GB2384046B - A double wall combuster tile arrangement - Google Patents

A double wall combuster tile arrangement

Info

Publication number
GB2384046B
GB2384046B GB0200778A GB0200778A GB2384046B GB 2384046 B GB2384046 B GB 2384046B GB 0200778 A GB0200778 A GB 0200778A GB 0200778 A GB0200778 A GB 0200778A GB 2384046 B GB2384046 B GB 2384046B
Authority
GB
United Kingdom
Prior art keywords
combuster
double wall
tile arrangement
tile
arrangement
Prior art date
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 - Fee Related
Application number
GB0200778A
Other versions
GB0200778D0 (en
GB2384046A (en
Inventor
Anthony Pidcock
Desmond Close
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB0200778A priority Critical patent/GB2384046B/en
Publication of GB0200778D0 publication Critical patent/GB0200778D0/en
Priority to US10/330,329 priority patent/US20030145604A1/en
Publication of GB2384046A publication Critical patent/GB2384046A/en
Priority to US10/880,463 priority patent/US20050034399A1/en
Application granted granted Critical
Publication of GB2384046B publication Critical patent/GB2384046B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • F23R3/42—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
    • 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
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
GB0200778A 2002-01-15 2002-01-15 A double wall combuster tile arrangement Expired - Fee Related GB2384046B (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB0200778A GB2384046B (en) 2002-01-15 2002-01-15 A double wall combuster tile arrangement
US10/330,329 US20030145604A1 (en) 2002-01-15 2002-12-30 Double wall combustor tile arrangement
US10/880,463 US20050034399A1 (en) 2002-01-15 2004-07-01 Double wall combustor tile arrangement

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0200778A GB2384046B (en) 2002-01-15 2002-01-15 A double wall combuster tile arrangement

Publications (3)

Publication Number Publication Date
GB0200778D0 GB0200778D0 (en) 2002-03-06
GB2384046A GB2384046A (en) 2003-07-16
GB2384046B true GB2384046B (en) 2005-07-06

Family

ID=9929059

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0200778A Expired - Fee Related GB2384046B (en) 2002-01-15 2002-01-15 A double wall combuster tile arrangement

Country Status (2)

Country Link
US (1) US20030145604A1 (en)
GB (1) GB2384046B (en)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1312865A1 (en) * 2001-11-15 2003-05-21 Siemens Aktiengesellschaft Gas turbine annular combustion chamber
DE10214570A1 (en) * 2002-04-02 2004-01-15 Rolls-Royce Deutschland Ltd & Co Kg Mixed air hole in gas turbine combustion chamber with combustion chamber shingles
US7464554B2 (en) * 2004-09-09 2008-12-16 United Technologies Corporation Gas turbine combustor heat shield panel or exhaust panel including a cooling device
US7954325B2 (en) * 2005-12-06 2011-06-07 United Technologies Corporation Gas turbine combustor
GB2444947B (en) * 2006-12-19 2009-04-08 Rolls Royce Plc Wall elements for gas turbine engine components
US20100095680A1 (en) * 2008-10-22 2010-04-22 Honeywell International Inc. Dual wall structure for use in a combustor of a gas turbine engine
US20100095679A1 (en) * 2008-10-22 2010-04-22 Honeywell International Inc. Dual wall structure for use in a combustor of a gas turbine engine
US8161752B2 (en) * 2008-11-20 2012-04-24 Honeywell International Inc. Combustors with inserts between dual wall liners
US8739404B2 (en) 2010-11-23 2014-06-03 General Electric Company Turbine components with cooling features and methods of manufacturing the same
US9958162B2 (en) 2011-01-24 2018-05-01 United Technologies Corporation Combustor assembly for a turbine engine
US8479521B2 (en) 2011-01-24 2013-07-09 United Technologies Corporation Gas turbine combustor with liner air admission holes associated with interspersed main and pilot swirler assemblies
US9068748B2 (en) 2011-01-24 2015-06-30 United Technologies Corporation Axial stage combustor for gas turbine engines
GB201114745D0 (en) * 2011-08-26 2011-10-12 Rolls Royce Plc Wall elements for gas turbine engines
JP5821550B2 (en) 2011-11-10 2015-11-24 株式会社Ihi Combustor liner
GB201222311D0 (en) * 2012-12-12 2013-01-23 Rolls Royce Plc A combusiton chamber
GB201303057D0 (en) * 2013-02-21 2013-04-03 Rolls Royce Plc A combustion chamber
CA2904200A1 (en) * 2013-03-05 2014-09-12 Rolls-Royce Corporation Dual-wall impingement, convection, effusion combustor tile
WO2014160565A1 (en) * 2013-03-26 2014-10-02 United Technologies Corporation Turbine engine and turbine engine component with improved cooling pedestals
US10352566B2 (en) 2013-06-14 2019-07-16 United Technologies Corporation Gas turbine engine combustor liner panel
GB201322838D0 (en) 2013-12-23 2014-02-12 Rolls Royce Plc A combustion chamber
EP3175177A1 (en) * 2014-07-30 2017-06-07 Siemens Aktiengesellschaft Multiple feed platefins within a hot gas path cooling system in a combustor basket in a combustion turbine engine
US20160258623A1 (en) * 2015-03-05 2016-09-08 United Technologies Corporation Combustor and heat shield configurations for a gas turbine engine
US10480787B2 (en) 2015-03-26 2019-11-19 United Technologies Corporation Combustor wall cooling channel formed by additive manufacturing
US10386067B2 (en) * 2016-09-15 2019-08-20 United Technologies Corporation Wall panel assembly for a gas turbine engine
EP3540314B1 (en) * 2016-11-11 2023-07-12 Kawasaki Jukogyo Kabushiki Kaisha Combustor liner for a gas turbine
US11435078B2 (en) * 2018-12-20 2022-09-06 Pratt & Whitney Canada Corp. Stand-off device for double-skin combustor liner
GB202000870D0 (en) 2020-01-21 2020-03-04 Rolls Royce Plc A combustion chamber, a combustion chamber tile and a combustion chamber segment

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2298267A (en) * 1995-02-23 1996-08-28 Rolls Royce Plc An arrangement of heat resistant tiles for a gas turbine engine combustor

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2087065B (en) * 1980-11-08 1984-11-07 Rolls Royce Wall structure for a combustion chamber
FR2646880A1 (en) * 1989-05-11 1990-11-16 Snecma THERMAL PROTECTION SHIRT FOR POST-COMBUSTION CHANNEL OR TRANSITION OF TURBOREACTOR
US5259758A (en) * 1992-11-25 1993-11-09 Wisconsin Oven Corporation Industrial oven with expandable surfaces
US5289677A (en) * 1992-12-16 1994-03-01 United Technologies Corporation Combined support and seal ring for a combustor
GB9926257D0 (en) * 1999-11-06 2000-01-12 Rolls Royce Plc Wall elements for gas turbine engine combustors
GB2361303B (en) * 2000-04-14 2004-10-20 Rolls Royce Plc Wall structure for a gas turbine engine combustor

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2298267A (en) * 1995-02-23 1996-08-28 Rolls Royce Plc An arrangement of heat resistant tiles for a gas turbine engine combustor

Also Published As

Publication number Publication date
GB0200778D0 (en) 2002-03-06
US20030145604A1 (en) 2003-08-07
GB2384046A (en) 2003-07-16

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20090115