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    Inter-turbine ducts with variable area ratios
    1.
    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
    2.
    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。

    SEAL PLATES FOR DIRECTING AIRFLOW THROUGH A TURBINE SECTION OF AN ENGINE AND TURBINE SECTIONS
    5.
    发明申请
    SEAL PLATES FOR DIRECTING AIRFLOW THROUGH A TURBINE SECTION OF AN ENGINE AND TURBINE SECTIONS 有权
    用于通过发动机和涡轮机部分的涡轮部分引导气流的密封板

    公开(公告)号：US20110123325A1

    公开(公告)日：2011-05-26

    申请号：US12622837

    申请日：2009-11-20

    申请人： Mark C. Morris ,  Larry Barr ,  Paul Couey ,  Stuart Andrew Harman ,  Douglas L. Ramerth ,  Luis A. Tapia

    发明人： Mark C. Morris ,  Larry Barr ,  Paul Couey ,  Stuart Andrew Harman ,  Douglas L. Ramerth ,  Luis A. Tapia

    IPC分类号： F01D1/02

    CPC分类号： F01D5/3015 ,  F01D5/082 ,  F05D2240/126 ,  Y02T50/676

    摘要： A seal plate for directing an airflow includes a hub, main pumping vanes, and splitter vanes. The hub has a tubular section and an annular flange section flared outwardly relative to the tubular section to define a flow surface. The main pumping vanes are disposed circumferentially on the flow surface around the annular flange section and each has a canted section located radially inward relative to a straight section and aligned with a flow direction of the airflow. The straight section extends along a first plane including a centerline of the seal plate. The splitter vanes are disposed circumferentially on the flow surface around the annular flange section such that at least one splitter vane is disposed between the straight sections of two adjacent main pumping vanes. Each splitter vane has a length that is less than a length of each of the two adjacent main pumping vanes.

    摘要翻译： 用于引导气流的密封板包括轮毂，主泵叶片和分流叶片。 轮毂具有管状部分和环形凸缘部分，其相对于管状部分向外张开以限定流动表面。 主泵叶片周向设置在环形凸缘部分周围的流动表面上，并且每个具有相对于直线部分径向向内定位并与气流的流动方向对准的倾斜部分。 直线部分沿着包括密封板的中心线的第一平面延伸。 分流叶片周向设置在环形凸缘部分周围的流动表面上，使得至少一个分流叶片设置在两个相邻的主泵叶片的直线部分之间。 每个分流叶片的长度小于两个相邻主泵叶片中的每一个的长度。

    Seal plates for directing airflow through a turbine section of an engine and turbine sections
    6.
    发明授权
    Seal plates for directing airflow through a turbine section of an engine and turbine sections 有权
    用于引导气流通过发动机和涡轮机部分的涡轮部分的密封板

    公开(公告)号：US08444387B2

    公开(公告)日：2013-05-21

    申请号：US12622837

    申请日：2009-11-20

    申请人： Mark C. Morris ,  Larry Barr ,  Paul Couey ,  Stuart Andrew Harman ,  Douglas L. Ramerth ,  Luis A. Tapia

    发明人： Mark C. Morris ,  Larry Barr ,  Paul Couey ,  Stuart Andrew Harman ,  Douglas L. Ramerth ,  Luis A. Tapia

    IPC分类号： B63H1/14

    CPC分类号： F01D5/3015 ,  F01D5/082 ,  F05D2240/126 ,  Y02T50/676

    摘要： A seal plate for directing an airflow includes a hub, main pumping vanes, and splitter vanes. The hub has a tubular section and an annular flange section flared outwardly relative to the tubular section to define a flow surface. The main pumping vanes are disposed circumferentially on the flow surface around the annular flange section and each has a canted section located radially inward relative to a straight section and aligned with a flow direction of the airflow. The straight section extends along a first plane including a centerline of the seal plate. The splitter vanes are disposed circumferentially on the flow surface around the annular flange section such that at least one splitter vane is disposed between the straight sections of two adjacent main pumping vanes. Each splitter vane has a length that is less than a length of each of the two adjacent main pumping vanes.

    摘要翻译： 用于引导气流的密封板包括轮毂，主泵叶片和分流叶片。 轮毂具有管状部分和环形凸缘部分，其相对于管状部分向外张开以限定流动表面。 主泵叶片周向设置在环形凸缘部分周围的流动表面上，并且每个具有相对于直线部分径向向内定位并与气流的流动方向对准的倾斜部分。 直线部分沿着包括密封板的中心线的第一平面延伸。 分流叶片周向设置在环形凸缘部分周围的流动表面上，使得至少一个分流叶片设置在两个相邻的主泵叶片的直线部分之间。 每个分流叶片的长度小于两个相邻主泵叶片中的每一个的长度。