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公开(公告)号：US20170357223A1
公开(公告)日：2017-12-14
申请号：US15182324
申请日：2016-06-14
Applicant: General Electric Company
Inventor： Xiaomo Jiang , Alston IIford Scipio , Sanji Ekanayake , Rebecca Evelyn Hefner
CPC classification number: G05B13/026 , G05B15/02 , G05B23/0243
Abstract: A control system for a gas turbine includes a processor. The processor configured to access data indicative of environmental conditions of a location of the gas turbine. The processor is configured to predict an occurrence of an event associated with the gas turbine based on the environmental conditions, wherein the event comprises a change in operation of the gas turbine due to the environmental conditions. The processor is configured to send a signal indicating the occurrence of the event to an electronic device.
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公开(公告)号：US09758877B2
公开(公告)日：2017-09-12
申请号：US14769499
申请日：2014-02-28
Applicant: General Electric Company
Inventor： Sal Esposito , Anthony M. Rossi , Mel Joseph Esmacher , Rebecca Evelyn Hefner , Trevor James Dale , Kelsey Elizabeth Beach
CPC classification number: C23F11/00 , B08B3/08 , C23F11/141 , F24F7/00
Abstract: Methods and compositions are disclosed for inhibiting corrosion on metal surfaces of gas turbine air compressors. The methods comprise contacting the metal surfaces with a corrosion inhibiting composition comprising at least one filming amine.
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13.发明申请GAS TURBINE ENGINE SYSTEMS AND METHODS FOR IMPARTING CORROSION RESISTANCE TO GAS TURBINE ENGINES 审中-公开气体涡轮发动机系统及其对燃气涡轮发动机耐腐蚀性的方法公开(公告)号：US20150159556A1
公开(公告)日：2015-06-11
申请号：US14098916
申请日：2013-12-06
Applicant: General Electric Company
Inventor： Alston IIford Scipio , Dale Joel Davis , Sanji Ekanayake , Paul Robert Fernandez , Rebecca Evelyn Hefner
IPC: F02C7/30
CPC classification number: F02C7/30 , F01D25/002 , F01D25/007 , F02C6/08 , F05D2210/20 , F05D2220/321 , F05D2220/3216 , F05D2260/95
Abstract: Methods and systems for imparting corrosion resistance to gas turbine engines are disclosed. Existing and/or supplemental piping is connected to existing compressor section air extraction and turbine section cooling air piping to supply water and anti-corrosion agents into areas of the gas turbine engine not ordinarily and/or directly accessible by injection of cleaning agents into the bellmouth of the turbine alone and/or repair methods. An anti-corrosion mixture is selectively supplied as a liquid-steam mixture to the compressor and/or the turbine sections of the gas turbine engine to coat the gas turbine engine components therein with a metal passivation coating which mitigates corrosion in the gas turbine engine.
Abstract translation: 公开了赋予燃气涡轮发动机耐腐蚀性的方法和系统。 现有和/或补充的管道连接到现有的压缩机部分空气抽出和涡轮部分冷却空气管道，以将燃料涡轮发动机的区域中的水和防腐剂供应到通常和/或直接通过将清洁剂注入到喇叭口 的涡轮机和/或修理方法。 选择性地将抗腐蚀混合物作为液体 - 蒸汽混合物供应到燃气涡轮发动机的压缩机和/或涡轮机部分，以用减轻燃气涡轮发动机中的腐蚀的金属钝化涂层涂覆其中的燃气涡轮发动机部件。
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公开(公告)号：US20150159506A1
公开(公告)日：2015-06-11
申请号：US14098644
申请日：2013-12-06
Applicant: General Electric Company
Inventor： Alston Ilford Scipio , Sanji Ekanayake , Dale J. Davis , Rebecca Evelyn Hefner , Brent Allen Clothier
CPC classification number: F01D25/002 , B08B3/02 , B08B3/08 , C11D3/3947 , C11D11/0041 , F01D25/007 , F05D2260/95 , Y02T50/672
Abstract: A gas turbine wash control system may perform a wash and a rinse of a gas turbine that is offline. An peracetic acid inter-rinse solution may be injected into the gas turbine. The gas turbine may be agitated and the peracetic acid inter-rinse solution drained. A second rinse of the gas turbine may be performed followed by the injection of an anticorrosive solution into the gas turbine.
Abstract translation: 燃气轮机洗涤控制系统可执行脱机的燃气轮机的洗涤和冲洗。 可以将过乙酸冲洗溶液注入到燃气轮机中。 可以搅拌燃气轮机并排出过乙酸冲洗溶液。 可以执行燃气轮机的第二冲洗，然后将防锈溶液注入到燃气轮机中。
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公开(公告)号：US11578656B2
公开(公告)日：2023-02-14
申请号：US16774675
申请日：2020-01-28
Applicant: General Electric Company
Inventor： Wolfgang Franz Dietrich Mohr , Joerg Pfistner , Kamel Tayebi , Murali Krishna Kalaga , Rebecca Evelyn Hefner
Abstract: Air filtration assemblies configured to provide instant detection of particles and/or improve particle filtration are disclosed. The assemblies may include an air inlet duct in fluid communication with a compressor of a gas turbine system. The air inlet duct may include an inlet for receiving intake air including intake air particles, and an outlet positioned opposite the inlet. The assembly may also include a plurality of vane filters at the inlet, an array of fabric filters positioned in the air inlet duct, downstream of the vane filters, and a silencer assembly positioned in the air inlet duct, downstream of the fabric filters. Additionally, the assembly may include an electrostatic component positioned in the air inlet duct, downstream of the fabric filters. The electrostatic component may be configured to charge the intake air particles that pass through the vane filters and the fabric filters.
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Patent Agency Ranking
公开(公告)号：US20190016478A1
公开(公告)日：2019-01-17
申请号：US16131457
申请日：2018-09-14
Applicant: General Electric Company
Inventor： Andrew Scott Kessie , Rebecca Evelyn Hefner
CPC classification number: B64F5/60 , B64F5/00 , G06Q10/06 , G07C5/008 , G08G5/0091
Abstract: Systems and methods for assessing and quantifying the environmental impact on a mechanical component are provided. In one embodiment, a method can include receiving one or more first set(s) of data from one or more first data acquisition system(s) configured to communicate with an onboard system of an aircraft. The method can further include receiving one or more second sets of data from one or more second data acquisition systems that are remote from the aircraft. The method can include determining an aggregate amount of the environmental condition experienced by a mechanical component of the aircraft based at least in part on the first sets of data and the second sets of data. The method can include predicting a level of distress associated with the mechanical component based at least in part on the aggregate amount of the environmental condition experienced by the mechanical component.
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公开(公告)号：US20170356346A1
公开(公告)日：2017-12-14
申请号：US15182359
申请日：2016-06-14
Applicant: General Electric Company
Inventor： Xiaomo Jiang , Rebecca Evelyn Hefner , Bradford George Foulkes , Jianxiong Chen , John Robert Korsedal
IPC: F02C7/30 , G05B19/042 , G05B13/02
CPC classification number: F02C7/30 , F02C9/00 , F04D27/0292 , F05D2260/607 , F05D2260/80 , F05D2270/11 , F05D2270/44 , G05B13/026 , G05B19/0428 , G05B2219/34477
Abstract: A control system for a gas turbine includes a processor. The processor configured to access one or more operating parameters of the gas turbine. The operating parameters are configured to specify how the gas turbine operates. The processor is configured to predict a rate of degradation to one or more parts of a compressor of the gas turbine due to one or more effects on the parts by operating the gas turbine according to the one or more operating parameters. The processor is configured to send an alert to an electronic device based at least in part on the rate of degradation of the compressor.
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18.发明授权公开(公告)号：US09671030B2
公开(公告)日：2017-06-06
申请号：US13690233
申请日：2012-11-30
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Paul Stephen Dimascio , Michael Douglas Arnett , Rebecca Evelyn Hefner , Christopher D. Higgins
CPC classification number: F16K31/002 , F01D11/003 , F01D11/18 , F01D17/085 , F05D2300/5021 , F16J15/164 , F16J15/445
Abstract: A metallic seal assembly, a turbine component, and a method of regulating flow in turbo-machinery are disclosed. The metallic seal assembly includes a sealing structure having thermally-responsive features. The thermally-responsive features deploy from or retract toward a surface of the sealing structure in response to a predetermined temperature change. The turbine component includes the metallic seal assembly. The method of regulating flow in turbo-machinery includes providing the metallic seal assembly and raising or retracting the thermally-responsive features in response to the predetermined temperature change.
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公开(公告)号：US09267393B2
公开(公告)日：2016-02-23
申请号：US13783831
申请日：2013-03-04
Applicant: General Electric Company
Inventor： Pablo de Jesus Diaz , Rebecca Evelyn Hefner
CPC classification number: F01D25/002 , B24C1/003 , B24C1/086 , F01D21/003 , F05D2230/72 , F05D2260/607 , Y02T50/675
Abstract: Aspects of the invention provide an apparatus for cleaning airfoils inside a gas turbine compressor. In one embodiment, an apparatus for cleaning at least one airfoil within a turbine compressor, includes: a hose for applying cleaning material to the at least one airfoil; and an articulation assembly for articulating a nozzle of the hose, the articulation assembly including: a main shaft attached to the hose at a first end; and an articulating trigger for rotating the first end of the main shaft. The apparatus may further include a borescope attached to the articulation assembly and a borescope monitor for viewing the at least one airfoil via the borescope.
Abstract translation: 本发明的方面提供一种用于清洁燃气涡轮压缩机内的翼型的装置。 在一个实施例中，一种用于清洁涡轮压缩机内的至少一个翼型件的装置包括：用于将清洁材料施加到所述至少一个翼型件的软管; 以及用于铰接所述软管的喷嘴的关节运动组件，所述关节运动组件包括：在第一端附接到所述软管的主轴; 以及用于旋转主轴的第一端的铰接扳机。 该装置还可以包括连接到铰接组件的管内窥镜和用于经由管道镜观察至少一个翼型件的管内窥镜监视器。
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公开(公告)号：US20150159505A1
公开(公告)日：2015-06-11
申请号：US14098627
申请日：2013-12-06
Applicant: General Electric Company
Inventor： Alston Ilford Scipio , Sanji Ekanayake , Dale J. Davis , Rebecca Evelyn Hefner
CPC classification number: F01D25/002 , B08B3/02 , B08B3/08 , C11D7/265 , C11D7/3209 , C11D11/0041
Abstract: A gas turbine wash control system may perform a wash and a rinse of a gas turbine that is offline. An inter-rinse solution may be injected into the gas turbine. The gas turbine may be agitated and the inter-rinse solution drained. A second rinse of the gas turbine may be performed followed by the injection of an anticorrosive solution into the gas turbine.
Abstract translation: 燃气轮机洗涤控制系统可执行脱机的燃气轮机的洗涤和冲洗。 冲洗液可以喷入燃气轮机。 可以搅动燃气轮机并排出冲洗溶液。 可以执行燃气轮机的第二冲洗，然后将防锈溶液注入到燃气轮机中。
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