RU2444681C2 - Камера сгорания для газовой турбины и газовая турбина - Google Patents

Камера сгорания для газовой турбины и газовая турбина Download PDF

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Publication number
RU2444681C2
RU2444681C2 RU2008140723/06A RU2008140723A RU2444681C2 RU 2444681 C2 RU2444681 C2 RU 2444681C2 RU 2008140723/06 A RU2008140723/06 A RU 2008140723/06A RU 2008140723 A RU2008140723 A RU 2008140723A RU 2444681 C2 RU2444681 C2 RU 2444681C2
Authority
RU
Russia
Prior art keywords
mixing chamber
bolt
combustion chamber
gas turbine
flange
Prior art date
Application number
RU2008140723/06A
Other languages
English (en)
Russian (ru)
Other versions
RU2008140723A (ru
Inventor
Петер ДИТРИХ (DE)
Петер ДИТРИХ
Милан ШМАЛЬ (DE)
Милан ШМАЛЬ
Мартин ШТАППЕР (DE)
Мартин ШТАППЕР
Original Assignee
Сименс Акциенгезелльшафт
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 Сименс Акциенгезелльшафт filed Critical Сименс Акциенгезелльшафт
Publication of RU2008140723A publication Critical patent/RU2008140723A/ru
Application granted granted Critical
Publication of RU2444681C2 publication Critical patent/RU2444681C2/ru

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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)
RU2008140723/06A 2006-03-15 2007-01-09 Камера сгорания для газовой турбины и газовая турбина RU2444681C2 (ru)

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
RU2008140723A RU2008140723A (ru) 2010-04-20
RU2444681C2 true RU2444681C2 (ru) 2012-03-10

Family

ID=38008336

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2008140723/06A RU2444681C2 (ru) 2006-03-15 2007-01-09 Камера сгорания для газовой турбины и газовая турбина

Country Status (4)

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

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2993315B8 (en) * 2014-09-05 2017-07-19 Ansaldo Energia Switzerland AG Apparatus for an assembly tool for mounting or dismantling, replacement and maintenance of a component of an engine
FR3038699B1 (fr) * 2015-07-08 2022-06-24 Snecma Chambre de combustion coudee d'une turbomachine

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1355728A (en) * 1971-12-09 1974-06-05 Westinghouse Electric Corp Gas turbine
EP0496659A1 (fr) * 1991-01-23 1992-07-29 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Chambre de combustion notamment pour turbine à gaz à paroi déformable
US5419114A (en) * 1992-07-18 1995-05-30 Man Gutehoffnungshutte Ag Thermoelastic connection of the injector tube and the flame tube of a gas turbine
RU94022720A (ru) * 1994-06-10 1996-06-20 Ставропольское высшее авиационное инженерное училище ПВО им.маршала авиации Судца В.А. Камера сгорания газотурбинного двигателя
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

Family Cites Families (5)

* 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
DE2523449C3 (de) * 1975-05-27 1981-03-26 Kraftwerk Union AG, 45473 Mülheim Brennkammer für Gasturbinen
IT1216611B (it) * 1988-04-21 1990-03-08 Nuovo Pignone Spa Dispositivo per mantenere la bocca anulare di uscita del convogliatore dei gas sempre centrata rispetto al gruppo ugelli di una turbina agas.
US6442946B1 (en) * 2000-11-14 2002-09-03 Power Systems Mfg., Llc Three degrees of freedom aft mounting system for gas turbine transition duct
DE10348447B4 (de) * 2003-10-17 2014-04-03 Siemens Aktiengesellschaft Montage- und Wartungshilfsmittel für eine Gasturbine

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1355728A (en) * 1971-12-09 1974-06-05 Westinghouse Electric Corp Gas turbine
EP0496659A1 (fr) * 1991-01-23 1992-07-29 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Chambre de combustion notamment pour turbine à gaz à paroi déformable
US5419114A (en) * 1992-07-18 1995-05-30 Man Gutehoffnungshutte Ag Thermoelastic connection of the injector tube and the flame tube of a gas turbine
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
RU94022720A (ru) * 1994-06-10 1996-06-20 Ставропольское высшее авиационное инженерное училище ПВО им.маршала авиации Судца В.А. Камера сгорания газотурбинного двигателя

Also Published As

Publication number Publication date
EP1994260B1 (de) 2017-09-20
CN101548135B (zh) 2011-06-08
WO2007104587A2 (de) 2007-09-20
EP1994260A2 (de) 2008-11-26
WO2007104587A3 (de) 2009-01-22
CN101548135A (zh) 2009-09-30
RU2008140723A (ru) 2010-04-20

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PC41 Official registration of the transfer of exclusive right

Effective date: 20210330

QZ41 Official registration of changes to a registered agreement (patent)

Free format text: LICENCE FORMERLY AGREED ON 20150707

Effective date: 20210407