GB1309180A - Cooling of gas turbine engine combustion chambers - Google Patents

Cooling of gas turbine engine combustion chambers

Info

Publication number
GB1309180A
GB1309180A GB4010371A GB4010371A GB1309180A GB 1309180 A GB1309180 A GB 1309180A GB 4010371 A GB4010371 A GB 4010371A GB 4010371 A GB4010371 A GB 4010371A GB 1309180 A GB1309180 A GB 1309180A
Authority
GB
United Kingdom
Prior art keywords
dimension
turbine engine
gas turbine
engine combustion
combustion chamber
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
GB4010371A
Other languages
English (en)
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.)
Brown Boveri Sulzer Turbomaschinen AG
Original Assignee
Brown Boveri Sulzer Turbomaschinen 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 Brown Boveri Sulzer Turbomaschinen AG filed Critical Brown Boveri Sulzer Turbomaschinen AG
Publication of GB1309180A publication Critical patent/GB1309180A/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

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)
  • Gas Burners (AREA)
  • Air Supply (AREA)
GB4010371A 1970-10-01 1971-08-26 Cooling of gas turbine engine combustion chambers Expired GB1309180A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH1454770A CH529916A (de) 1970-10-01 1970-10-01 Brennkammer für eine Gasturbinenanlage

Publications (1)

Publication Number Publication Date
GB1309180A true GB1309180A (en) 1973-03-07

Family

ID=4401724

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4010371A Expired GB1309180A (en) 1970-10-01 1971-08-26 Cooling of gas turbine engine combustion chambers

Country Status (7)

Country Link
JP (1) JPS5132163B1 (enExample)
BE (1) BE773194A (enExample)
CA (1) CA958550A (enExample)
CH (1) CH529916A (enExample)
DE (1) DE2054002C3 (enExample)
FR (1) FR2112220B3 (enExample)
GB (1) GB1309180A (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4723413A (en) * 1985-11-19 1988-02-09 MTU Munuch, GmbH Reverse flow combustion chamber, especially reverse flow ring combustion chamber, for gas turbine propulsion units, with at least one flame tube wall film-cooling arrangement

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA980584A (en) * 1972-11-10 1975-12-30 Edward E. Ekstedt Double walled impingement cooled combustor
US3845620A (en) * 1973-02-12 1974-11-05 Gen Electric Cooling film promoter for combustion chambers
US3995422A (en) * 1975-05-21 1976-12-07 General Electric Company Combustor liner structure
FR2426157B1 (fr) * 1978-05-20 1985-07-26 Rolls Royce Chambre de combustion de moteur a turbine a gaz a prise annulaire d'air refrigerant
FR2450349A1 (fr) * 1979-03-01 1980-09-26 Snecma Perfectionnement au refroidissement des parois de chambres de combustion par pellicule d'air
FR2490728A1 (fr) * 1980-09-25 1982-03-26 Snecma Dispositif de refroidissement par film d'air pour tube a flamme de moteur a turbine a gaz
US4380906A (en) * 1981-01-22 1983-04-26 United Technologies Corporation Combustion liner cooling scheme
GB2434199B (en) 2006-01-14 2011-01-05 Alstom Technology Ltd Combustor liner with heat shield

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4723413A (en) * 1985-11-19 1988-02-09 MTU Munuch, GmbH Reverse flow combustion chamber, especially reverse flow ring combustion chamber, for gas turbine propulsion units, with at least one flame tube wall film-cooling arrangement

Also Published As

Publication number Publication date
CH529916A (de) 1972-10-31
DE2054002B2 (de) 1973-08-09
CA958550A (en) 1974-12-03
FR2112220B3 (enExample) 1974-05-10
FR2112220A3 (enExample) 1972-06-16
JPS5132163B1 (enExample) 1976-09-10
DE2054002A1 (de) 1972-04-06
DE2054002C3 (de) 1974-03-07
BE773194A (fr) 1972-01-17

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee