DE8618859U1 - - Google Patents

Info

Publication number
DE8618859U1
DE8618859U1 DE19868618859 DE8618859U DE8618859U1 DE 8618859 U1 DE8618859 U1 DE 8618859U1 DE 19868618859 DE19868618859 DE 19868618859 DE 8618859 U DE8618859 U DE 8618859U DE 8618859 U1 DE8618859 U1 DE 8618859U1
Authority
DE
Germany
Legal status (The legal status 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 status listed.)
Expired
Application number
DE19868618859
Other languages
German (de)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Siemens AG
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
Priority to DE19868618859 priority Critical patent/DE8618859U1/de
Publication of DE8618859U1 publication Critical patent/DE8618859U1/de
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002Wall structures
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03044Impingement cooled combustion chamber walls or subassemblies
DE19868618859 1986-07-14 1986-07-14 Expired DE8618859U1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE19868618859 DE8618859U1 (en) 1986-07-14 1986-07-14

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19868618859 DE8618859U1 (en) 1986-07-14 1986-07-14

Publications (1)

Publication Number Publication Date
DE8618859U1 true DE8618859U1 (en) 1988-01-28

Family

ID=6796461

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19868618859 Expired DE8618859U1 (en) 1986-07-14 1986-07-14

Country Status (1)

Country Link
DE (1) DE8618859U1 (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19621069A1 (en) * 1996-05-24 1997-06-05 Siemens Ag Cover plate fixture holder for gas turbine exhaust duct
EP1503144A1 (en) * 2003-07-31 2005-02-02 United Technologies Corporation Combustor
WO2008017551A2 (en) * 2006-08-07 2008-02-14 Alstom Technology Ltd Combustion chamber of a combustion plant
DE102006040760A1 (en) * 2006-08-31 2008-03-06 Rolls-Royce Deutschland Ltd & Co Kg Lean-burning gas turbine combustion chamber wall, has Inflow holes formed perpendicularly over chamber wall, and damping openings formed by shingle, where shingle is spaced apart from chamber wall by using side part
WO2009053417A2 (en) * 2007-10-26 2009-04-30 Siemens Aktiengesellschaft Support ring for heat shield elements on aflame tube and a combustion chamber arrangement with said support ring
US8122726B2 (en) 2006-08-07 2012-02-28 Alstom Technology Ltd Combustion chamber of a combustion system
DE102013003444A1 (en) * 2013-02-26 2014-09-11 Rolls-Royce Deutschland Ltd & Co Kg Impact-cooled shingle of a gas turbine combustor with extended effusion holes
EP2770259A3 (en) * 2013-02-21 2015-10-21 Rolls-Royce plc A combustion chamber
WO2017097606A1 (en) * 2015-12-08 2017-06-15 Siemens Aktiengesellschaft Combustion chamber having resonators

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19621069A1 (en) * 1996-05-24 1997-06-05 Siemens Ag Cover plate fixture holder for gas turbine exhaust duct
EP1503144A1 (en) * 2003-07-31 2005-02-02 United Technologies Corporation Combustor
US7146815B2 (en) 2003-07-31 2006-12-12 United Technologies Corporation Combustor
US8006498B2 (en) 2006-08-07 2011-08-30 Alstom Technology Ltd Combustion chamber of a combustion system
WO2008017551A2 (en) * 2006-08-07 2008-02-14 Alstom Technology Ltd Combustion chamber of a combustion plant
WO2008017551A3 (en) * 2006-08-07 2008-04-17 Alstom Technology Ltd Combustion chamber of a combustion plant
US8122726B2 (en) 2006-08-07 2012-02-28 Alstom Technology Ltd Combustion chamber of a combustion system
DE102006040760A1 (en) * 2006-08-31 2008-03-06 Rolls-Royce Deutschland Ltd & Co Kg Lean-burning gas turbine combustion chamber wall, has Inflow holes formed perpendicularly over chamber wall, and damping openings formed by shingle, where shingle is spaced apart from chamber wall by using side part
WO2009053417A3 (en) * 2007-10-26 2010-05-20 Siemens Aktiengesellschaft Support ring for heat shield elements on aflame tube and a combustion chamber arrangement with said support ring
WO2009053417A2 (en) * 2007-10-26 2009-04-30 Siemens Aktiengesellschaft Support ring for heat shield elements on aflame tube and a combustion chamber arrangement with said support ring
CN101855497B (en) * 2007-10-26 2012-09-05 西门子公司 Support ring for heat shield elements on aflame tube and a combustion chamber arrangement with said support ring
RU2478881C2 (en) * 2007-10-26 2013-04-10 Сименс Акциенгезелльшафт Support ring for elements of thermal protection shield of flame tube, and system of combustion chamber with similar support ring
EP2770259A3 (en) * 2013-02-21 2015-10-21 Rolls-Royce plc A combustion chamber
DE102013003444A1 (en) * 2013-02-26 2014-09-11 Rolls-Royce Deutschland Ltd & Co Kg Impact-cooled shingle of a gas turbine combustor with extended effusion holes
US9518738B2 (en) 2013-02-26 2016-12-13 Rolls-Royce Deutschland Ltd & Co Kg Impingement-effusion cooled tile of a gas-turbine combustion chamber with elongated effusion holes
WO2017097606A1 (en) * 2015-12-08 2017-06-15 Siemens Aktiengesellschaft Combustion chamber having resonators

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