CH364144A - Combustion chamber for gas turbines - Google Patents

Combustion chamber for gas turbines

Info

Publication number
CH364144A
CH364144A CH6202158A CH6202158A CH364144A CH 364144 A CH364144 A CH 364144A CH 6202158 A CH6202158 A CH 6202158A CH 6202158 A CH6202158 A CH 6202158A CH 364144 A CH364144 A CH 364144A
Authority
CH
Switzerland
Prior art keywords
combustion chamber
gas turbines
turbines
gas
combustion
Prior art date
Application number
CH6202158A
Other languages
German (de)
Inventor
Jackson Pierce Lowell
Albert Benson John
Vernon Jaramillo Edward
Original Assignee
Gen Electric
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
Priority to US542809A priority Critical patent/US2973624A/en
Priority to GB1272058A priority patent/GB845971A/en
Priority to DEG24415A priority patent/DE1107455B/en
Priority to FR1195188D priority patent/FR1195188A/en
Application filed by Gen Electric filed Critical Gen Electric
Priority to CH6202158A priority patent/CH364144A/en
Priority to BE586496A priority patent/BE586496Q/en
Publication of CH364144A publication Critical patent/CH364144A/en

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)
CH6202158A 1955-10-26 1958-07-21 Combustion chamber for gas turbines CH364144A (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
US542809A US2973624A (en) 1955-10-26 1955-10-26 Cowled dome liners
GB1272058A GB845971A (en) 1958-07-21 1958-04-22 Improvements relating to combustion chambers for gas turbine engines
DEG24415A DE1107455B (en) 1958-04-28 1958-04-28 Combustion chamber for a gas turbine engine
FR1195188D FR1195188A (en) 1958-07-21 1958-04-30 Internal combustion chamber sleeve for gas turbine engines
CH6202158A CH364144A (en) 1958-07-21 1958-07-21 Combustion chamber for gas turbines
BE586496A BE586496Q (en) 1958-07-21 1960-01-13 Internal combustion chamber sleeve for gas turbine engines

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
CH364144A true CH364144A (en) 1962-08-31

Family

ID=4524033

Family Applications (1)

Application Number Title Priority Date Filing Date
CH6202158A CH364144A (en) 1955-10-26 1958-07-21 Combustion chamber for gas turbines

Country Status (4)

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

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL257968A (en) * 1959-11-20
GB943250A (en) * 1962-02-01 1963-12-04 Rolls Royce Improvements in or relating to gas turbine combustion chambers
GB2034874A (en) * 1978-11-03 1980-06-11 Gen Electric Gas turbine engine combustor
EP0035869B1 (en) * 1980-03-05 1984-07-11 Hitachi, Ltd. A gas turbine combustor
GB2125950B (en) * 1982-08-16 1986-09-24 Gen Electric Gas turbine combustor
FR2599821B1 (en) * 1986-06-04 1988-09-02 Snecma COMBUSTION CHAMBER FOR TURBOMACHINES WITH MIXING HOLES PROVIDING THE POSITIONING OF THE HOT WALL ON THE COLD WALL
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

Also Published As

Publication number Publication date
GB845971A (en) 1960-08-24
BE586496Q (en) 1960-05-03
FR1195188A (en) 1959-11-16

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