GB1563124A - Gas turbine fuel injection systems - Google Patents

Gas turbine fuel injection systems Download PDF

Info

Publication number
GB1563124A
GB1563124A GB38376/76A GB3837676A GB1563124A GB 1563124 A GB1563124 A GB 1563124A GB 38376/76 A GB38376/76 A GB 38376/76A GB 3837676 A GB3837676 A GB 3837676A GB 1563124 A GB1563124 A GB 1563124A
Authority
GB
United Kingdom
Prior art keywords
fuel
air
injector
flow
downstream
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
GB38376/76A
Other languages
English (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 GB1563124A publication Critical patent/GB1563124A/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
    • F23R3/10Air inlet arrangements for primary air
    • F23R3/12Air inlet arrangements for primary air inducing a vortex
    • F23R3/14Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • HELECTRICITY
    • H10SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
    • H10DINORGANIC ELECTRIC SEMICONDUCTOR DEVICES
    • H10D64/00Electrodes of devices having potential barriers
    • H10D64/60Electrodes characterised by their materials
    • H10D64/66Electrodes having a conductor capacitively coupled to a semiconductor by an insulator, e.g. MIS electrodes
    • H10D64/671Electrodes having a conductor capacitively coupled to a semiconductor by an insulator, e.g. MIS electrodes the conductor having lateral variation in doping or structure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2900/00Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/00016Preventing or reducing deposit build-up on burner parts, e.g. from carbon

Landscapes

  • Engineering & Computer Science (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)
GB38376/76A 1975-12-24 1976-09-16 Gas turbine fuel injection systems Expired GB1563124A (en)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
GB1563124A true GB1563124A (en) 1980-03-19

Family

ID=24583195

Family Applications (1)

Application Number Title Priority Date Filing Date
GB38376/76A Expired GB1563124A (en) 1975-12-24 1976-09-16 Gas turbine fuel injection systems

Country Status (5)

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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2127952A (en) * 1982-09-29 1984-04-18 British Gas Corp Burner assembly

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RO77519A2 (ro) * 1980-12-27 1983-09-26 Institutul National De Motoare Termice,Ro Injector de combustibili lichizi
US4653278A (en) * 1985-08-23 1987-03-31 General Electric Company Gas turbine engine carburetor
FR2673705A1 (fr) * 1991-03-06 1992-09-11 Snecma Chambre de combustion de turbomachine munie d'un dispositif anti-cokefaction du fond de ladite chambre.
DE4326802A1 (de) * 1993-08-10 1995-02-16 Abb Management Ag Brennstofflanze für flüssige und/oder gasförmige Brennstoffe sowie Verfahren zu deren Betrieb
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 (de) 2008-12-12 2010-06-16 Siemens Aktiengesellschaft Brennstofflanze für einen Brenner
FR3015638B1 (fr) * 2013-12-23 2019-05-31 Safran Aircraft Engines Segment d'obturation de traversee coulissante de systeme d'injection pour turbomachine

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE240617C (enrdf_load_stackoverflow) *
US1799551A (en) * 1929-04-01 1931-04-07 Forney Comb Engineering Compan Oil and steam burner nozzle
FR1094871A (fr) * 1959-01-22 1955-05-25 Thomson Houston Comp Francaise Perfectionnements aux appareils de combustion à combustible injecté
US2942790A (en) * 1959-01-23 1960-06-28 Gen Electric Air-atomizing liquid spray nozzle
FR1230621A (fr) * 1959-04-03 1960-09-19 Snecma Perfectionnement aux dispositifs de combustion
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
US3946552A (en) * 1973-09-10 1976-03-30 General Electric Company Fuel injection apparatus
US3972182A (en) * 1973-09-10 1976-08-03 General Electric Company Fuel injection apparatus
JPH041804U (enrdf_load_stackoverflow) * 1990-04-17 1992-01-09

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2127952A (en) * 1982-09-29 1984-04-18 British Gas Corp Burner assembly

Also Published As

Publication number Publication date
FR2336555A1 (fr) 1977-07-22
JPS6132576B2 (enrdf_load_stackoverflow) 1986-07-28
FR2336555B1 (enrdf_load_stackoverflow) 1982-10-08
DE2641605A1 (de) 1977-07-07
DE2641605C2 (de) 1986-06-19
IT1074074B (it) 1985-04-17
JPS5279112A (en) 1977-07-04

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GB1563124A (en) Gas turbine fuel injection systems

Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
746 Register noted 'licences of right' (sect. 46/1977)
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19940916