IT1110188B - Perfezionamenti apportati alle apparecchiature di combustione - Google Patents

Perfezionamenti apportati alle apparecchiature di combustione

Info

Publication number
IT1110188B
IT1110188B IT19837/78A IT1983778A IT1110188B IT 1110188 B IT1110188 B IT 1110188B IT 19837/78 A IT19837/78 A IT 19837/78A IT 1983778 A IT1983778 A IT 1983778A IT 1110188 B IT1110188 B IT 1110188B
Authority
IT
Italy
Prior art keywords
combustion equipment
refinements made
refinements
combustion
equipment
Prior art date
Application number
IT19837/78A
Other languages
English (en)
Other versions
IT7819837A0 (it
Original Assignee
Rolls Royce
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 Rolls Royce filed Critical Rolls Royce
Publication of IT7819837A0 publication Critical patent/IT7819837A0/it
Application granted granted Critical
Publication of IT1110188B publication Critical patent/IT1110188B/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
    • F23R3/02—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
    • 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

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)
  • Turbine Rotor Nozzle Sealing (AREA)
IT19837/78A 1977-02-04 1978-01-31 Perfezionamenti apportati alle apparecchiature di combustione IT1110188B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4558/77A GB1595224A (en) 1977-02-04 1977-02-04 Combustion equipment for gas turbine engines

Publications (2)

Publication Number Publication Date
IT7819837A0 IT7819837A0 (it) 1978-01-31
IT1110188B true IT1110188B (it) 1985-12-23

Family

ID=9779428

Family Applications (1)

Application Number Title Priority Date Filing Date
IT19837/78A IT1110188B (it) 1977-02-04 1978-01-31 Perfezionamenti apportati alle apparecchiature di combustione

Country Status (6)

Country Link
US (1) US4373342A (it)
JP (1) JPS53122004A (it)
DE (1) DE2804144A1 (it)
FR (1) FR2379698A1 (it)
GB (1) GB1595224A (it)
IT (1) IT1110188B (it)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4445338A (en) * 1981-10-23 1984-05-01 The United States Of America As Represented By The Secretary Of The Navy Swirler assembly for a vorbix augmentor
GB2109532B (en) * 1981-11-07 1985-01-03 Rolls Royce Gas fuel injector
US5220786A (en) * 1991-03-08 1993-06-22 General Electric Company Thermally protected venturi for combustor dome
US5239832A (en) * 1991-12-26 1993-08-31 General Electric Company Birdstrike resistant swirler support for combustion chamber dome
US5274995A (en) * 1992-04-27 1994-01-04 General Electric Company Apparatus and method for atomizing water in a combustor dome assembly
US5323604A (en) * 1992-11-16 1994-06-28 General Electric Company Triple annular combustor for gas turbine engine
US5303542A (en) * 1992-11-16 1994-04-19 General Electric Company Fuel supply control method for a gas turbine engine
US5289685A (en) * 1992-11-16 1994-03-01 General Electric Company Fuel supply system for a gas turbine engine
DE4432558A1 (de) * 1994-09-13 1996-03-14 Bmw Rolls Royce Gmbh Gasturbinen-Brennkammer mit Hitzeschild
US6082111A (en) * 1998-06-11 2000-07-04 Siemens Westinghouse Power Corporation Annular premix section for dry low-NOx combustors
EP1125087B1 (de) 1998-08-31 2005-05-18 Siemens Aktiengesellschaft Brenneranordnung
US6279323B1 (en) * 1999-11-01 2001-08-28 General Electric Company Low emissions combustor
US6286300B1 (en) 2000-01-27 2001-09-11 Honeywell International Inc. Combustor with fuel preparation chambers

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB579424A (en) * 1943-09-29 1946-08-02 Lucas Ltd Joseph Improvements relating to liquid fuel combustion apparatus for generating gases for power purposes
US2517015A (en) * 1945-05-16 1950-08-01 Bendix Aviat Corp Combustion chamber with shielded fuel nozzle
FR944310A (fr) * 1946-01-09 1949-04-01 Bendix Aviat Corp Brûleurs
US2616257A (en) * 1946-01-09 1952-11-04 Bendix Aviat Corp Combustion chamber with air inlet means providing a plurality of concentric strata of varying velocities
CH362883A (de) * 1958-08-26 1962-06-30 Schweizerische Lokomotiv Brennkammer, insbesondere für Gasturbinen
GB1136543A (en) * 1966-02-21 1968-12-11 Rolls Royce Liquid fuel combustion apparatus for gas turbine engines
US3403510A (en) * 1966-11-23 1968-10-01 United Aircraft Corp Removable and replaceable fuel nozzle holder assembly for an annular combustion burner
US3385055A (en) * 1966-11-23 1968-05-28 United Aircraft Corp Combustion chamber with floating swirler rings
JPS4931059Y1 (it) * 1970-11-30 1974-08-22
US3703259A (en) * 1971-05-03 1972-11-21 Gen Electric Air blast fuel atomizer
US3768250A (en) * 1971-12-01 1973-10-30 Mitsubishi Heavy Ind Ltd Combustion apparatus for a gas turbine
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
US3901446A (en) * 1974-05-09 1975-08-26 Us Air Force Induced vortex swirler
JPS5236881Y2 (it) * 1974-12-25 1977-08-23
US4044553A (en) * 1976-08-16 1977-08-30 General Motors Corporation Variable geometry swirler
IT1111808B (it) * 1978-03-28 1986-01-13 Rolls Royce Perfezionamenti apportati ai dispositivi di combustione di motori a turbina a gas

Also Published As

Publication number Publication date
FR2379698B1 (it) 1983-03-18
JPS53122004A (en) 1978-10-25
IT7819837A0 (it) 1978-01-31
FR2379698A1 (fr) 1978-09-01
DE2804144A1 (de) 1978-08-10
JPS619537B2 (it) 1986-03-24
US4373342A (en) 1983-02-15
GB1595224A (en) 1981-08-12

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