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1. 发明申请

US20090158746A1 Method of Regulation of the Temperature of Hot Gas of a Gas Turbine 有权
标题翻译：燃气轮机热气温度调节方法
公开(公告)号：US20090158746A1
公开(公告)日：2009-06-25
申请号：US12393276
申请日：2009-02-26
申请人： Joachim-Rene Nuding , Christoph Pels Leusden , Marco Tappen
发明人： Joachim-Rene Nuding , Christoph Pels Leusden , Marco Tappen
IPC分类号： F02C3/30
CPC分类号： F02C9/28 , F02C7/1435 , F05D2260/211 , F05D2270/0831 , F05D2270/303
摘要： The invention relates to a method of regulation of the temperature of a hot gas of a gas turbine, particularly of a stationary gas turbine used for generating electricity, which comprises injecting a liquid into an airflow, which can be drawn into a compressor and with the aid of which a fuel inside a combustion chamber, which is situated downstream, combusts while producing the hot gas that is subsequently expanded when flowing through the turbine part located downstream. A temperature measuring device is provided that measures the temperature of the airflow before the compressor, whereby the temperature of the hot gas is regulated by the quantity of fuel. The aim of the invention is to provide a regulation with which, during wet compression operation, the serviceable life of the components subjected to the action of hot gas is lengthened. To this end, the invention provides that the temperature measuring device is mounted before the injecting device, and that the temperature of the airflow is calculated at the entry of the compressor by using the measured temperature
摘要翻译：本发明涉及一种调节燃气轮机特别是用于发电的固定式燃气轮机的热气体的温度的方法，该方法包括将液体注入气流中，气流可以被吸入压缩机中，辅助其位于下游的燃烧室内的燃料燃烧，同时产生随后在流过位于下游的涡轮机部分时膨胀的热气体。提供了一种温度测量装置，其测量压缩机之前的气流的温度，由此燃烧气体的温度由燃料量调节。本发明的目的是提供一种调节方式，在湿式压缩操作期间，受热气体作用的部件的使用寿命延长。为此，本发明提供了在注射装置之前安装温度测量装置，并且通过使用测量的温度在压缩机入口处计算气流的温度

2. 发明授权

US08141369B2 Method of regulation of the temperature of hot gas of a gas turbine 有权
标题翻译：调节燃气轮机热气温度的方法
公开(公告)号：US08141369B2
公开(公告)日：2012-03-27
申请号：US12393276
申请日：2009-02-26
申请人： Joachim-Rene Nuding , Christoph Pels Leusden , Marco Tappen
发明人： Joachim-Rene Nuding , Christoph Pels Leusden , Marco Tappen
IPC分类号： F02C3/30
CPC分类号： F02C9/28 , F02C7/1435 , F05D2260/211 , F05D2270/0831 , F05D2270/303
摘要： The invention relates to a method of regulation of the temperature of a hot gas of a gas turbine, particularly of a stationary gas turbine used for generating electricity, which comprises injecting a liquid into an airflow, which can be drawn into a compressor and with the aid of which a fuel inside a combustion chamber, which is situated downstream, combusts while producing the hot gas that is subsequently expanded when flowing through the turbine part located downstream. A temperature measuring device is provided that measures the temperature of the airflow before the compressor, whereby the temperature of the hot gas is regulated by the quantity of fuel. The aim of the invention is to provide a regulation with which, during wet compression operation, the serviceable life of the components subjected to the action of hot gas is lengthened. To this end, the invention provides that the temperature measuring device is mounted before the injecting device, and that the temperature of the airflow is calculated at the entry of the compressor by using the measured temperature.
摘要翻译：本发明涉及一种调节燃气轮机特别是用于发电的固定式燃气轮机的热气体的温度的方法，该方法包括将液体注入气流中，气流可以被吸入压缩机中，辅助其位于下游的燃烧室内的燃料燃烧，同时产生随后在流过位于下游的涡轮机部分时膨胀的热气体。提供了一种温度测量装置，其测量压缩机之前的气流的温度，由此燃烧气体的温度由燃料量调节。本发明的目的是提供一种调节方式，在湿式压缩操作期间，受热气体作用的部件的使用寿命延长。为此，本发明提供了在喷射装置之前安装温度测量装置，并且通过使用测量的温度在压缩机入口处计算气流的温度。

3. 发明授权

US07513099B2 Temperature measuring device and regulation of the temperature of hot gas of a gas turbine 有权
标题翻译：温度测量装置和燃气轮机热气温度的调节
公开(公告)号：US07513099B2
公开(公告)日：2009-04-07
申请号：US10550972
申请日：2004-03-25
申请人： Joachim-Rene Nuding , Christoph Pels Leusden , Marco Tappen
发明人： Joachim-Rene Nuding , Christoph Pels Leusden , Marco Tappen
IPC分类号： F02C3/30 , F02C9/28
CPC分类号： F02C9/28 , F02C7/1435 , F05D2260/211 , F05D2270/0831 , F05D2270/303
摘要： The invention relates to a regulation of the temperature of a hot gas of a gas turbine, particularly of a stationary gas turbine used for generating electricity, which comprises an injecting device for injecting a liquid into an airflow, which can be drawn into a compressor and with the aid of which a fuel inside a combustion chamber, which is situated downstream, combusts while producing the hot gas that is subsequently expanded when flowing through the turbine part located downstream. A temperature measuring device is provided that measures the temperature of the airflow before the compressor, whereby the temperature of the hot gas is regulated by the quantity of fuel. The aim of the invention is to provide a regulation with which, during wet compression operation, the serviceable life of the components subjected to the action of hot gas is lengthened. To this end, the invention provides that the temperature measuring device is mounted before the injecting device, and that the temperature of the airflow is calculated at the entry of the compressor by using the measured temperature.
摘要翻译：本发明涉及燃气轮机特别是用于发电的固定燃气轮机的热气温度的调节，其包括用于将液体喷射到气流中的喷射装置，其可以被吸入压缩机和借助于此，位于下游的燃烧室内的燃料燃烧，同时产生随后在流过位于下游的涡轮机部分时膨胀的热气体。提供了一种温度测量装置，其测量压缩机之前的气流的温度，由此燃烧气体的温度由燃料量调节。本发明的目的是提供一种调节方式，在湿式压缩操作期间，受热气体作用的部件的使用寿命延长。为此，本发明提供了在喷射装置之前安装温度测量装置，并且通过使用测量的温度在压缩机入口处计算气流的温度。

4. 发明申请

US20060218930A1 Temperature measuring device and regulation of the temperature of hot gas of a gas turbine 有权
公开(公告)号：US20060218930A1
公开(公告)日：2006-10-05
申请号：US10550972
申请日：2004-03-25
申请人： Joachim-Rene Nuding , Christoph Leusden , Marco Tappen
发明人： Joachim-Rene Nuding , Christoph Leusden , Marco Tappen
IPC分类号： F02C3/30
CPC分类号： F02C9/28 , F02C7/1435 , F05D2260/211 , F05D2270/0831 , F05D2270/303
摘要： The invention relates to a regulation of the temperature of a hot gas of a gas turbine, particularly of a stationary gas turbine used for generating electricity, which comprises an injecting device for injecting a liquid into an airflow, which can be drawn into a compressor and with the aid of which a fuel inside a combustion chamber, which is situated downstream, combusts while producing the hot gas that is subsequently expanded when flowing through the turbine part located downstream. A temperature measuring device is provided that measures the temperature of the airflow before the compressor, whereby the temperature of the hot gas is regulated by the quantity of fuel. The aim of the invention is to provide a regulation with which, during wet compression operation, the serviceable life of the components subjected to the action of hot gas is lengthened. To this end, the invention provides that the temperature measuring device is mounted before the injecting device, and that the temperature of the airflow is calculated at the entry of the compressor by using the measured temperature.

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