CH380444A - Flame tube for combustion chambers - Google Patents

Flame tube for combustion chambers

Info

Publication number
CH380444A
CH380444A CH1120260A CH1120260A CH380444A CH 380444 A CH380444 A CH 380444A CH 1120260 A CH1120260 A CH 1120260A CH 1120260 A CH1120260 A CH 1120260A CH 380444 A CH380444 A CH 380444A
Authority
CH
Switzerland
Prior art keywords
combustion chambers
flame tube
flame
tube
chambers
Prior art date
Application number
CH1120260A
Other languages
German (de)
Inventor
Franklin Hayes Charles
Original Assignee
Gen Motors Corp
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 Gen Motors Corp filed Critical Gen Motors Corp
Publication of CH380444A publication Critical patent/CH380444A/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

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)
  • Spray-Type Burners (AREA)
CH1120260A 1959-10-05 1960-10-05 Flame tube for combustion chambers CH380444A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US844279A US3064425A (en) 1959-10-05 1959-10-05 Combustion liner

Publications (1)

Publication Number Publication Date
CH380444A true CH380444A (en) 1964-07-31

Family

ID=25292282

Family Applications (1)

Application Number Title Priority Date Filing Date
CH1120260A CH380444A (en) 1959-10-05 1960-10-05 Flame tube for combustion chambers

Country Status (3)

Country Link
US (1) US3064425A (en)
CH (1) CH380444A (en)
GB (1) GB891836A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2354504A1 (en) * 1972-11-02 1974-05-16 Gen Electric REINFORCEMENT FOR BURNER LINING

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3485043A (en) * 1968-02-01 1969-12-23 Gen Electric Shingled combustion liner
US3589128A (en) * 1970-02-02 1971-06-29 Avco Corp Cooling arrangement for a reverse flow gas turbine combustor
US3705492A (en) * 1971-01-11 1972-12-12 Gen Motors Corp Regenerative gas turbine system
US3742702A (en) * 1971-01-22 1973-07-03 Gen Motors Corp Regenerative gas turbine system
US3751910A (en) * 1972-02-25 1973-08-14 Gen Motors Corp Combustion liner
US3854285A (en) * 1973-02-26 1974-12-17 Gen Electric Combustor dome assembly
GB1552132A (en) * 1975-11-29 1979-09-12 Rolls Royce Combustion chambers for gas turbine engines
US4050241A (en) * 1975-12-22 1977-09-27 General Electric Company Stabilizing dimple for combustion liner cooling slot
US4008568A (en) * 1976-03-01 1977-02-22 General Motors Corporation Combustor support
US4132066A (en) * 1977-09-23 1979-01-02 United Technologies Corporation Combustor liner for gas turbine engine
US4244178A (en) * 1978-03-20 1981-01-13 General Motors Corporation Porous laminated combustor structure
US4180972A (en) * 1978-06-08 1980-01-01 General Motors Corporation Combustor support structure
GB2049152B (en) * 1979-05-01 1983-05-18 Rolls Royce Perforate laminated material
US4312186A (en) * 1979-10-17 1982-01-26 General Motors Corporation Shingled laminated porous material
US4413477A (en) * 1980-12-29 1983-11-08 General Electric Company Liner assembly for gas turbine combustor
US4928479A (en) * 1987-12-28 1990-05-29 Sundstrand Corporation Annular combustor with tangential cooling air injection
US4887663A (en) * 1988-05-31 1989-12-19 United Technologies Corporation Hot gas duct liner
US5181377A (en) * 1991-04-16 1993-01-26 General Electric Company Damped combustor cowl structure
US6823677B2 (en) * 2002-09-03 2004-11-30 Pratt & Whitney Canada Corp. Stress relief feature for aerated gas turbine fuel injector
US7043921B2 (en) * 2003-08-26 2006-05-16 Honeywell International, Inc. Tube cooled combustor
US7464537B2 (en) * 2005-04-04 2008-12-16 United Technologies Corporation Heat transfer enhancement features for a tubular wall combustion chamber
FR2887615B1 (en) * 2005-06-22 2007-08-31 Snecma Moteurs Sa CIRCULAR FITTING OF TURBOMACHINE COMBUSTION CHAMBER
FR2896575B1 (en) * 2006-01-26 2013-01-18 Snecma ANNULAR COMBUSTION CHAMBER OF A TURBOMACHINE
US7827801B2 (en) * 2006-02-09 2010-11-09 Siemens Energy, Inc. Gas turbine engine transitions comprising closed cooled transition cooling channels
FR2905166B1 (en) * 2006-08-28 2008-11-14 Snecma Sa ANNULAR COMBUSTION CHAMBER OF A TURBOMACHINE.
FR2910597B1 (en) * 2006-12-22 2009-03-20 Snecma Sa FURNITURE FOR BOTTOM OF COMBUSTION CHAMBER
DE102007050664A1 (en) * 2007-10-24 2009-04-30 Man Turbo Ag Burner for a turbomachine, baffle for such a burner and a turbomachine with such a burner
WO2017204229A1 (en) * 2016-05-23 2017-11-30 三菱日立パワーシステムズ株式会社 Combustor and gas turbine
RU205407U1 (en) * 2020-12-08 2021-07-13 Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") Combustion tube with expansion slots
CN117469698A (en) 2022-07-21 2024-01-30 通用电气公司 Performance factor of combustion liner

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2645081A (en) * 1949-08-19 1953-07-14 A V Roe Canada Ltd Spacing means for the wall sections of flame tubes
US2670601A (en) * 1950-10-17 1954-03-02 A V Roe Canada Ltd Spacing means for wall sections of flame tubes
US2884759A (en) * 1956-04-25 1959-05-05 Curtiss Wright Corp Combustion chamber construction

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2354504A1 (en) * 1972-11-02 1974-05-16 Gen Electric REINFORCEMENT FOR BURNER LINING

Also Published As

Publication number Publication date
GB891836A (en) 1962-03-21
US3064425A (en) 1962-11-20

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