利索-全球专利检索

  1. 登录
  2. 注册

搜索结果

10 条记录 (耗时 0.028 秒)

    Method to augment heat transfer using chamfered cylindrical depressions in cast internal cooling passages
    1.
    发明申请
    Method to augment heat transfer using chamfered cylindrical depressions in cast internal cooling passages 审中-公开
    在铸造内部冷却通道中使用倒角圆柱形凹陷来增加传热的方法

    公开(公告)号：US20070201980A1

    公开(公告)日：2007-08-30

    申请号：US11390616

    申请日：2006-03-27

    申请人： Mark Morris ,  Vivek Agarwal ,  Jason Smoke ,  William Baker ,  Luis Tapia

    发明人： Mark Morris ,  Vivek Agarwal ,  Jason Smoke ,  William Baker ,  Luis Tapia

    IPC分类号： F01D5/18

    CPC分类号： B22C9/10 ,  B22C9/04 ,  B22C9/103 ,  F01D5/187 ,  F05D2230/12 ,  F05D2230/21 ,  F05D2230/211 ,  F05D2250/192 ,  F05D2250/292 ,  F05D2260/2212 ,  F05D2260/2214 ,  F05D2260/22141 ,  Y02T50/676

    摘要： An air-cooled turbine blade is provided having an airfoil shape defined by a convex suction side wall, a concave pressure side wall, a leading edge, a trailing edge, a root and a tip, each wall including an interior surface that defines an interior with the edges, root and tip. The blade includes a plurality of independent cooling circuit flow paths within the blade interior and a roughened surface. The roughened surface is formed on an interior surface of at least one of the convex suction side wall and the concave pressure side wall, the roughened surface comprising a plurality of cylindrical depressions. Each depression includes a cylindrical wall coupled to a bottom wall by a chamfered edge formed therebetween, and the roughened surface defines at least a portion of one of the flow paths of the plurality of independent cooling circuit flow paths. Methods for forming the blade are also provided.

    摘要翻译： 提供一种风冷式涡轮叶片，其具有由凸形吸入侧壁，凹形压力侧壁，前缘，后缘，根部和尖端限定的翼型，每个壁包括限定内部的内表面 边缘，根部和尖端。 叶片包括在叶片内部和粗糙表面内的多个独立的冷却回路流动路径。 粗糙表面形成在凸吸入侧壁和凹压侧壁中的至少一个的内表面上，粗糙表面包括多个圆柱形凹陷。 每个凹陷包括通过其间形成的倒角边缘连接到底壁的圆柱形壁，粗糙表面限定多个独立冷却回路流动路径中的一个流路的至少一部分。 还提供了形成叶片的方法。

    TURBINE ENGINE COMPONENTS
    3.
    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
    4.
    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。