HEAT EXCHANGER ARTICLE WITH HOLLOW TUBE HAVING PLURALITY OF VANES
    37.
    发明申请
    HEAT EXCHANGER ARTICLE WITH HOLLOW TUBE HAVING PLURALITY OF VANES 审中-公开
    热交换器文章与具有多个空白的中空管

    公开(公告)号:US20160231065A1

    公开(公告)日:2016-08-11

    申请号:US14616819

    申请日:2015-02-09

    IPC分类号: F28F1/40

    CPC分类号: F28F1/40 F28F1/422

    摘要: A heat exchanger article includes a hollow tube that has a tube wall with an interior surface and an exterior surface. The interior surface defines a flow passage through the hollow tube. The hollow tube also includes a vane cluster in the flow passage. The vane cluster includes a plurality of vanes and each of the vanes extends inwardly from the tube wall.

    摘要翻译: 热交换器制品包括具有内壁和外表面的管壁的中空管。 内表面限定通过中空管的流动通道。 中空管还包括在流动通道中的叶片簇。 叶片簇包括多个叶片,并且每个叶片从管壁向内延伸。

    COOLED FUEL INJECTOR SYSTEM FOR A GAS TURBINE ENGINE
    38.
    发明申请
    COOLED FUEL INJECTOR SYSTEM FOR A GAS TURBINE ENGINE 审中-公开
    用于燃气涡轮发动机的冷却燃料喷射器系统

    公开(公告)号:US20160201917A1

    公开(公告)日:2016-07-14

    申请号:US14912117

    申请日:2014-08-14

    IPC分类号: F23R3/28 F02C7/18

    摘要: A fuel injector is provided for a gas turbine engine. The fuel injector includes a fuel conduit and a cooling fluid circuit through a strut. A gas turbine engine is provided that includes a multiple of fuel injectors in communication with a combustor and a cooling system in communication with each of the multiple of fuel injectors.

    摘要翻译: 燃气喷射器设置用于燃气涡轮发动机。 燃料喷射器包括通过支柱的燃料管道和冷却流体回路。 提供了一种燃气涡轮发动机,其包括与燃烧器连通的多个燃料喷射器和与多个燃料喷射器中的每一个连通的冷却系统。

    TUBE ASSEMBLY
    40.
    发明申请
    TUBE ASSEMBLY 有权
    管组件

    公开(公告)号:US20160003556A1

    公开(公告)日:2016-01-07

    申请号:US14789496

    申请日:2015-07-01

    IPC分类号: F28F1/00

    摘要: A tube assembly that may be for a fuel nozzle of a fuel system of a gas turbine engine may have a first tube defining a first flowpath along a centerline, a second tube generally spaced radially outward from the first tube with a first void located between and defined by the first and second tubes, and a support structure located in the first void and extending between the first and second tubes. The support structure is constructed and arranged to minimize or eliminate thermal conduction between the tubes. The entire assembly may be additive manufactured as one unitary piece. One example of a method of operation may include designed-for breakage of the structural support due to then al stresses thereby further minimizing thermal conduction between tubes.

    摘要翻译: 可用于燃气涡轮发动机的燃料系统的燃料喷嘴的管组件可以具有限定沿中心线的第一流动路径的第一管,大体上与第一管径向向外隔开的第二管, 由第一和第二管限定,以及位于第一空隙中并在第一和第二管之间延伸的支撑结构。 支撑结构被构造和布置成最小化或消除管之间的热传导。 整个组件可以是作为一体式制造的添加剂。 操作方法的一个实例可以包括由于由此而产生的结构支撑件的破坏,从而进一步最小化管之间的热传导。