PL2201299T3 - Support ring for heat shield elements on a flame tube and a combustion chamber arrangement with said support ring - Google Patents

Support ring for heat shield elements on a flame tube and a combustion chamber arrangement with said support ring

Info

Publication number
PL2201299T3
PL2201299T3 PL08842468T PL08842468T PL2201299T3 PL 2201299 T3 PL2201299 T3 PL 2201299T3 PL 08842468 T PL08842468 T PL 08842468T PL 08842468 T PL08842468 T PL 08842468T PL 2201299 T3 PL2201299 T3 PL 2201299T3
Authority
PL
Poland
Prior art keywords
support ring
combustion chamber
heat shield
flame tube
chamber arrangement
Prior art date
Application number
PL08842468T
Other languages
Polish (pl)
Inventor
Elke Henschel
Milan Schmahl
Martin Stapper
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 PL2201299T3 publication Critical patent/PL2201299T3/en

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
    • F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic 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
    • F23R3/42—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
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M2900/00—Special features of, or arrangements for combustion chambers
    • F23M2900/05002—Means for accommodate thermal expansion of the wall liner
    • 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
    • F23R2900/03041—Effusion cooled combustion chamber walls or domes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Combustion Of Fluid Fuel (AREA)
  • Gas Burners (AREA)
  • Portable Nailing Machines And Staplers (AREA)

Abstract

A support ring (113) for heat shield elements (111) o a flame tube (101) is disclosed, wherein at least one groove (119) on the outer side (115) of the support ring. The groove (119) has a groove wall (125) running at an angel with relation to the radial direction of the support ring (113). A combustion chamber arrangement with said support is also disclosed.
PL08842468T 2007-10-26 2008-10-23 Support ring for heat shield elements on a flame tube and a combustion chamber arrangement with said support ring PL2201299T3 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102007051649 2007-10-26
EP08842468A EP2201299B1 (en) 2007-10-26 2008-10-23 Support ring for heat shield elements on a flame tube and a combustion chamber arrangement with said support ring
PCT/EP2008/064333 WO2009053417A2 (en) 2007-10-26 2008-10-23 Support ring for heat shield elements on aflame tube and a combustion chamber arrangement with said support ring

Publications (1)

Publication Number Publication Date
PL2201299T3 true PL2201299T3 (en) 2011-10-31

Family

ID=40340467

Family Applications (1)

Application Number Title Priority Date Filing Date
PL08842468T PL2201299T3 (en) 2007-10-26 2008-10-23 Support ring for heat shield elements on a flame tube and a combustion chamber arrangement with said support ring

Country Status (6)

Country Link
EP (1) EP2201299B1 (en)
CN (1) CN101855497B (en)
AT (1) ATE509236T1 (en)
PL (1) PL2201299T3 (en)
RU (1) RU2478881C2 (en)
WO (1) WO2009053417A2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102012204103A1 (en) * 2012-03-15 2013-09-19 Siemens Aktiengesellschaft Heat shield element for a compressor air bypass around the combustion chamber
DE102017207392A1 (en) * 2017-05-03 2018-11-08 Siemens Aktiengesellschaft Silo combustion chamber and method for converting such

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE8618859U1 (en) * 1986-07-14 1988-01-28 Siemens AG, 1000 Berlin und 8000 München Heat shield
RU2076275C1 (en) * 1990-07-17 1997-03-27 Сименс АГ Length of pipe, flame tube in particular, with inner volume for direction of hot gas and thermal shield
US5749218A (en) * 1993-12-17 1998-05-12 General Electric Co. Wear reduction kit for gas turbine combustors
GB2298267B (en) * 1995-02-23 1999-01-13 Rolls Royce Plc An arrangement of heat resistant tiles for a gas turbine engine combustor
RU2212591C1 (en) * 2002-05-16 2003-09-20 Открытое акционерное общество "Научно-производственное объединение "Сатурн" Gas-turbine engine annular combustion chamber
RU2300706C2 (en) * 2005-05-05 2007-06-10 Открытое акционерное общество "Авиадвигатель" Tubular annular combustion chamber of gas-turbine engine
WO2008017550A1 (en) * 2006-08-07 2008-02-14 Alstom Technology Ltd Combustion chamber of a combustion installation

Also Published As

Publication number Publication date
RU2478881C2 (en) 2013-04-10
CN101855497B (en) 2012-09-05
EP2201299A2 (en) 2010-06-30
WO2009053417A2 (en) 2009-04-30
WO2009053417A3 (en) 2010-05-20
RU2010121163A (en) 2011-12-10
ATE509236T1 (en) 2011-05-15
CN101855497A (en) 2010-10-06
EP2201299B1 (en) 2011-05-11

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