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公开(公告)号：US09638055B2
公开(公告)日：2017-05-02
申请号：US15349283
申请日：2016-11-11
Applicant: General Electric Company
Inventor： Mark Carmine Bellino , Mark Lawrence Hunt
CPC classification number: F01D25/002 , B08B9/00 , B08B9/0321 , C23C4/185 , F01D5/187 , F01D5/188 , F01D25/12 , F04D29/582 , F04D29/701 , F05D2220/31 , F05D2220/32
Abstract: Blockages of turbomachine cooling circuit cooling holes resulting from coating processes can be removed by introducing a cleaning agent into the cooling circuit. The cooling circuit can be connected to a cleaning agent supply under pressure, adding force on the blockage to chemical action by the cleaning agent. The cleaning agent is chemically reactive with the coating material and substantially chemically non-reactive with the underlying material of the cooling circuit and other parts of the turbomachine. A neutralization agent can also be introduced to reduce toxicity and/or action of the cleaning agent. A turbomachine cooling hole cleaning method includes introducing a cleaning agent into a cooling circuit of a turbomachine part, pressurizing the cleaning agent in the cooling circuit until a first defined condition is met, and introducing a neutralization agent to the turbomachine part while the cleaning agent is applied to the cooling circuit.
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公开(公告)号：US09523287B2
公开(公告)日：2016-12-20
申请号：US13745136
申请日：2013-01-18
Applicant: General Electric Company
Inventor： Mark Carmine Bellino , Mark Lawrence Hunt
CPC classification number: F01D25/002 , B08B9/00 , B08B9/0321 , C23C4/185 , F01D5/187 , F01D5/188 , F01D25/12 , F04D29/582 , F04D29/701 , F05D2220/31 , F05D2220/32
Abstract: Blockages of turbomachine cooling circuit cooling holes resulting from coating processes can be removed by introducing a cleaning agent into the cooling circuit. The cooling circuit can be connected to a cleaning agent supply under pressure, adding force on the blockage to chemical action by the cleaning agent. The cleaning agent is chemically reactive with the coating material and substantially chemically non-reactive with the underlying material of the cooling circuit and other parts of the turbomachine. A neutralization agent can also be introduced to reduce toxicity and/or action of the cleaning agent.
Abstract translation: 可以通过将清洁剂引入冷却回路来除去由涂布过程产生的涡轮机冷却回路冷却孔的堵塞。 冷却回路可以在压力下连接到清洁剂供应源上，从而增加阻塞作用力，使清洁剂产生化学作用。 清洁剂与涂层材料具有化学反应性，并且与冷却回路和涡轮机的其它部分的基础材料基本上化学上不反应。 还可以引入中和剂以减少清洁剂的毒性和/或作用。
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公开(公告)号：US20160076578A1
公开(公告)日：2016-03-17
申请号：US14485296
申请日：2014-09-12
Applicant: General Electric Company
IPC: F16B39/08
Abstract: A nut anti-rotation cap includes an end wall having an inner surface configured to be operatively coupled to an end of a threaded mechanical fastener. Also included is at least one sidewall extending from the end wall, wherein the at least one sidewall is a solid wall configured to be secured to a nut engaged with the threaded mechanical fastener and to enclose an exposed portion of the threaded mechanical fastener.
Abstract translation: 螺母防旋转盖包括端壁，所述端壁具有构造成可操作地联接到螺纹机械紧固件的端部的内表面。 还包括从端壁延伸的至少一个侧壁，其中至少一个侧壁是实心壁，其构造成固定到与螺纹机械紧固件接合的螺母并且包围螺纹机械紧固件的暴露部分。
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公开(公告)号：US09259807B2
公开(公告)日：2016-02-16
申请号：US14105353
申请日：2013-12-13
Applicant: General Electric Company
Inventor： Gregory Scott Means , Steven Charles Woods , Mark Carmine Bellino , James Christopher Monaghan , Jonathan Dwight Berry , Patrick S. Riley
CPC classification number: F23R3/286 , B23P6/002 , B23P6/005 , B23P2700/13 , F02M2200/8061 , F02M2200/8069 , F05D2230/80 , F23R2900/00016 , F23R2900/00019 , F28F11/00 , Y10T29/49726 , Y10T29/49728
Abstract: A method for repairing a bundled tube fuel injector includes removing a portion of a pre-mix tube, aligning a tube tip with the remaining portion pre-mix tube and fixedly connecting the tube tip to the pre-mix tube. The method may further include removing an aft plate and an outer shroud from the bundled tube fuel injector so as to expose the pre-mix tube.
Abstract translation: 用于修复捆扎管式燃料喷射器的方法包括去除预混合管的一部分，将管尖与剩余部分预混合管对准，并将管尖固定连接到预混合管。 该方法还可以包括从捆扎管燃料喷射器移除尾板和外护罩，以暴露预混管。
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公开(公告)号：US20150167983A1
公开(公告)日：2015-06-18
申请号：US14105368
申请日：2013-12-13
Applicant: General Electric Company
Inventor： Johnie F. McConnaughhay , Steven Charles Woods , Mark Carmine Bellino , James Christopher Monaghan , Jonathan Dwight Berry
CPC classification number: F23R3/283 , F02C7/222 , F05D2230/30 , F05D2240/35 , F23D2900/00018 , F23R3/286 , F23R3/46 , F23R2900/00005 , F23R2900/00018
Abstract: A bundled tube fuel injector includes a fuel plenum defined within the bundled tube fuel injector and a plurality of pre-mix tubes that extend downstream from the fuel plenum substantially parallel to one another. Each pre-mix tube includes an end portion and a radially extending end surface. An additively manufactured tube tip is fixedly connected to the end portion of a corresponding pre-mix tube.
Abstract translation: 捆束管燃料喷射器包括限定在捆束管燃料喷射器内的燃料增压室和从燃料增压室的下游基本上彼此平行延伸的多个预混合管。 每个预混合管包括端部和径向延伸的端表面。 附加制造的管尖固定地连接到相应的预混合管的端部。
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Patent Agency Ranking
公开(公告)号：US20150167981A1
公开(公告)日：2015-06-18
申请号：US14105327
申请日：2013-12-13
Applicant: General Electric Company
Inventor： Steven Charles Woods , Gregory Scott Means , Mark Carmine Bellino , James Christopher Monaghan , Johnie F. McConnaughhay
Abstract: A bundled tube fuel injector includes a fuel plenum that is defined within the bundled tube fuel injector and a plurality of pre-mix tubes that extend downstream from the fuel plenum substantially parallel to one another. Each pre-mix tube includes an end portion and a radially extending end surface. The bundled tube fuel injector further includes a tube tip that is fixedly connected to the end portion of a corresponding pre-mix tube.
Abstract translation: 捆束管燃料喷射器包括限定在束管式燃料喷射器内的燃料增压室和从燃料增压室的下游基本上彼此平行延伸的多个预混管。 每个预混合管包括端部和径向延伸的端表面。 捆扎管燃料喷射器还包括固定地连接到相应的预混合管的端部的管末端。
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公开(公告)号：US08985049B2
公开(公告)日：2015-03-24
申请号：US13826017
申请日：2013-03-14
Applicant: General Electric Company
Inventor： Mark Carmine Bellino , Jonathan Matthew Lomas , Matthew Paul Berkebile , Michael Anthony DePalma, III
CPC classification number: B08B17/02 , B05C21/005 , C23C4/01 , C23C14/042 , C23C16/042 , F01D5/286 , F01D5/288 , F01D5/3092 , Y10T137/8376
Abstract: Pressure maskers for masking at least one passageway of an article include a body portion that surrounds at least a portion of the article around the at least one passageway, at least one fluid inlet connected to the body portion that provides a conduit for pressurized masking fluid to pass from an exterior of the pressure masker to an interior of the pressure masker, wherein the article is at least partially disposed within the interior of the pressure masker, and at least one seal that seals the body portion at least partially around the article such that the pressurized masking fluid that enters the interior of the pressure masker is at least partially forced through the at least one passageway.
Abstract translation: 用于掩蔽制品的至少一个通道的压力掩模包括围绕所述至少一个通道围绕所述制品的至少一部分的主体部分，连接到所述主体部分的至少一个流体入口，其提供用于加压掩蔽流体的管道 从压力屏蔽器的外部通过到压力掩蔽器的内部，其中制品至少部分地设置在压力掩蔽器的内部，以及至少一个密封件，其至少部分地围绕物品密封身体部分，使得 进入压力屏蔽器内部的加压掩模流体至少部分地被迫穿过至少一个通道。
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公开(公告)号：US09856734B2
公开(公告)日：2018-01-02
申请号：US14824566
申请日：2015-08-12
Applicant: General Electric Company
Inventor： Jacob Andrew Salm , Mark Carmine Bellino , James Ryan Connor , Gareth William David Lewis , Keith Alan Lord
IPC: F01D5/00 , G05B19/4099 , G05B15/02 , B23P6/00
CPC classification number: F01D5/005 , B23P6/007 , F01D5/284 , F01D5/288 , F05D2220/30 , F05D2230/30 , F05D2230/80 , F05D2300/2261 , G05B15/02 , G05B19/4099 , G05B2219/35128 , G05B2219/45147
Abstract: A system for adaptively machining a shroud of a blade used in a turbomachine is provided. The system may include a computer system including a module(s) configured to: extract geometric location data from a 3D model of the shroud after use in the turbomachine, the 3D model created by digitizing using a digitizing device. The geometric location data includes geometric location data of a hard face plane of the shroud exposed to wear during turbomachine operation and of a non-worn surface adjacent to the hard face plane substantially unexposed to wear during turbomachine operation. Comparing the geometric location data of the non-worn surface from the three-dimensional model to a manufacturing model of the blade determines a change in position of the non-worn surface from use of the blade in the turbomachine. The change in position is used to modify a machining instruction used by a machining device to repair the hard face plane.
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公开(公告)号：US09657899B2
公开(公告)日：2017-05-23
申请号：US13975763
申请日：2013-08-26
Applicant: General Electric Company
Inventor： Mark Carmine Bellino , Bill Damon Johnston, Jr. , Heath Ostebee , Brian Lee Tollison
CPC classification number: F16N21/00 , B23K1/0008 , B23K1/20 , B23K26/34 , B23K31/02 , Y10T29/4973
Abstract: Various embodiments include apparatuses adapted to be used as a replacement oil cartridge tip. In some embodiments apparatuses include a replacement swirler ring for an oil cartridge tip, the replacement swirler ring having an annular main body including an inner diameter surface sized to be joined to an outer diameter surface of the oil cartridge tip by a metal joining process including one of brazing, welding temperature or mechanical interference and an outer diameter surface including channels evenly spaced about a primary axis of the annular main body, wherein the annular ring includes a material that is at least as wear-resistant as a material of the oil cartridge tip.
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公开(公告)号：US20160169113A1
公开(公告)日：2016-06-16
申请号：US14568394
申请日：2014-12-12
Applicant: General Electric Company
Inventor： Mark Carmine Bellino , Lucas John Stoia , Christopher Paul Willis
CPC classification number: F02C7/24 , F01D9/023 , F01D25/145 , F02C7/28 , F02C7/32 , F05D2220/32 , F05D2240/15 , F05D2240/90 , F05D2260/30 , Y02T50/675
Abstract: Aft frame assemblies for aft ends of gas turbine transition pieces comprise a body comprising a downstream facing seal surface on an aft end, wherein at least a portion of the downstream facing seal surface configured to be exposed to a combustion discharge stream, a heat shield disposed proximate the aft end of the body, wherein the heat shield is configured to deflect at least a portion of the combustion discharge stream away from the aft end of the body, and, one or more heat shield supports connected to the body and configured to at least partially restrict deflection of the heat shield back towards the body.
Abstract translation: 用于燃气轮机过渡件的后端的后框架组件包括主体，该主体包括位于后端的下游面对的密封表面，其中下游侧面向密封表面的至少一部分构造成暴露于燃烧排放流， 靠近所述主体的后端，其中所述隔热罩构造成使所述燃烧排放流的至少一部分偏离所述主体的后端，以及一个或多个隔热支撑件，其连接到所述主体并且被配置为 至少部分地限制隔热板向身体的偏转。
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