WO2007104587A3 - Turbine à gaz à enveloppe du mélangeur réglable - Google Patents

Turbine à gaz à enveloppe du mélangeur réglable Download PDF

Info

Publication number
WO2007104587A3
WO2007104587A3 PCT/EP2007/050194 EP2007050194W WO2007104587A3 WO 2007104587 A3 WO2007104587 A3 WO 2007104587A3 EP 2007050194 W EP2007050194 W EP 2007050194W WO 2007104587 A3 WO2007104587 A3 WO 2007104587A3
Authority
WO
WIPO (PCT)
Prior art keywords
mounting
gas turbine
adjusting device
mixing housing
device therefor
Prior art date
Application number
PCT/EP2007/050194
Other languages
German (de)
English (en)
Other versions
WO2007104587A2 (fr
Inventor
Peter Dietrich
Milan Schmahl
Martin Stapper
Original Assignee
Siemens Ag
Peter Dietrich
Milan Schmahl
Martin Stapper
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, Peter Dietrich, Milan Schmahl, Martin Stapper filed Critical Siemens Ag
Priority to EP07700252.5A priority Critical patent/EP1994260B1/fr
Priority to CN2007800087709A priority patent/CN101548135B/zh
Publication of WO2007104587A2 publication Critical patent/WO2007104587A2/fr
Publication of WO2007104587A3 publication Critical patent/WO2007104587A3/fr

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • 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
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00—Function
    • F05B2260/30—Retaining components in desired mutual position
    • F05B2260/301—Retaining bolts or nuts
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F05D2230/644—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins for adjusting the position or the alignment, e.g. wedges or eccenters
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/24—Three-dimensional ellipsoidal
    • F05D2250/241—Three-dimensional ellipsoidal spherical
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/40—Movement of components
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/40—Movement of components
    • F05D2250/42—Movement of components with two degrees of freedom

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Gas Burners (AREA)

Abstract

Procédé de montage d'une turbine à gaz comprenant un tube à flamme (2), une enveloppe intérieure (8) et une enveloppe du mélangeur (4) disposée entre le tube à flamme (2) et l'enveloppe intérieure (8), caractérisé en ce qu'on effectue un réglage de l'enveloppe du mélangeur (4) par rapport au tube à flamme (2) et à l'enveloppe intérieure (8).
PCT/EP2007/050194 2006-03-15 2007-01-09 Turbine à gaz à enveloppe du mélangeur réglable WO2007104587A2 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP07700252.5A EP1994260B1 (fr) 2006-03-15 2007-01-09 Chambre de combustion pour une turbine à gaz avec un système de positionnement
CN2007800087709A CN101548135B (zh) 2006-03-15 2007-01-09 用于在燃气轮机内安装混合壳体的方法和为此的调整装置

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP06005259.4 2006-03-15
EP06005259 2006-03-15

Publications (2)

Publication Number Publication Date
WO2007104587A2 WO2007104587A2 (fr) 2007-09-20
WO2007104587A3 true WO2007104587A3 (fr) 2009-01-22

Family

ID=38008336

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2007/050194 WO2007104587A2 (fr) 2006-03-15 2007-01-09 Turbine à gaz à enveloppe du mélangeur réglable

Country Status (4)

Country Link
EP (1) EP1994260B1 (fr)
CN (1) CN101548135B (fr)
RU (1) RU2444681C2 (fr)
WO (1) WO2007104587A2 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2993315B8 (fr) * 2014-09-05 2017-07-19 Ansaldo Energia Switzerland AG Appareil pour outil d'assemblage pour le montage ou le démontage, le remplacement et l'entretien de composant d'un moteur
FR3038699B1 (fr) * 2015-07-08 2022-06-24 Snecma Chambre de combustion coudee d'une turbomachine

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB701099A (en) * 1950-05-22 1953-12-16 Lucas Ltd Joseph Improvements to combustion chambers
DE2258719A1 (de) * 1971-12-09 1973-06-14 Westinghouse Electric Corp Gasturbine
DE2523449A1 (de) * 1975-05-27 1976-12-02 Kraftwerk Union Ag Brennkammer fuer gasturbinen
DE3913223A1 (de) * 1988-04-21 1989-11-02 Nuovo Pignone Spa Vorrichtung zum staendigen halten der ringfoermigen auslassmuendung des gasausstroemraums zentriert um die duesenanordnung in einer gasturbine
DE4223733A1 (de) * 1992-07-18 1994-01-20 Gutehoffnungshuette Man Wärmeelastische Verbindung von Misch- und Flammrohr einer Gasturbine
US6442946B1 (en) * 2000-11-14 2002-09-03 Power Systems Mfg., Llc Three degrees of freedom aft mounting system for gas turbine transition duct
DE10348447A1 (de) * 2003-10-17 2005-07-07 Siemens Ag Montage- und Wartungshilfsmittel für eine Gasturbine

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2671857B1 (fr) * 1991-01-23 1994-12-09 Snecma Chambre de combustion, notamment pour turbine a gaz, a paroi deformable.
RU2100705C1 (ru) * 1993-02-03 1997-12-27 Акционерное общество открытого типа "Самарский научно-технический комплекс "Двигатели НК" Устройство для крепления жаровой трубы в корпусе камеры сгорания
RU2112181C1 (ru) * 1994-06-10 1998-05-27 Ставропольское высшее авиационное инженерное училище противовоздушной обороны им.Маршала авиации Судца В.А. Камера сгорания газотурбинного двигателя

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB701099A (en) * 1950-05-22 1953-12-16 Lucas Ltd Joseph Improvements to combustion chambers
DE2258719A1 (de) * 1971-12-09 1973-06-14 Westinghouse Electric Corp Gasturbine
DE2523449A1 (de) * 1975-05-27 1976-12-02 Kraftwerk Union Ag Brennkammer fuer gasturbinen
DE3913223A1 (de) * 1988-04-21 1989-11-02 Nuovo Pignone Spa Vorrichtung zum staendigen halten der ringfoermigen auslassmuendung des gasausstroemraums zentriert um die duesenanordnung in einer gasturbine
DE4223733A1 (de) * 1992-07-18 1994-01-20 Gutehoffnungshuette Man Wärmeelastische Verbindung von Misch- und Flammrohr einer Gasturbine
US6442946B1 (en) * 2000-11-14 2002-09-03 Power Systems Mfg., Llc Three degrees of freedom aft mounting system for gas turbine transition duct
DE10348447A1 (de) * 2003-10-17 2005-07-07 Siemens Ag Montage- und Wartungshilfsmittel für eine Gasturbine

Also Published As

Publication number Publication date
WO2007104587A2 (fr) 2007-09-20
RU2444681C2 (ru) 2012-03-10
CN101548135B (zh) 2011-06-08
CN101548135A (zh) 2009-09-30
RU2008140723A (ru) 2010-04-20
EP1994260A2 (fr) 2008-11-26
EP1994260B1 (fr) 2017-09-20

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