DE60332173D1 - Kostengünstiger frei beweglicher bund mit verbesserter dichtung und dämpfung für brennkammer - Google Patents

Kostengünstiger frei beweglicher bund mit verbesserter dichtung und dämpfung für brennkammer

Info

Publication number
DE60332173D1
DE60332173D1 DE60332173T DE60332173T DE60332173D1 DE 60332173 D1 DE60332173 D1 DE 60332173D1 DE 60332173 T DE60332173 T DE 60332173T DE 60332173 T DE60332173 T DE 60332173T DE 60332173 D1 DE60332173 D1 DE 60332173D1
Authority
DE
Germany
Prior art keywords
free
cushioning
combustion chamber
improved seal
cost
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 - Lifetime
Application number
DE60332173T
Other languages
English (en)
Inventor
Kenneth Parkman
Saeid Oskooei
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.)
Pratt and Whitney Canada Corp
Original Assignee
Pratt and Whitney Canada Corp
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 Pratt and Whitney Canada Corp filed Critical Pratt and Whitney Canada Corp
Application granted granted Critical
Publication of DE60332173D1 publication Critical patent/DE60332173D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means
    • 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
    • F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00012—Details of sealing devices

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE60332173T 2002-12-18 2003-11-18 Kostengünstiger frei beweglicher bund mit verbesserter dichtung und dämpfung für brennkammer Expired - Lifetime DE60332173D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/321,571 US6880341B2 (en) 2002-12-18 2002-12-18 Low cost combustor floating collar with improved sealing and damping
PCT/CA2003/001768 WO2004055439A1 (en) 2002-12-18 2003-11-18 Low cost combustor floating collar with improved sealing and damping

Publications (1)

Publication Number Publication Date
DE60332173D1 true DE60332173D1 (de) 2010-05-27

Family

ID=32592935

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60332173T Expired - Lifetime DE60332173D1 (de) 2002-12-18 2003-11-18 Kostengünstiger frei beweglicher bund mit verbesserter dichtung und dämpfung für brennkammer

Country Status (6)

Country Link
US (1) US6880341B2 (de)
EP (1) EP1676079B1 (de)
JP (1) JP2006510865A (de)
CA (1) CA2509933C (de)
DE (1) DE60332173D1 (de)
WO (1) WO2004055439A1 (de)

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US7149632B1 (en) * 2003-03-10 2006-12-12 General Electric Company On-line system and method for processing information relating to the wear of turbine components
DE102004010422A1 (de) * 2004-03-01 2005-09-22 Alstom Technology Ltd Dichtungskörper
US7134286B2 (en) * 2004-08-24 2006-11-14 Pratt & Whitney Canada Corp. Gas turbine floating collar arrangement
US7690207B2 (en) * 2004-08-24 2010-04-06 Pratt & Whitney Canada Corp. Gas turbine floating collar arrangement
US7156618B2 (en) * 2004-11-17 2007-01-02 Pratt & Whitney Canada Corp. Low cost diffuser assembly for gas turbine engine
US7533531B2 (en) * 2005-04-01 2009-05-19 Pratt & Whitney Canada Corp. Internal fuel manifold with airblast nozzles
US7500364B2 (en) 2005-11-22 2009-03-10 Honeywell International Inc. System for coupling flow from a centrifugal compressor to an axial combustor for gas turbines
FR2903171B1 (fr) * 2006-06-29 2008-10-17 Snecma Sa Agencement a liaison par crabot pour chambre de combustion de turbomachine
US7966819B2 (en) * 2006-09-26 2011-06-28 Parker-Hannifin Corporation Vibration damper for fuel injector
EP1936276A1 (de) 2006-12-22 2008-06-25 Siemens Aktiengesellschaft Brenner für eine Gasturbine
FR2911666B1 (fr) * 2007-01-18 2009-03-13 Snecma Sa Dispositif d'injection d'un melange d'air et de carburant, chambre de combustion et turbomachine munies d'un tel dispositif
US8769963B2 (en) * 2007-01-30 2014-07-08 Siemens Energy, Inc. Low leakage spring clip/ring combinations for gas turbine engine
US7861530B2 (en) * 2007-03-30 2011-01-04 Pratt & Whitney Canada Corp. Combustor floating collar with louver
US7926280B2 (en) * 2007-05-16 2011-04-19 Pratt & Whitney Canada Corp. Interface between a combustor and fuel nozzle
FR2920032B1 (fr) * 2007-08-13 2014-08-22 Snecma Diffuseur d'une turbomachine
FR2927949B1 (fr) * 2008-02-27 2010-03-26 Snecma Diffuseur de turbomachine comportant des voiles annulaires echancres
US8528336B2 (en) * 2009-03-30 2013-09-10 General Electric Company Fuel nozzle spring support for shifting a natural frequency
DE102009026881A1 (de) * 2009-06-10 2010-12-16 Air-Lng Gmbh Antrieb für eine Turbine nebst Antriebsverfahren
US8689563B2 (en) * 2009-07-13 2014-04-08 United Technologies Corporation Fuel nozzle guide plate mistake proofing
US8215115B2 (en) * 2009-09-28 2012-07-10 Hamilton Sundstrand Corporation Combustor interface sealing arrangement
US8978384B2 (en) 2011-11-23 2015-03-17 General Electric Company Swirler assembly with compressor discharge injection to vane surface
US20130180256A1 (en) * 2012-01-17 2013-07-18 General Electric Company Turbine fuel nozzle assembly and method for operating a turbine
US20130232977A1 (en) * 2012-03-08 2013-09-12 General Electric Company Fuel nozzle and a combustor for a gas turbine
US10378775B2 (en) 2012-03-23 2019-08-13 Pratt & Whitney Canada Corp. Combustor heat shield
US8683805B2 (en) * 2012-08-06 2014-04-01 General Electric Company Injector seal for a gas turbomachine
US10619855B2 (en) * 2012-09-06 2020-04-14 United Technologies Corporation Fuel delivery system with a cavity coupled fuel injector
US9097130B2 (en) 2012-09-13 2015-08-04 General Electric Company Seal for use between injector and combustion chamber in gas turbine
CN105874255B (zh) * 2014-01-09 2018-10-23 通用电气公司 用于管路单元的减振组件
US10161635B2 (en) * 2014-06-13 2018-12-25 Rolls-Royce Corporation Combustor with spring-loaded crossover tubes
EP2957833B1 (de) 2014-06-17 2018-10-24 Rolls-Royce Corporation Brennkammeranordnung mit rinnen
US10041413B2 (en) * 2015-06-05 2018-08-07 General Electric Company Igniter assembly for a gas turbine engine
FR3040765B1 (fr) * 2015-09-09 2017-09-29 Snecma Element d'appui pour amortir des deplacements axiaux de traversee coulissante de systeme d'injection pour turbomachine
CA3024170A1 (en) 2016-06-23 2017-12-28 Hexagon Technology As Boss with internal bearing

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US3703259A (en) * 1971-05-03 1972-11-21 Gen Electric Air blast fuel atomizer
US3879940A (en) 1973-07-30 1975-04-29 Gen Electric Gas turbine engine fuel delivery tube assembly
US3911672A (en) 1974-04-05 1975-10-14 Gen Motors Corp Combustor with ceramic liner
US3910036A (en) 1974-04-05 1975-10-07 Gen Motors Corp Igniter installation for combustor with ceramic liner
US4365470A (en) * 1980-04-02 1982-12-28 United Technologies Corporation Fuel nozzle guide and seal for a gas turbine engine
US4322945A (en) * 1980-04-02 1982-04-06 United Technologies Corporation Fuel nozzle guide heat shield for a gas turbine engine
US4454711A (en) 1981-10-29 1984-06-19 Avco Corporation Self-aligning fuel nozzle assembly
US4606190A (en) * 1982-07-22 1986-08-19 United Technologies Corporation Variable area inlet guide vanes
GB2134640A (en) 1983-02-03 1984-08-15 Rolls Royce Fuel vaporizing device for a gas turbine engine
US4870818A (en) * 1986-04-18 1989-10-03 United Technologies Corporation Fuel nozzle guide structure and retainer for a gas turbine engine
FR2639095B1 (fr) * 1988-11-17 1990-12-21 Snecma Chambre de combustion de turbomachine a bols de prevaporisation montes flottants
US5197290A (en) * 1990-03-26 1993-03-30 Fuel Systems Textron Inc. Variable area combustor air swirler
FR2679010B1 (fr) 1991-07-10 1993-09-24 Snecma Chambre de combustion de turbomachine a bols de prevaporisation demontables.
JP2806103B2 (ja) 1991-10-25 1998-09-30 日産自動車株式会社 ガスタービンの燃焼器
JPH09195799A (ja) 1996-01-17 1997-07-29 Mitsubishi Heavy Ind Ltd 燃焼器のスプリングシール装置
US6199367B1 (en) * 1996-04-26 2001-03-13 General Electric Company Air modulated carburetor with axially moveable fuel injector tip and swirler assembly responsive to fuel pressure
US6351949B1 (en) 1999-09-03 2002-03-05 Allison Advanced Development Company Interchangeable combustor chute
GB2355784B (en) 1999-10-27 2004-05-05 Abb Alstom Power Uk Ltd Gas turbine
US6581386B2 (en) * 2001-09-29 2003-06-24 General Electric Company Threaded combustor baffle

Also Published As

Publication number Publication date
CA2509933C (en) 2010-11-09
WO2004055439A1 (en) 2004-07-01
US6880341B2 (en) 2005-04-19
EP1676079A1 (de) 2006-07-05
JP2006510865A (ja) 2006-03-30
CA2509933A1 (en) 2004-07-01
EP1676079B1 (de) 2010-04-14
US20040118121A1 (en) 2004-06-24

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Legal Events

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8364 No opposition during term of opposition