ES372250A1 - Camara de combustion para turbina de gas. - Google Patents

Camara de combustion para turbina de gas.

Info

Publication number
ES372250A1
ES372250A1 ES372250A ES372250A ES372250A1 ES 372250 A1 ES372250 A1 ES 372250A1 ES 372250 A ES372250 A ES 372250A ES 372250 A ES372250 A ES 372250A ES 372250 A1 ES372250 A1 ES 372250A1
Authority
ES
Spain
Prior art keywords
air
admission
slots
combustion chamber
casing
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
ES372250A
Other languages
English (en)
Spanish (es)
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.)
Bennes Marrel SA
Original Assignee
Bennes Marrel SA
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 Bennes Marrel SA filed Critical Bennes Marrel SA
Publication of ES372250A1 publication Critical patent/ES372250A1/es
Expired 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
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/46Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • F23R3/48Flame tube interconnectors, e.g. cross-over tubes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22Fuel supply systems
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26Control of fuel supply
    • 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
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/54Reverse-flow combustion chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
  • Spray-Type Burners (AREA)
ES372250A 1968-10-18 1969-09-23 Camara de combustion para turbina de gas. Expired ES372250A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR69050513 1968-10-18

Publications (1)

Publication Number Publication Date
ES372250A1 true ES372250A1 (es) 1971-10-16

Family

ID=9695675

Family Applications (1)

Application Number Title Priority Date Filing Date
ES372250A Expired ES372250A1 (es) 1968-10-18 1969-09-23 Camara de combustion para turbina de gas.

Country Status (11)

Country Link
US (1) US3650106A (de)
AT (2) AT279483B (de)
BR (1) BR6913235D0 (de)
CA (1) CA917933A (de)
CH (1) CH531643A (de)
DE (3) DE1946905B2 (de)
ES (1) ES372250A1 (de)
FR (1) FR1592591A (de)
GB (1) GB1251749A (de)
NL (1) NL6915497A (de)
SE (1) SE356332B (de)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5089708A (de) * 1973-12-14 1975-07-18
CH586375A5 (de) * 1975-06-25 1977-03-31 Bbc Brown Boveri & Cie
JPS5242907U (de) * 1975-09-22 1977-03-26
US4129985A (en) * 1975-11-17 1978-12-19 Kawasaki Jukogyo Kabushiki Kaisha Combustor device of gas turbine engine
US4900246A (en) * 1977-05-25 1990-02-13 Phillips Petroleum Company Apparatus for burning nitrogen-containing fuels
GB2098720B (en) * 1979-01-12 1983-04-27 Gen Electric Stationary gas turbine combustor arrangements
US4393651A (en) * 1980-09-02 1983-07-19 Chandler Evans Inc. Fuel control method and apparatus
GB9108235D0 (en) * 1991-04-17 1991-06-05 Rolls Royce Plc A combustion chamber assembly
US5361577A (en) * 1991-07-15 1994-11-08 General Electric Company Spring loaded cross-fire tube
EP2157286A1 (de) * 2008-08-21 2010-02-24 Siemens Aktiengesellschaft Gasturbine mit angewinkeltem Mischgehäuse und Verfahren zur Turbinenanströmung
US20110091829A1 (en) * 2009-10-20 2011-04-21 Vinayak Barve Multi-fuel combustion system
US9388738B2 (en) * 2011-10-04 2016-07-12 Siemens Energy, Inc. Casing for a gas turbine engine
US9328925B2 (en) * 2012-11-15 2016-05-03 General Electric Company Cross-fire tube purging arrangement and method of purging a cross-fire tube
US20140137536A1 (en) * 2012-11-21 2014-05-22 General Electric Company Super telescoping cross-fire tube and method of assembling a combustor structure
US9353952B2 (en) * 2012-11-29 2016-05-31 General Electric Company Crossfire tube assembly with tube bias between adjacent combustors
JP2015135212A (ja) * 2014-01-17 2015-07-27 ヤンマー株式会社 ガスタービンエンジン
US10161635B2 (en) * 2014-06-13 2018-12-25 Rolls-Royce Corporation Combustor with spring-loaded crossover tubes
JP6325930B2 (ja) * 2014-07-24 2018-05-16 三菱日立パワーシステムズ株式会社 ガスタービン燃焼器
US10473117B2 (en) 2015-07-22 2019-11-12 United Technologies Corporation Diffuser case for a gas powered turbine

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2638745A (en) * 1943-04-01 1953-05-19 Power Jets Res & Dev Ltd Gas turbine combustor having tangential air inlets for primary and secondary air
US3172257A (en) * 1962-08-30 1965-03-09 Ingersoll Rand Co Hot gas power plant arrangement
GB998371A (en) * 1964-05-04 1965-07-14 Rolls Royce Ignition means for a continuous flow engine
CH434875A (de) * 1966-06-21 1967-04-30 Huber Robert Brennstoff-Einspritzventil mit elektromagnetischer Betätigung

Also Published As

Publication number Publication date
DE1966661A1 (de) 1973-07-12
AT301271B (de) 1972-07-15
US3650106A (en) 1972-03-21
FR1592591A (de) 1970-05-19
GB1251749A (de) 1971-10-27
NL6915497A (de) 1970-04-21
BR6913235D0 (pt) 1973-01-02
CA917933A (en) 1973-01-02
SE356332B (de) 1973-05-21
CH531643A (fr) 1972-12-15
DE1966660A1 (de) 1973-07-12
DE1946905A1 (de) 1970-05-06
DE1946905B2 (de) 1973-09-13
AT279483B (de) 1970-03-10

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