Gas turbine and the method of controlling bleed air volume for gas turbine

US11333073B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11333073-B2
Application numberUS-201916686551-A
CountryUS
Kind codeB2
Filing dateNov 18, 2019
Priority dateNov 20, 2018
Publication dateMay 17, 2022
Grant dateMay 17, 2022

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

To prevent or reduce an oversensitive change in the degree of opening of a bleed valve regulating the flow volume of a cooling air used to heat a fuel. A gas turbine includes: a compressor compressing an air; a combustor burning a fuel mixed with the air compressed by the compressor; a turbine configured to be driven by a combustion gas generated by the combustor; a heat exchanger causing the fuel to be supplied to the combustor to be heated through a cooling air bled from the compressor to be supplied to the turbine; a bleed valve regulating the flow volume of the cooling air; a first sensor measuring a fuel state value; a second sensor measuring a cooling air state value; and a control computer controlling the degree of opening of the bleed valve. The control computer stores therein data on reference values and dead bands including the corresponding reference value set for each of the fuel state value and the cooling air state value, and, when a measured value of at least one of the fuel state value and the cooling air state value has changed so much away from the corresponding reference value as to fall outside the corresponding dead band, controls the bleed valve such that the changed measured value is brought close to the corresponding reference value.

First claim

Opening claim text (preview).

What is claimed is: 1. A gas turbine comprising: a compressor configured to compress an air; a combustor configured to burn a fuel mixed with the air compressed by the compressor to generate a combustion gas; a turbine configured to be driven by the combustion gas generated by the combustor; a heat exchanger configured to cause the fuel to be supplied to the combustor to be heated through a cooling air bled from the compressor to be supplied to the turbine; a bleed valve configured to regulate a flow volume of the cooling air; a first sensor configured to measure a state value related to the fuel; a second sensor configured to measure a state value related to the cooling air; and a control computer configured to control a degree of opening of the bleed valve, wherein the control computer stores therein reference values and dead bands that are set for each of measured state values of the first sensor and the second sensor, and, when at least one of a measured state value measured by the first sensor and a measured state value measured by the second sensor has changed so much away from the corresponding reference value as to fall outside of the corresponding dead band, controls the bleed valve such that the changed measured state value is brought within the corresponding dead band, the state value related to the cooling air includes a cooling air temperature, and the control computer is configured to increase the degree of opening of the bleed valve to increase the cooling air flow volume in the case where the cooling air temperature has decreased to fall outside of the corresponding dead band.

Assignees

Inventors

Classifications

  • characterized by the cooling medium · CPC title

  • to improve fuel economy · CPC title

  • F02C7/224Primary

    Heating fuel before feeding to the burner · CPC title

  • F02C7/18Primary

    the medium being gaseous, e.g. air {(F02C7/125 takes precedence)} · CPC title

  • Temperature · CPC title

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Frequently asked questions

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What does patent US11333073B2 cover?
To prevent or reduce an oversensitive change in the degree of opening of a bleed valve regulating the flow volume of a cooling air used to heat a fuel. A gas turbine includes: a compressor compressing an air; a combustor burning a fuel mixed with the air compressed by the compressor; a turbine configured to be driven by a combustion gas generated by the combustor; a heat exchanger causing the f…
Who is the assignee on this patent?
Mitsubishi Hitachi Power Sys Ltd, Mitsubishi Power Ltd
What technology area does this patent fall under?
Primary CPC classification F02C7/224. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue May 17 2022 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 4 related publications on this page (citations in our corpus or others sharing the same primary CPC).