JPS52115911A - Method of reducing nox produced in gas turbine operation - Google Patents

Method of reducing nox produced in gas turbine operation

Info

Publication number
JPS52115911A
JPS52115911A JP2371977A JP2371977A JPS52115911A JP S52115911 A JPS52115911 A JP S52115911A JP 2371977 A JP2371977 A JP 2371977A JP 2371977 A JP2371977 A JP 2371977A JP S52115911 A JPS52115911 A JP S52115911A
Authority
JP
Japan
Prior art keywords
gas turbine
reducing nox
turbine operation
nox produced
produced
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
JP2371977A
Other languages
Japanese (ja)
Inventor
Shiyoo Henrii
Sukotsupu Arubuin
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.)
ExxonMobil Technology and Engineering Co
Original Assignee
Exxon Research and Engineering Co
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 Exxon Research and Engineering Co filed Critical Exxon Research and Engineering Co
Publication of JPS52115911A publication Critical patent/JPS52115911A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23CMETHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C13/00Apparatus in which combustion takes place in the presence of catalytic material
    • 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
    • F23R3/40Continuous combustion chambers using liquid or gaseous fuel characterised by the use of catalytic means
JP2371977A 1976-03-08 1977-03-04 Method of reducing nox produced in gas turbine operation Pending JPS52115911A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US66462176A 1976-03-08 1976-03-08

Publications (1)

Publication Number Publication Date
JPS52115911A true JPS52115911A (en) 1977-09-28

Family

ID=24666739

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2371977A Pending JPS52115911A (en) 1976-03-08 1977-03-04 Method of reducing nox produced in gas turbine operation

Country Status (7)

Country Link
JP (1) JPS52115911A (en)
CA (1) CA1070963A (en)
DE (1) DE2708940A1 (en)
FR (1) FR2353708A1 (en)
GB (1) GB1578665A (en)
IT (1) IT1075813B (en)
NL (1) NL7702494A (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0009523B1 (en) * 1978-10-02 1983-05-18 Exxon Research And Engineering Company A method of at least partially burning a hydrocarbon and/or carbonaceous fuel
US4375949A (en) 1978-10-03 1983-03-08 Exxon Research And Engineering Co. Method of at least partially burning a hydrocarbon and/or carbonaceous fuel
DE2908427C2 (en) * 1979-03-05 1983-04-14 L. & C. Steinmüller GmbH, 5270 Gummersbach Method for reducing NO ↓ X ↓ emissions from the combustion of nitrogenous fuels
DE3020145A1 (en) * 1980-05-28 1981-12-10 L. & C. Steinmüller GmbH, 5270 Gummersbach METHOD FOR CLEANING REACTION PRODUCTS
DE3447147A1 (en) * 1984-12-22 1986-06-26 Christian Dr.-Ing. 8570 Pegnitz Koch METHOD AND DEVICE FOR NITROGEN-FREE STEAM GENERATION WITH FOSSILE FUELS
DE3636024A1 (en) * 1986-10-23 1988-05-05 Rheinische Braunkohlenw Ag POWER PLANT PROCESS WITH A GAS TURBINE
GB8807859D0 (en) * 1988-04-05 1988-05-05 Nordsea Gas Technology Ltd Combination burners
DE10062253A1 (en) * 2000-12-14 2002-06-20 Rolls Royce Deutschland Gas turbine for aircraft has mesh of heat-resistant material, e.g. ceramic, in its combustion chamber
US10352571B2 (en) * 2016-01-15 2019-07-16 General Electric Company Catalytic ignition system

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE768049C (en) * 1940-12-20 1955-06-02 Messerschmitt Boelkow Blohm Gas turbine combustion chamber for constant pressure combustion with combustion muffle
US2632299A (en) * 1949-06-17 1953-03-24 United Aircraft Corp Precombustion chamber
JPS5626761B2 (en) * 1971-12-17 1981-06-20

Also Published As

Publication number Publication date
FR2353708A1 (en) 1977-12-30
CA1070963A (en) 1980-02-05
DE2708940A1 (en) 1977-09-15
IT1075813B (en) 1985-04-22
NL7702494A (en) 1977-09-12
GB1578665A (en) 1980-11-05

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