Method and apparatus for detecting combustion conditions in combustors of a sequential combustion gas turbine engine

US9429079B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9429079-B2
Application numberUS-201213647566-A
CountryUS
Kind codeB2
Filing dateOct 9, 2012
Priority dateOct 14, 2011
Publication dateAug 30, 2016
Grant dateAug 30, 2016

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  1. Title

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  2. Abstract

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  5. First independent claim

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Abstract

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In a method for operating a gas turbine ( 10 ), a CO2-containing gas is compressed in a compressor ( 13 ), the compressed gas is used to burn a fuel in at least one subsequent combustion chamber ( 14, 18 ), and the hot combustion gases are used to drive at least one turbine ( 17, 21 ). Improved control and performance can be achieved by measuring the species concentration of the gas mixture flowing through the gas turbine ( 10 ) at several points within the gas turbine ( 10 ) by a distributed plurality of species concentration sensors ( 22; 22 a - 1; 23 ), and utilizing the measured concentration values to control the gas turbine ( 10 ) and/or optimize the combustion performance of the gas turbine ( 10 ).

First claim

Opening claim text (preview).

We claim: 1. A method for operating a gas turbine, in which turbine a CO 2 -containing gas is compressed in a compressor, the compressed gas being used to burn a fuel in a first combustor having first burners to form hot combustion gas that is fed to a first turbine to drive the first turbine, the gas turbine also comprising a second combustor having second burners downstream of the first turbine that forms hot combustion gas that is fed to a second turbine to drive the second turb…

Assignees

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Classifications

  • Mechanical Engineering · mapped topic

  • Mechanical Engineering · mapped topic

  • Mechanical Engineering · mapped topic

  • Mechanical Engineering · mapped topic

  • F02C3/34Primary

    Mechanical Engineering · mapped topic

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What does patent US9429079B2 cover?
In a method for operating a gas turbine ( 10 ), a CO2-containing gas is compressed in a compressor ( 13 ), the compressed gas is used to burn a fuel in at least one subsequent combustion chamber ( 14, 18 ), and the hot combustion gases are used to drive at least one turbine ( 17, 21 ). Improved control and performance can be achieved by measuring the species concentration of the gas mixture flo…
Who is the assignee on this patent?
Alstom Technology Ltd, General Electric Technology Gmbh
What technology area does this patent fall under?
Primary CPC classification F02C3/34. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Aug 30 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).