IT988000B - COOLING STRUCTURE OF THE ENCLOSURE OF THE COM BUSTION CHAMBER OF GAS TURBOMOTORS - Google Patents

COOLING STRUCTURE OF THE ENCLOSURE OF THE COM BUSTION CHAMBER OF GAS TURBOMOTORS

Info

Publication number
IT988000B
IT988000B IT24706/73A IT2470673A IT988000B IT 988000 B IT988000 B IT 988000B IT 24706/73 A IT24706/73 A IT 24706/73A IT 2470673 A IT2470673 A IT 2470673A IT 988000 B IT988000 B IT 988000B
Authority
IT
Italy
Prior art keywords
turbomotors
enclosure
gas
cooling structure
bustion chamber
Prior art date
Application number
IT24706/73A
Other languages
Italian (it)
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
Application granted granted Critical
Publication of IT988000B publication Critical patent/IT988000B/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • 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
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
IT24706/73A 1972-06-01 1973-05-29 COOLING STRUCTURE OF THE ENCLOSURE OF THE COM BUSTION CHAMBER OF GAS TURBOMOTORS IT988000B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US25888572A 1972-06-01 1972-06-01

Publications (1)

Publication Number Publication Date
IT988000B true IT988000B (en) 1975-03-20

Family

ID=22982555

Family Applications (1)

Application Number Title Priority Date Filing Date
IT24706/73A IT988000B (en) 1972-06-01 1973-05-29 COOLING STRUCTURE OF THE ENCLOSURE OF THE COM BUSTION CHAMBER OF GAS TURBOMOTORS

Country Status (6)

Country Link
JP (1) JPS4954711A (en)
BE (1) BE799958A (en)
CA (1) CA982828A (en)
DE (1) DE2327244A1 (en)
FR (1) FR2186602B1 (en)
IT (1) IT988000B (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4291531A (en) * 1978-04-06 1981-09-29 Rolls-Royce Limited Gas turbine engine
GB2042086B (en) * 1979-02-26 1983-10-12 Gen Electric Gas turbine engine seal
USH903H (en) * 1982-05-03 1991-04-02 General Electric Company Cool tip combustor
JPS5932863U (en) * 1982-08-27 1984-02-29 三菱重工業株式会社 gas turbine combustor
US5351478A (en) * 1992-05-29 1994-10-04 General Electric Company Compressor casing assembly
JPH0610772U (en) * 1992-07-14 1994-02-10 三菱重工業株式会社 Drain discharge device for container refrigeration unit
FR2829193B1 (en) 2001-08-30 2005-04-08 Snecma Moteurs AIR COLLECTION SYSTEM OF A COMPRESSOR

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2640319A (en) * 1949-02-12 1953-06-02 Packard Motor Car Co Cooling of gas turbines
US3015937A (en) * 1958-07-03 1962-01-09 James V Giliberty Temperature modulating system for internal combustion turbines and the like
GB987625A (en) * 1963-10-14 1965-03-31 Rolls Royce Improvements in or relating to axial flow compressors, for example for aircraft gas turbine engines
FR1536426A (en) * 1966-07-05 1968-08-16 Gas turbine machines

Also Published As

Publication number Publication date
CA982828A (en) 1976-02-03
BE799958A (en) 1973-09-17
FR2186602A1 (en) 1974-01-11
FR2186602B1 (en) 1977-02-11
DE2327244A1 (en) 1973-12-13
JPS4954711A (en) 1974-05-28

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