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    GAS TURBINE ENGINE COOLING FLUID METERING SYSTEM
    2.
    发明申请
    GAS TURBINE ENGINE COOLING FLUID METERING SYSTEM 审中-公开
    气体涡轮发动机冷却流量计量系统

    公开(公告)号：US20160047311A1

    公开(公告)日：2016-02-18

    申请号：US14818944

    申请日：2015-08-05

    Applicant: United Technologies Corporation

    Inventor： John H. Mosley ,  Michelle Diana Stearns ,  Michael Luther Comeau ,  James P. Chasse

    IPC: F02C7/12 ,  F02C3/04

    CPC classification number: F02C7/12 ,  F01D25/12 ,  F02C3/04 ,  F02C7/18 ,  G01F1/42 ,  Y02T50/675

    Abstract: A cooling fluid system for a gas turbine engine includes a fluid source. A turbine section includes first and second components. A fluid supply system has a primary pipe that is configured to provide a cooling supply fluid from the fluid source to a fluid fitting having a fluid junction. The fluid junction is in fluid communication with and is configured to supply a first cooling fluid to the first component. The fluid junction is in fluid communication with and is configured to supply a second cooling fluid to the second component. A flow meter is upstream from the fluid junction and is configured to receive the cooling supply fluid.

    Abstract translation: 用于燃气涡轮发动机的冷却流体系统包括流体源。 涡轮部分包括第一和第二部件。 流体供应系统具有主管，其被构造成将冷却供给流体从流体源提供到具有流体结的流体配件。 流体连接处与第一部件流体连通并且构造成将第一冷却流体供应到第一部件。 流体连接点与第二部件流体连通并且构造成将第二冷却流体供应到第二部件。 流量计位于流体接头的上游，并被配置为接收冷却供应流体。

    Gas turbine engine cooling fluid metering system
    3.
    发明授权
    Gas turbine engine cooling fluid metering system 有权

    公开(公告)号：US11939919B2

    公开(公告)日：2024-03-26

    申请号：US16439090

    申请日：2019-06-12

    Applicant: United Technologies Corporation

    Inventor： John H. Mosley ,  Michelle Diana Stearns ,  Michael Luther Comeau ,  James P. Chasse

    IPC: F02C7/12 ,  F01D25/12 ,  F02C3/04 ,  F02C7/18 ,  G01F1/42

    CPC classification number: F02C7/12 ,  F01D25/12 ,  F02C3/04 ,  F02C7/18 ,  G01F1/42 ,  Y02T50/60

    Abstract: A fluid supply system for a gas turbine engine includes a first component and a second component. A fluid fitting has a fluid junction. The fluid junction includes a first fluid port in fluid communication with and configured to supply a first cooling fluid to the first component. The fluid junction includes a second fluid port in fluid communication with and configured to supply a second cooling fluid to the second component. A primary pipe is fluidly connected to the fluid fitting. A flow meter is arranged upstream from the fluid junction and is configured to receive a cooling supply fluid from a fluid source. Thee flow meter is a wall having an orifice and a surface that is radiused and convex facing into the cooling supply fluid. A secondary pipe is secured to the fluid fitting and is configured to supply the second cooling fluid to the second component. A turbine section includes the first and second components. The primary pipe is configured to provide the cooling supply fluid from the fluid source to the fluid fitting.

    GAS TURBINE ENGINE COOLING FLUID METERING SYSTEM
    5.
    发明申请
    GAS TURBINE ENGINE COOLING FLUID METERING SYSTEM 审中-公开

    公开(公告)号：US20200032711A1

    公开(公告)日：2020-01-30

    申请号：US16439090

    申请日：2019-06-12

    Applicant: United Technologies Corporation

    Inventor： John H. Mosley ,  Michelle Diana Stearns ,  Michael Luther Comeau ,  James P. Chasse

    IPC: F02C7/12 ,  F01D25/12 ,  F02C7/18 ,  F02C3/04

    Abstract: A fluid supply system for a gas turbine engine includes a first component and a second component. A fluid fitting has a fluid junction. The fluid junction includes a first fluid port in fluid communication with and configured to supply a first cooling fluid to the first component. The fluid junction includes a second fluid port in fluid communication with and configured to supply a second cooling fluid to the second component. A primary pipe is fluidly connected to the fluid fitting. A flow meter is arranged upstream from the fluid junction and is configured to receive a cooling supply fluid from a fluid source. Thee flow meter is a wall having an orifice and a surface that is radiused and convex facing into the cooling supply fluid. A secondary pipe is secured to the fluid fitting and is configured to supply the second cooling fluid to the second component. A turbine section includes the first and second components. The primary pipe is configured to provide the cooling supply fluid from the fluid source to the fluid fitting.

    PRE-SKEWED CAPTURE PLATE
    9.
    发明申请
    PRE-SKEWED CAPTURE PLATE 有权
    预先捕获的板

    公开(公告)号：US20160341123A1

    公开(公告)日：2016-11-24

    申请号：US14715876

    申请日：2015-05-19

    Applicant: United Technologies Corporation

    Inventor： Pawel Socha ,  Usman Khan ,  Richard Joseph Bulkovitch, JR. ,  Michael Luther Comeau ,  Jonathan C. Reuben ,  Kelsey Honious

    IPC: F02C7/06 ,  F02C3/06 ,  F02C7/20

    CPC classification number: F02C7/06 ,  F01D9/065 ,  F02C3/06 ,  F02C7/20 ,  F05D2220/32 ,  F05D2230/60 ,  Y02T50/672

    Abstract: A coupling arrangement for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a conduit between a first frame case defining a frame axis and a second frame case. A flange is coupled to the conduit defining a first axis and abuts the first frame case. A capture plate coupled to the conduit defines a second axis and abuts the second frame case. The first axis is offset relative to the second axis in an axial direction relative to the frame axis.

    Abstract translation: 根据本公开的示例性方面的用于燃气涡轮发动机的联接装置尤其包括限定框架轴线的第一框架壳体与第二框架壳体之间的导管。 凸缘联接到限定第一轴线的导管并且邻接第一框架壳体。 联接到导管的捕获板限定第二轴线并邻接第二框架壳体。 第一轴线相对于第二轴线相对于框架轴线沿轴向方向偏移。

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