IT1124886B - COMBUSTION CHAMBER FOR GAS TURBO ENGINE - Google Patents

COMBUSTION CHAMBER FOR GAS TURBO ENGINE

Info

Publication number
IT1124886B
IT1124886B IT26982/79A IT2698279A IT1124886B IT 1124886 B IT1124886 B IT 1124886B IT 26982/79 A IT26982/79 A IT 26982/79A IT 2698279 A IT2698279 A IT 2698279A IT 1124886 B IT1124886 B IT 1124886B
Authority
IT
Italy
Prior art keywords
combustion chamber
turbo engine
gas turbo
engine
gas
Prior art date
Application number
IT26982/79A
Other languages
Italian (it)
Other versions
IT7926982A0 (en
Inventor
Jacob Sherman Hoffman
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 IT7926982A0 publication Critical patent/IT7926982A0/en
Application granted granted Critical
Publication of IT1124886B publication Critical patent/IT1124886B/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
    • 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
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient 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)
IT26982/79A 1978-11-03 1979-10-31 COMBUSTION CHAMBER FOR GAS TURBO ENGINE IT1124886B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US95759178A 1978-11-03 1978-11-03

Publications (2)

Publication Number Publication Date
IT7926982A0 IT7926982A0 (en) 1979-10-31
IT1124886B true IT1124886B (en) 1986-05-14

Family

ID=25499810

Family Applications (1)

Application Number Title Priority Date Filing Date
IT26982/79A IT1124886B (en) 1978-11-03 1979-10-31 COMBUSTION CHAMBER FOR GAS TURBO ENGINE

Country Status (5)

Country Link
JP (1) JPS5582231A (en)
DE (1) DE2944139A1 (en)
FR (1) FR2440524A1 (en)
GB (1) GB2034874A (en)
IT (1) IT1124886B (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2161914B (en) * 1980-12-10 1986-06-11 Rolls Royce Combustion equipment for a gas turbine engine
GB2125950B (en) * 1982-08-16 1986-09-24 Gen Electric Gas turbine combustor
GB2134243A (en) * 1983-01-27 1984-08-08 Rolls Royce Combustion equipment for a gas turbine engine
US4566280A (en) * 1983-03-23 1986-01-28 Burr Donald N Gas turbine engine combustor splash ring construction
FR2604509B1 (en) * 1986-09-25 1988-11-18 Snecma PROCESS FOR PRODUCING A COOLING FILM FOR A TURBOMACHINE COMBUSTION CHAMBER, FILM THUS PRODUCED AND COMBUSTION CHAMBER COMPRISING SAME
US4916906A (en) * 1988-03-25 1990-04-17 General Electric Company Breach-cooled structure
IT1255613B (en) * 1992-09-24 1995-11-09 Eniricerche Spa LOW EMISSION COMBUSTION SYSTEM FOR GAS TURBINES
DE19547703C2 (en) * 1995-12-20 1999-02-18 Mtu Muenchen Gmbh Combustion chamber, in particular ring combustion chamber, for gas turbine engines
DE10048864A1 (en) * 2000-10-02 2002-04-11 Rolls Royce Deutschland Combustion chamber head for a gas turbine
JP2002317650A (en) * 2001-04-24 2002-10-31 Mitsubishi Heavy Ind Ltd Gas turbine combustor
FR2901349B1 (en) * 2006-05-19 2008-09-05 Snecma Sa COMBUSTION CHAMBER OF A TURBOMACHINE
EP2261565A1 (en) * 2009-06-09 2010-12-15 Siemens Aktiengesellschaft Gas turbine reactor and gas turbines
RU2451881C2 (en) * 2009-10-06 2012-05-27 Открытое акционерное общество "Всероссийский дважды ордена Трудового Красного Знамени теплотехнический научно-исследовательский институт" Premixing combustion chamber of gas turbine plant

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2482E (en) * 1902-04-30 1904-04-27 Gaston Charles Emile De Bonnec Continuous combustion turbo-engine system
CH255541A (en) * 1947-05-12 1948-06-30 Bbc Brown Boveri & Cie Cooled metal combustion chamber for generating heating and propellant gases.
US2729062A (en) * 1951-07-06 1956-01-03 Dresser Operations Inc Power plant combustion chamber
US2974485A (en) * 1958-06-02 1961-03-14 Gen Electric Combustor for fluid fuels
GB845971A (en) * 1958-07-21 1960-08-24 Gen Electric Improvements relating to combustion chambers for gas turbine engines
US3338051A (en) * 1965-05-28 1967-08-29 United Aircraft Corp High velocity ram induction burner
US3369363A (en) * 1966-01-19 1968-02-20 Gen Electric Integral spacing rings for annular combustion chambers
FR2055720A1 (en) * 1969-08-01 1971-04-30 Snecma
CA980584A (en) * 1972-11-10 1975-12-30 Edward E. Ekstedt Double walled impingement cooled combustor
US3986347A (en) * 1973-12-06 1976-10-19 Phillips Petroleum Company Combustor process for low-level NOx and CO emissions
GB1498269A (en) * 1975-05-23 1978-01-18 Snecma Gas turbine combustion chambers
DE2636520A1 (en) * 1976-08-13 1978-02-16 Daimler Benz Ag Spherical combustion chamber for gas turbines - has spherical secondary wall with inlets accelerating swirling in combustion chamber

Also Published As

Publication number Publication date
IT7926982A0 (en) 1979-10-31
JPS5582231A (en) 1980-06-20
GB2034874A (en) 1980-06-11
DE2944139A1 (en) 1980-05-14
FR2440524A1 (en) 1980-05-30

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