-
公开(公告)号：US20180230849A1
公开(公告)日：2018-08-16
申请号：US15383043
申请日：2016-12-19
Applicant: General Electric Company
Inventor： Bradly Aaron Kippel , Raymond Pang , Scott Richard Baker , Harold Lamar Jordan, JR. , Rex Allen Morgan , Kamlesh Mundra
CPC classification number: F01D17/14 , F01D25/30 , F02C9/20 , F05D2220/32 , F05D2270/306 , F05D2270/313 , F05D2270/331
Abstract: The present disclosure is direct to a system for regulating a velocity of gases in a turbomachine. The system includes an exhaust section of the turbomachine. The system also includes a damper having an actuator and a restriction. The damper is positioned within the exhaust section and is operable to adjust the velocity of the gases based on a position of the restriction. The system further includes a controller communicatively coupled to the damper. The controller is configured to control the position of the restriction to regulate the velocity of the gases relative to a predetermined velocity range.
-
Patent Agency Ranking
公开(公告)号：US20140260312A1
公开(公告)日：2014-09-18
申请号：US13801259
申请日：2013-03-13
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Lewis Berkley Davis, JR. , Rex Allen Morgan , Harold Lamar Jordan, JR. , Scott Richard Baker
IPC: F02C9/00
CPC classification number: F02C9/00 , F02C9/28 , F05D2270/0831 , F05D2270/20 , F05D2270/303 , F05D2270/44
Abstract: A method of tuning a gas turbine includes receiving a first plurality of operating parameters as the gas turbine engine is operated at a first operating state. Further, the method includes operating the gas turbine engine at a second operating state to measure a second plurality of operating parameters at the second operating state. In addition, the method includes operating the gas turbine engine at a third operating state to measure a third plurality of operating parameters at the third operating state, wherein the first, second, and third operating states are different from each other. Additionally, the method includes generating a correction factor based on the first, second, and third plurality of operating parameters. The method also includes adjusting the operation of the gas turbine engine based on the correction factor.
Abstract translation: 调节燃气轮机的方法包括当燃气涡轮发动机在第一操作状态下操作时接收第一多个操作参数。 此外，该方法包括在第二操作状态下操作燃气涡轮发动机，以在第二操作状态下测量第二多个操作参数。 此外，该方法包括在第三操作状态下操作燃气涡轮发动机，以在第三操作状态下测量第三多个操作参数，其中第一，第二和第三操作状态彼此不同。 另外，该方法包括基于第一，第二和第三多个操作参数产生校正因子。 该方法还包括基于校正因子调整燃气涡轮发动机的运行。
-
公开(公告)号：US20210324757A1
公开(公告)日：2021-10-21
申请号：US17326801
申请日：2021-05-21
Applicant: General Electric Company
Inventor： Bradly Aaron Kippel , Raymond Pang , Scott Richard Baker , Harold Lamar Jordan, JR. , Rex Allen Morgan , Kamlesh Mundra
Abstract: The present disclosure is direct to a system for regulating a velocity of gases in a turbomachine. The system includes an exhaust section of the turbomachine. The system also includes a damper having an actuator and a restriction. The damper is positioned within the exhaust section and is operable to adjust the velocity of the gases based on a position of the restriction. The system further includes a controller communicatively coupled to the damper. The controller is configured to control the position of the restriction to regulate the velocity of the gases relative to a predetermined velocity range.
-
公开(公告)号：US20150007574A1
公开(公告)日：2015-01-08
申请号：US13937078
申请日：2013-07-08
Applicant: General Electric Company
IPC: F02C9/00
CPC classification number: F02C9/00 , F02C9/28 , F05D2260/80 , F05D2260/821 , F05D2270/11
Abstract: A system includes a gas turbine system including a compressor, a combustor, and a turbine. The system also includes a controller communicatively coupled to the gas turbine system and configured to control operations of the gas turbine system. The system further includes a life consumption model configured to determine an operating life of the gas turbine system based on both a health status of one or more components of the gas turbine system and operating conditions of the gas turbine system. The controller is configured to utilize at least the life consumption model to derive a control action for the gas turbine system.
Abstract translation: 一种系统包括包括压缩机，燃烧器和涡轮机的燃气轮机系统。 该系统还包括通信地耦合到燃气涡轮机系统并被配置为控制燃气轮机系统的操作的控制器。 该系统还包括寿命模型，其构造成基于燃气轮机系统的一个或多个部件的健康状况和燃气轮机系统的运行状况来确定燃气轮机系统的运行寿命。 控制器被配置为利用至少寿命模型来导出燃气轮机系统的控制动作。
-
公开(公告)号：US09476361B2
公开(公告)日：2016-10-25
申请号：US13937078
申请日：2013-07-08
Applicant: General Electric Company
CPC classification number: F02C9/00 , F02C9/28 , F05D2260/80 , F05D2260/821 , F05D2270/11
Abstract: A system includes a gas turbine system including a compressor, a combustor, and a turbine. The system also includes a controller communicatively coupled to the gas turbine system and configured to control operations of the gas turbine system. The system further includes a life consumption model configured to determine an operating life of the gas turbine system based on both a health status of one or more components of the gas turbine system and operating conditions of the gas turbine system. The controller is configured to utilize at least the life consumption model to derive a control action for the gas turbine system.
Abstract translation: 一种系统包括包括压缩机，燃烧器和涡轮机的燃气轮机系统。 该系统还包括通信地耦合到燃气涡轮机系统并被配置为控制燃气轮机系统的操作的控制器。 该系统还包括寿命模型，其构造成基于燃气轮机系统的一个或多个部件的健康状况和燃气轮机系统的运行状况来确定燃气轮机系统的运行寿命。 控制器被配置为利用至少寿命模型来导出燃气轮机系统的控制动作。
-
公开(公告)号：US09422869B2
公开(公告)日：2016-08-23
申请号：US13801259
申请日：2013-03-13
Applicant: General Electric Company
Inventor： Lewis Berkley Davis, Jr. , Rex Allen Morgan , Harold Lamar Jordan, Jr. , Scott Richard Baker
CPC classification number: F02C9/00 , F02C9/28 , F05D2270/0831 , F05D2270/20 , F05D2270/303 , F05D2270/44
Abstract: A method of tuning a gas turbine includes receiving a first plurality of operating parameters as the gas turbine engine is operated at a first operating state. Further, the method includes operating the gas turbine engine at a second operating state to measure a second plurality of operating parameters at the second operating state. In addition, the method includes operating the gas turbine engine at a third operating state to measure a third plurality of operating parameters at the third operating state, wherein the first, second, and third operating states are different from each other. Additionally, the method includes generating a correction factor based on the first, second, and third plurality of operating parameters. The method also includes adjusting the operation of the gas turbine engine based on the correction factor.
Abstract translation: 调节燃气轮机的方法包括当燃气涡轮发动机在第一操作状态下操作时接收第一多个操作参数。 此外，该方法包括在第二操作状态下操作燃气涡轮发动机，以在第二操作状态下测量第二多个操作参数。 此外，该方法包括在第三操作状态下操作燃气涡轮发动机，以在第三操作状态下测量第三多个操作参数，其中第一，第二和第三操作状态彼此不同。 另外，该方法包括基于第一，第二和第三多个操作参数产生校正因子。 该方法还包括基于校正因子调整燃气涡轮发动机的运行。
-
-
-
-
-
Search Results
6
records
(took 0.012 seconds)
