IT1075001B - Camere di combustione particolarmente per motori a turbina a gas e metodo per farle funzionare - Google Patents

Camere di combustione particolarmente per motori a turbina a gas e metodo per farle funzionare

Info

Publication number
IT1075001B
IT1075001B IT22270/76A IT2227076A IT1075001B IT 1075001 B IT1075001 B IT 1075001B IT 22270/76 A IT22270/76 A IT 22270/76A IT 2227076 A IT2227076 A IT 2227076A IT 1075001 B IT1075001 B IT 1075001B
Authority
IT
Italy
Prior art keywords
operate
combustion chamber
gas turbine
turbine engines
chamber particularly
Prior art date
Application number
IT22270/76A
Other languages
English (en)
Original Assignee
Phillips Petroleum 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
Priority claimed from US05/567,829 external-priority patent/US4007001A/en
Priority claimed from US05/567,920 external-priority patent/US4006589A/en
Application filed by Phillips Petroleum Co filed Critical Phillips Petroleum Co
Application granted granted Critical
Publication of IT1075001B publication Critical patent/IT1075001B/it

Links

Classifications

    • 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
    • F23C7/008—Flow control devices
    • 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 
    • F23C6/00—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion
    • F23C6/04—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection
    • F23C6/045—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection with staged combustion in a single enclosure
    • 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
    • F23R3/26—Controlling the air flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/40—Movement of components
    • F05D2250/41—Movement of components with one degree of freedom
    • F05D2250/411—Movement of components with one degree of freedom in rotation

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Of Fluid Fuel (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Spray-Type Burners (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
  • Gas Burners (AREA)
  • Air Supply (AREA)
IT22270/76A 1975-04-14 1976-04-13 Camere di combustione particolarmente per motori a turbina a gas e metodo per farle funzionare IT1075001B (it)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US05/567,829 US4007001A (en) 1975-04-14 1975-04-14 Combustors and methods of operating same
US05/567,920 US4006589A (en) 1975-04-14 1975-04-14 Low emission combustor with fuel flow controlled primary air flow and circumferentially directed secondary air flows

Publications (1)

Publication Number Publication Date
IT1075001B true IT1075001B (it) 1985-04-22

Family

ID=27074587

Family Applications (1)

Application Number Title Priority Date Filing Date
IT22270/76A IT1075001B (it) 1975-04-14 1976-04-13 Camere di combustione particolarmente per motori a turbina a gas e metodo per farle funzionare

Country Status (6)

Country Link
JP (1) JPS51133826A (it)
DE (2) DE2616452C3 (it)
FR (1) FR2308053A1 (it)
GB (1) GB1536166A (it)
IT (1) IT1075001B (it)
SE (1) SE429158B (it)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4151713A (en) * 1977-03-15 1979-05-01 United Technologies Corporation Burner for gas turbine engine
JPS54103652U (it) * 1977-12-29 1979-07-21
GB2085146B (en) * 1980-10-01 1985-06-12 Gen Electric Flow modifying device
US4861263A (en) * 1982-03-04 1989-08-29 Phillips Petroleum Company Method and apparatus for the recovery of hydrocarbons
EP3111139B1 (en) * 2014-02-11 2020-07-15 Ancora S.p.A. Burner
GB2565761A (en) * 2017-07-28 2019-02-27 Tunley Enginering Combustion engine fuel mixture system
CN109113792A (zh) * 2018-10-30 2019-01-01 常胜 复合加力涡轮
CN109268141A (zh) * 2018-10-30 2019-01-25 常胜 多燃料发动机

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3859786A (en) * 1972-05-25 1975-01-14 Ford Motor Co Combustor
ZA729071B (en) * 1972-10-05 1973-10-31 Aqua Chem Inc Reduction of gaseous pollutants in combustion flue gas
JPS4967222A (it) * 1972-10-31 1974-06-29

Also Published As

Publication number Publication date
DE2616452B2 (de) 1979-04-12
DE7611803U1 (de) 1978-12-07
SE429158B (sv) 1983-08-15
DE2616452C3 (de) 1979-12-06
DE2616452A1 (de) 1976-10-28
GB1536166A (en) 1978-12-20
FR2308053A1 (fr) 1976-11-12
JPS51133826A (en) 1976-11-19
FR2308053B1 (it) 1980-11-14

Similar Documents

Publication Publication Date Title
IT1051760B (it) Equipaggiamento di combustione per motori a turbina a gas
IT1099412B (it) Perfezionamenti apportati ai dispositivi di combustione per motori a turbina a gas
IT998522B (it) Apparato di combustione per motori a turbina a gas
IT1073329B (it) Ugello di scarico a spinta orientabile particolarmente per turbomotori a gas
IT1054914B (it) Perfezionamenti relativi a motori a turbina a gas
IT1064440B (it) Camere di combustione per motori a turbina a gas
IT989653B (it) Camera di combustione per motori a turbina a gas
IT1096395B (it) Perfezionamenti apportati ai bruciatori di combustibile per motori a turbina a gas
IT7851897A0 (it) Perfezionamento nei filtri per i gas di scarico di motori a combustione
FR2333954A1 (fr) Mecanisme moteur de turbines a gaz
IT1075182B (it) Perfezionamento nelle motrici a turbina a gas
IT1063517B (it) Metodo e apparato per estrarre palette di statore particolarmente di turbomotori a gas
IT1066722B (it) Disposizione di comando di geometria per motori a turbina a gas
IT1064537B (it) Sistemi di accensione a scarica di scintilla per motori a turbina di gas
FR2315611A1 (fr) Moteur-turbine a gaz
IT1132977B (it) Turbina di un turbocompressore dei gas di scarico per motori endotermici
IT1026678B (it) Perfezionamenti relativi a camere di combustione di motori a turbina a gas
IT1065017B (it) Iniettori di combustibile per motori a tureina a gas
IT1098799B (it) Complesso di iniettore di combustibile per un motore a turbina a gas
IT971654B (it) Camera di combustione per turbine a gas e metodo per il funzionamen to della stessa
IT1089612B (it) Apparecchio di combustione per un motore da turbina a gas
IT1031830B (it) Paletta raffreddata per motori a turbina a gas
IT1073112B (it) Perfezionamenti in o relativi a cappotature per motori a turbina a gas
GB1541706A (en) Exhaust nozzles for gas turbine engines
IT1075001B (it) Camere di combustione particolarmente per motori a turbina a gas e metodo per farle funzionare