GB0524739D0 - Gas turbine sub-assemblies - Google Patents

Gas turbine sub-assemblies

Info

Publication number
GB0524739D0
GB0524739D0 GBGB0524739.0A GB0524739A GB0524739D0 GB 0524739 D0 GB0524739 D0 GB 0524739D0 GB 0524739 A GB0524739 A GB 0524739A GB 0524739 D0 GB0524739 D0 GB 0524739D0
Authority
GB
United Kingdom
Prior art keywords
assemblies
gas turbine
turbine sub
sub
gas
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.)
Granted
Application number
GBGB0524739.0A
Other versions
GB2432902B (en
GB2432902A (en
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.)
General Electric Technology GmbH
Original Assignee
Alstom Technology 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 Alstom Technology AG filed Critical Alstom Technology AG
Priority to GB0524739A priority Critical patent/GB2432902B/en
Publication of GB0524739D0 publication Critical patent/GB0524739D0/en
Publication of GB2432902A publication Critical patent/GB2432902A/en
Application granted granted Critical
Publication of GB2432902B publication Critical patent/GB2432902B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F23R3/002—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
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/005—Combined with pressure or heat exchangers
    • 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
    • F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00017—Assembling combustion chamber liners or subparts

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)
GB0524739A 2005-12-03 2005-12-03 Gas turbine sub-assemblies Expired - Fee Related GB2432902B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB0524739A GB2432902B (en) 2005-12-03 2005-12-03 Gas turbine sub-assemblies

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0524739A GB2432902B (en) 2005-12-03 2005-12-03 Gas turbine sub-assemblies

Publications (3)

Publication Number Publication Date
GB0524739D0 true GB0524739D0 (en) 2006-01-11
GB2432902A GB2432902A (en) 2007-06-06
GB2432902B GB2432902B (en) 2011-01-12

Family

ID=35686057

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0524739A Expired - Fee Related GB2432902B (en) 2005-12-03 2005-12-03 Gas turbine sub-assemblies

Country Status (1)

Country Link
GB (1) GB2432902B (en)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2929690B1 (en) * 2008-04-03 2012-08-17 Snecma Propulsion Solide COMBUSTION CHAMBER SECTORIZED IN CMC FOR GAS TURBINE
FR2929689B1 (en) 2008-04-03 2013-04-12 Snecma Propulsion Solide GAS TURBINE COMBUSTION CHAMBER WITH SECTORIZED INTERNAL AND EXTERNAL WALLS
EP2282124A1 (en) * 2009-08-03 2011-02-09 Alstom Technology Ltd Method for retrofitting a combustion chamber of a gas turbine
IT1397226B1 (en) * 2009-12-30 2013-01-04 Ansaldo Energia Spa MAINTENANCE METHOD OF A COMBUSTION CHAMBER OF A GAS TURBINE SYSTEM.
ITMI20101285A1 (en) * 2010-07-13 2012-01-14 Ansaldo Energia Spa METHOD AND TOOL FOR MAINTENANCE OF A GAS TURBINE COMBUSTION CHAMBER
EP2442032A1 (en) * 2010-10-12 2012-04-18 Siemens Aktiengesellschaft Wear segment in the turbine stator vane anchoring of the external shell of an annular combustion chamber
WO2015038293A1 (en) 2013-09-11 2015-03-19 United Technologies Corporation Combustor liner
DE102014204468A1 (en) * 2014-03-11 2015-10-01 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine combustor and method for its production
DE102014204466A1 (en) * 2014-03-11 2015-10-01 Rolls-Royce Deutschland Ltd & Co Kg Combustion chamber of a gas turbine
GB201413194D0 (en) 2014-07-25 2014-09-10 Rolls Royce Plc A liner element for a combustor, and a related method
GB201501817D0 (en) 2015-02-04 2015-03-18 Rolls Royce Plc A combustion chamber and a combustion chamber segment
GB2545459B (en) 2015-12-17 2020-05-06 Rolls Royce Plc A combustion chamber
EP3236155B1 (en) * 2016-04-22 2020-05-06 Rolls-Royce plc Combustion chamber with segmented wall
GB201613110D0 (en) 2016-07-29 2016-09-14 Rolls Royce Plc A combustion chamber
GB201613299D0 (en) 2016-08-02 2016-09-14 Rolls Royce Plc A method of assembling an annular combustion chamber assembly
US10935236B2 (en) 2016-11-10 2021-03-02 Raytheon Technologies Corporation Non-planar combustor liner panel for a gas turbine engine combustor
US10830433B2 (en) 2016-11-10 2020-11-10 Raytheon Technologies Corporation Axial non-linear interface for combustor liner panels in a gas turbine combustor
US10655853B2 (en) 2016-11-10 2020-05-19 United Technologies Corporation Combustor liner panel with non-linear circumferential edge for a gas turbine engine combustor
US10935235B2 (en) 2016-11-10 2021-03-02 Raytheon Technologies Corporation Non-planar combustor liner panel for a gas turbine engine combustor
US10801730B2 (en) * 2017-04-12 2020-10-13 Raytheon Technologies Corporation Combustor panel mounting systems and methods
US11047575B2 (en) 2019-04-15 2021-06-29 Raytheon Technologies Corporation Combustor heat shield panel
US11215367B2 (en) 2019-10-03 2022-01-04 Raytheon Technologies Corporation Mounting a ceramic component to a non-ceramic component in a gas turbine engine
CN116642200A (en) 2022-02-15 2023-08-25 通用电气公司 Integrated dome deflector member for a dome of a burner
CN117091159A (en) 2022-05-13 2023-11-21 通用电气公司 Combustor liner
CN117091158A (en) 2022-05-13 2023-11-21 通用电气公司 Combustor chamber mesh structure
CN117091162A (en) 2022-05-13 2023-11-21 通用电气公司 Burner with dilution hole structure
CN117091161A (en) 2022-05-13 2023-11-21 通用电气公司 Combustor liner hollow plate design and construction
CN117091157A (en) 2022-05-13 2023-11-21 通用电气公司 Plate hanger structure for durable combustor liner

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB647302A (en) * 1948-05-14 1950-12-13 Edgar Phillips Peregrine Improvements in or relating to linings for combustion chambers and the like
DE1173734B (en) * 1962-10-11 1964-07-09 Siemens Ag Combustion chamber, especially for gas turbines, with a lining made of refractory bricks
US3826088A (en) * 1973-02-01 1974-07-30 Gen Electric Gas turbine engine augmenter cooling liner stabilizers and supports
DE3625056C2 (en) * 1986-07-24 1997-05-28 Siemens Ag Refractory lining, in particular for combustion chambers of gas turbine plants
DE58908665D1 (en) * 1988-06-13 1995-01-05 Siemens Ag HEAT SHIELD ARRANGEMENT WITH LOW COOLING FLUID REQUIREMENT.
US4944151A (en) * 1988-09-26 1990-07-31 Avco Corporation Segmented combustor panel
FR2840974B1 (en) * 2002-06-13 2005-12-30 Snecma Propulsion Solide SEAL RING FOR COMBUSTION CAHMBERS AND COMBUSTION CHAMBER COMPRISING SUCH A RING

Also Published As

Publication number Publication date
GB2432902B (en) 2011-01-12
GB2432902A (en) 2007-06-06

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Legal Events

Date Code Title Description
732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)

Free format text: REGISTERED BETWEEN 20170727 AND 20170802

PCNP Patent ceased through non-payment of renewal fee

Effective date: 20221203