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公开(公告)号：US20170252689A1
公开(公告)日：2017-09-07
申请号：US15060658
申请日：2016-03-04
Applicant: General Electric Company
Inventor： Ameya Chandrakant Joshi , Bradly Aaron Kippel
CPC classification number: B01D46/0068 , B01D46/002 , B01D46/2403 , B01D46/4272
Abstract: A pulse jet cleaning system is disclosed having at least one diverter device and having at least one control valve configured for receiving pulse air from a pulse air manifold and controllably passing a pulse of pulse air downstream to clean the filter assemblies. The at least one diverter is configured for receiving the pulse from the control valve and diverting the pulse into a plurality of outlet ports for providing pulse air to at least two blowpipes for cleaning a filter assembly.
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公开(公告)号：US10035095B2
公开(公告)日：2018-07-31
申请号：US15060658
申请日：2016-03-04
Applicant: General Electric Company
Inventor： Ameya Chandrakant Joshi , Bradly Aaron Kippel
CPC classification number: B01D46/0068 , B01D46/002 , B01D46/2403 , B01D46/4272
Abstract: A pulse jet cleaning system is disclosed having at least one diverter device and having at least one control valve configured for receiving pulse air from a pulse air manifold and controllably passing a pulse of pulse air downstream to clean the filter assemblies. The at least one diverter is configured for receiving the pulse from the control valve and diverting the pulse into a plurality of outlet ports for providing pulse air to at least two blowpipes for cleaning a filter assembly.
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3.发明授权公开(公告)号：US09422868B2
公开(公告)日：2016-08-23
申请号：US13859388
申请日：2013-04-09
Applicant: General Electric Company
Inventor： Korey Frederic Rendo , David Wesley Ball, Jr. , Diego Fernando Rancruel , Ameya Chandrakant Joshi , Michael Brian Smith
IPC: F02C7/224
CPC classification number: F02C7/224
Abstract: A simple cycle gas turbomachine includes a compressor portion, and a turbine portion having an outlet. At least one combustor is fluidically connected to the compressor portion and the turbine portion. An exhaust member includes an inlet, fluidically connected to the outlet of the turbine portion, a first outlet and a second outlet. A fuel conditioning system includes a heat exchange member provided with a first circuit having an exhaust gas inlet fluidically connected to the second outlet of the exhaust member and an exhaust gas inlet, a second circuit having an inlet fluidically connected to a source of fuel and an outlet fluidically connected to the at least one combustor. A conditioned fluid conduit is fluidically connected between a source of conditioned fluid and one of the combustor assembly and the first outlet of the exhaust member.
Abstract translation: 简单的循环气体涡轮机包括压缩机部分和具有出口的涡轮机部分。 至少一个燃烧器流体地连接到压缩机部分和涡轮机部分。 排气构件包括流体连接到涡轮部分的出口的入口，第一出口和第二出口。 燃料调节系统包括具有第一回路的热交换构件，该第一回路具有与排气构件的第二出口流体连接的排气入口和排气入口，第二回路具有与燃料源流体连接的入口和 出口流体连接到至少一个燃烧器。 调节流体导管流体地连接在调节流体源和燃烧器组件之一和排气构件的第一出口之间。
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4.发明申请公开(公告)号：US20140298816A1
公开(公告)日：2014-10-09
申请号：US13859388
申请日：2013-04-09
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Korey Frederic Rendo , David Wesley Ball, JR. , Diego Fernando Rancruel , Ameya Chandrakant Joshi , Michael Brian Smith
IPC: F02C7/224
CPC classification number: F02C7/224
Abstract: A simple cycle gas turbomachine includes a compressor portion, and a turbine portion having an outlet. At least one combustor is fluidically connected to the compressor portion and the turbine portion. An exhaust member includes an inlet, fluidically connected to the outlet of the turbine portion, a first outlet and a second outlet. A fuel conditioning system includes a heat exchange member provided with a first circuit having an exhaust gas inlet fluidically connected to the second outlet of the exhaust member and an exhaust gas inlet, a second circuit having an inlet fluidically connected to a source of fuel and an outlet fluidically connected to the at least one combustor. A conditioned fluid conduit is fluidically connected between a source of conditioned fluid and one of the combustor assembly and the first outlet of the exhaust member.
Abstract translation: 简单的循环气体涡轮机包括压缩机部分和具有出口的涡轮机部分。 至少一个燃烧器流体地连接到压缩机部分和涡轮机部分。 排气构件包括流体连接到涡轮部分的出口的入口，第一出口和第二出口。 燃料调节系统包括具有第一回路的热交换构件，该第一回路具有与排气构件的第二出口流体连接的排气入口和排气入口，第二回路具有与燃料源流体连接的入口和 出口流体连接到至少一个燃烧器。 调节流体导管流体地连接在调节流体源和燃烧器组件之一和排气构件的第一出口之间。
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