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Patent Agency Ranking
公开(公告)号：US20180266317A1
公开(公告)日：2018-09-20
申请号：US15463711
申请日：2017-03-20
Applicant: General Electric Company
Inventor： Hua ZHANG , Naveen Ghattadhahalli Parmeshwar , Christopher Conrad Frese , Valery Ivanovich Ponyavin , Bradly Aaron Kippel
Abstract: The present application provides a gas turbine engine. The gas turbine engine may include a compressor and an inlet air system positioned upstream of the compressor. The inlet air system may include a wetted media pad for evaporative cooling. The wetted media pad may include a number of synthetic media sheets with a number of micro-channels therein.
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公开(公告)号：US10780385B2
公开(公告)日：2020-09-22
申请号：US15608591
申请日：2017-05-30
Applicant: General Electric Company
Inventor： Bradly Aaron Kippel , Christopher Conrad Frese
Abstract: In one embodiment, a system includes an intake section including a filter and one or more strain gauges. The system also includes a processor configured to receive strain information for the filter from the one or more strain gauges and determine an operating condition of the filter based at least in part on the strain information.
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公开(公告)号：US20200063757A1
公开(公告)日：2020-02-27
申请号：US16112061
申请日：2018-08-24
Applicant: General Electric Company
Inventor： Alan Eskandar , Valery Ivanovich Ponyavin , Hua Zhang , Christopher Conrad Frese
Abstract: A system includes an inlet duct disposed about an inlet axis, wherein the inlet duct is configured to direct an airflow along the inlet axis to a compressor inlet. The inlet includes an inlet heating system and a heating portion having a longitudinal axis that is substantially perpendicular to the inlet axis. The inlet heating system includes a first conduit substantially parallel to the longitudinal axis that is configured to distribute a heated fluid directly to the airflow via a first set of openings of a first end zone of the first conduit and a second set of openings of a second zone of the first conduit. The first end zone is configured to receive the heated fluid from a heating source, the second zone is coupled to the first end zone, and the second zone is configured to receive the heated fluid from the first end zone.
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公开(公告)号：US10124283B2
公开(公告)日：2018-11-13
申请号：US15358431
申请日：2016-11-22
Applicant: General Electric Company
Inventor： Christopher Conrad Frese , Bradly Kippel
IPC: B01D46/00
Abstract: A filter assembly for a gas turbine system includes a filter element configured to remove entrained particles from air which passes through the filter element in a first direction toward a central air passageway. A motion generator arranged to rotate the filter element about a longitudinal axis extending in an airflow direction of the air passageway to cause particles accumulated on the filter element to fall downwardly away from the filter element due to gravity.
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15.发明申请TURBOMACHINE LOAD COUPLING DEVICE HAVING A NATURAL CONVECTION VENTILATION SYSTEM 审中-公开具有自然通风通风系统的涡轮负载耦合装置公开(公告)号：US20160348584A1
公开(公告)日：2016-12-01
申请号：US14721355
申请日：2015-05-26
Applicant: General Electric Company
CPC classification number: F02C7/18 , F01D15/00 , F01D15/10 , F02C3/04 , F02C7/36 , F05D2220/32 , F05D2240/14 , F05D2240/35 , F24F7/04 , F24F2007/004
Abstract: A load coupling device includes a housing including an interior portion, an ambient air inlet provided in the housing, and a load coupling guard arranged in the housing. The load coupling guard includes a turbomachine end and a load end and a passage extending therebetween. A vent extends upwardly from the load coupling guard. The vent is fluidically exposed to the load end. An ambient air inlet passage is formed in the load coupling guard and fluidically connects the ambient air inlet and the vent. The load end is substantially fluidically isolated from the turbomachine end.
Abstract translation: 负载联接装置包括壳体，该壳体包括内部部分，设置在壳体中的环境空气入口和布置在壳体中的负载联接防护件。 负载联接防护罩包括涡轮机端和负载端以及在它们之间延伸的通道。 通风口从负载联轴器保护罩向上延伸。 通风口流体地暴露于负载端。 环境空气入口通道形成在负载联接器护罩中并且流体地连接环境空气入口和通风口。 负载端基本上与涡轮机端流体隔离。
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