CH468557A - Gasturbinentriebwerk - Google Patents

Gasturbinentriebwerk

Info

Publication number
CH468557A
CH468557A CH1467466A CH1467466A CH468557A CH 468557 A CH468557 A CH 468557A CH 1467466 A CH1467466 A CH 1467466A CH 1467466 A CH1467466 A CH 1467466A CH 468557 A CH468557 A CH 468557A
Authority
CH
Switzerland
Prior art keywords
gas turbine
turbine engine
engine
gas
turbine
Prior art date
Application number
CH1467466A
Other languages
English (en)
Inventor
Chase Campbell Thomas
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
Application filed by Gen Electric filed Critical Gen Electric
Publication of CH468557A publication Critical patent/CH468557A/de

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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/14Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

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)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
CH1467466A 1966-01-19 1966-10-12 Gasturbinentriebwerk CH468557A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US521571A US3369363A (en) 1966-01-19 1966-01-19 Integral spacing rings for annular combustion chambers

Publications (1)

Publication Number Publication Date
CH468557A true CH468557A (de) 1969-02-15

Family

ID=24077240

Family Applications (1)

Application Number Title Priority Date Filing Date
CH1467466A CH468557A (de) 1966-01-19 1966-10-12 Gasturbinentriebwerk

Country Status (7)

Country Link
US (1) US3369363A (de)
BE (1) BE688143A (de)
CH (1) CH468557A (de)
DE (1) DE1476801B2 (de)
FR (1) FR1510874A (de)
GB (1) GB1138547A (de)
NL (1) NL158584B (de)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1520428A (fr) * 1966-12-08 1968-04-12 Snecma Elément de paroi d'une chambre de combustion
US3542486A (en) * 1968-09-27 1970-11-24 Gen Electric Film cooling of structural members in gas turbine engines
US3899876A (en) * 1968-11-15 1975-08-19 Secr Defence Brit Flame tube for a gas turbine combustion equipment
FR2155835B1 (de) * 1971-10-08 1974-05-31 Snecma
US3777484A (en) * 1971-12-08 1973-12-11 Gen Electric Shrouded combustion liner
US3845620A (en) * 1973-02-12 1974-11-05 Gen Electric Cooling film promoter for combustion chambers
US4109459A (en) * 1974-07-19 1978-08-29 General Electric Company Double walled impingement cooled combustor
US3995422A (en) * 1975-05-21 1976-12-07 General Electric Company Combustor liner structure
US4222230A (en) * 1978-08-14 1980-09-16 General Electric Company Combustor dome assembly
GB2034874A (en) * 1978-11-03 1980-06-11 Gen Electric Gas turbine engine combustor
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
US4527397A (en) * 1981-03-27 1985-07-09 Westinghouse Electric Corp. Turbine combustor having enhanced wall cooling for longer combustor life at high combustor outlet gas temperatures
US4566280A (en) * 1983-03-23 1986-01-28 Burr Donald N Gas turbine engine combustor splash ring construction
CN85107191A (zh) * 1984-10-04 1986-09-24 西屋电气公司 具有内气膜冷却的冲击式冷却燃气轮机燃烧室
DE3540942A1 (de) * 1985-11-19 1987-05-21 Mtu Muenchen Gmbh Umkehrbrennkammer, insbesondere umkehrringbrennkammer, fuer gasturbinentriebwerke, mit mindestens einer flammrohrwandfilmkuehleinrichtung
FR2604509B1 (fr) * 1986-09-25 1988-11-18 Snecma Procede de realisation d'un film de refroidissement pour chambre de combustion de turbomachine, film ainsi realise et chambre de combustion le comportant
US6250082B1 (en) 1999-12-03 2001-06-26 General Electric Company Combustor rear facing step hot side contour method and apparatus
US6675582B2 (en) 2001-05-23 2004-01-13 General Electric Company Slot cooled combustor line
US6554563B2 (en) * 2001-08-13 2003-04-29 General Electric Company Tangential flow baffle
US7975487B2 (en) * 2006-09-21 2011-07-12 Solar Turbines Inc. Combustor assembly for gas turbine engine
US8104288B2 (en) * 2008-09-25 2012-01-31 Honeywell International Inc. Effusion cooling techniques for combustors in engine assemblies
CN114543117B (zh) * 2020-11-25 2023-08-08 中国航发商用航空发动机有限责任公司 燃油喷嘴及航空发动机
CN113266849B (zh) * 2021-05-18 2022-08-05 中国航发湖南动力机械研究所 气膜冷却结构及涡轮发动机燃烧室火焰筒

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2658337A (en) * 1947-12-23 1953-11-10 Lucas Ltd Joseph Combustion chamber for prime movers
US2657531A (en) * 1948-01-22 1953-11-03 Gen Electric Wall cooling arrangement for combustion devices
US2699648A (en) * 1950-10-03 1955-01-18 Gen Electric Combustor sectional liner structure with annular inlet nozzles
GB743149A (en) * 1953-08-06 1956-01-11 Lucas Industries Ltd Liquid fuel combustion chambers for prime movers
BE535905A (de) * 1954-02-23
US2973624A (en) * 1955-10-26 1961-03-07 Gen Electric Cowled dome liners
US2884759A (en) * 1956-04-25 1959-05-05 Curtiss Wright Corp Combustion chamber construction
US2979898A (en) * 1958-04-25 1961-04-18 United Aircraft Corp Hooded crossover tube
NL257968A (de) * 1959-11-20

Also Published As

Publication number Publication date
GB1138547A (en) 1969-01-01
US3369363A (en) 1968-02-20
NL158584B (nl) 1978-11-15
BE688143A (de) 1967-03-16
DE1476801A1 (de) 1969-10-16
NL6613784A (de) 1967-07-20
DE1476801B2 (de) 1971-04-08
FR1510874A (fr) 1968-01-26

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