CH262382A - Combustion turbine plant. - Google Patents

Combustion turbine plant.

Info

Publication number
CH262382A
CH262382A CH262382DA CH262382A CH 262382 A CH262382 A CH 262382A CH 262382D A CH262382D A CH 262382DA CH 262382 A CH262382 A CH 262382A
Authority
CH
Switzerland
Prior art keywords
turbine plant
combustion turbine
combustion
plant
turbine
Prior art date
Application number
Other languages
German (de)
Inventor
Limited Metropolitan-V Company
Original Assignee
Vickers Electrical Co 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 Vickers Electrical Co Ltd filed Critical Vickers Electrical Co Ltd
Publication of CH262382A publication Critical patent/CH262382A/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
CH262382D 1944-11-28 1946-09-05 Combustion turbine plant. CH262382A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB262382X 1944-11-28

Publications (1)

Publication Number Publication Date
CH262382A true CH262382A (en) 1949-06-30

Family

ID=10240490

Family Applications (1)

Application Number Title Priority Date Filing Date
CH262382D CH262382A (en) 1944-11-28 1946-09-05 Combustion turbine plant.

Country Status (5)

Country Link
BE (1) BE468998A (en)
CH (1) CH262382A (en)
FR (1) FR943200A (en)
GB (1) GB588847A (en)
NL (1) NL67338C (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0030880B1 (en) * 1979-12-13 1983-08-31 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Injection device for the combustion chamber of a turbine engine
CH666340A5 (en) * 1985-05-29 1988-07-15 Bbc Brown Boveri & Cie Gas turbine combustion chamber - has fuel lines to burner nozzles extending through secondary air duct and contained in tubes connected to atmosphere
EP0350503A1 (en) * 1987-12-14 1990-01-17 Sundstrand Corp Fuel injectors for turbine engines.
EP0577862A1 (en) * 1992-07-03 1994-01-12 Abb Research Ltd. Afterburner

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2648950A (en) * 1949-08-24 1953-08-18 Westinghouse Electric Corp Gas turbine engine apparatus designed to burn wet pulverized fuel
US3003316A (en) * 1953-02-10 1961-10-10 Rolls Royce Cooling means for forked exhaust ducts of gas turbine engines
US2861424A (en) * 1954-04-09 1958-11-25 Douglas Aircraft Co Inc Fuel supply means for combustion apparatus
US2944388A (en) * 1955-02-24 1960-07-12 Thompson Ramo Wooldridge Inc Air atomizing spray bar
US2942414A (en) * 1956-07-03 1960-06-28 Thompson Ramo Wooldridge Inc Umbrella spraybar afterburner arrangement
BE795529A (en) * 1972-02-17 1973-06-18 Gen Electric IGNITER MOUNTED ON A TURBOREACTOR THRUST INCREASING DEVICE AND AIR COOLED
US4070826A (en) * 1975-12-24 1978-01-31 General Electric Company Low pressure fuel injection system
US4798048A (en) * 1987-12-21 1989-01-17 United Technologies Corporation Augmentor pilot
US4887425A (en) * 1988-03-18 1989-12-19 General Electric Company Fuel spraybar
US8869941B2 (en) * 2009-11-16 2014-10-28 Textron Innovations Inc. Dual-path fluid injection jet
US9638422B2 (en) * 2012-06-22 2017-05-02 Delavan Inc. Active purge mechanism with backflow preventer for gas turbine fuel injectors
WO2015054136A1 (en) 2013-10-07 2015-04-16 United Technologies Corporation Air cooled fuel injector for a turbine engine
EP3109550B1 (en) * 2015-06-19 2019-09-04 Rolls-Royce Corporation Turbine cooled cooling air flowing through a tubular arrangement

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0030880B1 (en) * 1979-12-13 1983-08-31 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Injection device for the combustion chamber of a turbine engine
CH666340A5 (en) * 1985-05-29 1988-07-15 Bbc Brown Boveri & Cie Gas turbine combustion chamber - has fuel lines to burner nozzles extending through secondary air duct and contained in tubes connected to atmosphere
EP0350503A1 (en) * 1987-12-14 1990-01-17 Sundstrand Corp Fuel injectors for turbine engines.
EP0350503A4 (en) * 1987-12-14 1990-05-14 Sundstrand Corp Fuel injectors for turbine engines.
EP0577862A1 (en) * 1992-07-03 1994-01-12 Abb Research Ltd. Afterburner
US5431018A (en) * 1992-07-03 1995-07-11 Abb Research Ltd. Secondary burner having a through-flow helmholtz resonator

Also Published As

Publication number Publication date
NL67338C (en)
GB588847A (en) 1947-06-04
FR943200A (en) 1949-03-01
BE468998A (en)

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