GB9926242D0 - Combustion apparatus - Google Patents

Combustion apparatus

Info

Publication number
GB9926242D0
GB9926242D0 GBGB9926242.0A GB9926242A GB9926242D0 GB 9926242 D0 GB9926242 D0 GB 9926242D0 GB 9926242 A GB9926242 A GB 9926242A GB 9926242 D0 GB9926242 D0 GB 9926242D0
Authority
GB
United Kingdom
Prior art keywords
combustion apparatus
combustion
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Withdrawn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
GBGB9926242.0A
Other versions
GB2356041A (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 GB9926242A priority Critical patent/GB2356041A/en
Publication of GB9926242D0 publication Critical patent/GB9926242D0/en
Publication of GB2356041A publication Critical patent/GB2356041A/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Withdrawn legal-status Critical Current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
    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/06—Arrangement of apertures along the flame tube

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)
GB9926242A 1999-11-05 1999-11-05 Wall element for combustion apparatus Withdrawn GB2356041A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9926242A GB2356041A (en) 1999-11-05 1999-11-05 Wall element for combustion apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9926242A GB2356041A (en) 1999-11-05 1999-11-05 Wall element for combustion apparatus

Publications (2)

Publication Number Publication Date
GB9926242D0 true GB9926242D0 (en) 2000-01-12
GB2356041A GB2356041A (en) 2001-05-09

Family

ID=10864025

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9926242A Withdrawn GB2356041A (en) 1999-11-05 1999-11-05 Wall element for combustion apparatus

Country Status (1)

Country Link
GB (1) GB2356041A (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2373319B (en) * 2001-03-12 2005-03-30 Rolls Royce Plc Combustion apparatus
DE102012016493A1 (en) 2012-08-21 2014-02-27 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine combustor with impingement-cooled bolts of the combustion chamber shingles
GB201315871D0 (en) 2013-09-06 2013-10-23 Rolls Royce Plc A combustion chamber arrangement
WO2015116269A2 (en) * 2013-11-04 2015-08-06 United Technologies Corporation Quench aperture body for a turbine engine combustor
US10670273B2 (en) 2017-09-08 2020-06-02 Raytheon Technologies Corporation Cooling configurations for combustor attachment features
US10670274B2 (en) 2017-09-08 2020-06-02 Raytheon Technologies Corporation Cooling configurations for combustor attachment features
US10619857B2 (en) 2017-09-08 2020-04-14 United Technologies Corporation Cooling configuration for combustor attachment feature
US10670275B2 (en) 2017-09-08 2020-06-02 Raytheon Technologies Corporation Cooling configurations for combustor attachment features
US11359810B2 (en) 2017-12-22 2022-06-14 Raytheon Technologies Corporation Apparatus and method for mitigating particulate accumulation on a component of a gas turbine
GB202000870D0 (en) 2020-01-21 2020-03-04 Rolls Royce Plc A combustion chamber, a combustion chamber tile and a combustion chamber segment

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5329772A (en) * 1992-12-09 1994-07-19 General Electric Company Cast slot-cooled single nozzle combustion liner cap

Also Published As

Publication number Publication date
GB2356041A (en) 2001-05-09

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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)