FR2336555B1 - - Google Patents

Info

Publication number
FR2336555B1
FR2336555B1 FR7628437A FR7628437A FR2336555B1 FR 2336555 B1 FR2336555 B1 FR 2336555B1 FR 7628437 A FR7628437 A FR 7628437A FR 7628437 A FR7628437 A FR 7628437A FR 2336555 B1 FR2336555 B1 FR 2336555B1
Authority
FR
France
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
FR7628437A
Other languages
French (fr)
Other versions
FR2336555A1 (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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of FR2336555A1 publication Critical patent/FR2336555A1/en
Application granted granted Critical
Publication of FR2336555B1 publication Critical patent/FR2336555B1/fr
Granted legal-status Critical Current

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
    • 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
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L29/00—Semiconductor devices specially adapted for rectifying, amplifying, oscillating or switching and having potential barriers; Capacitors or resistors having potential barriers, e.g. a PN-junction depletion layer or carrier concentration layer; Details of semiconductor bodies or of electrodes thereof ; Multistep manufacturing processes therefor
    • H01L29/40—Electrodes ; Multistep manufacturing processes therefor
    • H01L29/43—Electrodes ; Multistep manufacturing processes therefor characterised by the materials of which they are formed
    • H01L29/49—Metal-insulator-semiconductor electrodes, e.g. gates of MOSFET
    • H01L29/4983—Metal-insulator-semiconductor electrodes, e.g. gates of MOSFET with a lateral structure, e.g. a Polysilicon gate with a lateral doping variation or with a lateral composition variation or characterised by the sidewalls being composed of conductive, resistive or dielectric material
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2900/00—Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/00016—Preventing or reducing deposit build-up on burner parts, e.g. from carbon

Landscapes

  • Engineering & Computer Science (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Power Engineering (AREA)
  • Condensed Matter Physics & Semiconductors (AREA)
  • General Physics & Mathematics (AREA)
  • Physics & Mathematics (AREA)
  • Ceramic Engineering (AREA)
  • Computer Hardware Design (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Spray-Type Burners (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)
FR7628437A 1975-12-24 1976-09-22 PERFECTED CARBURATION SYSTEM FOR GAS TURBINE Granted FR2336555A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US64403875A 1975-12-24 1975-12-24

Publications (2)

Publication Number Publication Date
FR2336555A1 FR2336555A1 (en) 1977-07-22
FR2336555B1 true FR2336555B1 (en) 1982-10-08

Family

ID=24583195

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7628437A Granted FR2336555A1 (en) 1975-12-24 1976-09-22 PERFECTED CARBURATION SYSTEM FOR GAS TURBINE

Country Status (5)

Country Link
JP (1) JPS5279112A (en)
DE (1) DE2641605C2 (en)
FR (1) FR2336555A1 (en)
GB (1) GB1563124A (en)
IT (1) IT1074074B (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RO77519A2 (en) * 1980-12-27 1983-09-26 Institutul National De Motoare Termice,Ro FLUID FUEL INJECTOR
GB2127952A (en) * 1982-09-29 1984-04-18 British Gas Corp Burner assembly
US4653278A (en) * 1985-08-23 1987-03-31 General Electric Company Gas turbine engine carburetor
FR2673705A1 (en) * 1991-03-06 1992-09-11 Snecma Combustion chamber of a turbine engine equipped with an anti-coking device for the bottom of said chamber
DE4326802A1 (en) * 1993-08-10 1995-02-16 Abb Management Ag Fuel lance for liquid and / or gaseous fuels and process for their operation
US5408830A (en) * 1994-02-10 1995-04-25 General Electric Company Multi-stage fuel nozzle for reducing combustion instabilities in low NOX gas turbines
US6718770B2 (en) * 2002-06-04 2004-04-13 General Electric Company Fuel injector laminated fuel strip
US7013649B2 (en) * 2004-05-25 2006-03-21 General Electric Company Gas turbine engine combustor mixer
EP2196734A1 (en) * 2008-12-12 2010-06-16 Siemens Aktiengesellschaft Fuel lance for a burner
FR3015638B1 (en) * 2013-12-23 2019-05-31 Safran Aircraft Engines TURBOMACHINE INJECTION SYSTEM SLIDING RUN END SEGMENT SEGMENT

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE240617C (en) *
US1799551A (en) * 1929-04-01 1931-04-07 Forney Comb Engineering Compan Oil and steam burner nozzle
FR1094871A (en) * 1959-01-22 1955-05-25 Thomson Houston Comp Francaise Improvements to injected fuel combustion devices
US2942790A (en) * 1959-01-23 1960-06-28 Gen Electric Air-atomizing liquid spray nozzle
FR1230621A (en) * 1959-04-03 1960-09-19 Snecma Improvement in combustion devices
US2968925A (en) * 1959-11-25 1961-01-24 William E Blevans Fuel nozzle head for anti-coking
US3121996A (en) * 1961-10-02 1964-02-25 Lucas Industries Ltd Liquid fuel combustion apparatus
US3648457A (en) * 1970-04-30 1972-03-14 Gen Electric Combustion apparatus
US3899884A (en) * 1970-12-02 1975-08-19 Gen Electric Combustor systems
US3768250A (en) * 1971-12-01 1973-10-30 Mitsubishi Heavy Ind Ltd Combustion apparatus for a gas turbine
GB1435083A (en) * 1972-08-10 1976-05-12 Rolls Royce Gas turbine engine combustion equipment
US3972182A (en) * 1973-09-10 1976-08-03 General Electric Company Fuel injection apparatus
US3946552A (en) * 1973-09-10 1976-03-30 General Electric Company Fuel injection apparatus
JPH041804U (en) * 1990-04-17 1992-01-09

Also Published As

Publication number Publication date
DE2641605A1 (en) 1977-07-07
DE2641605C2 (en) 1986-06-19
IT1074074B (en) 1985-04-17
FR2336555A1 (en) 1977-07-22
JPS6132576B2 (en) 1986-07-28
JPS5279112A (en) 1977-07-04
GB1563124A (en) 1980-03-19

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Legal Events

Date Code Title Description
ST Notification of lapse