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    TURBINE ENGINE COMPONENTS
    1.
    发明申请
    TURBINE ENGINE COMPONENTS 有权
    涡轮发动机组件

    公开(公告)号：US20100329846A1

    公开(公告)日：2010-12-30

    申请号：US12490840

    申请日：2009-06-24

    申请人： Dhinagaran Ramachandran ,  Balamurugan Srinivasan ,  Gopal Muthiah ,  Jyothishkumar Venkataramanan ,  Jong Liu ,  Luis Tapia ,  Malak Fouad Malak

    发明人： Dhinagaran Ramachandran ,  Balamurugan Srinivasan ,  Gopal Muthiah ,  Jyothishkumar Venkataramanan ,  Jong Liu ,  Luis Tapia ,  Malak Fouad Malak

    IPC分类号： F01D5/14

    CPC分类号： F01D5/187 ,  F01D5/186 ,  F05D2250/314 ,  F05D2260/221 ,  Y02T50/676

    摘要： A turbine engine component includes a wall, a main opening, and two clusters of two or more auxiliary openings. The wall includes cool and hot air sides. The main opening extends between the cool air side and the hot air side and has an inlet and an outlet. The inlet is formed on the cool air side, and the outlet is formed on the hot air side. The first cluster of two or more auxiliary openings extends from the main opening to the hot air side. The second cluster of two or more auxiliary openings extends from the main opening to the hot air side. The main opening may be cylindrical or conical with a converging passage extending from the cool air side to the hot air side. The converging main opening may enhance flow through the auxiliary openings especially at high blowing ratios.

    摘要翻译： 涡轮发动机部件包括壁，主开口和两个或更多个辅助开口的两个簇。 墙壁包括凉爽和热的空气两侧。 主开口在冷空气侧和热空气侧之间延伸并具有入口和出口。 入口形成在冷空气侧，出口形成在热空气侧。 两个或更多个辅助开口的第一簇从主开口延伸到热空气侧。 两个或更多个辅助开口的第二组从主开口延伸到热空气侧。 主开口可以是圆柱形或圆锥形的，具有从冷空气侧延伸到热空气侧的会聚通道。 会聚主开口可以增强通过辅助开口的流动，特别是在高吹风比下。

    Turbine engine components
    2.
    发明授权
    Turbine engine components 有权
    涡轮发动机部件

    公开(公告)号：US08371814B2

    公开(公告)日：2013-02-12

    申请号：US12490840

    申请日：2009-06-24

    申请人： Dhinagaran Ramachandran ,  Balamurugan Srinivasan ,  Gopal Muthiah ,  Jyothishkumar Venkataramanan ,  Jong Liu ,  Luis Tapia ,  Malak Fouad Malak

    发明人： Dhinagaran Ramachandran ,  Balamurugan Srinivasan ,  Gopal Muthiah ,  Jyothishkumar Venkataramanan ,  Jong Liu ,  Luis Tapia ,  Malak Fouad Malak

    IPC分类号： F01D5/18

    CPC分类号： F01D5/187 ,  F01D5/186 ,  F05D2250/314 ,  F05D2260/221 ,  Y02T50/676

    摘要： A turbine engine component includes a wall, a main opening, and two clusters of two or more auxiliary openings. The wall includes cool and hot air sides. The main opening extends between the cool air side and the hot air side and has an inlet and an outlet. The inlet is formed on the cool air side, and the outlet is formed on the hot air side. The first cluster of two or more auxiliary openings extends from the main opening to the hot air side. The second cluster of two or more auxiliary openings extends from the main opening to the hot air side. The main opening may be cylindrical or conical with a converging passage extending from the cool air side to the hot air side. The converging main opening may enhance flow through the auxiliary openings especially at high blowing ratios.

    摘要翻译： 涡轮发动机部件包括壁，主开口和两个或更多个辅助开口的两个簇。 墙壁包括凉爽和热的空气两侧。 主开口在冷空气侧和热空气侧之间延伸并具有入口和出口。 入口形成在冷空气侧，出口形成在热空气侧。 两个或更多个辅助开口的第一簇从主开口延伸到热空气侧。 两个或更多个辅助开口的第二组从主开口延伸到热空气侧。 主开口可以是圆柱形或圆锥形的，具有从冷空气侧延伸到热空气侧的会聚通道。 会聚主开口可以增强通过辅助开口的流动，特别是在高吹风比下。

    Inter-turbine ducts with variable area ratios
    8.
    发明授权
    Inter-turbine ducts with variable area ratios 有权
    具有可变面积比的涡轮机间管道

    公开(公告)号：US09534497B2

    公开(公告)日：2017-01-03

    申请号：US13462738

    申请日：2012-05-02

    申请人： Vinayender Kuchana ,  Balamurugan Srinivasan ,  Sujatha Guntu ,  Malak Fouad Malak ,  Paul Couey ,  Craig Mckeever

    发明人： Vinayender Kuchana ,  Balamurugan Srinivasan ,  Sujatha Guntu ,  Malak Fouad Malak ,  Paul Couey ,  Craig Mckeever

    IPC分类号： F01D9/04 ,  F01D5/14

    CPC分类号： F01D5/145 ,  F01D9/041 ,  Y02T50/671 ,  Y02T50/673

    摘要： A turbine section of a gas turbine engine is annular about a longitudinal axis. The turbine section includes a first turbine with a first inlet and a first outlet; a second turbine with a second inlet and a second outlet; and an inter-turbine duct extending from the first outlet to the second inlet and configured to direct an air flow from the first turbine to the second turbine. The inter-turbine duct has a first station with a first meridional area, a second station with a second meridional area, and a third station with a third meridional area. The first station is upstream of the second station and the second station is upstream of the third station, and the second meridional area is less than or equal to the first meridional area.

    摘要翻译： 燃气涡轮发动机的涡轮机部分围绕纵向轴线是环形的。 涡轮部分包括具有第一入口和第一出口的第一涡轮机; 具有第二入口和第二出口的第二涡轮机; 以及从所述第一出口延伸到所述第二入口并且构造成将空气流从所述第一涡轮引导到所述第二涡轮机的涡轮机间管道。 所述涡轮机间通道具有具有第一子午区域的第一站，具有第二子午区域的第二站和具有第三子午线区域的第三站。 第一站位于第二站的上游，第二站位于第三站的上游，第二子午区小于或等于第一子午区。

    INTER-TURBINE DUCTS WITH VARIABLE AREA RATIOS
    9.
    发明申请
    INTER-TURBINE DUCTS WITH VARIABLE AREA RATIOS 有权
    具有可变区域的涡轮泵

    公开(公告)号：US20130294908A1

    公开(公告)日：2013-11-07

    申请号：US13462738

    申请日：2012-05-02

    申请人： Vinayender Kuchana ,  Balamurugan Srinivasan ,  Sujatha Guntu ,  Malak Fouad Malak ,  Paul Couey ,  Craig Mckeever

    发明人： Vinayender Kuchana ,  Balamurugan Srinivasan ,  Sujatha Guntu ,  Malak Fouad Malak ,  Paul Couey ,  Craig Mckeever

    IPC分类号： F01D1/04

    CPC分类号： F01D5/145 ,  F01D9/041 ,  Y02T50/671 ,  Y02T50/673

    摘要： A turbine section of a gas turbine engine is annular about a longitudinal axis. The turbine section includes a first turbine with a first inlet and a first outlet; a second turbine with a second inlet and a second outlet; and an inter-turbine duct extending from the first outlet to the second inlet and configured to direct an air flow from the first turbine to the second turbine. The inter-turbine duct has a first station with a first meridional area, a second station with a second meridional area, and a third station with a third meridional area. The first station is upstream of the second station and the second station is upstream of the third station, and the second meridional area is less than or equal to the first meridional area.

    摘要翻译： 燃气涡轮发动机的涡轮机部分围绕纵向轴线是环形的。 涡轮部分包括具有第一入口和第一出口的第一涡轮机; 具有第二入口和第二出口的第二涡轮机; 以及从所述第一出口延伸到所述第二入口并且构造成将空气流从所述第一涡轮引导到所述第二涡轮机的涡轮机间管道。 所述涡轮机间通道具有具有第一子午区域的第一站，具有第二子午区域的第二站和具有第三子午线区域的第三站。 第一站位于第二站的上游，第二站位于第三站的上游，第二子午区小于或等于第一子午区。