IT1111808B - Perfezionamenti apportati ai dispositivi di combustione di motori a turbina a gas - Google Patents

Perfezionamenti apportati ai dispositivi di combustione di motori a turbina a gas

Info

Publication number
IT1111808B
IT1111808B IT2053879A IT2053879A IT1111808B IT 1111808 B IT1111808 B IT 1111808B IT 2053879 A IT2053879 A IT 2053879A IT 2053879 A IT2053879 A IT 2053879A IT 1111808 B IT1111808 B IT 1111808B
Authority
IT
Italy
Prior art keywords
gas turbine
turbine engines
combustion devices
combustion
devices
Prior art date
Application number
IT2053879A
Other languages
English (en)
Other versions
IT7920538D0 (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
Priority to GB1189378 priority Critical
Application filed by Rolls Royce filed Critical Rolls Royce
Publication of IT7920538D0 publication Critical patent/IT7920538D0/it
Application granted granted Critical
Publication of IT1111808B publication Critical patent/IT1111808B/it

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/10Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
    • F23D11/12Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour characterised by the shape or arrangement of the outlets from the nozzle
    • 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
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
IT2053879A 1978-03-28 1979-02-26 Perfezionamenti apportati ai dispositivi di combustione di motori a turbina a gas IT1111808B (it)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1189378 1978-03-28

Publications (2)

Publication Number Publication Date
IT7920538D0 IT7920538D0 (it) 1979-02-26
IT1111808B true IT1111808B (it) 1986-01-13

Family

ID=9994594

Family Applications (1)

Application Number Title Priority Date Filing Date
IT2053879A IT1111808B (it) 1978-03-28 1979-02-26 Perfezionamenti apportati ai dispositivi di combustione di motori a turbina a gas

Country Status (5)

Country Link
US (1) US4237694A (it)
JP (1) JPS5857656B2 (it)
DE (1) DE2912103C2 (it)
FR (1) FR2421342A1 (it)
IT (1) IT1111808B (it)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1595224A (en) * 1977-02-04 1981-08-12 Rolls Royce Combustion equipment for gas turbine engines
JPS6228369B2 (it) * 1980-06-30 1987-06-19 Hitachi Ltd
US4389848A (en) * 1981-01-12 1983-06-28 United Technologies Corporation Burner construction for gas turbines
GB2093584B (en) * 1981-02-21 1984-12-19 Rolls Royce Improvements in or relating to fuel burners and combustion equipment for use in gas turbine engines
JPH0370128B2 (it) * 1981-05-12 1991-11-06 Hitachi Ltd
JPH0480292B2 (it) * 1983-03-22 1992-12-18 Hitachi Ltd
US5339635A (en) * 1987-09-04 1994-08-23 Hitachi, Ltd. Gas turbine combustor of the completely premixed combustion type
US4903492A (en) * 1988-09-07 1990-02-27 The United States Of America As Represented By The Secretary Of The Air Force Dilution air dispensing apparatus
US5085039A (en) * 1989-12-07 1992-02-04 Sundstrand Corporation Coanda phenomena combustor for a turbine engine
US5205117A (en) * 1989-12-21 1993-04-27 Sundstrand Corporation High altitude starting two-stage fuel injection
US5261224A (en) * 1989-12-21 1993-11-16 Sundstrand Corporation High altitude starting two-stage fuel injection apparatus
US5284019A (en) * 1990-06-12 1994-02-08 The United States Of America As Represented By The Secretary Of The Air Force Double dome, single anular combustor with daisy mixer
US5142858A (en) * 1990-11-21 1992-09-01 General Electric Company Compact flameholder type combustor which is staged to reduce emissions
US5251447A (en) * 1992-10-01 1993-10-12 General Electric Company Air fuel mixer for gas turbine combustor
US5351477A (en) * 1993-12-21 1994-10-04 General Electric Company Dual fuel mixer for gas turbine combustor
FR2727192B1 (fr) 1994-11-23 1996-12-20 Snecma Systeme d'injection d'une chambre de combustion a deux tetes
US6240731B1 (en) * 1997-12-31 2001-06-05 United Technologies Corporation Low NOx combustor for gas turbine engine
DE59912076D1 (de) * 1998-08-31 2005-06-23 Siemens Ag Brenneranordnung
DE10219354A1 (de) * 2002-04-30 2003-11-13 Rolls Royce Deutschland Gasturbinenbrennkammer mit gezielter Kraftstoffeinbringung zur Verbesserung der Homogenität des Kraftstoff-Luft-Gemisches
WO2009022449A1 (ja) * 2007-08-10 2009-02-19 Kawasaki Jukogyo Kabushiki Kaisha 燃焼装置
DE102007043626A1 (de) * 2007-09-13 2009-03-19 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenmagerbrenner mit Kraftstoffdüse mit kontrollierter Kraftstoffinhomogenität
RU2452896C2 (ru) * 2009-07-27 2012-06-10 Виталий Алексеевич Алтунин Головка кольцевой камеры сгорания газотурбинного двигателя
US8925325B2 (en) * 2011-03-18 2015-01-06 Delavan Inc. Recirculating product injection nozzle

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE503026A (it) * 1950-07-17
GB1136543A (en) * 1966-02-21 1968-12-11 Rolls Royce Liquid fuel combustion apparatus for gas turbine engines
US3713588A (en) * 1970-11-27 1973-01-30 Gen Motors Corp Liquid fuel spray nozzles with air atomization
GB1380931A (en) * 1971-01-11 1975-01-15 Lefebvre A H Methods of liquid fuel injection and to airblast atomizers
US3703259A (en) * 1971-05-03 1972-11-21 Gen Electric Air blast fuel atomizer
SE371685B (it) * 1972-04-21 1974-11-25 Stal Laval Turbin Ab
US3917173A (en) * 1972-04-21 1975-11-04 Stal Laval Turbin Ab Atomizing apparatus for finely distributing a liquid in an air stream
GB1427146A (en) * 1972-09-07 1976-03-10 Rolls Royce Combustion apparatus for gas turbine engines
FR2330871B2 (it) * 1972-11-13 1980-12-12 Snecma
US3811278A (en) * 1973-02-01 1974-05-21 Gen Electric Fuel injection apparatus
FR2249243B2 (it) * 1973-10-26 1978-09-15 Snecma
FR2269646B1 (it) * 1974-04-30 1976-12-17 Snecma
US3905192A (en) * 1974-08-29 1975-09-16 United Aircraft Corp Combustor having staged premixing tubes
JPS5254825A (en) * 1975-10-31 1977-05-04 Hitachi Ltd Gas turbine combustor
JPS5637418B2 (it) * 1977-10-07 1981-08-31

Also Published As

Publication number Publication date
FR2421342A1 (fr) 1979-10-26
DE2912103C2 (it) 1985-01-10
JPS54134207A (en) 1979-10-18
JPS5857656B2 (it) 1983-12-21
DE2912103A1 (de) 1979-10-11
US4237694A (en) 1980-12-09
IT7920538D0 (it) 1979-02-26

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