IT1197110B - Turbina a gas - Google Patents

Turbina a gas

Info

Publication number
IT1197110B
IT1197110B IT21513/86A IT2151386A IT1197110B IT 1197110 B IT1197110 B IT 1197110B IT 21513/86 A IT21513/86 A IT 21513/86A IT 2151386 A IT2151386 A IT 2151386A IT 1197110 B IT1197110 B IT 1197110B
Authority
IT
Italy
Prior art keywords
gas turbine
turbine
gas
Prior art date
Application number
IT21513/86A
Other languages
English (en)
Other versions
IT8621513A0 (it
IT8621513A1 (it
Inventor
John William Vinson
Chi-Ping Kwong Pamela
Paul Edward Sabla
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 IT8621513A0 publication Critical patent/IT8621513A0/it
Publication of IT8621513A1 publication Critical patent/IT8621513A1/it
Application granted granted Critical
Publication of IT1197110B publication Critical patent/IT1197110B/it

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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C7/00—Combustion apparatus characterised by arrangements for air supply
    • F23C7/002—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
    • F23C7/004—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion using vanes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/20—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
    • F23D14/22—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
    • F23D14/24—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other at least one of the fluids being submitted to a swirling motion
    • 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
    • F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00002—Gas turbine combustors adapted for fuels having low heating value [LHV]
    • 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
    • Y02T50/678—Aviation using fuels of non-fossil origin

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
IT21513/86A 1985-08-23 1986-08-22 Turbina a gas IT1197110B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/768,600 US4653278A (en) 1985-08-23 1985-08-23 Gas turbine engine carburetor

Publications (3)

Publication Number Publication Date
IT8621513A0 IT8621513A0 (it) 1986-08-22
IT8621513A1 IT8621513A1 (it) 1988-02-22
IT1197110B true IT1197110B (it) 1988-11-25

Family

ID=25082953

Family Applications (1)

Application Number Title Priority Date Filing Date
IT21513/86A IT1197110B (it) 1985-08-23 1986-08-22 Turbina a gas

Country Status (8)

Country Link
US (1) US4653278A (it)
JP (1) JPS6270629A (it)
CA (1) CA1250439A (it)
CH (1) CH682002A5 (it)
DE (1) DE3626545A1 (it)
FR (1) FR2586453B1 (it)
GB (2) GB2179435B (it)
IT (1) IT1197110B (it)

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US5239832A (en) * 1991-12-26 1993-08-31 General Electric Company Birdstrike resistant swirler support for combustion chamber dome
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Also Published As

Publication number Publication date
CA1250439A (en) 1989-02-28
GB8902546D0 (en) 1989-03-22
GB2179435B (en) 1990-02-21
IT8621513A0 (it) 1986-08-22
IT8621513A1 (it) 1988-02-22
GB2179435A (en) 1987-03-04
GB2211596A (en) 1989-07-05
JPS6270629A (ja) 1987-04-01
GB2211596B (en) 1990-03-07
CH682002A5 (it) 1993-06-30
US4653278A (en) 1987-03-31
FR2586453A1 (fr) 1987-02-27
DE3626545A1 (de) 1987-02-26
FR2586453B1 (fr) 1992-11-06
GB8613546D0 (en) 1986-07-09

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