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GB2009859B - Combustion apparatus - Google Patents

Combustion apparatus

Info

Publication number
GB2009859B
GB2009859B GB7840058A GB7840058A GB2009859B GB 2009859 B GB2009859 B GB 2009859B GB 7840058 A GB7840058 A GB 7840058A GB 7840058 A GB7840058 A GB 7840058A GB 2009859 B GB2009859 B GB 2009859B
Authority
GB
United Kingdom
Prior art keywords
combustion apparatus
combustion
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
GB7840058A
Other versions
GB2009859A (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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Publication of GB2009859A publication Critical patent/GB2009859A/en
Application granted granted Critical
Publication of GB2009859B publication Critical patent/GB2009859B/en
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
    • 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
    • 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)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
  • Gas Burners (AREA)
  • Extrusion Moulding Of Plastics Or The Like (AREA)
GB7840058A 1977-10-11 1978-10-10 Combustion apparatus Expired GB2009859B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7730487A FR2406075A1 (en) 1977-10-11 1977-10-11 COMBUSTION APPARATUS AND ITS EMBODIMENT PROCESS

Publications (2)

Publication Number Publication Date
GB2009859A GB2009859A (en) 1979-06-20
GB2009859B true GB2009859B (en) 1982-04-07

Family

ID=9196335

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7840058A Expired GB2009859B (en) 1977-10-11 1978-10-10 Combustion apparatus

Country Status (3)

Country Link
DE (1) DE2844349C2 (en)
FR (1) FR2406075A1 (en)
GB (1) GB2009859B (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3117515C2 (en) * 1980-05-07 1983-11-10 Brown, Boveri & Cie Ag, 6800 Mannheim Overflow housing
US4878283A (en) * 1987-08-31 1989-11-07 United Technologies Corporation Augmentor liner construction
DE19528406A1 (en) * 1995-08-02 1997-02-06 Bmw Rolls Royce Gmbh Gas turbine combustion chamber with air transfer ports - has shot blasted, rolled raster or fluting design upstream of ports to specified raster dimension
JP2018054210A (en) * 2016-09-28 2018-04-05 株式会社Ihi Liner for combustor
CN112984559A (en) * 2021-03-19 2021-06-18 中国联合重型燃气轮机技术有限公司 Flame tube, combustion chamber, and gas turbine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE466639A (en) * 1944-12-13
GB818634A (en) * 1955-09-29 1959-08-19 Birmingham Small Arms Co Ltd Improvements in or relating to combustion chambers for gas turbines
BE551418A (en) * 1955-10-28
DE1171207B (en) * 1960-04-01 1964-05-27 United Aircraft Corp Can burner for a gas turbine combustion chamber
US3712062A (en) * 1968-04-17 1973-01-23 Gen Electric Cooled augmentor liner
GB1320482A (en) * 1971-01-25 1973-06-13 Secr Defence Cooling of hot fluid ducts

Also Published As

Publication number Publication date
FR2406075B1 (en) 1980-04-04
FR2406075A1 (en) 1979-05-11
DE2844349C2 (en) 1986-07-17
DE2844349A1 (en) 1979-04-12
GB2009859A (en) 1979-06-20

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Legal Events

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

Effective date: 19971010