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1. 发明申请

US20050053459A1 Microcircuit cooling for a turbine airfoil 有权
标题翻译：用于涡轮机翼的微电路冷却
公开(公告)号：US20050053459A1
公开(公告)日：2005-03-10
申请号：US10802260
申请日：2004-03-16
申请人： Frank Cunha , Keith Santeler , Scott Gayman , Eric Couch
发明人： Frank Cunha , Keith Santeler , Scott Gayman , Eric Couch
IPC分类号： F01D5/00 , F01D5/08 , F01D5/18 , F02C7/16 , F02C7/18
CPC分类号： F01D5/187 , F01D5/186 , F05D2250/25 , F05D2260/2212 , F05D2260/22141 , Y02T50/676
摘要： A turbine airfoil includes a plurality of cooling circuits embedded within the pressure and suction sidewalls and a first and a second flow passage. The first flow passage feeds the coolant fluid to the cooling circuits that are embedded only within the pressure sidewall and the second flow passage feeds the coolant fluid to the cooling circuits that are embedded only within the suction sidewall. A method embodiment of the present comprises placing the inlets of the cooling circuits embedded within the first sidewall in flow communication with only one of the flow passages and placing the inlets of the cooling circuits embedded within the second sidewall in flow communication with at least one of the other flow passages to minimize the difference in sink pressures of the suction and pressure sidewalls to ensure ingestion of the coolant fluid into the inlets of the respective cooling circuits.
摘要翻译：涡轮机翼片包括嵌入压力和抽吸侧壁内的多个冷却回路以及第一和第二流动通道。第一流动通道将冷却剂流体供给到仅在压力侧壁内嵌入的冷却回路，而第二流动通道将冷却剂流体供给到仅嵌入在吸力侧壁内的冷却回路。本发明的方法实施例包括将嵌入在第一侧壁内的冷却回路的入口放置成仅与流动通道中的一个流体连通，并且将嵌入在第二侧壁内的冷却回路的入口与至少一个其他流动通道以最小化吸入和压力侧壁的吸收压力的差异，以确保将冷却剂流体摄入相应冷却回路的入口。

2. 发明申请

US20060263221A1 Turbine airfoil platform cooling circuit 有权
标题翻译：涡轮机翼平台冷却回路
公开(公告)号：US20060263221A1
公开(公告)日：2006-11-23
申请号：US11134927
申请日：2005-05-23
申请人： Frank Cunha , Eric Couch , Keith Santeler , Scott Gayman , Eric Hudson , Christopher Joe , Eric Letizia
发明人： Frank Cunha , Eric Couch , Keith Santeler , Scott Gayman , Eric Hudson , Christopher Joe , Eric Letizia
IPC分类号： F01D11/00
CPC分类号： F01D9/02 , F01D5/187 , F01D25/12 , F05D2240/81 , Y02T50/676
摘要： An airfoil assembly includes an airfoil extending away from a platform. One or more cooling circuits are formed through the platform in order to provide cooling of the platform. The cooling circuit may include a downwardly directed inlet receiving cooling air from below the platform. The cooling air is then directed in a direction generally parallel to the outer surface of the platform and through exits formed through the outer surface of the platform. The cooling circuit may optionally include a plurality of pedestals extending from an outer wall to an inner wall of the cooling circuit to increase the rigidity and the cooling function of the cooling circuit.
摘要翻译：机翼组件包括远离平台延伸的翼型件。通过平台形成一个或多个冷却回路以提供平台的冷却。冷却回路可以包括从平台下方接收冷却空气的向下定向的入口。然后将冷却空气沿大致平行于平台的外表面的方向引导并通过平台的外表面形成的出口。冷却回路可以可选地包括从冷却回路的外壁延伸到内壁的多个基座，以增加冷却回路的刚度和冷却功能。

3. 发明授权

US07097425B2 Microcircuit cooling for a turbine airfoil 有权
标题翻译：用于涡轮机翼的微电路冷却
公开(公告)号：US07097425B2
公开(公告)日：2006-08-29
申请号：US10802260
申请日：2004-03-16
申请人： Frank J. Cunha , Keith Santeler , Scott W. Gayman , Eric Couch
发明人： Frank J. Cunha , Keith Santeler , Scott W. Gayman , Eric Couch
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , F01D5/186 , F05D2250/25 , F05D2260/2212 , F05D2260/22141 , Y02T50/676
摘要： A turbine airfoil includes a plurality of cooling circuits embedded within the pressure and suction sidewalls and a first and a second flow passage. The first flow passage feeds the coolant fluid to the cooling circuits that are embedded only within the pressure sidewall and the second flow passage feeds the coolant fluid to the cooling circuits that are embedded only within the suction sidewall. A method embodiment of the present comprises placing the inlets of the cooling circuits embedded within the first sidewall in flow communication with only one of the flow passages and placing the inlets of the cooling circuits embedded within the second sidewall in flow communication with at least one of the other flow passages to minimize the difference in sink pressures of the suction and pressure sidewalls to ensure ingestion of the coolant fluid into the inlets of the respective cooling circuits.
摘要翻译：涡轮机翼片包括嵌入压力和抽吸侧壁内的多个冷却回路以及第一和第二流动通道。第一流动通道将冷却剂流体供给到仅在压力侧壁内嵌入的冷却回路，而第二流动通道将冷却剂流体供给到仅嵌入在吸力侧壁内的冷却回路。本发明的方法实施例包括将嵌入在第一侧壁内的冷却回路的入口放置成仅与流动通道中的一个流体连通，并且将嵌入在第二侧壁内的冷却回路的入口与至少一个其他流动通道以最小化吸入和压力侧壁的吸收压力的差异，以确保将冷却剂流体摄入相应冷却回路的入口。

4. 发明授权

US07114647B2 Data analysis system and method 失效
标题翻译：数据分析系统及方法
公开(公告)号：US07114647B2
公开(公告)日：2006-10-03
申请号：US10716691
申请日：2003-11-18
申请人： Timothy W. Giraldin , Patrick W. Giraldin , Regan E. Kelly , Martin F. Crowley , Eric Couch , Y-Tin Gross
发明人： Timothy W. Giraldin , Patrick W. Giraldin , Regan E. Kelly , Martin F. Crowley , Eric Couch , Y-Tin Gross
IPC分类号： G06F17/00
CPC分类号： G06Q30/02 , G07C9/00103 , G07C9/00111 , G07C11/00 , G07C2011/02 , G07C2011/04
摘要： A system and method of communication for a confined area of a facility are disclosed. Personal identification information of a guest is received into at least one of a set of stations distributed throughout the confined area to register the guest. Demographic information regarding the registered guest is received. The movement of the guest is monitored over time, and the guest movement information is stored. Reports are created on the demographic and movements of the guest.
摘要翻译：公开了一种用于设施的密闭区域的系统和通信方法。访客的个人识别信息被接收到分布在整个限制区域中的一组站点中的至少一个以注册客人。收到有关登记的客人的人口统计信息。随着时间的推移监视客人的移动，并存储客人移动信息。报告是根据客人的人口和动态创建的。

5. 发明授权

US07708528B2 Platform mate face contours for turbine airfoils 有权
标题翻译：涡轮翼型平台配合面轮廓
公开(公告)号：US07708528B2
公开(公告)日：2010-05-04
申请号：US11220291
申请日：2005-09-06
申请人： Eric Couch , Frank J. Cunha
发明人： Eric Couch , Frank J. Cunha
IPC分类号： F01D5/30
CPC分类号： F01D5/22 , F01D25/12 , F05D2240/81 , F05D2250/70 , F05D2250/71 , F05D2260/20 , F05D2260/202 , F05D2260/221
摘要： Gas turbine engine components having an airfoil extending outwardly of a platform are mounted in adjacent relationship, and such that cooling air flows outwardly of a gap between mating faces of the platforms. The location of localized hot spots is identified on the platform, and the mating faces are designed to provide cooling air through the gap to address these hot spots. A suction side edge of the platform has a curved portion extending inwardly into the platform, and the pressure side has a curved portion bulging outwardly away from the airfoil. When these two portions on adjacent components mate, a gap is provided between two platforms that provides leakage cooling air to the hot spot.
摘要翻译：具有从平台向外延伸的翼型件的燃气涡轮发动机部件以相邻的关系安装，并且使得冷却空气从平台的配合面之间的间隙向外流动。在平台上识别局部热点的位置，并且配合面设计成通过间隙提供冷却空气以解决这些热点。平台的吸入侧边缘具有向内延伸到平台中的弯曲部分，并且压力侧具有从翼型向外凸出的弯曲部分。当相邻部件上的这两个部分配合时，在两个平台之间提供间隙，这两个平台向热点提供泄漏的冷却空气。

6. 发明申请

US20090304516A1 PLATFORM MATE FACE CONTOURS FOR TURBINE AIRFOILS 有权
标题翻译：平台风力发动机风力发电机表面
公开(公告)号：US20090304516A1
公开(公告)日：2009-12-10
申请号：US11220291
申请日：2005-09-06
申请人： Eric Couch , Frank J. Cunha
发明人： Eric Couch , Frank J. Cunha
IPC分类号： F01D5/14
CPC分类号： F01D5/22 , F01D25/12 , F05D2240/81 , F05D2250/70 , F05D2250/71 , F05D2260/20 , F05D2260/202 , F05D2260/221
摘要： Gas turbine engine components having an airfoil extending outwardly of a platform are mounted in adjacent relationship, and such that cooling air flows outwardly of a gap between mating faces of the platforms. The location of localized hot spots is identified on the platform, and the mating faces are designed to provide cooling air through the gap to address these hot spots. A suction side edge of the platform has a curved portion extending inwardly into the platform, and the pressure side has a curved portion bulging outwardly away from the airfoil. When these two portions on adjacent components mate, a gap is provided between two platforms that provides leakage cooling air to the hot spot.
摘要翻译：具有从平台向外延伸的翼型件的燃气涡轮发动机部件以相邻的关系安装，并且使得冷却空气从平台的配合面之间的间隙向外流动。在平台上识别局部热点的位置，并且配合面设计成通过间隙提供冷却空气以解决这些热点。平台的吸入侧边缘具有向内延伸到平台中的弯曲部分，并且压力侧具有从翼型向外凸出的弯曲部分。当相邻部件上的这两个部分配合时，在两个平台之间提供间隙，这两个平台向热点提供泄漏的冷却空气。

7. 发明申请

US20070177975A1 Film cooling method and hole manufacture 有权
标题翻译：薄膜冷却方法和孔制造
公开(公告)号：US20070177975A1
公开(公告)日：2007-08-02
申请号：US11340911
申请日：2006-01-27
申请人： Blake Luczak , Eric Couch
发明人： Blake Luczak , Eric Couch
IPC分类号： F01D5/18
CPC分类号： F01D5/186 , B22C9/103 , F02C7/185 , F05D2230/12 , F05D2230/13 , F05D2230/21 , F05D2230/211 , F05D2230/90 , F05D2240/121 , F05D2240/303 , F05D2260/204 , F05D2300/611 , Y02T50/676
摘要： A cooled cast part has an exterior surface. A cooling passageway system extends from at least one inlet port to a plurality of outlet ports. The passageway system includes a first passageway to at least a first of the outlets and surrounding at least one post. The system includes a second passageway to at least a second of the outlets passing through the at least one post.
摘要翻译：冷却的铸造件具有外表面。冷却通道系统从至少一个入口延伸到多个出口。通道系统包括到至少第一出口并围绕至少一个柱的第一通道。该系统包括通过至少一个柱的至少一个第二出口的第二通道。

8. 发明授权

US07147149B2 Cashless spending system and method 失效
标题翻译：无现金支出制度和方法
公开(公告)号：US07147149B2
公开(公告)日：2006-12-12
申请号：US10716802
申请日：2003-11-18
申请人： Timothy W. Giraldin , Patrick W. Giraldin , Regan E. Kelly , Martin F. Crowley , Eric Couch , Y-Tin Gross
发明人： Timothy W. Giraldin , Patrick W. Giraldin , Regan E. Kelly , Martin F. Crowley , Eric Couch , Y-Tin Gross
IPC分类号： G06K5/00
CPC分类号： G06Q30/02 , G06Q20/10 , G07C9/00103 , G07C9/00111 , G07C11/00 , G07C2011/02 , G07C2011/04
摘要： A method and system are disclosed for the communication for a confined area of a facility. Personal identification information of a group member into at least one of a set of stations distributed throughout the confined area. Monetary deposit information for the member group is received, and transaction information is received from at least one cashless station. Transaction reports are created.
摘要翻译：公开了用于设施的限制区域的通信的方法和系统。将组成员的个人识别信息分配到分布在整个限制区域内的一组站点中的至少一个。收到成员组的货币存款信息，从至少一个无现金站收到交易信息。创建交易报告。

9. 发明申请

US20050073407A1 Route planning system and method 审中-公开
标题翻译：路线规划制度及方法
公开(公告)号：US20050073407A1
公开(公告)日：2005-04-07
申请号：US10716800
申请日：2003-11-18
申请人： Timothy Giraldin , Patrick Giraldin , Regan Kelly , Martin Crowley , Eric Couch , Y-Tin Gross
发明人： Timothy Giraldin , Patrick Giraldin , Regan Kelly , Martin Crowley , Eric Couch , Y-Tin Gross
IPC分类号： G06Q10/00 , G06Q30/00 , G07C9/00 , G07C11/00 , G08B1/08
CPC分类号： G06Q10/02 , G06Q30/02 , G07C9/00103 , G07C9/00111 , G07C11/00 , G07C2011/02 , G07C2011/04
摘要： A system and method of communication are disclosed for communication for a confined area of a facility. Personal identification information of a guest is received into at least one of a set of stations distributed throughout the confined area. At least one person icon or place icon is displayed on a map of the confined area. A select signal indicative of at least one of said person icons or place icons is received. Direction indicia to the selected icon is displayed.
摘要翻译：公开了一种用于通信设施的限制区域的通信系统和方法。访客的个人识别信息被接收到分布在整个限制区域内的一组站点中的至少一个。在限制区域的地图上显示至少一个人图标或地点图标。接收到指示所述人物图标或地点图标中的至少一个的选择信号。显示所选图标的方向标记。

10. 发明授权

US07255536B2 Turbine airfoil platform cooling circuit 有权
标题翻译：涡轮机翼平台冷却回路
公开(公告)号：US07255536B2
公开(公告)日：2007-08-14
申请号：US11134927
申请日：2005-05-23
申请人： Frank J. Cunha , Eric Couch , Keith A. Santeler , Scott W. Gayman , Eric A. Hudson , Christopher Joe , Eric Letizia
发明人： Frank J. Cunha , Eric Couch , Keith A. Santeler , Scott W. Gayman , Eric A. Hudson , Christopher Joe , Eric Letizia
IPC分类号： F01D5/18
CPC分类号： F01D9/02 , F01D5/187 , F01D25/12 , F05D2240/81 , Y02T50/676
摘要： An airfoil assembly includes an airfoil extending away from a platform. One or more cooling circuits are formed through the platform in order to provide cooling of the platform. The cooling circuit may include a downwardly directed inlet receiving cooling air from below the platform. The cooling air is then directed in a direction generally parallel to the outer surface of the platform and through exits formed through the outer surface of the platform. The cooling circuit may optionally include a plurality of pedestals extending from an outer wall to an inner wall of the cooling circuit to increase the rigidity and the cooling function of the cooling circuit.
摘要翻译：机翼组件包括远离平台延伸的翼型件。通过平台形成一个或多个冷却回路以提供平台的冷却。冷却回路可以包括从平台下方接收冷却空气的向下定向的入口。然后将冷却空气沿大致平行于平台的外表面的方向引导并通过平台的外表面形成的出口。冷却回路可以可选地包括从冷却回路的外壁延伸到内壁的多个基座，以增加冷却回路的刚度和冷却功能。

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