JPS57122223A - Method of air supply and its apparatus for gas turbine combustor - Google Patents

Method of air supply and its apparatus for gas turbine combustor

Info

Publication number
JPS57122223A
JPS57122223A JP630281A JP630281A JPS57122223A JP S57122223 A JPS57122223 A JP S57122223A JP 630281 A JP630281 A JP 630281A JP 630281 A JP630281 A JP 630281A JP S57122223 A JPS57122223 A JP S57122223A
Authority
JP
Japan
Prior art keywords
rate
air
decreased
time
rated load
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.)
Granted
Application number
JP630281A
Other languages
Japanese (ja)
Other versions
JPH0240935B2 (en
Inventor
Seiichi Kirikami
Ryoichiro Oshima
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.)
Hitachi Ltd
Original Assignee
Hitachi Ltd
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 Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP630281A priority Critical patent/JPS57122223A/en
Publication of JPS57122223A publication Critical patent/JPS57122223A/en
Publication of JPH0240935B2 publication Critical patent/JPH0240935B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/26Controlling the air flow

Abstract

PURPOSE:To lower the rate of exhausted product at the starting time for rated load, by increasing the excess rate of air at the time of rated load by feeding the air so that the equivalent ratio is made 1 at the starting time. CONSTITUTION:Ignition property is stabilized, complete combustion is performed, and the rate of generation of CO is decreased in a gas turbine combustor, by making the air fuel ratio in this area large by arranging the apparatus in the manner so that the equivalent ratio in the primary combustion area A is to be nearly 1 at the starting time. At the time of the rated load, the excess rate of air in the primary combustion area A is made large, so that the rate of reaction between oxygen and nitrogen in the air is decreased, as a result, the rate of generation of NOX is decreased. With the above-mentioned arrangement, the rate of exhausted matter from the combustor at the starting time and the time of rated load is decreased.
JP630281A 1981-01-21 1981-01-21 Method of air supply and its apparatus for gas turbine combustor Granted JPS57122223A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP630281A JPS57122223A (en) 1981-01-21 1981-01-21 Method of air supply and its apparatus for gas turbine combustor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP630281A JPS57122223A (en) 1981-01-21 1981-01-21 Method of air supply and its apparatus for gas turbine combustor

Publications (2)

Publication Number Publication Date
JPS57122223A true JPS57122223A (en) 1982-07-30
JPH0240935B2 JPH0240935B2 (en) 1990-09-13

Family

ID=11634574

Family Applications (1)

Application Number Title Priority Date Filing Date
JP630281A Granted JPS57122223A (en) 1981-01-21 1981-01-21 Method of air supply and its apparatus for gas turbine combustor

Country Status (1)

Country Link
JP (1) JPS57122223A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6196333A (en) * 1984-10-18 1986-05-15 Mitsubishi Heavy Ind Ltd Gas turbine combustor bypass valve controlling method
JP2004176582A (en) * 2002-11-26 2004-06-24 Mitsubishi Heavy Ind Ltd Gas turbine power plant, control method of the same, and gas turbine control device

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0356837U (en) * 1989-10-03 1991-05-31

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4026642Y1 (en) * 1964-06-29 1965-09-10
JPS5046806U (en) * 1973-08-31 1975-05-10
JPS5244313A (en) * 1975-10-03 1977-04-07 Nissan Motor Co Ltd Combustor used for a gas turbine
JPS5517095A (en) * 1978-06-29 1980-02-06 Gen Electric Combustion controller

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4026642Y1 (en) * 1964-06-29 1965-09-10
JPS5046806U (en) * 1973-08-31 1975-05-10
JPS5244313A (en) * 1975-10-03 1977-04-07 Nissan Motor Co Ltd Combustor used for a gas turbine
JPS5517095A (en) * 1978-06-29 1980-02-06 Gen Electric Combustion controller

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6196333A (en) * 1984-10-18 1986-05-15 Mitsubishi Heavy Ind Ltd Gas turbine combustor bypass valve controlling method
JPH0555769B2 (en) * 1984-10-18 1993-08-17 Mitsubishi Heavy Ind Ltd
JP2004176582A (en) * 2002-11-26 2004-06-24 Mitsubishi Heavy Ind Ltd Gas turbine power plant, control method of the same, and gas turbine control device

Also Published As

Publication number Publication date
JPH0240935B2 (en) 1990-09-13

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