FR979409A - Combustion chamber, in particular for gas turbines - Google Patents

Combustion chamber, in particular for gas turbines

Info

Publication number
FR979409A
FR979409A FR979409DA FR979409A FR 979409 A FR979409 A FR 979409A FR 979409D A FR979409D A FR 979409DA FR 979409 A FR979409 A FR 979409A
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
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.)
Sulzer AG
Original Assignee
Sulzer AG
Gebrueder Sulzer AG
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 Sulzer AG, Gebrueder Sulzer AG filed Critical Sulzer AG
Application granted granted Critical
Publication of FR979409A publication Critical patent/FR979409A/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
    • F23R3/002—Wall structures
    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
FR979409D 1948-02-21 1949-01-24 Combustion chamber, in particular for gas turbines Expired FR979409A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH669751X 1948-02-21

Publications (1)

Publication Number Publication Date
FR979409A true FR979409A (en) 1951-04-26

Family

ID=4527580

Family Applications (1)

Application Number Title Priority Date Filing Date
FR979409D Expired FR979409A (en) 1948-02-21 1949-01-24 Combustion chamber, in particular for gas turbines

Country Status (5)

Country Link
CH (1) CH262073A (en)
DE (1) DE807571C (en)
FR (1) FR979409A (en)
GB (1) GB669751A (en)
NL (1) NL72931C (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1021208B (en) * 1954-02-23 1957-12-19 Gen Electric Lining for the additional burner of a jet engine for aircraft

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1064759B (en) * 1954-08-06 1959-09-03 Helmut Ph G A R Von Zborowski Burner for ramjet engines
DE1029196B (en) * 1955-10-01 1958-04-30 Messerschmitt Boelkow Blohm Annular combustion chamber for internal combustion turbines, especially aircraft internal combustion turbines
US3038309A (en) * 1959-07-21 1962-06-12 Gen Electric Cooling liner for jet engine afterburner
US4201047A (en) * 1976-06-10 1980-05-06 Morgan J Randolph Low emission combustors
US4898000A (en) * 1986-04-14 1990-02-06 Allied-Signal Inc. Emergency power unit
DE58907451D1 (en) * 1988-10-12 1994-05-19 Ruhrgas Ag Burners, especially high speed burners.
CA2141066A1 (en) * 1994-02-18 1995-08-19 Urs Benz Process for the cooling of an auto-ignition combustion chamber
GB2397643A (en) * 2002-12-04 2004-07-28 Alstom A combustion chamber burner including a corrugated burner outlet
KR102071168B1 (en) * 2016-05-23 2020-01-29 미츠비시 히타치 파워 시스템즈 가부시키가이샤 Combustor, gas turbine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1021208B (en) * 1954-02-23 1957-12-19 Gen Electric Lining for the additional burner of a jet engine for aircraft

Also Published As

Publication number Publication date
NL72931C (en)
CH262073A (en) 1949-06-15
GB669751A (en) 1952-04-09
DE807571C (en) 1951-07-02

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