GB9924120D0 - A wall structure for a combustor of a gas turbine engine - Google Patents

A wall structure for a combustor of a gas turbine engine

Info

Publication number
GB9924120D0
GB9924120D0 GBGB9924120.0A GB9924120A GB9924120D0 GB 9924120 D0 GB9924120 D0 GB 9924120D0 GB 9924120 A GB9924120 A GB 9924120A GB 9924120 D0 GB9924120 D0 GB 9924120D0
Authority
GB
United Kingdom
Prior art keywords
combustor
gas turbine
turbine engine
wall structure
wall
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.)
Withdrawn
Application number
GBGB9924120.0A
Other versions
GB2355301A (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.)
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 GB9924120A priority Critical patent/GB2355301A/en
Publication of GB9924120D0 publication Critical patent/GB9924120D0/en
Publication of GB2355301A publication Critical patent/GB2355301A/en
Withdrawn legal-status Critical Current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
    • F23R3/002—Wall structures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2214/00—Cooling

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)
GB9924120A 1999-10-13 1999-10-13 A wall structure for a combustor of a gas turbine engine Withdrawn GB2355301A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9924120A GB2355301A (en) 1999-10-13 1999-10-13 A wall structure for a combustor of a gas turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9924120A GB2355301A (en) 1999-10-13 1999-10-13 A wall structure for a combustor of a gas turbine engine

Publications (2)

Publication Number Publication Date
GB9924120D0 true GB9924120D0 (en) 1999-12-15
GB2355301A GB2355301A (en) 2001-04-18

Family

ID=10862589

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9924120A Withdrawn GB2355301A (en) 1999-10-13 1999-10-13 A wall structure for a combustor of a gas turbine engine

Country Status (1)

Country Link
GB (1) GB2355301A (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0601418D0 (en) * 2006-01-25 2006-03-08 Rolls Royce Plc Wall elements for gas turbine engine combustors
GB2444947B (en) * 2006-12-19 2009-04-08 Rolls Royce Plc Wall elements for gas turbine engine components
US10655855B2 (en) 2013-08-30 2020-05-19 Raytheon Technologies Corporation Gas turbine engine wall assembly with support shell contour regions
GB201603166D0 (en) 2016-02-24 2016-04-06 Rolls Royce Plc A combustion chamber
US10739001B2 (en) 2017-02-14 2020-08-11 Raytheon Technologies Corporation Combustor liner panel shell interface for a gas turbine engine combustor
US10823411B2 (en) 2017-02-23 2020-11-03 Raytheon Technologies Corporation Combustor liner panel end rail cooling enhancement features for a gas turbine engine combustor
US10830434B2 (en) 2017-02-23 2020-11-10 Raytheon Technologies Corporation Combustor liner panel end rail with curved interface passage for a gas turbine engine combustor
US10677462B2 (en) 2017-02-23 2020-06-09 Raytheon Technologies Corporation Combustor liner panel end rail angled cooling interface passage for a gas turbine engine combustor
US10718521B2 (en) 2017-02-23 2020-07-21 Raytheon Technologies Corporation Combustor liner panel end rail cooling interface passage for a gas turbine engine combustor
US10941937B2 (en) 2017-03-20 2021-03-09 Raytheon Technologies Corporation Combustor liner with gasket for gas turbine engine
DE102019212039A1 (en) * 2019-08-12 2021-02-18 Rolls-Royce Deutschland Ltd & Co Kg Combustion chamber assembly with segmented wall structure and relief channel in the area of a segmentation slot and manufacturing process

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4361010A (en) * 1980-04-02 1982-11-30 United Technologies Corporation Combustor liner construction
GB2087065B (en) * 1980-11-08 1984-11-07 Rolls Royce Wall structure for a combustion chamber
US4622821A (en) * 1985-01-07 1986-11-18 United Technologies Corporation Combustion liner for a gas turbine engine
DE3803086C2 (en) * 1987-02-06 1997-06-26 Gen Electric Combustion chamber for a gas turbine engine
GB9803291D0 (en) * 1998-02-18 1998-04-08 Chapman H C Combustion apparatus

Also Published As

Publication number Publication date
GB2355301A (en) 2001-04-18

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)