中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

5 records (took 0.007 seconds)

    TURBOMACHINE COMBUSTOR ASSEMBLY AND METHOD OF OPERATING A TURBOMACHINE
    2.
    发明申请
    TURBOMACHINE COMBUSTOR ASSEMBLY AND METHOD OF OPERATING A TURBOMACHINE 审中-公开
    涡轮搅拌机总成和操作涡轮机的方法

    公开(公告)号：WO2013073984A1

    公开(公告)日：2013-05-23

    申请号：PCT/RU2011/000908

    申请日：2011-11-17

    Applicant: GENERAL ELECTRIC COMPANY ,  SLOBODYANSKIY, llya Aleksandrovich ,  STRYAPUNIN, Sergey Aleksandrovich ,  TRETYAKOV, Dmitry Vladlenovich

    Inventor： SLOBODYANSKIY, llya Aleksandrovich ,  STRYAPUNIN, Sergey Aleksandrovich ,  TRETYAKOV, Dmitry Vladlenovich

    IPC: F23R3/34

    CPC classification number: F23R3/002 ,  F23R3/346

    Abstract: A turbomachine combustor assembly includes a combustor body having a combustor outlet, and a combustion liner arranged within the combustor body. The combustion liner defines a combustion chamber. An injection nozzle is arranged within the combustor body upstream from the combustion chamber. The injection nozzle is configured and disposed to deliver a first fluid toward the combustion chamber. A fluid module is mounted to the combustor body downstream from the combustion chamber. The fluid module includes a fluid module body that defines a fluid zone, a first injector member mounted to the fluid module body and configured to deliver a second fluid into the fluid zone at a first orientation, and a second injector member mounted to the fluid module body and configured to deliver a third fluid into the fluid zone at a second orientation that is distinct from the first orientation.

    Abstract translation: 涡轮机械燃烧器组件包括具有燃烧器出口的燃烧器主体和布置在燃烧器主体内的燃烧衬套。 燃烧衬套限定燃烧室。 在燃烧器主体的上游设置有喷射喷嘴。 注射喷嘴被配置和设置成将第一流体朝向燃烧室输送。 流体模块安装到燃烧器主体在燃烧室下游。 流体模块包括限定流体区域的流体模块主体，安装到流体模块主体并被配置成在第一取向处将第二流体输送到流体区域中的第一喷射器构件，以及安装到流体模块的第二喷射器构件 主体并且构造成在与第一方向不同的第二方向上将第三流体输送到流体区域中。

    TURBOMACHINE COMBUSTOR ASSEMBLY
    4.
    发明申请
    TURBOMACHINE COMBUSTOR ASSEMBLY 审中-公开
    涡轮搅拌机总成

    公开(公告)号：WO2013147633A8

    公开(公告)日：2014-10-16

    申请号：PCT/RU2012000232

    申请日：2012-03-29

    Applicant: EXXONMOBIL UPSTREAM RES CO ,  GEN ELECTRIC ,  SOKOLOV ALEXANDER NIKOLAY ,  TRETYAKOV DMITRY VLADLENOVICH ,  SLOBODYANSKIY ILYA ALEKSANDROVICH

    Inventor： SOKOLOV ALEXANDER NIKOLAY ,  TRETYAKOV DMITRY VLADLENOVICH ,  SLOBODYANSKIY ILYA ALEKSANDROVICH

    IPC: F23R3/04 ,  F23C7/02 ,  F23C9/08 ,  F23R3/28

    CPC classification number: F23R3/04 ,  F02C3/04 ,  F02C7/18 ,  F05D2240/35 ,  F23C7/02 ,  F23C9/08 ,  F23C2900/06041 ,  F23R3/002 ,  F23R3/283 ,  F23R3/286 ,  F23R2900/03041

    Abstract: A turbomachine combustor assembly includes a combustor body (20), and a combustor liner (24) arranged within the combustor body (20). The combustor liner (24) defines a combustion chamber (30) having a head end (32) and a discharge end (37). A plurality of combustor nozzles (44-49) are arranged in an annular array at the head end (32) of the combustion chamber (30), and a fluid delivery nozzle (90) is arranged substantially centrally within the annular array at the head end (32) of the combustion chamber (30). The fluid delivery nozzle (90) includes a first end portion (98) that extends to a second end portion (99) through a wall portion (100). The wall portion (100) includes at least one combustion chamber outlet (113). The fluid delivery nozzle (90) is configured to deliver a non-combustible fluid into the at least one of the plurality of combustor nozzles (44-49) and the combustion chamber (30).

    Abstract translation: 涡轮机械燃烧器组件包括燃烧器主体（20）和布置在燃烧器主体（20）内的燃烧器衬套（24）。 燃烧器衬套（24）限定具有头端（32）和排出端（37）的燃烧室（30）。 多个燃烧器喷嘴（44-49）在燃烧室（30）的头端（32）处以环形阵列布置，并且流体输送喷嘴（90）基本上设置在头部的环形阵列内的中心 燃烧室（30）的端部（32）。 流体输送喷嘴（90）包括通过壁部（100）延伸到第二端部（99）的第一端部（98）。 壁部分（100）包括至少一个燃烧室出口（113）。 流体输送喷嘴（90）构造成将不可燃流体输送到多个燃烧器喷嘴（44-49）和燃烧室（30）中的至少一个。

Patent Agency Ranking