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Patent Agency Ranking
公开(公告)号：US20140083078A1
公开(公告)日：2014-03-27
申请号：US13629512
申请日：2012-09-27
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Constantin Dinu , Daniel Aaron Kessler
CPC classification number: F02C9/40 , F02C3/22 , Y02E20/16 , Y02E20/328
Abstract: A system, including a turbine fluid supply system, including a fuel supply assembly, including a first fuel supply configured to supply a first fuel to a gas turbine engine; and a second fuel supply configured to supply a second fuel to the gas turbine engine, wherein the first fuel has a greater carbon content than the second fuel, and a diluent supply assembly comprising at least one diluent supply configured to supply at least one diluent to the gas turbine engine; and a controller having instructions to control the first fuel supply, the second fuel supply, or the at least one diluent supply to adjust a percentage of carbon in a combustor of the gas turbine engine to maintain a ratio of carbonaceous emissions in an exhaust gas per unit of energy produced by the gas turbine engine at or below a threshold ratio.
Abstract translation: 一种包括涡轮流体供应系统的系统，包括燃料供应组件，包括构造成将第一燃料供应到燃气涡轮发动机的第一燃料供应; 以及第二燃料供应，其构造成将第二燃料供应到所述燃气涡轮发动机，其中所述第一燃料具有比所述第二燃料更大的碳含量，以及稀释剂供应组件，其包括至少一种稀释剂供应，所述稀释剂供应构造成供应至少一种稀释剂 燃气轮机; 以及控制器，其具有控制第一燃料供应，第二燃料供应或至少一个稀释剂供应的指令，以调节燃气涡轮发动机的燃烧器中的碳的百分比，以维持排气中碳质排放的比例 由燃气涡轮发动机产生的等于或低于阈值比的能量单位。
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公开(公告)号：US20180080347A1
公开(公告)日：2018-03-22
申请号：US15270892
申请日：2016-09-20
Applicant: General Electric Company
Inventor： Edward Michael Yanosik , Daniel Aaron Kessler
CPC classification number: F01K23/101 , F01K13/02 , F02C6/18 , F02C7/18 , F02C9/18 , Y02E20/14 , Y02E20/16 , Y02E20/326
Abstract: An embodiment includes a power production system having a compressor system compressing a fluid. The system further includes a combustor system combusting compressed fluid and a fuel. The system additionally includes a turbine system configured produce power and an exhaust stream and a first exhaust processing system fluidly coupled to the turbine system and configured to receive the exhaust stream. The system also includes a first bleed system fluidly coupled to a first location in the compressor system, to a second location downstream of the compressor system and upstream of the first exhaust processing system, to a third location in the first exhaust processing system, to a fourth location downstream of the first exhaust processing system, or a combination thereof, and configured to redirect a first compressor extraction from the first location to the second location, to the third location, to the fourth location, or to the combination thereof.
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公开(公告)号：US09739199B2
公开(公告)日：2017-08-22
申请号：US14928560
申请日：2015-10-30
Applicant: General Electric Company
Inventor： Daniel Aaron Kessler , Christopher Hung Vu , Veronica Elizabeth Vela
CPC classification number: F02C7/143 , F01D17/085 , F02C9/18 , F05D2220/32 , F05D2220/3218 , F05D2260/211 , F05D2270/112 , F05D2270/303 , F05D2270/54
Abstract: A control system for a gas turbine includes a controller. The controller includes a processor configured to access an operational parameter associated with the gas turbine. The processor is configured to calculate a bias based on the operational parameter, wherein the bias indicates an amount of change in a temperature of an oxidant entering a compressor of the turbine to reach a reference temperature. The processor is further configured to control the temperature of the oxidant based on the bias to improve power output of the gas turbine.
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公开(公告)号：US10907511B2
公开(公告)日：2021-02-02
申请号：US15270892
申请日：2016-09-20
Applicant: General Electric Company
Inventor： Edward Michael Yanosik , Daniel Aaron Kessler
Abstract: An embodiment includes a power production system having a compressor system compressing a fluid. The system further includes a combustor system combusting compressed fluid and a fuel. The system additionally includes a turbine system configured produce power and an exhaust stream and a first exhaust processing system fluidly coupled to the turbine system and configured to receive the exhaust stream. The system also includes a first bleed system fluidly coupled to a first location in the compressor system, to a second location downstream of the compressor system and upstream of the first exhaust processing system, to a third location in the first exhaust processing system, to a fourth location downstream of the first exhaust processing system, or a combination thereof, and configured to redirect a first compressor extraction from the first location to the second location, to the third location, to the fourth location, or to the combination thereof.
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公开(公告)号：US20170122208A1
公开(公告)日：2017-05-04
申请号：US14928560
申请日：2015-10-30
Applicant: General Electric Company
Inventor： Daniel Aaron Kessler , Christopher Hung Vu , Veronica Elizabeth Vela
CPC classification number: F02C7/143 , F01D17/085 , F02C9/18 , F05D2220/32 , F05D2220/3218 , F05D2260/211 , F05D2270/112 , F05D2270/303 , F05D2270/54
Abstract: A control system for a gas turbine includes a controller. The controller includes a processor configured to access an operational parameter associated with the gas turbine. The processor is configured to calculate a bias based on the operational parameter, wherein the bias indicates an amount of change in a temperature of an oxidant entering a compressor of the turbine to reach a reference temperature. The processor is further configured to control the temperature of the oxidant based on the bias to improve power output of the gas turbine.
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