MX2010003082A - Camara de combustion. - Google Patents

Camara de combustion.

Info

Publication number
MX2010003082A
MX2010003082A MX2010003082A MX2010003082A MX2010003082A MX 2010003082 A MX2010003082 A MX 2010003082A MX 2010003082 A MX2010003082 A MX 2010003082A MX 2010003082 A MX2010003082 A MX 2010003082A MX 2010003082 A MX2010003082 A MX 2010003082A
Authority
MX
Mexico
Prior art keywords
sliding
wall portion
combustion chamber
sliding wall
inner casing
Prior art date
Application number
MX2010003082A
Other languages
English (en)
Inventor
Glynn Milner
Original Assignee
Siemens Ag
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 Siemens Ag filed Critical Siemens Ag
Publication of MX2010003082A publication Critical patent/MX2010003082A/es

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
    • F23R3/06—Arrangement of apertures along the flame tube
    • 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
    • F23R3/002—Wall structures
    • 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
    • F23R3/26—Controlling the air 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
    • F23R3/42—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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03044—Impingement cooled combustion chamber walls or subassemblies

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)
  • Gas Burners (AREA)
  • Portable Nailing Machines And Staplers (AREA)

Abstract

Se proporciona una c?mara de combusti?n (1), que comprende una carcasa interna (2) con una superficie deslizante (23) y una carcasa externa (3) con una porci?n de pared deslizante (21). La superficie deslizante (23) y la porci?n de la pared deslizante (21) se unen de manera deslizable una a la otra. Ubica por lo menos un agujero de refrigeraci?n (11) en la porci?n de pared deslizante (21). El agujero de refrigeraci?n (11) se ubica por lo menos parcialmente de tal manera que la porci?n de pared deslizante (21) se abre debido a un movimiento deslizante de la superficie deslizante (23) con relaci?n a la porci?n de pared deslizante (21) cuando la carcasa interna (2) se expande t?rmicamente y/o se cierra debido a un movimiento deslizante de la superficie deslizante (23) con relaci?n a la porci?n de pared deslizante (21) cuando la carcasa interna (2) se contrae t?rmicamente. M?s a?n, se describe una turbina de gas que comprende una c?mara de combusti?n de la invenci?n.
MX2010003082A 2007-09-24 2008-09-05 Camara de combustion. MX2010003082A (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP07018754A EP2039999A1 (en) 2007-09-24 2007-09-24 Combustion chamber
PCT/EP2008/061801 WO2009040232A1 (en) 2007-09-24 2008-09-05 Combustion chamber

Publications (1)

Publication Number Publication Date
MX2010003082A true MX2010003082A (es) 2010-04-12

Family

ID=38835038

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2010003082A MX2010003082A (es) 2007-09-24 2008-09-05 Camara de combustion.

Country Status (7)

Country Link
US (1) US8156724B2 (es)
EP (1) EP2039999A1 (es)
CN (1) CN101809370B (es)
CA (1) CA2700300A1 (es)
MX (1) MX2010003082A (es)
RU (1) RU2470227C2 (es)
WO (1) WO2009040232A1 (es)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5537895B2 (ja) * 2009-10-21 2014-07-02 川崎重工業株式会社 ガスタービン燃焼器
JP2012202258A (ja) * 2011-03-24 2012-10-22 Mitsubishi Heavy Ind Ltd 冷却装置、燃焼器およびガスタービン
US8893382B2 (en) * 2011-09-30 2014-11-25 General Electric Company Combustion system and method of assembling the same
US9115669B2 (en) 2011-10-28 2015-08-25 United Technologies Corporation Gas turbine engine exhaust nozzle cooling valve
JP2013100765A (ja) * 2011-11-08 2013-05-23 Ihi Corp インピンジ冷却機構、タービン翼及び燃焼器
US9657949B2 (en) 2012-10-15 2017-05-23 Pratt & Whitney Canada Corp. Combustor skin assembly for gas turbine engine
CN107013942A (zh) * 2017-05-17 2017-08-04 大连海事大学 预混合低旋流喷嘴的燃气轮机燃烧室
CN107781847B (zh) * 2017-09-22 2023-04-11 中国华能集团公司 双气体燃料的燃烧器及采用该燃烧器的燃气轮机运行方法
JP7191723B2 (ja) * 2019-02-27 2022-12-19 三菱重工業株式会社 ガスタービン燃焼器及びガスタービン
US11415046B1 (en) * 2019-06-04 2022-08-16 United States Of America As Represented By The Secretary Of The Air Force Disk engine with circumferential swirl radial combustor

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2655787A (en) * 1949-11-21 1953-10-20 United Aircraft Corp Gas turbine combustion chamber with variable area primary air inlet
GB721209A (en) * 1951-09-24 1955-01-05 Power Jets Res & Dev Ltd Combustion apparatus
US2837893A (en) * 1952-12-12 1958-06-10 Phillips Petroleum Co Automatic primary and secondary air flow regulation for gas turbine combustion chamber
GB877823A (en) * 1959-01-29 1961-09-20 Rolls Royce Improvements in or relating to combustion chambers
JPS5857655B2 (ja) * 1976-08-27 1983-12-21 株式会社日立製作所 ガスタ−ビン用燃焼器
SU1449775A1 (ru) * 1987-04-30 1989-01-07 Производственное Объединение Турбостроения "Ленинградский Металлический Завод" Выходной патрубок секционной камеры сгорани газотурбинной установки
SU1643878A1 (ru) * 1989-01-03 1991-04-23 Производственное Объединение Атомного Турбостроения "Харьковский Турбинный Завод" Им.С.М.Кирова Кольцева камера сгорани газотурбинного двигател
ITMI991207A1 (it) * 1999-05-31 2000-12-01 Nuovo Pignone Spa Camera di combustione per turbine a gas
FR2897922B1 (fr) * 2006-02-27 2008-10-10 Snecma Sa Agencement pour une chambre de combustion de turboreacteur
EP1936468A1 (en) 2006-12-22 2008-06-25 Siemens Aktiengesellschaft Bi-metallic elements for adjusting a cooling channel

Also Published As

Publication number Publication date
US20100218509A1 (en) 2010-09-02
EP2039999A1 (en) 2009-03-25
CN101809370B (zh) 2012-06-13
US8156724B2 (en) 2012-04-17
WO2009040232A1 (en) 2009-04-02
RU2470227C2 (ru) 2012-12-20
CA2700300A1 (en) 2009-04-02
CN101809370A (zh) 2010-08-18
RU2010116161A (ru) 2011-11-10

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