利索-全球专利检索

  1. 登录
  2. 注册

搜索结果

7 条记录 (耗时 0.026 秒)

    INDUSTRIAL GAS TURBINE EXHAUST SYSTEM WITH MODULAR STRUTS AND COLLARS
    2.
    发明申请
    INDUSTRIAL GAS TURBINE EXHAUST SYSTEM WITH MODULAR STRUTS AND COLLARS 有权
    工业气体涡轮排放系统与模块化和COLLARS

    公开(公告)号：US20150143815A1

    公开(公告)日：2015-05-28

    申请号：US14087060

    申请日：2013-11-22

    申请人： Anil L. Salunkhe ,  John A. Orosa ,  Yevgeniy Shteyman ,  Matthew R. Porter ,  Lijuan Han ,  Matthew J. Delisa, III ,  Daniel F. Riveros

    发明人： Anil L. Salunkhe ,  John A. Orosa ,  Yevgeniy Shteyman ,  Matthew R. Porter ,  Lijuan Han ,  Matthew J. Delisa, III ,  Daniel F. Riveros

    IPC分类号： F01D25/30

    CPC分类号： F01D25/30 ,  F01D25/28 ,  F02C7/20 ,  Y10T29/49231

    摘要： An integrated single-piece exhaust system (SPEX) with modular construction that facilitates design changes for enhanced aerodynamics, structural integrity or serviceability. The SPEX defines splined or curved exhaust path surfaces, such as a series of cylindrical and frusto-conical sections that mimic curves. The constructed sections may include: (i) a tail cone assembly fabricated from conical sections that taper downstream to a reduced diameter; or (ii) an area-ruled cross section axially aligned with one or more rows of turbine struts; or both features. Modular inner and outer diameter inlet lips enhance transitional flow between the last row blades and the SPEX, as well as enhance structural integrity. Modular strut collars have large radius profiles between the SPEX annular inner diameter and outer diameter flow surfaces, for enhanced airflow and constant thickness walls for uniform heat transfer and thermal expansion. Scalloped mounting flanges enhance structural integrity and longevity.

    摘要翻译： 具有模块化结构的集成单件式排气系统（SPEX），有助于设计更改，提高空气动力学，结构完整性或可维护性。 SPEX定义了花键或弯曲的排气路径表面，例如模拟曲线的一系列圆柱形和截头圆锥形截面。 构造的部分可以包括：（i）由圆锥形部分制造的尾锥组件，其锥形下游到减小的直径; 或（ii）与一排或多排涡轮支架轴向对准的面积划线的横截面; 或两个功能。 模块化的内径和外径入口唇缘增强了最后一排叶片和SPEX之间的过渡流，并增强了结构完整性。 模块化支柱套环在SPEX环形内径和外径流动表面之间具有大的半径分布，用于增强气流和恒定厚度的壁，以实现均匀的热传递和热膨胀。 扇形安装法兰增强了结构的完整性和使用寿命。

    Modular industrial gas turbine exhaust system
    3.
    发明授权
    Modular industrial gas turbine exhaust system 有权
    模块化工业燃气轮机排气系统

    公开(公告)号：US09587519B2

    公开(公告)日：2017-03-07

    申请号：US14087086

    申请日：2013-11-22

    申请人： Anil L. Salunkhe ,  John A. Orosa ,  Yevgeniy Shteyman ,  Matthew R. Porter ,  Lijuan Han ,  Matthew J. Delisa, III ,  Daniel F. Riveros

    发明人： Anil L. Salunkhe ,  John A. Orosa ,  Yevgeniy Shteyman ,  Matthew R. Porter ,  Lijuan Han ,  Matthew J. Delisa, III ,  Daniel F. Riveros

    IPC分类号： F01D25/30 ,  F02K1/04 ,  F02K1/80 ,  F01D9/04 ,  F01D25/16 ,  F01D25/24

    CPC分类号： F01D25/30 ,  F01D9/041 ,  F01D25/162 ,  F01D25/243 ,  F02K1/04 ,  F02K1/80 ,  F05D2230/51 ,  F05D2250/232

    摘要： An integrated single-piece exhaust system (SPEX) with modular construction that facilitates design changes for enhanced aerodynamics, structural integrity or serviceability. The SPEX defines splined or curved exhaust path surfaces, such as a series of cylindrical and frusto-conical sections that mimic curves. The constructed sections may include: (i) a tail cone assembly fabricated from conical sections that taper downstream to a reduced diameter; or (ii) an area-ruled cross section axially aligned with one or more rows of turbine struts; or both features. Modular inner and outer diameter inlet lips enhance transitional flow between the last row blades and the SPEX, as well as enhance structural integrity. Modular strut collars have large radius profiles between the SPEX annular inner diameter and outer diameter flow surfaces, for enhanced airflow and constant thickness walls for uniform heat transfer and thermal expansion. Scalloped mounting flanges enhance structural integrity and longevity.

    摘要翻译： 具有模块化结构的集成单件式排气系统（SPEX），有助于设计更改，提高空气动力学，结构完整性或可维护性。 SPEX定义了花键或弯曲的排气路径表面，例如模拟曲线的一系列圆柱形和截头圆锥形截面。 构造的部分可以包括：（i）由圆锥形部分制造的尾锥组件，其锥形下游到减小的直径; 或（ii）与一排或多排涡轮支架轴向对准的面积划线的横截面; 或两个功能。 模块化的内径和外径入口唇缘增强了最后一排叶片和SPEX之间的过渡流，并增强了结构完整性。 模块化支柱套环在SPEX环形内径和外径流动表面之间具有大的半径分布，用于增强气流和恒定厚度的壁，以实现均匀的热传递和热膨胀。 扇形安装法兰增强了结构的完整性和使用寿命。

    MODULAR INDUSTRIAL GAS TURBINE EXHAUST SYSTEM
    4.
    发明申请
    MODULAR INDUSTRIAL GAS TURBINE EXHAUST SYSTEM 有权
    模块化工业气体排气系统

    公开(公告)号：US20150143816A1

    公开(公告)日：2015-05-28

    申请号：US14087086

    申请日：2013-11-22

    申请人： Anil L. Salunkhe ,  John A. Orosa ,  Yevgeniy Shteyman ,  Matthew R. Porter ,  Lijuan Han ,  Matthew J. Delisa, III ,  Daniel F. Riveros

    发明人： Anil L. Salunkhe ,  John A. Orosa ,  Yevgeniy Shteyman ,  Matthew R. Porter ,  Lijuan Han ,  Matthew J. Delisa, III ,  Daniel F. Riveros

    IPC分类号： F01D25/30

    CPC分类号： F01D25/30 ,  F01D9/041 ,  F01D25/162 ,  F01D25/243 ,  F02K1/04 ,  F02K1/80 ,  F05D2230/51 ,  F05D2250/232

    摘要： An integrated single-piece exhaust system (SPEX) with modular construction that facilitates design changes for enhanced aerodynamics, structural integrity or serviceability. The SPEX defines splined or curved exhaust path surfaces, such as a series of cylindrical and frusto-conical sections that mimic curves. The constructed sections may include: (i) a tail cone assembly fabricated from conical sections that taper downstream to a reduced diameter; or (ii) an area-ruled cross section axially aligned with one or more rows of turbine struts; or both features. Modular inner and outer diameter inlet lips enhance transitional flow between the last row blades and the SPEX, as well as enhance structural integrity. Modular strut collars have large radius profiles between the SPEX annular inner diameter and outer diameter flow surfaces, for enhanced airflow and constant thickness walls for uniform heat transfer and thermal expansion. Scalloped mounting flanges enhance structural integrity and longevity.

    摘要翻译： 具有模块化结构的集成单件式排气系统（SPEX），有助于设计更改，提高空气动力学，结构完整性或可维护性。 SPEX定义了花键或弯曲的排气路径表面，例如模拟曲线的一系列圆柱形和截头圆锥形截面。 构造的部分可以包括：（i）由圆锥形部分制造的尾锥组件，其锥形下游到减小的直径; 或（ii）与一排或多排涡轮支架轴向对准的面积划线的横截面; 或两个功能。 模块化的内径和外径入口唇缘增强了最后一排叶片和SPEX之间的过渡流，并增强了结构完整性。 模块化支柱套环在SPEX环形内径和外径流动表面之间具有大的半径分布，用于增强气流和恒定厚度的壁，以实现均匀的热传递和热膨胀。 扇形安装法兰增强了结构的完整性和使用寿命。

    INDUSTRIAL GAS TURBINE EXHAUST SYSTEM WITH SPLINED PROFILE TAIL CONE
    5.
    发明申请
    INDUSTRIAL GAS TURBINE EXHAUST SYSTEM WITH SPLINED PROFILE TAIL CONE 有权
    工业气体涡轮机排气系统

    公开(公告)号：US20150143813A1

    公开(公告)日：2015-05-28

    申请号：US14087040

    申请日：2013-11-22

    申请人： Anil L. Salunkhe ,  John A. Orosa ,  Yevgeniy Shteyman ,  Matthew R. Porter ,  Lijuan Han ,  Matthew J. Delisa, III

    发明人： Anil L. Salunkhe ,  John A. Orosa ,  Yevgeniy Shteyman ,  Matthew R. Porter ,  Lijuan Han ,  Matthew J. Delisa, III

    IPC分类号： F01D25/30

    CPC分类号： F01D25/30 ,  F01D5/143 ,  F01D9/041 ,  F01D11/001 ,  F01D25/162 ,  F01D25/243 ,  F05D2250/15

    摘要： An integrated single-piece exhaust system (SPEX) with modular construction that facilitates design changes for enhanced aerodynamics, structural integrity or serviceability. The SPEX defines splined or curved exhaust path surfaces, such as a series of cylindrical and frusto-conical sections that mimic curves. The constructed sections may include: (i) a tail cone assembly fabricated from conical sections that taper downstream to a reduced diameter; or (ii) an area-ruled cross section axially aligned with one or more rows of turbine struts; or both features. Modular inner and outer diameter inlet lips enhance transitional flow between the last row blades and the SPEX, as well as enhance structural integrity. Modular strut collars have large radius profiles between the SPEX annular inner diameter and outer diameter flow surfaces, for enhanced airflow and constant thickness walls for uniform heat transfer and thermal expansion. Scalloped mounting flanges enhance structural integrity and longevity.

    摘要翻译： 具有模块化结构的集成单件式排气系统（SPEX），有助于设计更改，提高空气动力学，结构完整性或可维护性。 SPEX定义了花键或弯曲的排气路径表面，例如模拟曲线的一系列圆柱形和截头圆锥形截面。 构造的部分可以包括：（i）由圆锥形部分制造的尾锥组件，其锥形下游到减小的直径; 或（ii）与一排或多排涡轮支架轴向对准的面积划线的横截面; 或两个功能。 模块化的内径和外径入口唇缘增强了最后一排叶片和SPEX之间的过渡流，并增强了结构完整性。 模块化支柱套环在SPEX环形内径和外径流动表面之间具有大的半径分布，用于增强气流和恒定厚度的壁，以实现均匀的热传递和热膨胀。 扇形安装法兰增强了结构的完整性和使用寿命。

    INDUSTRIAL GAS TURBINE EXHAUST SYSTEM DIFFUSER INLET LIP
    7.
    发明申请
    INDUSTRIAL GAS TURBINE EXHAUST SYSTEM DIFFUSER INLET LIP 有权
    工业气体涡轮排气系统扩散器进样口

    公开(公告)号：US20150143810A1

    公开(公告)日：2015-05-28

    申请号：US14087042

    申请日：2013-11-22

    申请人： Anil L. Salunkhe ,  John A. Orosa ,  Yevgeniy Shteyman ,  Lijuan Han ,  Matthew J. Delisa, III ,  Daniel F. Riveros

    发明人： Anil L. Salunkhe ,  John A. Orosa ,  Yevgeniy Shteyman ,  Lijuan Han ,  Matthew J. Delisa, III ,  Daniel F. Riveros

    IPC分类号： F01D25/30

    CPC分类号： F01D25/30 ,  F01D5/143 ,  F01D9/041 ,  F01D11/001 ,  F01D25/162 ,  F01D25/243 ,  F02K1/78 ,  F02K1/80 ,  F02K1/82 ,  F05D2250/15

    摘要： An integrated single-piece exhaust system (SPEX) with modular construction that facilitates design changes for enhanced aerodynamics, structural integrity or serviceability. The SPEX defines splined or curved exhaust path surfaces, such as a series of cylindrical and frusto-conical sections that mimic curves. The constructed sections may include: (i) a tail cone assembly fabricated from conical sections that taper downstream to a reduced diameter; or (ii) an area-ruled cross section axially aligned with one or more rows of turbine struts; or both features. Modular inner and outer diameter inlet lips enhance transitional flow between the last row blades and the SPEX, as well as enhance structural integrity. Modular strut collars have large radius profiles between the SPEX annular inner diameter and outer diameter flow surfaces, for enhanced airflow and constant thickness walls for uniform heat transfer and thermal expansion. Scalloped mounting flanges enhance structural integrity and longevity.

    摘要翻译： 具有模块化结构的集成单件式排气系统（SPEX），有助于设计更改，提高空气动力学，结构完整性或可维护性。 SPEX定义了花键或弯曲的排气路径表面，例如模拟曲线的一系列圆柱形和截头圆锥形截面。 构造的部分可以包括：（i）由圆锥形部分制造的尾锥组件，其锥形下游到减小的直径; 或（ii）与一排或多排涡轮支架轴向对准的面积划线的横截面; 或两个功能。 模块化的内径和外径入口唇缘增强了最后一排叶片和SPEX之间的过渡流，并增强了结构完整性。 模块化支柱套环在SPEX环形内径和外径流动表面之间具有大的半径分布，用于增强气流和恒定厚度的壁，以实现均匀的热传递和热膨胀。 扇形安装法兰增强了结构的完整性和使用寿命。