JPS5774522A - Combustion for gas turbine - Google Patents

Combustion for gas turbine

Info

Publication number
JPS5774522A
JPS5774522A JP15055480A JP15055480A JPS5774522A JP S5774522 A JPS5774522 A JP S5774522A JP 15055480 A JP15055480 A JP 15055480A JP 15055480 A JP15055480 A JP 15055480A JP S5774522 A JPS5774522 A JP S5774522A
Authority
JP
Japan
Prior art keywords
air
burning
gas
flow
controlled
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP15055480A
Other languages
Japanese (ja)
Inventor
Takashi Yamaguchi
Kokichi Uematsu
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
IHI Corp
Original Assignee
IHI Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by IHI Corp filed Critical IHI Corp
Priority to JP15055480A priority Critical patent/JPS5774522A/en
Publication of JPS5774522A publication Critical patent/JPS5774522A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE: To maintain a burning temperature at a value over a gas ignition point even at the lowest load and to enable even fuel gas of low calory to be burnt stably by a method werein a device which detects burning temperature, gas flow and controls an air quantity proportional to a load is provided on a combustor for a gas turbine.
CONSTITUTION: Burning air is divided at inlet E' into the air passing through a burning zone 16 and that passing through the outside part 18. The air flow passing through the burning zone 16 is controlled by adjusting the opening of an air flow regulating value 19 so that the ratio by weight of fuel gas to air can take a fixed value. The residual air passes through the outside part 18. By the control of the regulating value 19, the flow of the fuel gas is detected with FIC and the burning temperature is detected with TICA for the back-up, the air flow through the outside part 18 is controlled, as a result, the air flow of the burning zone 16 is controlled. The burning gas is mixed sufficiently with air, part of gas is burnt by a catalyst 20 at the inlet of a combustion chamber 17 and the residue is burnt completely by vapor phase reaction in the combustion chamber 17.
COPYRIGHT: (C)1982,JPO&Japio
JP15055480A 1980-10-27 1980-10-27 Combustion for gas turbine Pending JPS5774522A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP15055480A JPS5774522A (en) 1980-10-27 1980-10-27 Combustion for gas turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15055480A JPS5774522A (en) 1980-10-27 1980-10-27 Combustion for gas turbine

Publications (1)

Publication Number Publication Date
JPS5774522A true JPS5774522A (en) 1982-05-10

Family

ID=15499409

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15055480A Pending JPS5774522A (en) 1980-10-27 1980-10-27 Combustion for gas turbine

Country Status (1)

Country Link
JP (1) JPS5774522A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2013157218A (en) * 2012-01-30 2013-08-15 Mitsubishi Heavy Ind Ltd Starting method of solid oxide fuel cell
WO2019167276A1 (en) * 2018-03-02 2019-09-06 三菱日立パワーシステムズ株式会社 Fuel gas storage system for gas turbine and method for supplying fuel gas to gas turbine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2013157218A (en) * 2012-01-30 2013-08-15 Mitsubishi Heavy Ind Ltd Starting method of solid oxide fuel cell
WO2019167276A1 (en) * 2018-03-02 2019-09-06 三菱日立パワーシステムズ株式会社 Fuel gas storage system for gas turbine and method for supplying fuel gas to gas turbine

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