FR1233390A - Combustion chamber, especially for gas turbines - Google Patents

Combustion chamber, especially for gas turbines

Info

Publication number
FR1233390A
FR1233390A FR803374A FR803374A FR1233390A FR 1233390 A FR1233390 A FR 1233390A FR 803374 A FR803374 A FR 803374A FR 803374 A FR803374 A FR 803374A FR 1233390 A FR1233390 A FR 1233390A
Authority
FR
France
Prior art keywords
combustion chamber
gas turbines
turbines
gas
combustion
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
FR803374A
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.)
Schweizerische Lokomotiv und Maschinenfabrik AG (SLM)
Original Assignee
Schweizerische Lokomotiv und Maschinenfabrik AG (SLM)
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 Schweizerische Lokomotiv und Maschinenfabrik AG (SLM) filed Critical Schweizerische Lokomotiv und Maschinenfabrik AG (SLM)
Application granted granted Critical
Publication of FR1233390A publication Critical patent/FR1233390A/en
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
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • 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
    • F23R3/60Support structures; Attaching or mounting means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Production Of Liquid Hydrocarbon Mixture For Refining Petroleum (AREA)
FR803374A 1958-08-26 1959-08-24 Combustion chamber, especially for gas turbines Expired FR1233390A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH6330158A CH362883A (en) 1958-08-26 1958-08-26 Combustion chamber, in particular for gas turbines

Publications (1)

Publication Number Publication Date
FR1233390A true FR1233390A (en) 1960-10-12

Family

ID=4524881

Family Applications (1)

Application Number Title Priority Date Filing Date
FR803374A Expired FR1233390A (en) 1958-08-26 1959-08-24 Combustion chamber, especially for gas turbines

Country Status (3)

Country Link
CH (1) CH362883A (en)
FR (1) FR1233390A (en)
GB (1) GB925633A (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5287511A (en) * 1976-01-17 1977-07-21 Koukuu Uchiyuu Gijiyutsu Kenki Gas turbine combustor
GB1595224A (en) * 1977-02-04 1981-08-12 Rolls Royce Combustion equipment for gas turbine engines
US6101814A (en) * 1999-04-15 2000-08-15 United Technologies Corporation Low emissions can combustor with dilution hole arrangement for a turbine engine

Also Published As

Publication number Publication date
CH362883A (en) 1962-06-30
GB925633A (en) 1963-05-08

Similar Documents

Publication Publication Date Title
FR1197035A (en) High temperature resistant combustion chamber
FR1227773A (en) Gas turbine engine fins
FR1187946A (en) Combustion chamber
CH457040A (en) Combustion chamber, especially for gas turbines
FR1388005A (en) Gas turbine combustion chamber
AT257279B (en) Combustion chamber for gas turbines
BE607939A (en) Combustion chamber for gas turbo-engine
FR1097536A (en) Combustion chamber for jet engines, gas turbines and the like
FR883358A (en) Combustion chamber, in particular for gas turbine installation
CH409525A (en) Combustion chamber for gas turbines
CH364144A (en) Combustion chamber for gas turbines
FR1233390A (en) Combustion chamber, especially for gas turbines
FR1144928A (en) Combustion chamber for gas turbine
FR1330443A (en) Combustion chamber for gas turbo-engine
CH411464A (en) Combustion chamber for gas turbines
FR1266445A (en) Combustion chamber for gas turbine
FR1259852A (en) Annular combustion chamber for gas turbines
FR1248897A (en) Combustion chamber for turbo-engine
FR1202390A (en) Annular combustion chamber for gas turbines
FR1094299A (en) Gas turbine combustion chamber
FR1160155A (en) Gas injector, especially for high pressure synthesis
FR1331728A (en) Combustion chamber for gas turbines
FR1299453A (en) Combustion chamber for gas turbo-engine
FR1289263A (en) Combustion chamber for gas turbo-engine
BE603908A (en) Combustion chamber for gas turbo-engine