Turbine including flue gas recirculation combustor

US10590847B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10590847-B2
Application numberUS-201715812898-A
CountryUS
Kind codeB2
Filing dateNov 14, 2017
Priority dateDec 21, 2016
Publication dateMar 17, 2020
Grant dateMar 17, 2020

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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.

A flue gas recirculation combustor includes a combustor chamber configured such that fuel and combustion gas are injected therein to cause combustion and having a nozzle-side end and a combustor outlet, a nozzle can connected to the nozzle-side end of the combustor chamber, a plurality of nozzles disposed in the nozzle can and configured such that an injection direction thereof is directed to a side of the combustor chamber, and a sleeve disposed in a premixing space defined between the nozzle can and the nozzle-side end of the combustor chamber, the sleeve including a recirculation pathway to recirculate combustion air from the combustor chamber to the premixing space.

First claim

Opening claim text (preview).

What is claimed is: 1. A flue gas recirculation combustor comprising: a combustor chamber configured to receive fuel and combustion gas to cause combustion, the combustor chamber including a nozzle-side end and a combustor outlet; a nozzle can connected to the nozzle-side end of the combustor chamber; a plurality of nozzles disposed in the nozzle can and arranged such that an injection direction thereof is directed to a side of the combustor chamber; and a sleeve disposed in a premixing space defined between the nozzle can and the nozzle-side end of the combustor chamber, the sleeve including a recirculation pathway to recirculate combustion air from the combustor chamber to the premixing space, the recirculation pathway including a bypass path and an ejector nozzle, the ejector nozzle including a nozzle casing, an injection control needle assembly disposed in the nozzle casting, a combustor flow path connecting at least one point of the nozzle casting and the nozzle-side end of the combustor chamber, and a premix flow path connecting a side of the nozzle casting and the premixing space. 2. The flue gas recirculation combustor of claim 1 , wherein the plurality of nozzles is configured to premix and inject combustion air and fuel. 3. The flue gas recirculation combustor of claim 1 , wherein the recirculation pathway is provided on an inner surface of the sleeve along a circumferential direction. 4. The flue gas recirculation combustor of claim 1 , wherein the nozzle casing has a closed end, the nozzle casing including a narrowed portion provided at an open end of the nozzle casing to inject gases from the combustor chamber to the premixing space, and a partition longitudinally dividing the nozzle casing. 5. The flue gas recirculation combustor of claim 4 , wherein the injection control needle assembly includes a needle arranged longitudinally at a center of the nozzle casing, a movable member arranged at an end of the needle to move the needle horizontally along the center of the nozzle casing, a first elastic member arranged between the partition of the nozzle casing and the movable member, and a second elastic member provided between the movable member and the closed end of the nozzle casing. 6. The flue gas recirculation combustor of claim 5 , wherein the injection control needle assembly further includes an elasticity adjusting member arranged at the closed end of the nozzle casing to be connected to the second elastic member. 7. The flue gas recirculation combustor of claim 5 , wherein the injection control needle assembly further includes at least one ring stopper to limit horizontal movement of the movable member in the nozzle casing. 8. The flue gas recirculation combustor of claim 5 , wherein an inlet end of the combustor flow path is connected to the nozzle-side end of the combustor chamber and an outlet end of the combustor flow path is connected to a side of the nozzle casing, the outlet end including a combustor pressure path communicating with a space between the partition and the movable member, and a recirculation flow path communicating with an injection path in the nozzle casing. 9. The flue gas recirculation combustor of claim 5 , wherein an inlet end of the premix flow path is provided at a nozzle-side end of the sleeve and an outlet end of the premix flow path is provided at a side of the nozzle casing and in communication with a space between the movable member and the closed end of the nozzle casing. 10. A flue gas recirculation combustor comprising: a combustor chamber configured to receive fuel and combustion gas to cause combustion, the combustor chamber including a nozzle-side end and a combustor outlet; a nozzle can connected to the nozzle-side end of the combustor chamber; a plurality of nozzles disposed in the nozzle can and arranged such that an injection direction thereof is directed to a side of the combustor chamber; and a sleeve disposed in a premixing space defined between the nozzle can and the nozzle-side end of the combustor chamber, the sleeve including a plurality of bypass paths and at least one ejector nozzle, wherein the ejector nozzle is arranged between one bypass path and a neighboring bypass path, the plurality of bypass paths being arranged at a predetermined interval on an inner surface of the sleeve along a circumferential direction, and the ejector nozzle including a nozzle casting, an injection control needle assembly disposed in the nozzle casting, a combustor flow path connecting at least one point of the nozzle casting and the nozzle-side end of the combustor chamber, and a premix flow path connecting a side of the nozzle casting and the premixing space. 11. The flue gas recirculation combustor of claim 10 , wherein the nozzle casing has a cylindrical shape with a closed end, the nozzle casing including a narrowed portion provided at an open end of the nozzle casing to inject gases from the combustor chamber to the premixing space, and a partition longitudinally dividing the nozzle casing. 12. The flue gas recirculation combustor of claim 11 , wherein the injection control needle assembly includes a needle arranged longitudinally at a center of the nozzle casing, a movable member arranged at an end of the needle to move the needle horizontally along the center of the nozzle casing, a first elastic member arranged between the partition of the nozzle casing and the movable member, and a second elastic member provided between the movable member and the closed end of the nozzle casing. 13. The flue gas recirculation combustor of claim 12 , wherein the injection control needle assembly further includes an elasticity adjusting member arranged at the closed end of the nozzle casing to be connected to the second elastic member. 14. A flue gas recirculation combustor comprising: a combustor chamber configured to receive fuel and combustion gas to cause combustion, the combustor chamber including a nozzle-side end and a combustor outlet; a nozzle can connected to the nozzle-side end of the combustor chamber; a plurality of nozzles disposed in the nozzle can and arranged such that an injection direction thereof is directed to a side of the combustor chamber: and a sleeve disposed in a premixing space defined between the nozzle can and the nozzle-side end of the combustor chamber, the sleeve including one or more ejector nozzles, the one or more ejector nozzles including a nozzle casing, an injection control needle assembly disposed in the nozzle casing, a combustor flow path connecting at least one point of the nozzle casing and the nozzle-side end of the combustor chamber, and a premix flow path connecting a side of the nozzle casing and the premixing space, wherein an inlet end of the combustor flow path is connected to the nozzle-side end of the combustor chamber and an outlet end of the combustor flow path is connected to a side of the nozzle casing, the outlet end including a combustor pressure path communicating with a space between the partition and the movable member, and a recirculation flow path communicating with an injection path in the nozzle casing. 15. The flue gas recirculation combustor of claim 14 , wherein an inlet end of the premix flow path is provided at a nozzle-side end of the sleeve and an outlet end of the premix flow path is provided at a side of the nozzle casing and in communication with a space between the movable member and the closed end of the nozzle casing. 16. The flue gas recirculation combustor of claim 14 , wherein the one or more ejector nozzle

Assignees

Inventors

Classifications

  • Premixing fluegas with fuel and combustion air · CPC title

  • Combustion chambers comprising an annular arrangement of {several essentially tubular} flame tubes within a common annular casing or within individual casings · CPC title

  • Combustion apparatus characterised by arrangements for returning combustion products or flue gases to the combustion chamber (fluidised bed combustion apparatus with means for recirculation of particles entrained from the bed F23C10/02; fluidised bed combustion apparatus with devices for removal and partial reintroduction of material from the bed F23C10/26) · CPC title

  • Control of recirculation rate · CPC title

  • Combustors or associated equipment · CPC title

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What does patent US10590847B2 cover?
A flue gas recirculation combustor includes a combustor chamber configured such that fuel and combustion gas are injected therein to cause combustion and having a nozzle-side end and a combustor outlet, a nozzle can connected to the nozzle-side end of the combustor chamber, a plurality of nozzles disposed in the nozzle can and configured such that an injection direction thereof is directed to a…
Who is the assignee on this patent?
Doosan Heavy Ind & Construction Co Ltd, Doosan Heavy Ind Constr Co Ltd
What technology area does this patent fall under?
Primary CPC classification F23R3/286. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Mar 17 2020 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 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).