MX349279B - Método y aparato para rayo inyector de líquido estampado. - Google Patents

Método y aparato para rayo inyector de líquido estampado.

Info

Publication number
MX349279B
MX349279B MX2014008029A MX2014008029A MX349279B MX 349279 B MX349279 B MX 349279B MX 2014008029 A MX2014008029 A MX 2014008029A MX 2014008029 A MX2014008029 A MX 2014008029A MX 349279 B MX349279 B MX 349279B
Authority
MX
Mexico
Prior art keywords
spoke
swaged
head
fuel injection
liquid fuel
Prior art date
Application number
MX2014008029A
Other languages
English (en)
Other versions
MX2014008029A (es
Inventor
Alexander Ilich Krichever
Mario Eugene Abreu
Norm Turoff
John Frederick Lockyer
Christopher Zdzislaw Twardochleb
David Marc Stansel
Original Assignee
Solar Turbines Inc
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 Solar Turbines Inc filed Critical Solar Turbines Inc
Publication of MX2014008029A publication Critical patent/MX2014008029A/es
Publication of MX349279B publication Critical patent/MX349279B/es

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
    • B21K25/00—Uniting components to form integral members, e.g. turbine wheels and shafts, caulks with inserts, with or without shaping of the components
    • 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
    • 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
    • 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
    • F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • 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
    • F23R2900/00005—Preventing fatigue failures or reducing mechanical stress in gas turbine components
    • 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
    • F23R2900/00017—Assembling combustion chamber liners or subparts
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49229—Prime mover or fluid pump making
    • Y10T29/49231—I.C. [internal combustion] engine making

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Forging (AREA)

Abstract

Se proporciona un rayo de inyección de combustible líquido (24) para un motor de turbina de gas; el rayo de inyección de combustible líquido (24) puede incluir un extremo de entrada y un extremo de salida; el rayo de inyección de combustible líquido (24) además puede incluir un cabezal (30) ubicado en el extremo de entrada y un tallo (32) que se extiende a lo largo de un eje longitudinal (A) desde el cabezal (30) hasta el extremo de salida; el tallo (32) puede definir un pasaje de fluido (34) en el mismo; el cabezal puede incluir una cavidad (36) con una pared interior (40); la pared interior (40) puede incluir una saliente anular (46).
MX2014008029A 2011-12-29 2012-12-14 Método y aparato para rayo inyector de líquido estampado. MX349279B (es)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201161581539P 2011-12-29 2011-12-29
US13/560,192 US9296038B2 (en) 2011-12-29 2012-07-27 Method and apparatus for swaged liquid injector spoke
PCT/US2012/069806 WO2013101506A1 (en) 2011-12-29 2012-12-14 Method and apparatus for swaged liquid injector spoke

Publications (2)

Publication Number Publication Date
MX2014008029A MX2014008029A (es) 2014-08-21
MX349279B true MX349279B (es) 2017-07-20

Family

ID=48694057

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2014008029A MX349279B (es) 2011-12-29 2012-12-14 Método y aparato para rayo inyector de líquido estampado.

Country Status (5)

Country Link
US (1) US9296038B2 (es)
CN (1) CN104024602B (es)
DE (1) DE112012005537T5 (es)
MX (1) MX349279B (es)
WO (1) WO2013101506A1 (es)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6301774B2 (ja) * 2014-08-01 2018-03-28 三菱日立パワーシステムズ株式会社 ガスタービン燃焼器
WO2016121475A1 (ja) * 2015-01-30 2016-08-04 日立オートモティブシステムズ株式会社 燃料噴射弁
US20230235702A1 (en) * 2022-01-21 2023-07-27 Delavan Inc. Connecting fuel injectors and nozzles to manifolds
US11852076B2 (en) 2022-01-21 2023-12-26 Collins Engine Nozzles, Inc. Brazing using localized heating
US11859544B1 (en) * 2022-06-16 2024-01-02 Solar Turbines Incorporated Turbine exhaust gas recirculation mixer box

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4028888A (en) * 1974-05-03 1977-06-14 Norwalk-Turbo Inc. Fuel distribution manifold to an annular combustion chamber
US5467926A (en) 1994-02-10 1995-11-21 Solar Turbines Incorporated Injector having low tip temperature
US5613363A (en) 1994-09-26 1997-03-25 General Electric Company Air fuel mixer for gas turbine combustor
US5822992A (en) 1995-10-19 1998-10-20 General Electric Company Low emissions combustor premixer
US5826429A (en) * 1995-12-22 1998-10-27 General Electric Co. Catalytic combustor with lean direct injection of gas fuel for low emissions combustion and methods of operation
US5680765A (en) 1996-01-05 1997-10-28 Choi; Kyung J. Lean direct wall fuel injection method and devices
US6238206B1 (en) 1997-05-13 2001-05-29 Maxon Corporation Low-emissions industrial burner
EP0911583B1 (de) 1997-10-27 2003-03-12 ALSTOM (Switzerland) Ltd Verfahren zum Betrieb eines Vormischbrenners
US6763663B2 (en) 2001-07-11 2004-07-20 Parker-Hannifin Corporation Injector with active cooling
US6868676B1 (en) * 2002-12-20 2005-03-22 General Electric Company Turbine containing system and an injector therefor
JP2005201613A (ja) 2004-01-13 2005-07-28 Tadao Hirokawa 液体燃料用火口
US7703288B2 (en) 2005-09-30 2010-04-27 Solar Turbines Inc. Fuel nozzle having swirler-integrated radial fuel jet
US20070074571A1 (en) 2005-10-03 2007-04-05 Haynes Kevin M Ultrasonic sensor self test
US8387398B2 (en) * 2007-09-14 2013-03-05 Siemens Energy, Inc. Apparatus and method for controlling the secondary injection of fuel
US8099940B2 (en) 2008-12-18 2012-01-24 Solar Turbines Inc. Low cross-talk gas turbine fuel injector
EP2282115A1 (en) 2009-07-30 2011-02-09 Alstom Technology Ltd Burner of a gas turbine

Also Published As

Publication number Publication date
CN104024602B (zh) 2017-03-08
US20130168472A1 (en) 2013-07-04
US9296038B2 (en) 2016-03-29
DE112012005537T5 (de) 2014-09-18
MX2014008029A (es) 2014-08-21
WO2013101506A1 (en) 2013-07-04
CN104024602A (zh) 2014-09-03

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