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    Gas turbine engine compressor with a biased inner ring
    1.
    发明授权
    Gas turbine engine compressor with a biased inner ring 有权
    具有偏置内圈的燃气涡轮发动机压缩机

    公开(公告)号：US09341194B2

    公开(公告)日：2016-05-17

    申请号：US13666758

    申请日：2012-11-01

    Applicant: Solar Turbines Incorporated

    Inventor： John Frederick Lockyer

    IPC: F04D29/56 ,  F01D17/16 ,  F01D11/00

    CPC classification number: F04D29/563 ,  F01D11/001 ,  F01D17/162 ,  F05D2300/501

    Abstract: An inner bushing assembly (280) to provide a biasing force between a guide vane (260) and an inner ring half (261) of a gas turbine engine compressor (200) is disclosed. The inner bushing assembly (280) includes a first bushing (281), a second bushing (282), and a biasing element (283). The first bushing (281) is configured to be installed about an inner vane shaft (267) of the guide vane (260) adjacent to an airfoil (265) of the guide vane (260). The second bushing (282) is configured to be installed about the inner vane shaft (267) distal to the airfoil (265). The biasing element (283) is configured to be installed about the inner vane shaft (267) between the first bushing (281) and the second bushing (282).

    Abstract translation: 公开了一种用于在燃气涡轮发动机压缩机（200）的引导叶片（260）和内环半部（261）之间提供偏置力的内衬套组件（280）。 内衬套组件（280）包括第一衬套（281），第二衬套（282）和偏压元件（283）。 第一衬套（281）构造成围绕与导叶（260）的翼型件（265）相邻的导叶（260）的内叶片轴（267）安装。 第二衬套（282）构造成围绕翼型（265）远侧的内叶片轴（267）安装。 偏置元件（283）构造成围绕第一衬套（281）和第二衬套（282）之间的内部叶片轴（267）安装。

    COMPRESSOR WASH WITH AIR TO TURBINE COOLING PASSAGES
    2.
    发明申请
    COMPRESSOR WASH WITH AIR TO TURBINE COOLING PASSAGES 有权
    压缩机与空气一起洗涤到涡轮冷却通道

    公开(公告)号：US20140209123A1

    公开(公告)日：2014-07-31

    申请号：US13756293

    申请日：2013-01-31

    Applicant: SOLAR TURBINES INCORPORATED

    Inventor： John Frederick Lockyer

    IPC: F01D25/00

    CPC classification number: F01D25/002 ,  F04D19/02 ,  F04D29/705

    Abstract: A system and method for washing a gas turbine engine. The method for washing the gas turbine engine includes coupling a pressurized air supply assembly to an air supply and to a secondary air system, cranking a compressor rotor assembly of the gas turbine engine, supplying pressurized offline buffer air from the air supply to the pressurized air supply assembly, and spraying a cleaner into the compressor.

    Abstract translation: 一种用于清洗燃气涡轮发动机的系统和方法。 用于清洗燃气涡轮发动机的方法包括将加压空气供应组件连接到空气源和二次空气系统，起动燃气涡轮发动机的压缩机转子组件，将加压的离线缓冲空气从空气供应提供给加压空气 供应组件，并将清洁剂喷洒到压缩机中。

    COMPRESSOR WASH WITH AIR TO BEARING BUFFERING SYSTEM
    3.
    发明申请
    COMPRESSOR WASH WITH AIR TO BEARING BUFFERING SYSTEM 审中-公开
    压缩机用空气冲洗至轴承缓冲系统

    公开(公告)号：US20140208762A1

    公开(公告)日：2014-07-31

    申请号：US13756321

    申请日：2013-01-31

    Applicant: SOLAR TURBINES INCORPORATED

    Inventor： John Frederick Lockyer

    IPC: F02C7/00

    CPC classification number: F01D25/002

    Abstract: A system and method for washing a gas turbine engine. The method for washing the gas turbine engine includes coupling a pressurized air supply assembly to an air supply and to a secondary air system, cranking a compressor rotor assembly of the gas turbine engine, supplying pressurized offline buffer air from the air supply to the pressurized air supply assembly, and spraying a cleaner into the compressor.

    Abstract translation: 一种用于清洗燃气涡轮发动机的系统和方法。 用于清洗燃气涡轮发动机的方法包括将加压空气供应组件连接到空气源和二次空气系统，起动燃气涡轮发动机的压缩机转子组件，将加压的离线缓冲空气从空气供应提供给加压空气 供应组件，并将清洁剂喷洒到压缩机中。

    GAS TURBINE OFFLINE COMPRESSOR WASH WITH BUFFER AIR FROM COMBUSTOR
    4.
    发明申请
    GAS TURBINE OFFLINE COMPRESSOR WASH WITH BUFFER AIR FROM COMBUSTOR 有权
    气体涡轮压缩机与COMBUSTOR的缓冲器空气洗涤

    公开(公告)号：US20140209124A1

    公开(公告)日：2014-07-31

    申请号：US13756342

    申请日：2013-01-31

    Applicant: SOLAR TURBINES INCORPORATED

    Inventor： John Frederick Lockyer

    IPC: F01D25/00

    CPC classification number: F01D25/002 ,  F02C6/08

    Abstract: A system and method for washing a gas turbine engine. The method for washing the gas turbine engine includes coupling a pressurized air supply assembly to an air supply and to a secondary air system, cranking a compressor rotor assembly of the gas turbine engine, supplying pressurized offline buffer air from the air supply to the pressurized air supply assembly, and spraying a cleaner into the compressor.

    Abstract translation: 一种用于清洗燃气涡轮发动机的系统和方法。 用于清洗燃气涡轮发动机的方法包括将加压空气供应组件连接到空气源和二次空气系统，起动燃气涡轮发动机的压缩机转子组件，将加压的离线缓冲空气从空气供应提供给加压空气 供应组件，并将清洁剂喷洒到压缩机中。

    GAS TURBINE ENGINE COMPRESSOR WITH A BIASED INNER RING
    5.
    发明申请
    GAS TURBINE ENGINE COMPRESSOR WITH A BIASED INNER RING 有权
    气动涡轮发动机压缩机与一个偏心的内圈

    公开(公告)号：US20140119895A1

    公开(公告)日：2014-05-01

    申请号：US13666758

    申请日：2012-11-01

    Applicant: SOLAR TURBINES INCORPORATED

    Inventor： John Frederick Lockyer

    IPC: F04D29/00 ,  F04D29/54

    CPC classification number: F04D29/563 ,  F01D11/001 ,  F01D17/162 ,  F05D2300/501

    Abstract: An inner bushing assembly (280) to provide a biasing force between a guide vane (260) and an inner ring half (261) of a gas turbine engine compressor (200) is disclosed. The inner bushing assembly (280) includes a first bushing (281), a second bushing (282), and a biasing element (283). The first bushing (281) is configured to be installed about an inner vane shaft (267) of the guide vane (260) adjacent to an airfoil (265) of the guide vane (260). The second bushing (282) is configured to be installed about the inner vane shaft (267) distal to the airfoil (265). The biasing element (283) is configured to be installed about the inner vane shaft (267) between the first bushing (281) and the second bushing (282).

    Abstract translation: 公开了一种用于在燃气涡轮发动机压缩机（200）的引导叶片（260）和内环半部（261）之间提供偏置力的内衬套组件（280）。 内衬套组件（280）包括第一衬套（281），第二衬套（282）和偏置元件（283）。 第一衬套（281）构造成围绕与导叶（260）的翼型件（265）相邻的导叶（260）的内叶片轴（267）安装。 第二衬套（282）构造成围绕翼型（265）远侧的内叶片轴（267）安装。 偏置元件（283）构造成围绕第一衬套（281）和第二衬套（282）之间的内部叶片轴（267）安装。

    Compressor wash with air to turbine cooling passages
    7.
    发明授权
    Compressor wash with air to turbine cooling passages 有权
    压缩机用空气清洗至涡轮冷却通道

    公开(公告)号：US08778091B1

    公开(公告)日：2014-07-15

    申请号：US13756293

    申请日：2013-01-31

    Applicant: Solar Turbines Incorporated

    Inventor： John Frederick Lockyer

    IPC: B08B9/00

    CPC classification number: F01D25/002 ,  F04D19/02 ,  F04D29/705

    Abstract: A system and method for washing a gas turbine engine. The method for washing the gas turbine engine includes coupling a pressurized air supply assembly to an air supply and to a secondary air system, cranking a compressor rotor assembly of the gas turbine engine, supplying pressurized offline buffer air from the air supply to the pressurized air supply assembly, and spraying a cleaner into the compressor.

    Abstract translation: 一种用于清洗燃气涡轮发动机的系统和方法。 用于清洗燃气涡轮发动机的方法包括将加压空气供应组件连接到空气源和二次空气系统，起动燃气涡轮发动机的压缩机转子组件，将加压的离线缓冲空气从空气供应提供给加压空气 供应组件，并将清洁剂喷洒到压缩机中。

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