FR943200A - Improvements to combustion chambers for internal combustion turbines - Google Patents

Improvements to combustion chambers for internal combustion turbines

Info

Publication number
FR943200A
FR943200A FR943200DA FR943200A FR 943200 A FR943200 A FR 943200A FR 943200D A FR943200D A FR 943200DA FR 943200 A FR943200 A FR 943200A
Authority
FR
France
Prior art keywords
turbines
combustion
internal combustion
chambers
combustion chambers
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
Other languages
French (fr)
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.)
Metropolitan Vickers Electrical Co Ltd
Original Assignee
Metropolitan 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 Metropolitan Vickers Electrical Co Ltd filed Critical Metropolitan Vickers Electrical Co Ltd
Application granted granted Critical
Publication of FR943200A publication Critical patent/FR943200A/en
Expired legal-status Critical Current

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR943200D 1944-11-28 1946-08-28 Improvements to combustion chambers for internal combustion turbines Expired FR943200A (en)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
FR943200A true FR943200A (en) 1949-03-01

Family

ID=10240490

Family Applications (1)

Application Number Title Priority Date Filing Date
FR943200D Expired FR943200A (en) 1944-11-28 1946-08-28 Improvements to combustion chambers for internal combustion turbines

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 (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2628791A1 (en) * 1988-03-18 1989-09-22 Gen Electric FUEL DISPERSION BAR AND POSTCOMBUSTION CHAMBER COMPRISING SAME

Families Citing this family (16)

* 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
FR2471480A1 (en) * 1979-12-13 1981-06-19 Snecma INJECTION DEVICE FOR A COMBUSTION CHAMBER FOR 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
US4955201A (en) * 1987-12-14 1990-09-11 Sundstrand Corporation Fuel injectors for turbine engines
US4798048A (en) * 1987-12-21 1989-01-17 United Technologies Corporation Augmentor pilot
DE59208193D1 (en) * 1992-07-03 1997-04-17 Abb Research Ltd Afterburner
EP2501483B1 (en) * 2009-11-16 2015-08-19 Bell Helicopter Textron 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
EP3055536B1 (en) * 2013-10-07 2020-04-08 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 (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2628791A1 (en) * 1988-03-18 1989-09-22 Gen Electric FUEL DISPERSION BAR AND POSTCOMBUSTION CHAMBER COMPRISING SAME

Also Published As

Publication number Publication date
GB588847A (en) 1947-06-04
NL67338C (en)
CH262382A (en) 1949-06-30
BE468998A (en)

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