Gas turbine power plant with exhaust gas recirculation

US9869246B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9869246-B2
Application numberUS-201414467648-A
CountryUS
Kind codeB2
Filing dateAug 25, 2014
Priority dateFeb 29, 2012
Publication dateJan 16, 2018
Grant dateJan 16, 2018

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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 method for operating a gas turbine power plant, and a gas turbine power plant in which fresh air is delivered to a compressor inlet and is accelerated in the compressor inlet and a recirculated first exhaust gas substream is delivered into a region of the compressor inlet in which the fresh air is accelerated to an extent such that the difference between total pressure and static pressure in the fresh air is greater than or equal to a pressure difference which is required in order to suck a target mass flow of the recirculated first exhaust gas substream into the compressor inlet.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method for operating a gas turbine power plant with exhaust gas recirculation, the gas turbine power plant including a gas turbine with a compressor having an inlet, a waste heat recovery steam generator, an exhaust gas divider, a recirculation line, and an exhaust gas recooler, said method comprising: delivering fresh air into the compressor inlet, the fresh air being accelerated in the compressor inlet; controlling the exhaust gas divider to divide exhaust gases from the gas turbine into (1) a first exhaust gas substream for recirculation into an intake stream of the gas turbine and (2) into a second exhaust gas substream for discharge from the gas turbine power plant; recirculating the first exhaust gas substream for delivery, separately from the fresh air, into the compressor inlet; delivering the recirculated first exhaust gas substream, separately from the fresh air, as far as a region of the compressor inlet in which the fresh air is accelerated to an extent such that a difference between total pressure and static pressure in the accelerated fresh air is greater than or equal to a pressure difference for sucking a target mass flow of the recirculated first exhaust gas substream into the compressor inlet; introducing the recirculated first exhaust gas substream to the accelerated fresh air via a plurality of delivery ducts arranged so as to be distributed circumferentially, upstream of the compressor, on a diameter of an intake duct and concentrically to a shaft of the gas turbine; and controlling a quantity of the recirculated first exhaust gas substream by changing an axial position of outlet orifices of the plurality of delivery ducts relative to the compressor inlet. 2. The method as claimed in claim 1 , comprising: conducting fresh air into a flow duct of the recirculated first exhaust gas substream via a control or regulating element when the gas turbine is under part load and/or is being started. 3. A gas turbine power plant, comprising: a gas turbine; a waste heat recovery steam generator; a compressor having a compressor inlet; an exhaust gas divider configured to, during operation, divide exhaust gases (1) into a first exhaust gas substream for recirculation into an intake stream of the gas turbine and (2) into a second exhaust gas substream for discharge from the gas turbine power plant; a plurality of ducts for introducing the recirculated first exhaust gas substream to fresh air delivered to the compressor inlet in the intake stream, the plurality of ducts being arranged so as to be distributed circumferentially, upstream of the compressor, on a diameter of an intake duct and concentrically to a shaft of the gas turbine, an axial distance from outlet orifices of the plurality of ducts to the compressor inlet being adjustable in order to regulate or control a quantity of the recirculated first exhaust gas substream, the outlet orifices being sufficiently close to the compressor that, when the gas turbine is in operation, a static pressure at the outlet orifices is sufficiently low that a difference between total pressure and static pressure of the intake stream is greater than or equal to a pressure difference which is required in order to suck a target mass flow of the recirculated first exhaust gas substream into the compressor intel; and a recirculation line for recirculating the first exhaust gas substream from the exhaust gas divider and connected to the plurality of ducts. 4. The gas turbine power plant as claimed in 3 , wherein the recirculation line is connected to an inlet for fresh air via a control or regulating element.

Assignees

Inventors

Classifications

  • Regulating means specially adapted therefor (F01K23/105, F01K23/108 take precedence) · CPC title

  • Air intakes for gas-turbine plants or jet-propulsion plants · CPC title

  • using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants (using waste heat as source of energy for refrigeration plants F25B27/02; using the waste heat of a gasturbine for steam generation or in a steam cycle see F01K23/10) · CPC title

  • making use of surplus or waste energy · CPC title

  • to optimize the performance of a machine · CPC title

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Frequently asked questions

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What does patent US9869246B2 cover?
A method for operating a gas turbine power plant, and a gas turbine power plant in which fresh air is delivered to a compressor inlet and is accelerated in the compressor inlet and a recirculated first exhaust gas substream is delivered into a region of the compressor inlet in which the fresh air is accelerated to an extent such that the difference between total pressure and static pressure in …
Who is the assignee on this patent?
Alstom Technology Ltd, Ansaldo Energia Switzerland AG
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 Jan 16 2018 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 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).