GB2091410B - Fuel nozzle for a gas turbine engine - Google Patents

Fuel nozzle for a gas turbine engine

Info

Publication number
GB2091410B
GB2091410B GB8136226A GB8136226A GB2091410B GB 2091410 B GB2091410 B GB 2091410B GB 8136226 A GB8136226 A GB 8136226A GB 8136226 A GB8136226 A GB 8136226A GB 2091410 B GB2091410 B GB 2091410B
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
fuel nozzle
nozzle
fuel
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.)
Expired
Application number
GB8136226A
Other versions
GB2091410A (en
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies 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
Priority claimed from US06/212,176 external-priority patent/US4418543A/en
Priority claimed from US06/212,175 external-priority patent/US4395874A/en
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of GB2091410A publication Critical patent/GB2091410A/en
Application granted granted Critical
Publication of GB2091410B publication Critical patent/GB2091410B/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/36—Details, e.g. burner cooling means, noise reduction means
    • F23D11/38—Nozzles; Cleaning devices therefor
GB8136226A 1980-12-02 1981-12-01 Fuel nozzle for a gas turbine engine Expired GB2091410B (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US06/212,176 US4418543A (en) 1980-12-02 1980-12-02 Fuel nozzle for gas turbine engine
US06/212,175 US4395874A (en) 1980-12-02 1980-12-02 Fuel nozzles with water injection for gas turbine engines

Publications (2)

Publication Number Publication Date
GB2091410A GB2091410A (en) 1982-07-28
GB2091410B true GB2091410B (en) 1984-08-22

Family

ID=26906850

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8136226A Expired GB2091410B (en) 1980-12-02 1981-12-01 Fuel nozzle for a gas turbine engine

Country Status (6)

Country Link
DE (1) DE3147564A1 (en)
FR (1) FR2495229B1 (en)
GB (1) GB2091410B (en)
IL (1) IL64422A (en)
IT (1) IT1139889B (en)
SE (1) SE456601B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3642122C1 (en) * 1986-12-10 1988-06-09 Mtu Muenchen Gmbh Fuel injector
DE19860785A1 (en) * 1998-12-30 2000-07-06 Abb Alstom Power Ch Ag Atomizer to atomize liquid fuel in combustion chamber of gas turbine, for example, has fluidic device with annular outer channel formed between outer and inner pipe and delivering fluid under pressure to interact with spray cone

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2965303A (en) * 1959-03-30 1960-12-20 United Aircraft Corp Coolant injection in a fuel nozzle
GB1114728A (en) * 1967-03-20 1968-05-22 Rolls Royce Burner e.g. for a gas turbine engine combustion chamber
DE2012941A1 (en) * 1969-04-01 1970-10-15 Parker-Hannifin Corp., Cleveland, Ohio (V.St.A.) Liquid fuel injector
US3684186A (en) * 1970-06-26 1972-08-15 Ex Cell O Corp Aerating fuel nozzle
GB1377184A (en) * 1971-02-02 1974-12-11 Secr Defence Gas turbine engine combustion apparatus
US3768250A (en) * 1971-12-01 1973-10-30 Mitsubishi Heavy Ind Ltd Combustion apparatus for a gas turbine
JPS5342897B2 (en) * 1972-11-09 1978-11-15
FR2206796A5 (en) * 1972-11-13 1974-06-07 Snecma
FR2249243B2 (en) * 1973-10-26 1978-09-15 Snecma
GB1421399A (en) * 1972-11-13 1976-01-14 Snecma Fuel injectors
US3866413A (en) * 1973-01-22 1975-02-18 Parker Hannifin Corp Air blast fuel atomizer
US3979069A (en) * 1974-10-11 1976-09-07 Luigi Garofalo Air-atomizing fuel nozzle
US4139157A (en) * 1976-09-02 1979-02-13 Parker-Hannifin Corporation Dual air-blast fuel nozzle
US4290558A (en) * 1979-09-18 1981-09-22 United Technologies Corporation Fuel nozzle with water injection

Also Published As

Publication number Publication date
FR2495229A1 (en) 1982-06-04
IT8125388A0 (en) 1981-12-02
DE3147564C2 (en) 1991-07-11
FR2495229B1 (en) 1987-07-03
GB2091410A (en) 1982-07-28
IL64422A (en) 1986-09-30
IT1139889B (en) 1986-09-24
DE3147564A1 (en) 1982-08-19
SE456601B (en) 1988-10-17
SE8107164L (en) 1982-06-03
IL64422A0 (en) 1982-03-31

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20001201