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公开(公告)号:US07762004B2
公开(公告)日:2010-07-27
申请号:US12010513
申请日:2008-01-25
IPC分类号: G01B3/14
CPC分类号: F01D25/285 , B23Q3/063 , F05D2230/64 , F05D2230/68 , F05D2250/182 , F05D2250/183 , F05D2260/80 , G01B3/26 , G01B3/42 , G01B5/0004 , G01B5/14 , G01B5/205
摘要: An inspection tool for a turbine bucket shroud includes: a clamp device for clamping a dovetail portion of a turbine bucket; a template plate provided with an aperture defined by a edge shaped to conform to a specified shape of the turbine bucket shroud, wherein the template is moveable to a location over the turbine bucket shroud in a direction toward the clamp device, and wherein, at the location, the aperture represents a design specification location for the turbine bucket shroud relative to the dovetail portion of the bucket. A measurement gauge is provided for measuring gaps between edges of the shroud and edges of the template aperture.
摘要翻译: 一种用于涡轮机桶护罩的检查工具包括:用于夹紧涡轮桶的燕尾部分的夹紧装置; 模板板,其设置有由形状为符合涡轮机桶护罩的指定形状的边缘限定的孔,其中模板可沿着朝向夹紧装置的方向移动到涡轮机桶护罩上方的位置,并且其中,在 位置,孔表示相对于桶的燕尾部分的涡轮机桶护罩的设计规格位置。 提供测量计用于测量护罩的边缘与模板孔的边缘之间的间隙。
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公开(公告)号:US09015987B2
公开(公告)日:2015-04-28
申请号:US12344524
申请日:2008-12-28
申请人: Todd Moran , Darrell Hollis , Frank Bowers , Leo Desjardins , Michael Cruse , Kevin Keegan , Bret Warren
发明人: Todd Moran , Darrell Hollis , Frank Bowers , Leo Desjardins , Michael Cruse , Kevin Keegan , Bret Warren
CPC分类号: G08B21/18 , A01M23/00 , A01M23/16 , A01M31/002 , A01M99/00 , G01C15/00 , G08C2201/51 , H04Q9/00
摘要: Disclosed is a trap including a status LED configured to indicate a trap status, a door sensor configured to indicate a door status, and a status button, configured to: 1) wake a micro controller such that the telemetry-enabled trap can be registered with a telemetry system, and 2) cause the status LED to indicate at least the trap status and the door status. Also disclosed is a method for monitoring the trap. The method includes receiving GPS data, monitoring the GPS data for valid positional information, and receiving an event message from a trap tracker module.
摘要翻译: 公开了一种包括配置为指示陷阱状态的状态LED的陷阱,被配置为指示门状态的门传感器和状态按钮,其被配置为:1)唤醒微控制器,使得能够向遥控器发送陷阱, 遥测系统,以及2)使状态LED至少指示陷阱状态和门状态。 还公开了一种用于监测陷阱的方法。 该方法包括接收GPS数据,监测GPS数据以获取有效位置信息,以及从陷阱跟踪器模块接收事件消息。
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公开(公告)号:US20090193707A1
公开(公告)日:2009-08-06
申请号:US12344524
申请日:2008-12-28
申请人: Todd Moran , Darrel Hollis , Frank Bowers , Leo Desjardins , Michael Cruse , Kevin Keegan , Bret Warren
发明人: Todd Moran , Darrel Hollis , Frank Bowers , Leo Desjardins , Michael Cruse , Kevin Keegan , Bret Warren
CPC分类号: G08B21/18 , A01M23/00 , A01M23/16 , A01M31/002 , A01M99/00 , G01C15/00 , G08C2201/51 , H04Q9/00
摘要: Disclosed is a trap including a status LED configured to indicate a trap status, a door sensor configured to indicate a door status, and a status button, configured to: 1) wake a micro controller such that the telemetry-enabled trap can be registered with a telemetry system, and 2) cause the status LED to indicate at least the trap status and the door status. Also disclosed is a method for monitoring the trap. The method includes receiving GPS data, monitoring the GPS data for valid positional information, and receiving an event message from a trap tracker module.
摘要翻译: 公开了一种包括配置为指示陷阱状态的状态LED的陷阱,被配置为指示门状态的门传感器和状态按钮,其被配置为:1)唤醒微控制器,使得能够向遥控器发送陷阱, 遥测系统,以及2)使状态LED至少指示陷阱状态和门状态。 还公开了一种用于监测陷阱的方法。 该方法包括接收GPS数据,监测GPS数据以获取有效位置信息,以及从陷阱跟踪器模块接收事件消息。
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公开(公告)号:US20090064520A1
公开(公告)日:2009-03-12
申请号:US12010513
申请日:2008-01-25
CPC分类号: F01D25/285 , B23Q3/063 , F05D2230/64 , F05D2230/68 , F05D2250/182 , F05D2250/183 , F05D2260/80 , G01B3/26 , G01B3/42 , G01B5/0004 , G01B5/14 , G01B5/205
摘要: An inspection tool for a turbine bucket shroud includes: a clamp device for clamping a dovetail portion of a turbine bucket; a template plate provided with an aperture defined by a edge shaped to conform to a specified shape of the turbine bucket shroud, wherein the template is moveable to a location over the turbine bucket shroud in a direction toward the clamp device, and wherein, at the location, the aperture represents a design specification location for the turbine bucket shroud relative to the dovetail portion of the bucket. A measurement gauge is provided for measuring gaps between edges of the shroud and edges of the template aperture.
摘要翻译: 一种用于涡轮机桶护罩的检查工具包括:用于夹紧涡轮桶的燕尾部分的夹紧装置; 模板板,其设置有由形状为符合涡轮机桶护罩的指定形状的边缘限定的孔,其中模板可沿着朝向夹紧装置的方向移动到涡轮机桶护罩上方的位置,并且其中,在 位置,孔表示相对于桶的燕尾部分的涡轮机桶护罩的设计规格位置。 提供测量计用于测量护罩的边缘与模板孔的边缘之间的间隙。
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公开(公告)号:US20080292466A1
公开(公告)日:2008-11-27
申请号:US11805528
申请日:2007-05-24
申请人: Daniel Tragesser , Ian Reeves , Christopher Thompson , Todd Moran
发明人: Daniel Tragesser , Ian Reeves , Christopher Thompson , Todd Moran
IPC分类号: F01D5/12
CPC分类号: F01D5/225 , F05D2230/232 , F05D2230/238 , Y10T29/49318
摘要: The present application further describes a method for extending the operating life of a tip shrouded turbine blade that includes the steps of: 1) removing an end located cutter tooth from a seal rail of a tip shroud, the end located cutter tooth including a cutter tooth located at the end of one of the suction side and pressure side of the seal rail of the tip shroud; and 2) attaching a center located cutter tooth to the seal rail of the tip shroud, the center located cutter tooth including a cutter tooth that is located in the approximate center of the seal rail of the tip shroud. In such method, the center located cutter tooth may be attached to the seal rail such that the center located cutter tooth is inside the airfoil if it were projected radially outward from the narrowest point below a tip shroud fillet.
摘要翻译: 本申请进一步描述了一种用于延长尖端覆盖的涡轮机叶片的使用寿命的方法,其包括以下步骤:1)从尖端护罩的密封轨道移除端部定位的切割齿,该端部定位的切割齿包括切割齿 位于尖端护罩的密封导轨的吸力侧和压力侧之一的端部; 以及2)将中心定位的切割齿附接到尖端护罩的密封轨道,所述中心定位的切割齿包括位于尖端护罩的密封轨道的大致中心处的切割齿。 在这种方法中,位于中心的切割齿可以附接到密封轨道,使得如果中心定位的切割齿从尖端护罩圆角下方的最窄点径向向外突出,则其位于翼型内部。
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公开(公告)号:US09009965B2
公开(公告)日:2015-04-21
申请号:US11805528
申请日:2007-05-24
申请人: Daniel Tragesser , Ian Reeves , Christopher Thompson , Todd Moran
发明人: Daniel Tragesser , Ian Reeves , Christopher Thompson , Todd Moran
CPC分类号: F01D5/225 , F05D2230/232 , F05D2230/238 , Y10T29/49318
摘要: The present application further describes a method for extending the operating life of a tip shrouded turbine blade that includes the steps of: 1) removing an end located cutter tooth from a seal rail of a tip shroud, the end located cutter tooth including a cutter tooth located at the end of one of the suction side and pressure side of the seal rail of the tip shroud; and 2) attaching a center located cutter tooth to the seal rail of the tip shroud, the center located cutter tooth including a cutter tooth that is located in the approximate center of the seal rail of the tip shroud. In such method, the center located cutter tooth may be attached to the seal rail such that the center located cutter tooth is inside the airfoil if it were projected radially outward from the narrowest point below a tip shroud fillet.
摘要翻译: 本申请进一步描述了一种用于延长尖端覆盖的涡轮机叶片的使用寿命的方法,其包括以下步骤:1)从尖端护罩的密封轨道移除端部定位的切割齿,该端部定位的切割齿包括切割齿 位于尖端护罩的密封导轨的吸力侧和压力侧之一的端部; 以及2)将中心定位的切割齿附接到尖端护罩的密封轨道,所述中心定位的切割齿包括位于尖端护罩的密封轨道的大致中心的切割齿。 在这种方法中,位于中心的切割齿可以附接到密封轨道,使得如果中心定位的切割齿从尖端护罩圆角下方的最窄点径向向外突出,则其位于翼型内部。
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