Double walled impingement cooled combustor
    41.
    发明授权
    Double walled impingement cooled combustor 失效
    双壁冲击冷却燃烧器

    公开(公告)号:US4109459A

    公开(公告)日:1978-08-29

    申请号:US551545

    申请日:1975-02-21

    CPC classification number: F23R3/08 F23R3/002 F05B2260/201 Y02T50/675

    Abstract: A combustor for use in a gas turbine engine is provided with a first wall defining a combustion zone; an outer casing partially defining a cooling plenum about the first wall; a second wall spaced apart from the first wall and defining together therewith a second plenum, the second wall bearing a plurality of perforations for passing fluid from the first plenum in impinging streams upon the first wall; and a plurality of ribs extending between the first and second walls and compartmentalizing the second plenum. The ribs add substantial stiffness to the combustor as well as providing for independently controlled cooling of the substantially isolated compartments formed thereby. The impinging streams provided by the perforations in the second wall substantially increase local fluid velocities and conductive heat transfer.

    Abstract translation: 用于燃气涡轮发动机的燃烧器设置有限定燃烧区的第一壁; 外壳,其围绕第一壁部分地限定冷却气室; 与所述第一壁间隔开并与其一起限定第二增压室的第二壁,所述第二壁承载多个穿孔,用于将来自所述第一增压室的流体流入所述第一壁; 以及在所述第一壁和所述第二壁之间延伸并且间隔所述第二增压室的多个肋。 这些肋向燃烧器增加了相当大的刚度,并且为由其形成的基本隔离的隔室提供独立控制的冷却。 由第二壁中的穿孔提供的冲击流基本上增加了局部流体速度和传导热传递。

    COMBUSTOR CAP ASSEMBLY
    47.
    发明申请

    公开(公告)号:US20160054004A1

    公开(公告)日:2016-02-25

    申请号:US14462646

    申请日:2014-08-19

    Abstract: A combustor cap assembly includes an annular shroud and an impingement plate coupled to the shroud. The impingement plate at least partially defines a plurality of impingement cooling holes and a cooling flow return passage. A cap plate is coupled to the impingement plate. The cap plate includes an impingement side which faces a second side portion of the impingement plate where the impingement side is axially spaced from the second side portion to define an impingement air plenum therebetween. The cooling flow return passage is in fluid communication with the impingement air plenum. A fluid conduit extends from a first side portion of the impingement plate towards a first end portion of the shroud. The fluid conduit is in fluid communication with the cooling flow return passage and provides for fluid communication out of the impingement air plenum.

    Abstract translation: 燃烧器盖组件包括环形护罩和联接到护罩的冲击板。 冲击板至少部分地限定多个冲击冷却孔和冷却流回流通道。 盖板联接到冲击板。 盖板包括面对冲击板的第二侧部的冲击侧,其中冲击侧与第二侧部轴向间隔开,以在其间限定冲击空气增压室。 冷却回流通道与冲击空气通风室流体连通。 流体导管从冲击板的第一侧部朝向护罩的第一端部延伸。 流体导管与冷却流回流通道流体连通,并提供流体连通到冲击空气通风室外。

    COMBUSTOR CAP ASSEMBLY
    48.
    发明申请

    公开(公告)号:US20160054003A1

    公开(公告)日:2016-02-25

    申请号:US14462639

    申请日:2014-08-19

    Abstract: A combustor cap assembly includes an impingement plate coupled to an annular shroud and a cap plate which is coupled to the impingement plate and forms an impingement air plenum therebetween. The cap assembly further includes a flow conditioning plate which is coupled to a forward end portion of the shroud. The flow conditioning plate includes an inner band portion, an outer band portion and an annular portion which extends radially therebetween. The annular portion includes upstream side, a downstream side and a plurality of flow conditioning passages which provide for fluid communication through the upstream and downstream sides. The inner band portion of the flow conditioning plate at least partially defines an exhaust channel. The exhaust channel is in fluid communication with the impingement air plenum and an exhaust outlet. The exhaust outlet is positioned to route cooling air from the impingement air plenum into an annular flow passage defined within a combustor.

    Abstract translation: 燃烧器盖组件包括联接到环形护罩的冲击板和联接到冲击板的盖板,并在其间形成冲击空气增压室。 盖组件还包括流动调节板,其联接到护罩的前端部分。 流量调节板包括内带部分,外带部分和径向地延伸的环形部分。 环形部分包括上游侧,下游侧和多个流动调节通道,其提供通过上游侧和下游侧的流体连通。 流量调节板的内带部分至少部分地限定排气通道。 排气通道与冲击空气通风室和排气出口流体连通。 排气出口被定位成将冷却空气从冲击空气压力通道引导到限定在燃烧器内的环形流动通道中。

    TURBINE ENGINE COMBUSTOR WALL WITH NON-UNIFORM DISTRIBUTION OF EFFUSION APERTURES
    49.
    发明申请
    TURBINE ENGINE COMBUSTOR WALL WITH NON-UNIFORM DISTRIBUTION OF EFFUSION APERTURES 有权
    涡轮发动机燃烧器壁与非均匀分布的冲击力

    公开(公告)号:US20130340437A1

    公开(公告)日:2013-12-26

    申请号:US13531132

    申请日:2012-06-22

    Abstract: A turbine engine combustor wall includes support shell and a heat shield. The support shell includes shell quench apertures, first impingement apertures, and second impingement apertures. The combustor heat shield includes shield quench apertures fluidly coupled with the shell quench apertures, first effusion apertures fluidly coupled with the first impingement apertures, and second effusion apertures fluidly coupled with the second impingement apertures. The shield quench apertures and the first effusion apertures are configured in a first axial region of the heat shield, and the second effusion apertures are configured in a second axial region of the heat shield located axially between the first axial region and a downstream end of the heat shield. A density of the first effusion apertures in the first axial region is greater than a density of the second effusion apertures in the second axial region.

    Abstract translation: 涡轮发动机燃烧器壁包括支撑壳和隔热罩。 支撑壳包括壳体淬火孔,第一冲击孔和第二冲击孔。 燃烧器热屏蔽包括与壳体骤冷孔流体耦合的屏蔽骤冷孔,与第一冲击孔流体连接的第一渗出孔以及与第二冲击孔流体连接的第二渗出孔。 所述屏蔽骤冷孔和所述第一渗出孔构造在所述隔热罩的第一轴向区域中,并且所述第二渗出孔构造在所述隔热罩的第二轴向区域中,所述第二轴向区域轴向位于所述第一轴向区域和所述第一轴向区域的下游端之间 隔热板。 第一轴向区域中的第一渗出孔的密度大于第二轴向区域中的第二渗出孔的密度。

    BIDIRECTIONAL PUMPING & ENERGY RECOVERY SYSTEM
    50.
    发明申请
    BIDIRECTIONAL PUMPING & ENERGY RECOVERY SYSTEM 有权
    双向抽水和能源回收系统

    公开(公告)号:US20120153620A1

    公开(公告)日:2012-06-21

    申请号:US13026057

    申请日:2011-02-11

    Abstract: A fluid pumping and energy recovery device may include a housing that defines an impeller chamber and a motor/generator chamber. An impeller may reside within the impeller chamber; and a motor/generator may reside in the motor/generator chamber. The motor/generator may include a stator and a rotor. The rotor may be coupled to the impeller and supported (e.g., by magnetic bearings) to rotate in the stator. The rotor may generate electrical power in a generating mode and rotate in response to electrical power applied to the stator in a motoring mode. Seals may be adapted to hydraulically isolate the pump chamber from the motor/generator chamber by sealing against a rotating surface of the device. In certain instances, sealing is achieved using a bidirectional seal.

    Abstract translation: 流体泵送和能量回收装置可以包括限定叶轮室和马达/发电机室的壳体。 叶轮可以驻留在叶轮室内; 并且电动机/发电机可以驻留在电动机/发电机室中。 马达/发电机可以包括定子和转子。 转子可以联接到叶轮并且被支撑(例如通过磁性轴承)以在定子中旋转。 转子可以在发电模式下产生电力并且响应于以电动模式施加到定子的电力而旋转。 密封件可以适于通过密封装置的旋转表面来将泵室与电动机/发电机室液压隔离。 在某些情况下,使用双向密封实现密封。

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