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    Turbine blades and turbine blade cooling systems and methods
    22.
    发明申请
    Turbine blades and turbine blade cooling systems and methods 有权
    涡轮叶片和涡轮叶片冷却系统及方法

    公开(公告)号：US20080131278A1

    公开(公告)日：2008-06-05

    申请号：US11606731

    申请日：2006-11-30

    申请人： Victor Hugo Silva Correia ,  Robert Francis Manning ,  Bhanu Mahasamudram Reddy

    发明人： Victor Hugo Silva Correia ,  Robert Francis Manning ,  Bhanu Mahasamudram Reddy

    IPC分类号： B64C11/20

    CPC分类号： F01D5/187 ,  F01D5/20 ,  F05D2260/202 ,  Y02T50/673 ,  Y02T50/676

    摘要： A turbine blade with improved tip cooling includes an airfoil having a tip cap and a tip wall extending outwardly from the tip cap. A recessed portion of the tip wall forms a tip shelf. At least one tip shelf hole extends through the tip shelf in flow communication with an internal airfoil cooling circuit. At least one tip wall opening extends through the recessed portion of the tip wall radially outward of the tip shelf in flow communication with the internal cooling circuit. The recessed tip wall portion may be tapered from a wider base to a minimum thickness. In a cooling method, cooling air channeled through the tip wall openings joins and mixes with a stream of hot combustion gases downstream of where cooling air channeled through the tip shelf openings joins and mixes with the stream of hot gasses to enhance convection cooling of the blade tip. A system for cooling a blade includes at least one tip shelf hole and at least one tip wall opening for channeling cooling air from an internal cooling circuit toward a stream of hot combustion gases for improved cooling of at least the blade tip.

    摘要翻译： 具有改进的尖端冷却的涡轮机叶片包括具有尖端帽和从顶盖向外延伸的顶端壁的翼型件。 尖端壁的凹陷部分形成尖端架。 至少一个尖端搁架孔延伸穿过末端架，与内部翼型件冷却回路流通。 至少一个尖端壁开口延伸穿过顶端壁的位于尖端架的径向外侧的凹部，与内部冷却回路流通。 凹入的顶壁部分可以从更宽的基部到最小厚度成锥形。 在冷却方法中，通过尖端壁开口引导的冷却空气与下游的热燃烧气体流接合并混合，其中通过尖端搁架开口引导的冷却空气与热气流混合并增强了叶片的对流冷却 小费。 用于冷却叶片的系统包括至少一个尖端搁架孔和至少一个尖端壁开口，用于将冷却空气从内部冷却回路引向热燃烧气体流，以改善至少叶片尖端的冷却。

    COMPONENT AND METHOD OF FABRICATING THE SAME
    24.
    发明申请
    COMPONENT AND METHOD OF FABRICATING THE SAME 审中-公开
    组分及其制备方法

    公开(公告)号：US20130104517A1

    公开(公告)日：2013-05-02

    申请号：US13285747

    申请日：2011-10-31

    申请人： Victor Hugo Silva Correia ,  Robert Francis Manning

    发明人： Victor Hugo Silva Correia ,  Robert Francis Manning

    IPC分类号： F02C7/12

    CPC分类号： F01D5/18 ,  F01D25/12 ,  Y02T50/676

    摘要： A component for a gas turbine engine is provided. The component includes a cooling aperture and a plug filling at least a portion of the cooling aperture to prevent airflow through the cooling aperture. The plug is configured to melt at a predetermined temperature during operation of the gas turbine engine to permit airflow through the cooling aperture.

    摘要翻译： 提供了一种用于燃气涡轮发动机的部件。 该部件包括冷却孔和插入冷却孔的至少一部分的塞子，以防止气流通过冷却孔。 塞子构造成在燃气涡轮发动机的运行期间在预定温度下熔化以允许气流通过冷却孔。

    TURBINE AIRFOIL WITH METERED COOLING CAVITY
    27.
    发明申请
    TURBINE AIRFOIL WITH METERED COOLING CAVITY 审中-公开
    具有计量冷却空气的涡轮机空气

    公开(公告)号：US20090293495A1

    公开(公告)日：2009-12-03

    申请号：US12129375

    申请日：2008-05-29

    申请人： Victor Hugo Silva Correia ,  Daniel Edward Demers ,  Robert Francis Manning

    发明人： Victor Hugo Silva Correia ,  Daniel Edward Demers ,  Robert Francis Manning

    IPC分类号： F02C7/18 ,  F01D9/02

    CPC分类号： F01D5/186 ,  F01D5/189 ,  F05D2260/201

    摘要： A turbine airfoil for a gas turbine engine includes: (a) spaced-apart pressure and suction sidewalls extending between a leading edge and a trailing edge; (b) a first cavity disposed between the pressure and suction sidewalls, the first cavity being adapted to be fed cooling air from a source within the engine, and connected to at least one film cooling hole which communicates with an exterior surface of the airfoil; (c) a second cavity disposed between the pressure and suction sidewalls, the second cavity being adapted to be fed cooling air from a source within the engine, and connected to at least one film cooling hole which communicates solely with the suction sidewall of the airfoil; and (d) a metering structure adapted to substantially restrict air flow into the second cavity.

    摘要翻译： 用于燃气涡轮发动机的涡轮机翼片包括：（a）在前缘和后缘之间延伸的间隔开的压力和吸力侧壁; （b）设置在压力侧和吸力侧壁之间的第一空腔，第一空腔适于从发动机内的源供给冷却空气，并连接到与翼型件的外表面连通的至少一个薄膜冷却孔; （c）设置在所述压力和吸力侧壁之间的第二腔，所述第二腔适于从所述发动机内的源供给冷却空气，并且连接到至少一个仅与所述翼型的吸力侧壁连通的薄膜冷却孔 ; 和（d）适于基本上限制空气流入第二腔的计量结构。

    HYBRID IMPINGEMENT COOLED AIRFOIL
    28.
    发明申请
    HYBRID IMPINGEMENT COOLED AIRFOIL 有权
    混合气体冷却空气

    公开(公告)号：US20090245999A1

    公开(公告)日：2009-10-01

    申请号：US12055101

    申请日：2008-03-25

    申请人： David Allen Flodman ,  Jason David Shapiro ,  Robert Francis Manning ,  Mark Douglas Gledhill ,  Tyler Frederick Hooper

    发明人： David Allen Flodman ,  Jason David Shapiro ,  Robert Francis Manning ,  Mark Douglas Gledhill ,  Tyler Frederick Hooper

    IPC分类号： F01D5/18

    CPC分类号： F01D5/189 ,  F05D2260/201 ,  F05D2260/202 ,  Y02T50/676

    摘要： A turbine nozzle for a gas turbine engine includes: (a) spaced-apart arcuate inner and outer bands; (b) a hollow, airfoil-shaped turbine vane extending between the inner and outer bands, the interior of the vane defining at least a forward cavity and a mid-cavity positioned aft of the forward cavity; (c) a hollow impingement insert received inside the mid-cavity, the impingement insert having walls which are pierced with at least one impingement cooling hole; (d) a passage in the turbine vane at a radially outer end of the forward cavity adapted to be coupled to a source of cooling air; and (e) a passage in the inner band in fluid communication with a radially inner end of the forward cavity and a radially inner end of the impingement insert.

    摘要翻译： 用于燃气涡轮发动机的涡轮喷嘴包括：（a）间隔开的弓形内部和外部带; （b）在所述内部和外部带之间延伸的中空翼型涡轮机叶片，所述叶片的内部至少限定前腔和位于所述前腔后面的中空腔; （c）容纳在中空腔内的中空冲击插入件，冲击插入件具有用至少一个冲击冷却孔刺穿的壁; （d）在所述前腔的径向外端处的涡轮叶片中的通道，其适于联接到冷却空气源; 和（e）内带中的与前腔的径向内端流体连通的通道和冲击插入件的径向内端。

    System and method for routing both toll-free and caller-paid telephone calls to call service centers
    29.
    发明授权
    System and method for routing both toll-free and caller-paid telephone calls to call service centers 失效
    用于将免费电话和主叫付费电话呼叫路由到呼叫服务中心的系统和方法

    公开(公告)号：US07224789B2

    公开(公告)日：2007-05-29

    申请号：US11322444

    申请日：2005-12-29

    申请人： Gayle Roberta Ekstrom ,  Robert Francis Manning

    发明人： Gayle Roberta Ekstrom ,  Robert Francis Manning

    IPC分类号： H04M3/00 ,  H04M7/00

    CPC分类号： H04M3/5237 ,  H04Q3/0029 ,  H04Q3/64 ,  H04Q2213/13072 ,  H04Q2213/13107 ,  H04Q2213/13345

    摘要： A system and method of routing both caller-paid and toll-free telephone calls includes a local exchange network and an interexchange network in communication with a call routing processor. The call routing processor receives status information on at least two call service centers and provides routing instructions to both the interexchange and local exchange networks. The method includes the steps of a call controller in a local exchange network communicating with a call routing processor also in communication with an interexchange network, the call controller identifying calls to call service centers and requesting instructions from the call routing processor.

    摘要翻译： 一种用于路由呼叫者支付和免费电话呼叫的系统和方法包括本地交换网络和与呼叫路由处理器通信的互联网络。 呼叫路由处理器在至少两个呼叫服务中心上接收状态信息，并向局域交换网络和本地交换网络提供路由指令。 该方法包括步骤：本地交换网络中的呼叫控制器与呼叫路由处理器进行通信，所述呼叫路由处理器也与局域网通信，呼叫控制器识别呼叫服务中心的呼叫并从呼叫路由处理器请求指令。