Patents by Inventor Thorsten Engler
Thorsten Engler has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).
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Patent number: 10774751Abstract: A gas turbine has a compressor providing compressed air, a combustion chamber provided with a burner, and an expansion turbine, wherein a bypass flow channel is also provided designed to supply compressed air past the burner and to supply a hot gas flow generated in the combustion chamber during operation of the gas turbine. The opening cross section of the bypass flow channel can be adjusted, and an adjustment unit is designed to adjust the opening cross section of the bypass flow channel such that the modification speed of the opening cross section is selected such that the relative combustion chamber pressure drop or a material temperature of the combustion chamber is substantially constant, in particular that the relative combustion chamber pressure drop or the material temperature of the combustion chamber does not vary by more than 10%.Type: GrantFiled: October 23, 2014Date of Patent: September 15, 2020Assignee: Siemens AktiengesellschaftInventors: Thorsten Engler, Manuel Gutermuth, Thomas Kerstiens, Matthias Kleinenhammann, Norbert Knüwer, Kai Süselbeck, Marc Tertilt, Ulrich Wagner, Frank Weidner
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Patent number: 10662881Abstract: A method for operating a gas turbine plant having a compressor and a turbine, where a limit value of a guide blade adjustment for the compressor of the gas turbine is identified depending on at least one drive shaft speed of the gas turbine plant. For the at least one drive shaft speed, a maximum allowable turbine entry temperature corresponding to the limit value of the guide vane adjustment for the compressor or a maximum allowable temperature for the turbine of the gas turbine, which is dependent on the turbine entry temperature, is identified. The gas turbine is operated in consideration of the identified maximum allowable turbine entry temperature or the identified maximum allowable temperature.Type: GrantFiled: February 5, 2015Date of Patent: May 26, 2020Assignee: Siemens AktiengesellschaftInventors: Rebecca Dierkes, Thorsten Engler, Markus Gorynski, Ansgar Sternemann
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Patent number: 10408135Abstract: A method for operating a gas turbine below the nominal power includes: determining a lower power threshold value of the gas turbine which causes the gas turbine to leave a CO-emission-compliant partial load range of the gas turbine; providing a specified threshold value for output gas turbine power, wherein the specified threshold value is less than the nominal power of the gas turbine; and operating the gas turbine at an output gas turbine power above the specified threshold value at a constant exhaust gas temperature, wherein the inlet guide blades of a compressor of the gas turbine are closed further in order to reduce the output gas turbine power. A sufficiently large valve is selected for the specified threshold value so that increases of the primary zone temperature, combustion temperature, and exhaust temperature extend over a CO-emission-compliant partial load range of the gas turbine that is as large as possible.Type: GrantFiled: February 12, 2014Date of Patent: September 10, 2019Assignee: Siemens AktiengesellschaftInventors: Thorsten Engler, Markus Gorynski, Manuel Gutermuth, Philipp Kreutzer, Marco Link, Nicolas Savilius, Kai Suselbeck, Marc Tertilt
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Patent number: 10036275Abstract: A method for testing an overspeed protection apparatus of a single-shaft system that includes: a) operating the system at nominal speed and under electrical load, wherein the load is selected to be low enough that, after dropping the load, the speed of the system rises such that the speed remains below steam turbine threshold speed lower than gas turbine threshold speed, such that first overspeed protection is triggered when the speed of the steam turbine reaches the steam turbine threshold speed, and second overspeed protection is triggered when the speed of the gas turbine reaches the gas turbine threshold speed; b) dropping the load; c) increasing the mass flow of the steam introduced into the steam turbine and/or of the fuel introduced into the gas turbine such that the speed of the steam turbine reaches the steam turbine threshold speed; d) testing whether the first overspeed protection is triggered.Type: GrantFiled: September 8, 2014Date of Patent: July 31, 2018Assignee: Siemens AktiengesellschaftInventors: Martin Ophey, Martin Bennauer, Thorsten Engler, Susanne Haas, Andreas Pahl, Marian-Peter Pieczyk, Martin Stapper, David Veltmann
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Patent number: 9915166Abstract: A gas turbine includes an intake tract and a compressor having a compressor flow channel. The compressor further includes an inlet guide vane row positioned in the compressor flow channel having inlet guide vanes that can be adjusted. The gas turbine has an icing sensor unit having at least one sensor arranged between a first compressor blade row and a first compressor guide vane row. The first compressor blade row is thereby arranged in the compressor flow channel directly downstream of the inlet guide vane row, and the first compressor guide vane row is arranged directly downstream of the first compressor blade row. A method detects an imminent icing of the compressor, and the compressor is safeguarded therefrom such that at least inlet guide vanes of the inlet guide vane row are adjusted such that the acceleration of an intake air mass flow is reduced.Type: GrantFiled: February 20, 2014Date of Patent: March 13, 2018Assignee: Siemens AktiengesellschaftInventors: Thorsten Engler, Markus Gorynski, Manuel Gutermuth, Philipp Kreutzer, Marco Link, Nicolas Savilius, Kai Suselbeck, Marc Tertilt
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Publication number: 20160348592Abstract: A method for operating a gas turbine plant having a compressor and a turbine, where a limit value of a guide blade adjustment for the compressor of the gas turbine is identified depending on at least one drive shaft speed of the gas turbine plant. For the at least one drive shaft speed, a maximum allowable turbine entry temperature corresponding to the limit value of the guide vane adjustment for the compressor or a maximum allowable temperature for the turbine of the gas turbine, which is dependent on the turbine entry temperature, is identified. The gas turbine is operated in consideration of the identified maximum allowable turbine entry temperature or the identified maximum allowable temperature.Type: ApplicationFiled: February 5, 2015Publication date: December 1, 2016Applicant: Siemens AktiengesellschaftInventors: Rebecca Dierkes, Thorsten Engler, Markus Gorynski, Ansgar Sternemann
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Publication number: 20160273457Abstract: A gas turbine has a compressor providing compressed air, a combustion chamber provided with a burner, and an expansion turbine, wherein a bypass flow channel is also provided designed to supply compressed air past the burner and to supply a hot gas flow generated in the combustion chamber during operation of the gas turbine. The opening cross section of the bypass flow channel can be adjusted, and an adjustment unit is designed to adjust the opening cross section of the bypass flow channel such that the modification speed of the opening cross section is selected such that the relative combustion chamber pressure drop or a material temperature of the combustion chamber is substantially constant, in particular that the relative combustion chamber pressure drop or the material temperature of the combustion chamber does not vary by more than 10%.Type: ApplicationFiled: October 23, 2014Publication date: September 22, 2016Applicant: Siemens AktiengesellschaftInventors: Thorsten Engler, Manuel Gutermuth, Thomas Kerstiens, Matthias Kleinenhammann, Norbert Knüwer, Kai Süselbeck, Marc Tertilt, Ulrich Wagner, Frank Weidner
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Publication number: 20160201501Abstract: A method for testing an overspeed protection apparatus of a single-shaft system that includes: a) operating the system at nominal speed and under electrical load, wherein the load is selected to be low enough that, after dropping the load, the speed of the system rises such that the speed remains below steam turbine threshold speed lower than gas turbine threshold speed, such that first overspeed protection is triggered when the speed of the steam turbine reaches the steam turbine threshold speed, and second overspeed protection is triggered when the speed of the gas turbine reaches the gas turbine threshold speed; b) dropping the load; c) increasing the mass flow of the steam introduced into the steam turbine and/or of the fuel introduced into the gas turbine such that the speed of the steam turbine reaches the steam turbine threshold speed; d) testing whether the first overspeed protection is triggered.Type: ApplicationFiled: September 8, 2014Publication date: July 14, 2016Applicant: Siemens AktiengesellschaftInventors: Martin Ophey, Martin Bennauer, Thorsten Engler, Susanne Haas, Andreas Pahl, Marian-Peter Pieczyk, Martin Stapper, David Veltmann
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Publication number: 20160024960Abstract: A gas turbine includes an intake tract and a compressor having a compressor flow channel. The compressor further includes an inlet guide vane row positioned in the compressor flow channel having inlet guide vanes that can be adjusted. The gas turbine has an icing sensor unit having at least one sensor arranged between a first compressor blade row and a first compressor guide vane row. The first compressor blade row is thereby arranged in the compressor flow channel directly downstream of the inlet guide vane row, and the first compressor guide vane row is arranged directly downstream of the first compressor blade row. A method detects an imminent icing of the compressor, and the compressor is safeguarded therefrom such that at least inlet guide vanes of the inlet guide vane row are adjusted such that the acceleration of an intake air mass flow is reduced.Type: ApplicationFiled: February 20, 2014Publication date: January 28, 2016Applicant: Siemens AktiengesellschaftInventors: Thorsten Engler, Markus Gorynski, Manuel Gutermuth, Philipp Kreutzer, Marco Link, Nicolas Savilius, Kai Suselbeck, Marc Tertilt
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Publication number: 20150369137Abstract: A method for operating a gas turbine below the nominal power includes: determining a lower power threshold value of the gas turbine which causes the gas turbine to leave a CO-emission-compliant partial load range of the gas turbine; providing a specified threshold value for output gas turbine power, wherein the specified threshold value is less than the nominal power of the gas turbine; and operating the gas turbine at an output gas turbine power above the specified threshold value at a constant exhaust gas temperature, wherein the inlet guide blades of a compressor of the gas turbine are closed further in order to reduce the output gas turbine power. A sufficiently large valve is selected for the specified threshold value so that increases of the primary zone temperature, combustion temperature, and exhaust temperature extend over a CO-emission-compliant partial load range of the gas turbine that is as large as possible.Type: ApplicationFiled: February 12, 2014Publication date: December 24, 2015Applicant: Siemens AktiengesellschaftInventors: Thorsten Engler, Markus Gorynski, Manuel Gutermuth, Philipp Kreutzer, Marco Link, Nicolas Savilius, Kai Suselbeck, Marc Tertilt