

    申请日：1997-12-22

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Kramer, Stephen K. ,  Hauck, Stephen F. ,  Snyder, Timothy S. ,  Sowa, William A.

    IPC: F23C7/00 ,  F23D17/00

    CPC classification number: F23C7/002 ,  F05B2250/232 ,  F05B2250/322 ,  F23C2900/07002 ,  F23D17/002

    Abstract: A tangential air entry fuel nozzle (10) has a combustor inlet port (20) to permit air and fuel to exit into a combustor (56). The port includes a convergent surface (116), a combustor surface, and a cylindrical surface (118) extending therebetween. The convergent surface extends a first distance along the longitudinal axis (26) of the nozzle, the cylindrical surface extends a second distance along the axis, and the second distance is at least 30% of the first distance.

    Abstract translation: 切向进气燃料喷嘴（10）具有燃烧器入口（20），以允许空气和燃料离开燃烧器（56）。 该端口包括会聚表面（116），燃烧器表面和在它们之间延伸的圆柱形表面（118）。 会聚表面沿着喷嘴的纵向轴线（26）延伸第一距离，圆柱形表面沿轴线延伸第二距离，第二距离为第一距离的至少30％。

    Two stream tangential entry nozzle
    17.
    发明公开
    Two stream tangential entry nozzle 失效
    Tangentiale ZweistromEintrittsdüse

    公开(公告)号：EP0849528A2

    公开(公告)日：1998-06-24

    申请号：EP97310460.7

    申请日：1997-12-22

    Applicant: UNITED TECHNOLOGIES CORPORATION

    Inventor： Kramer, Stephen K. ,  Hauck, Peter F.

    IPC: F23C7/00 ,  F23D17/00

    CPC classification number: F23D17/002 ,  F23C7/002 ,  F23C2900/07002 ,  F23D14/02 ,  F23D2206/10

    Abstract: A tangential air entry fuel nozzle 10 has a combustor inlet port 20 to permit air and fuel to exit into a combustor. The port includes a convergent surface 116, a divergent surface 117, and a cylindrical surface 118 extending therebetween. The convergent surface 116 extends a first distance along the longitudinal axis of the nozzle, the cylindrical surface 118 extends a second distance along the axis, and the second distance is at least 5% of the first distance.

    Abstract translation: 切向空气进入燃料喷嘴10具有燃烧器入口20，以允许空气和燃料离开燃烧器。 该端口包括会聚表面116，发散表面117和在它们之间延伸的圆柱形表面118。 会聚表面116沿着喷嘴的纵向轴线延伸第一距离，圆柱形表面118沿轴线延伸第二距离，第二距离为第一距离的至少5％。

    DECOUPLED GAS TURBINE ENGINE
    19.
    发明公开
    DECOUPLED GAS TURBINE ENGINE 审中-公开
    ENTKOPPELTER GASTURBINENMOTOR

    公开(公告)号：EP2993330A1

    公开(公告)日：2016-03-09

    申请号：EP15183631.9

    申请日：2015-09-03

    Applicant: United Technologies Corporation

    Inventor： Suciu, Gabriel L. ,  Kramer, Stephen K. ,  Chandler, Jesse M.

    IPC: F02C3/10

    CPC classification number: F01D9/02 ,  F01D5/04 ,  F01D5/06 ,  F01D13/003 ,  F02C3/04 ,  F02C3/05 ,  F02C3/085 ,  F02C3/10 ,  F02C3/103 ,  F02C3/14 ,  F02C7/04 ,  F05D2220/32 ,  F05D2240/24 ,  F05D2240/35 ,  F05D2250/312 ,  F05D2250/314

    Abstract: A gas turbine engine (20) includes a high spool assembly (22) and a low spool assembly (26) each having a rotational axis (24, 28) that are spaced from one-another. The engine further includes a combustor (30) that may have a centerline (44) spaced from the rotational axes of each spool assembly (22, 26). Turning ducts (50, 52, 54, 56) of the engine are configured to re-direct airflow from one spool assembly (26) to the next and/or between one spool assembly (24, 26) and the combustor (30).

    Abstract translation: 一种燃气涡轮发动机（20）包括一个高阀芯组件（22）和一个具有与另一个间隔开的旋转轴线（24,28）的低阀芯组件（26）。 发动机还包括燃烧器（30），其可以具有与每个阀芯组件（22,26）的旋转轴线间隔开的中心线（44）。 发动机的转向管道（50,52,54,56）构造成将气流从一个线轴组件（26）重新引导到下一个和/或在一个线轴组件（24,26）和燃烧器（30）之间和/或之间。

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