DE69312362T2 - Brennkammer mit Verdünnungsleitschaufeln - Google Patents

Brennkammer mit Verdünnungsleitschaufeln

Info

Publication number
DE69312362T2
DE69312362T2 DE69312362T DE69312362T DE69312362T2 DE 69312362 T2 DE69312362 T2 DE 69312362T2 DE 69312362 T DE69312362 T DE 69312362T DE 69312362 T DE69312362 T DE 69312362T DE 69312362 T2 DE69312362 T2 DE 69312362T2
Authority
DE
Germany
Prior art keywords
combustion chamber
guide vanes
dilution
dilution guide
vanes
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 - Fee Related
Application number
DE69312362T
Other languages
English (en)
Other versions
DE69312362D1 (de
Inventor
Richard Wade Stickles
Willard James Dodds
Paul Edward Sabla
George Edward Cook
Craig Louis Loconti
Gary Mac Holloway
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 DE69312362D1 publication Critical patent/DE69312362D1/de
Application granted granted Critical
Publication of DE69312362T2 publication Critical patent/DE69312362T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • 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
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
DE69312362T 1992-03-30 1993-03-26 Brennkammer mit Verdünnungsleitschaufeln Expired - Fee Related DE69312362T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/860,635 US5239818A (en) 1992-03-30 1992-03-30 Dilution pole combustor and method

Publications (2)

Publication Number Publication Date
DE69312362D1 DE69312362D1 (de) 1997-08-28
DE69312362T2 true DE69312362T2 (de) 1998-02-19

Family

ID=25333651

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69312362T Expired - Fee Related DE69312362T2 (de) 1992-03-30 1993-03-26 Brennkammer mit Verdünnungsleitschaufeln

Country Status (5)

Country Link
US (1) US5239818A (de)
EP (1) EP0564183B1 (de)
JP (1) JPH0788947B2 (de)
CA (1) CA2089296A1 (de)
DE (1) DE69312362T2 (de)

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ES2117402T3 (es) * 1994-01-24 1998-08-01 Siemens Ag Procedimiento para la combustion de un combustible en aire comprimido.
JPH09511321A (ja) * 1994-03-04 1997-11-11 ボルボ エアロ コーポレイション 保炎器
US5526640A (en) * 1994-05-16 1996-06-18 Technical Directions, Inc. Gas turbine engine including a bearing support tube cantilevered from a turbine nozzle wall
DE19651881A1 (de) * 1996-12-13 1998-06-18 Asea Brown Boveri Brennkammer mit integrierten Leitschaufeln
US6240731B1 (en) * 1997-12-31 2001-06-05 United Technologies Corporation Low NOx combustor for gas turbine engine
DE10062253A1 (de) * 2000-12-14 2002-06-20 Rolls Royce Deutschland Fluggasturbine mit Brennraum mit Festkörpergerüst
FR2825779B1 (fr) 2001-06-06 2003-08-29 Snecma Moteurs Chambre de combustion munie d'un systeme de fixation de fond de chambre
CA2399534C (en) * 2001-08-31 2007-01-02 Mitsubishi Heavy Industries, Ltd. Gasturbine and the combustor thereof
DE10214574A1 (de) * 2002-04-02 2003-10-16 Rolls Royce Deutschland Brennkammer für ein Luftstrahltriebwerk mit Sekundärluftzuführung
US7044009B2 (en) * 2002-05-20 2006-05-16 Caterpillar Inc. Dilution tunnel
JP3978086B2 (ja) * 2002-05-31 2007-09-19 三菱重工業株式会社 航空機用ガスタービンシステム，及びガスタービンシステム並びにその動作方法
US7093441B2 (en) * 2003-10-09 2006-08-22 United Technologies Corporation Gas turbine annular combustor having a first converging volume and a second converging volume, converging less gradually than the first converging volume
WO2006053825A1 (de) * 2004-11-16 2006-05-26 Alstom Technology Ltd Gasturbinenanlage und zugehörige brennkammer
US20060130486A1 (en) * 2004-12-17 2006-06-22 Danis Allen M Method and apparatus for assembling gas turbine engine combustors
EP1703208B1 (de) * 2005-02-04 2007-07-11 Enel Produzione S.p.A. Dämpfung von thermoakustischen Schwingungen in einer Gasturbinenbrennkammer mit ringförmiger Kammer
EP1847778A1 (de) * 2006-04-21 2007-10-24 Siemens Aktiengesellschaft Vormischverbrennungsanlage für Gasturbine und Verfahren zum Betrieb
US7874138B2 (en) * 2008-09-11 2011-01-25 Siemens Energy, Inc. Segmented annular combustor
US9068751B2 (en) * 2010-01-29 2015-06-30 United Technologies Corporation Gas turbine combustor with staged combustion
US8769955B2 (en) 2010-06-02 2014-07-08 Siemens Energy, Inc. Self-regulating fuel staging port for turbine combustor
DE102012015449A1 (de) * 2012-08-03 2014-02-20 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenbrennkammer mit Mischluftöffnungen und Luftleitelementen in modularer Bauweise
US9482432B2 (en) * 2012-09-26 2016-11-01 United Technologies Corporation Gas turbine engine combustor with integrated combustor vane having swirler
US9404654B2 (en) * 2012-09-26 2016-08-02 United Technologies Corporation Gas turbine engine combustor with integrated combustor vane
US9335050B2 (en) * 2012-09-26 2016-05-10 United Technologies Corporation Gas turbine engine combustor
US20140366544A1 (en) * 2013-06-13 2014-12-18 Pratt & Whitney Canada Corp. Combustor exit duct for gas turbine engines
EP3084303B1 (de) * 2013-12-19 2022-01-26 Raytheon Technologies Corporation Thermomechanische vertiefungsanordnung für eine brennkammerwandanordnung
EP3087266B1 (de) * 2013-12-23 2019-10-09 United Technologies Corporation Mehrfach durchströmte verdünnungsöffnungskonfiguration für einen gasturbinenmotor und betriebsverfahren
FR3019587B1 (fr) * 2014-04-03 2019-09-13 Safran Helicopter Engines Tuyau de dilution pour chambre de combustion et chambre de combustion associee.
US10054314B2 (en) * 2015-12-17 2018-08-21 General Electric Company Slotted injector for axial fuel staging
US11428413B2 (en) 2016-03-25 2022-08-30 General Electric Company Fuel injection module for segmented annular combustion system
US10641491B2 (en) * 2016-03-25 2020-05-05 General Electric Company Cooling of integrated combustor nozzle of segmented annular combustion system
US10563869B2 (en) 2016-03-25 2020-02-18 General Electric Company Operation and turndown of a segmented annular combustion system
US10584876B2 (en) * 2016-03-25 2020-03-10 General Electric Company Micro-channel cooling of integrated combustor nozzle of a segmented annular combustion system
US10520194B2 (en) 2016-03-25 2019-12-31 General Electric Company Radially stacked fuel injection module for a segmented annular combustion system
US10605459B2 (en) * 2016-03-25 2020-03-31 General Electric Company Integrated combustor nozzle for a segmented annular combustion system
US10584880B2 (en) * 2016-03-25 2020-03-10 General Electric Company Mounting of integrated combustor nozzles in a segmented annular combustion system
US10830442B2 (en) 2016-03-25 2020-11-10 General Electric Company Segmented annular combustion system with dual fuel capability
US10641176B2 (en) * 2016-03-25 2020-05-05 General Electric Company Combustion system with panel fuel injector
US10690350B2 (en) 2016-11-28 2020-06-23 General Electric Company Combustor with axially staged fuel injection
US11156362B2 (en) 2016-11-28 2021-10-26 General Electric Company Combustor with axially staged fuel injection
EP3418638B1 (de) * 2017-06-21 2021-03-24 General Electric Company Brennkammer mit wärmetauscher
US10816202B2 (en) 2017-11-28 2020-10-27 General Electric Company Combustor liner for a gas turbine engine and an associated method thereof
US11181005B2 (en) * 2018-05-18 2021-11-23 Raytheon Technologies Corporation Gas turbine engine assembly with mid-vane outer platform gap
FR3094777B1 (fr) * 2019-04-04 2021-06-25 Safran Aircraft Engines Chambre de combustion principale de turboréacteur équipée d’une grille en aval de ses bruleurs
US11614233B2 (en) 2020-08-31 2023-03-28 General Electric Company Impingement panel support structure and method of manufacture
US11994293B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus support structure and method of manufacture
US11460191B2 (en) * 2020-08-31 2022-10-04 General Electric Company Cooling insert for a turbomachine
US11371702B2 (en) 2020-08-31 2022-06-28 General Electric Company Impingement panel for a turbomachine
US11994292B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus for turbomachine
US11255545B1 (en) 2020-10-26 2022-02-22 General Electric Company Integrated combustion nozzle having a unified head end
GB202112642D0 (en) * 2021-09-06 2021-10-20 Rolls Royce Plc Controlling soot
US11767766B1 (en) 2022-07-29 2023-09-26 General Electric Company Turbomachine airfoil having impingement cooling passages

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL108658C (de) * 1958-07-31
US3316714A (en) * 1963-06-20 1967-05-02 Rolls Royce Gas turbine engine combustion equipment
DE1252470B (de) * 1964-08-14 1967-10-19 Bordes Joseph Szydlowski (Frankreich) Ringförmige Brennkammer, insbesondere für Gasturbinentriebwerke
GB1034260A (en) * 1964-12-02 1966-06-29 Rolls Royce Aerofoil-shaped blade for use in a fluid flow machine
US3608310A (en) * 1966-06-27 1971-09-28 Gen Motors Corp Turbine stator-combustor structure
US3460345A (en) * 1967-12-28 1969-08-12 Lucas Industries Ltd Combustion apparatus for gas turbine engines
US4226083A (en) * 1978-01-19 1980-10-07 United Technologies Corporation Method and apparatus for reducing nitrous oxide emissions from combustors
US4292801A (en) * 1979-07-11 1981-10-06 General Electric Company Dual stage-dual mode low nox combustor
US4445339A (en) * 1980-11-24 1984-05-01 General Electric Co. Wingtip vortex flame stabilizer for gas turbine combustor flame holder
US4698963A (en) * 1981-04-22 1987-10-13 The United States Of America As Represented By The Department Of Energy Low NOx combustor
US4819438A (en) * 1982-12-23 1989-04-11 United States Of America Steam cooled rich-burn combustor liner
US4984429A (en) * 1986-11-25 1991-01-15 General Electric Company Impingement cooled liner for dry low NOx venturi combustor
DE3811293A1 (de) * 1988-04-02 1989-10-12 Asea Brown Boveri Brennkammer einer gasturbine

Also Published As

Publication number Publication date
JPH0618034A (ja) 1994-01-25
JPH0788947B2 (ja) 1995-09-27
US5239818A (en) 1993-08-31
CA2089296A1 (en) 1993-10-01
EP0564183A1 (de) 1993-10-06
DE69312362D1 (de) 1997-08-28
EP0564183B1 (de) 1997-07-23

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee