CA2901077C - Automated tuning of multiple fuel gas turbine combustion systems - Google Patents

Automated tuning of multiple fuel gas turbine combustion systems Download PDF

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Publication number
CA2901077C
CA2901077C CA2901077A CA2901077A CA2901077C CA 2901077 C CA2901077 C CA 2901077C CA 2901077 A CA2901077 A CA 2901077A CA 2901077 A CA2901077 A CA 2901077A CA 2901077 C CA2901077 C CA 2901077C
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CA
Canada
Prior art keywords
gas turbine
fuel gas
multiple fuel
turbine combustion
combustion systems
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CA2901077A
Other languages
French (fr)
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CA2901077A1 (en
Inventor
Christopher Chandler
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Gas Turbine Efficiency Sweden AB
Original Assignee
Gas Turbine Efficiency Sweden AB
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Gas Turbine Efficiency Sweden AB filed Critical Gas Turbine Efficiency Sweden AB
Priority claimed from PCT/US2013/026291 external-priority patent/WO2013126278A1/en
Priority claimed from US13/767,920 external-priority patent/US9354618B2/en
Publication of CA2901077A1 publication Critical patent/CA2901077A1/en
Application granted granted Critical
Publication of CA2901077C publication Critical patent/CA2901077C/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

Method for automated control of the gas turbine fuel composition through automated modification of the ratio of fuel gas from multiple sources The method includes providing first and second fuel sources, sensing the operational parameters of a turbine, determining whether the operational parameters are within preset operational limits and adjusting the ratio of the first fuel source to the second filet source, based on whether the operational parameters are within the preset operational limits.
CA2901077A 2013-02-15 2013-02-15 Automated tuning of multiple fuel gas turbine combustion systems Active CA2901077C (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/767,920 2013-02-15
PCT/US2013/026291 WO2013126278A1 (en) 2012-02-22 2013-02-15 Automated tuning of multiple fuel gas turbine combustion systems
US13/767,920 US9354618B2 (en) 2009-05-08 2013-02-15 Automated tuning of multiple fuel gas turbine combustion systems

Publications (2)

Publication Number Publication Date
CA2901077A1 CA2901077A1 (en) 2013-08-29
CA2901077C true CA2901077C (en) 2021-05-18

Family

ID=54010685

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2901077A Active CA2901077C (en) 2013-02-15 2013-02-15 Automated tuning of multiple fuel gas turbine combustion systems

Country Status (2)

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CA (1) CA2901077C (en)
MX (2) MX365197B (en)

Also Published As

Publication number Publication date
MX365197B (en) 2019-05-27
CA2901077A1 (en) 2013-08-29
MX2019001330A (en) 2019-07-08
MX2015010589A (en) 2017-06-20

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Effective date: 20180207