DE69724532D1 - Führung für eine Brennstoffdüse - Google Patents

Führung für eine Brennstoffdüse

Info

Publication number
DE69724532D1
DE69724532D1 DE69724532T DE69724532T DE69724532D1 DE 69724532 D1 DE69724532 D1 DE 69724532D1 DE 69724532 T DE69724532 T DE 69724532T DE 69724532 T DE69724532 T DE 69724532T DE 69724532 D1 DE69724532 D1 DE 69724532D1
Authority
DE
Germany
Prior art keywords
guide
fuel nozzle
nozzle
fuel
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
DE69724532T
Other languages
English (en)
Other versions
DE69724532T2 (de
Inventor
Randal G Mckinney
Franklin J Davis
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies 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 United Technologies Corp filed Critical United Technologies Corp
Publication of DE69724532D1 publication Critical patent/DE69724532D1/de
Application granted granted Critical
Publication of DE69724532T2 publication Critical patent/DE69724532T2/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
    • F23R3/02—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
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Spray-Type Burners (AREA)
DE69724532T 1996-06-27 1997-06-24 Führung für eine Brennstoffdüse Expired - Lifetime DE69724532T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/671,463 US6032457A (en) 1996-06-27 1996-06-27 Fuel nozzle guide
US671463 1996-06-27

Publications (2)

Publication Number Publication Date
DE69724532D1 true DE69724532D1 (de) 2003-10-09
DE69724532T2 DE69724532T2 (de) 2004-04-08

Family

ID=24694614

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69724532T Expired - Lifetime DE69724532T2 (de) 1996-06-27 1997-06-24 Führung für eine Brennstoffdüse

Country Status (4)

Country Link
US (1) US6032457A (de)
EP (1) EP0816761B1 (de)
JP (1) JPH1061954A (de)
DE (1) DE69724532T2 (de)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6792757B2 (en) 2002-11-05 2004-09-21 Honeywell International Inc. Gas turbine combustor heat shield impingement cooling baffle
US7197877B2 (en) * 2004-08-04 2007-04-03 Siemens Power Generation, Inc. Support system for a pilot nozzle of a turbine engine
FR2894327B1 (fr) * 2005-12-05 2008-05-16 Snecma Sa Dispositif d'injection d'un melange d'air et de carburant, chambre de combustion et turbomachine munies d'un tel dispositif
DE112007002152T5 (de) * 2006-09-14 2009-07-23 Solar Turbines Inc., San Diego Prallplattenkuppelanordnung für einen Turbinenmotor
US7721548B2 (en) * 2006-11-17 2010-05-25 Pratt & Whitney Canada Corp. Combustor liner and heat shield assembly
US7748221B2 (en) * 2006-11-17 2010-07-06 Pratt & Whitney Canada Corp. Combustor heat shield with variable cooling
US7681398B2 (en) * 2006-11-17 2010-03-23 Pratt & Whitney Canada Corp. Combustor liner and heat shield assembly
US20090255118A1 (en) * 2008-04-11 2009-10-15 General Electric Company Method of manufacturing mixers
US20100089020A1 (en) * 2008-10-14 2010-04-15 General Electric Company Metering of diluent flow in combustor
EP2182285A1 (de) * 2008-10-29 2010-05-05 Siemens Aktiengesellschaft Brennereinsatz für eine Gasturbinenbrennkammer und Gasturbine
US8689563B2 (en) * 2009-07-13 2014-04-08 United Technologies Corporation Fuel nozzle guide plate mistake proofing
FR2956724B1 (fr) 2010-02-23 2012-03-16 Snecma Systeme d'injection de carburant pour une chambre de combustion de turbomachine
US9021675B2 (en) 2011-08-15 2015-05-05 United Technologies Corporation Method for repairing fuel nozzle guides for gas turbine engine combustors using cold metal transfer weld technology
WO2014081334A1 (en) * 2012-11-21 2014-05-30 General Electric Company Anti-coking liquid fuel cartridge
US20150033746A1 (en) * 2013-08-02 2015-02-05 Solar Turbines Incorporated Heat shield with standoffs
JP6240327B2 (ja) 2013-11-27 2017-11-29 ゼネラル・エレクトリック・カンパニイ 流体ロックとパージ装置とを有する燃料ノズル
EP3087321B1 (de) 2013-12-23 2020-03-25 General Electric Company Brennstoffdüsestruktur für luftunterstützte brennstoffeinspritzung
WO2015147935A1 (en) 2013-12-23 2015-10-01 General Electric Company Fuel nozzle with flexible support structures
US9534786B2 (en) * 2014-08-08 2017-01-03 Pratt & Whitney Canada Corp. Combustor heat shield
US10670272B2 (en) * 2014-12-11 2020-06-02 Raytheon Technologies Corporation Fuel injector guide(s) for a turbine engine combustor
US10591164B2 (en) 2015-03-12 2020-03-17 General Electric Company Fuel nozzle for a gas turbine engine
US10267521B2 (en) 2015-04-13 2019-04-23 Pratt & Whitney Canada Corp. Combustor heat shield
GB201515883D0 (en) * 2015-09-08 2015-10-21 Rolls Royce Plc Cooling apparatus for a fuel injector
DE102016224632A1 (de) * 2016-12-09 2018-06-14 Rolls-Royce Deutschland Ltd & Co Kg Plattenförmiges Bauteil einer Gasturbine sowie Verfahren zu dessen Herstellung
GB201701380D0 (en) 2016-12-20 2017-03-15 Rolls Royce Plc A combustion chamber and a combustion chamber fuel injector seal
US10851996B2 (en) * 2018-07-06 2020-12-01 Rolls-Royce North American Technologies Inc. Turbulators for cooling heat shield of a combustor
US20200309373A1 (en) * 2019-03-25 2020-10-01 United Technologies Corporation Aftermarket repair process for a fuel nozzle guide heat shield of a gas turbine engine
US11603799B2 (en) 2020-12-22 2023-03-14 General Electric Company Combustor for a gas turbine engine

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3273343A (en) * 1965-03-08 1966-09-20 Dickens Inc Combustion chamber construction in gas turbine power plant
US3451215A (en) * 1967-04-03 1969-06-24 Gen Electric Fluid impingement starting means
US3589127A (en) * 1969-02-04 1971-06-29 Gen Electric Combustion apparatus
US3914348A (en) * 1974-02-25 1975-10-21 Aerojet General Co Platelet-venturi carburetor for combustion engine
US4322945A (en) * 1980-04-02 1982-04-06 United Technologies Corporation Fuel nozzle guide heat shield for a gas turbine engine
US4365470A (en) * 1980-04-02 1982-12-28 United Technologies Corporation Fuel nozzle guide and seal for a gas turbine engine
GB2135440B (en) * 1983-02-19 1986-06-25 Rolls Royce Mounting combustion chambers
US4870818A (en) * 1986-04-18 1989-10-03 United Technologies Corporation Fuel nozzle guide structure and retainer for a gas turbine engine
US4686823A (en) * 1986-04-28 1987-08-18 United Technologies Corporation Sliding joint for an annular combustor
US4914918A (en) * 1988-09-26 1990-04-10 United Technologies Corporation Combustor segmented deflector
US4934145A (en) * 1988-10-12 1990-06-19 United Technologies Corporation Combustor bulkhead heat shield assembly
FR2639095B1 (fr) * 1988-11-17 1990-12-21 Snecma Chambre de combustion de turbomachine a bols de prevaporisation montes flottants
US5157914A (en) * 1990-12-27 1992-10-27 United Technologies Corporation Modulated gas turbine cooling air
FR2679010B1 (fr) * 1991-07-10 1993-09-24 Snecma Chambre de combustion de turbomachine a bols de prevaporisation demontables.
US5255508A (en) * 1991-11-01 1993-10-26 United Technologies Corporation Fuel nozzle assembly and method for making the assembly
US5430935A (en) * 1993-07-14 1995-07-11 Yaworsky; Chester E. Method for repairing a combustion chamber assembly
US5463864A (en) * 1993-12-27 1995-11-07 United Technologies Corporation Fuel nozzle guide for a gas turbine engine combustor
US5419115A (en) * 1994-04-29 1995-05-30 United Technologies Corporation Bulkhead and fuel nozzle guide assembly for an annular combustion chamber

Also Published As

Publication number Publication date
EP0816761A3 (de) 1999-10-06
JPH1061954A (ja) 1998-03-06
EP0816761A2 (de) 1998-01-07
DE69724532T2 (de) 2004-04-08
EP0816761B1 (de) 2003-09-03
US6032457A (en) 2000-03-07

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition