FR1195188A - Internal combustion chamber sleeve for gas turbine engines - Google Patents

Internal combustion chamber sleeve for gas turbine engines

Info

Publication number
FR1195188A
FR1195188A FR1195188DA FR1195188A FR 1195188 A FR1195188 A FR 1195188A FR 1195188D A FR1195188D A FR 1195188DA FR 1195188 A FR1195188 A FR 1195188A
Authority
FR
France
Prior art keywords
internal combustion
combustion chamber
gas turbine
turbine engines
chamber sleeve
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of FR1195188A publication Critical patent/FR1195188A/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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/06—Arrangement of apertures along the flame tube
    • F23R3/08—Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • F23R3/48—Flame tube interconnectors, e.g. cross-over tubes

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)
FR1195188D 1958-07-21 1958-04-30 Internal combustion chamber sleeve for gas turbine engines Expired FR1195188A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH6202158A CH364144A (en) 1958-07-21 1958-07-21 Combustion chamber for gas turbines

Publications (1)

Publication Number Publication Date
FR1195188A true FR1195188A (en) 1959-11-16

Family

ID=4524033

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1195188D Expired FR1195188A (en) 1958-07-21 1958-04-30 Internal combustion chamber sleeve for gas turbine engines

Country Status (4)

Country Link
BE (1) BE586496Q (en)
CH (1) CH364144A (en)
FR (1) FR1195188A (en)
GB (1) GB845971A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1155940B (en) * 1959-11-20 1963-10-17 Rolls Royce Combustion device for gas turbine engines
FR2440524A1 (en) * 1978-11-03 1980-05-30 Gen Electric COMBUSTION CHAMBER REDUCING GAS EMISSIONS
EP0248731A1 (en) * 1986-06-04 1987-12-09 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Gas turbine combustion chamber having mixing orifices which assure the positioning of a hot wall on a cool wall

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB943250A (en) * 1962-02-01 1963-12-04 Rolls Royce Improvements in or relating to gas turbine combustion chambers
DE3164647D1 (en) * 1980-03-05 1984-08-16 Hitachi Ltd A gas turbine combustor
GB2125950B (en) * 1982-08-16 1986-09-24 Gen Electric Gas turbine combustor
GB2221979B (en) * 1988-08-17 1992-03-25 Rolls Royce Plc A combustion chamber for a gas turbine engine
DE4444961A1 (en) * 1994-12-16 1996-06-20 Mtu Muenchen Gmbh Device for cooling in particular the rear wall of the flame tube of a combustion chamber for gas turbine engines

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1155940B (en) * 1959-11-20 1963-10-17 Rolls Royce Combustion device for gas turbine engines
FR2440524A1 (en) * 1978-11-03 1980-05-30 Gen Electric COMBUSTION CHAMBER REDUCING GAS EMISSIONS
EP0248731A1 (en) * 1986-06-04 1987-12-09 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Gas turbine combustion chamber having mixing orifices which assure the positioning of a hot wall on a cool wall
FR2599821A1 (en) * 1986-06-04 1987-12-11 Snecma COMBUSTION CHAMBER FOR TURBOMACHINES WITH MIXING ORIFICES ENSURING THE POSITIONING OF THE HOT WALL ON THE COLD WALL

Also Published As

Publication number Publication date
GB845971A (en) 1960-08-24
CH364144A (en) 1962-08-31
BE586496Q (en) 1960-05-03

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