Power generation system and method for starting power generation system

US9638102B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9638102-B2
Application numberUS-201414260803-A
CountryUS
Kind codeB2
Filing dateApr 24, 2014
Priority dateApr 26, 2013
Publication dateMay 2, 2017
Grant dateMay 2, 2017

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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 gas turbine includes a compressor and a combustor; a SOFC having a cathode and an anode; a first compression air supply line supplying compression air to the combustor; a second compression air supply line supplying compression air to the cathode; an exhaust air supply line supplying exhaust air discharged from the cathode to the combustor; a first fuel gas supply line supplying a fuel gas to the combustor; a second fuel gas supply line supplying a fuel gas to the anode; a fuel gas supply ratio change unit capable of changing a supply ratio of the fuel gas supplied to the combustor and the fuel gas supplied to the anode; an exhaust fuel gas supply line supplying an exhaust fuel gas discharged from the anode to the combustor; and a controller performing open-close control of the control valves and according to an operation state of the SOFC.

First claim

Opening claim text (preview).

The invention claimed is: 1. A power generation system comprising: a gas turbine having a compressor and a combustor; a fuel cell having a cathode and an anode; a first compression oxidant supply line configured to supply a compression oxidant compressed in the compressor to the combustor; a second compression oxidant supply line configured to supply at least a part of the compression oxidant compressed in the compressor to the cathode; an exhaust oxidant supply line configured to supply an exhaust oxidant discharged from the cathode to the combustor; a first fuel gas supply line configured to supply a fuel gas to the combustor; a second fuel gas supply line configured to supply the fuel gas to the anode; a fuel gas supply ratio change unit capable of changing a supply ratio between the fuel gas supplied to the combustor and the fuel gas supplied to the anode; an exhaust fuel gas supply line configured to supply an exhaust fuel gas discharged from the anode to the combustor; and a control unit configured to control the fuel gas supply ratio change unit in accordance with a temperature of the fuel cell, wherein the fuel cell is provided with a power generation chamber temperature detector configured to detect a temperature of a power generation chamber of the fuel cell, and before the fuel cell completes start-up, the control unit performs control of decreasing a fuel gas flow rate supplied to the combustor by ΔL and of increasing a fuel gas flow rate supplied to the anode by ΔL by the fuel gas supply ratio change unit. 2. The power generation system according to claim 1 , further comprising: a steam supply line configured to supply steam to the anode; and a steam supply flow rate adjusting unit configured to adjust a supply flow rate of the steam supplied to the anode, wherein the steam supply flow rate adjusting unit increases the supply flow rate of the steam supplied to the anode, before the control of increasing the fuel gas flow rate supplied to the anode by ΔL is completed. 3. The power generation system according to claim 2 , further comprising an exhausted heat recovery boiler configured to generate steam from a flue gas from the gas turbine, wherein the steam supply line is connected to the exhausted heat recovery boiler at one end thereof, and connected to the anode at the other end thereof.

Assignees

Inventors

Classifications

  • using a compressor turbine assembly · CPC title

  • Cross-Sectional Technologies · mapped topic

  • Cross-Sectional Technologies · mapped topic

  • Heating fuel before feeding to the burner · CPC title

  • supplying working fluid to a user, e.g. a chemical process, which returns working fluid to a turbine of the plant · CPC title

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Frequently asked questions

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What does patent US9638102B2 cover?
A gas turbine includes a compressor and a combustor; a SOFC having a cathode and an anode; a first compression air supply line supplying compression air to the combustor; a second compression air supply line supplying compression air to the cathode; an exhaust air supply line supplying exhaust air discharged from the cathode to the combustor; a first fuel gas supply line supplying a fuel gas to…
Who is the assignee on this patent?
Mitsubishi Hitachi Power Sys
What technology area does this patent fall under?
Primary CPC classification F02C6/08. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue May 02 2017 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).