FR2112220B3 - - Google Patents

Info

Publication number
FR2112220B3
FR2112220B3 FR7134809A FR7134809A FR2112220B3 FR 2112220 B3 FR2112220 B3 FR 2112220B3 FR 7134809 A FR7134809 A FR 7134809A FR 7134809 A FR7134809 A FR 7134809A FR 2112220 B3 FR2112220 B3 FR 2112220B3
Authority
FR
France
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
FR7134809A
Other languages
French (fr)
Other versions
FR2112220A3 (xx
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 FR2112220A3 publication Critical patent/FR2112220A3/fr
Application granted granted Critical
Publication of FR2112220B3 publication Critical patent/FR2112220B3/fr
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
    • F23R3/06Arrangement of apertures along the flame tube
    • F23R3/08Arrangement 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)
  • Gas Burners (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR7134809A 1970-10-01 1971-09-28 Expired FR2112220B3 (xx)

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 (2)

Publication Number Publication Date
FR2112220A3 FR2112220A3 (xx) 1972-06-16
FR2112220B3 true FR2112220B3 (xx) 1974-05-10

Family

ID=4401724

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7134809A Expired FR2112220B3 (xx) 1970-10-01 1971-09-28

Country Status (7)

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

Families Citing this family (9)

* 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
DE2919857C2 (de) * 1978-05-20 1982-09-02 Rolls-Royce Ltd., London Flammrohrkopf mit Kühlring für Gasturbinenbrennkammern
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
DE3540942A1 (de) * 1985-11-19 1987-05-21 Mtu Muenchen Gmbh Umkehrbrennkammer, insbesondere umkehrringbrennkammer, fuer gasturbinentriebwerke, mit mindestens einer flammrohrwandfilmkuehleinrichtung
GB2434199B (en) 2006-01-14 2011-01-05 Alstom Technology Ltd Combustor liner with heat shield

Also Published As

Publication number Publication date
JPS5132163B1 (xx) 1976-09-10
FR2112220A3 (xx) 1972-06-16
CA958550A (en) 1974-12-03
BE773194A (fr) 1972-01-17
DE2054002C3 (de) 1974-03-07
CH529916A (de) 1972-10-31
GB1309180A (en) 1973-03-07
DE2054002B2 (de) 1973-08-09
DE2054002A1 (de) 1972-04-06

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