GB9926260D0 - Wall elements for gas turbine engines combustors - Google Patents

Wall elements for gas turbine engines combustors

Info

Publication number
GB9926260D0
GB9926260D0 GBGB9926260.2A GB9926260A GB9926260D0 GB 9926260 D0 GB9926260 D0 GB 9926260D0 GB 9926260 A GB9926260 A GB 9926260A GB 9926260 D0 GB9926260 D0 GB 9926260D0
Authority
GB
United Kingdom
Prior art keywords
combustors
gas turbine
wall elements
turbine engines
engines
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Withdrawn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
GBGB9926260.2A
Other versions
GB2356042A (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 GB9926260A priority Critical patent/GB2356042A/en
Publication of GB9926260D0 publication Critical patent/GB9926260D0/en
Publication of GB2356042A publication Critical patent/GB2356042A/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Withdrawn legal-status Critical Current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
    • F23R3/02—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)
GB9926260A 1999-11-06 1999-11-06 Improvements in or relating to wall elements for gas turbine engines Withdrawn GB2356042A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9926260A GB2356042A (en) 1999-11-06 1999-11-06 Improvements in or relating to wall elements for gas turbine engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9926260A GB2356042A (en) 1999-11-06 1999-11-06 Improvements in or relating to wall elements for gas turbine engines

Publications (2)

Publication Number Publication Date
GB9926260D0 true GB9926260D0 (en) 2000-01-12
GB2356042A GB2356042A (en) 2001-05-09

Family

ID=10864038

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9926260A Withdrawn GB2356042A (en) 1999-11-06 1999-11-06 Improvements in or relating to wall elements for gas turbine engines

Country Status (1)

Country Link
GB (1) GB2356042A (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7581385B2 (en) * 2005-11-03 2009-09-01 United Technologies Corporation Metering sheet and iso-grid arrangement for a non axi-symmetric shaped cooling liner within a gas turbine engine exhaust duct
GB0601418D0 (en) 2006-01-25 2006-03-08 Rolls Royce Plc Wall elements for gas turbine engine combustors
EP1813869A3 (en) 2006-01-25 2013-08-14 Rolls-Royce plc Wall elements for gas turbine engine combustors
GB0601413D0 (en) 2006-01-25 2006-03-08 Rolls Royce Plc Wall elements for gas turbine engine combustors
US8307657B2 (en) * 2009-03-10 2012-11-13 General Electric Company Combustor liner cooling system
GB201114745D0 (en) * 2011-08-26 2011-10-12 Rolls Royce Plc Wall elements for gas turbine engines
EP2956647B1 (en) * 2013-02-14 2019-05-08 United Technologies Corporation Combustor liners with u-shaped cooling channels and method of cooling
EP3039347B1 (en) * 2013-08-30 2019-10-23 United Technologies Corporation Gas turbine engine wall assembly with support shell contour regions
US20160238249A1 (en) * 2013-10-18 2016-08-18 United Technologies Corporation Combustor wall having cooling element(s) within a cooling cavity
US10690348B2 (en) 2013-11-04 2020-06-23 Raytheon Technologies Corporation Turbine engine combustor heat shield with one or more cooling elements
GB201501971D0 (en) 2015-02-06 2015-03-25 Rolls Royce Plc A combustion chamber
GB2545459B (en) 2015-12-17 2020-05-06 Rolls Royce Plc A combustion chamber
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 (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4071194A (en) * 1976-10-28 1978-01-31 The United States Of America As Represented By The Secretary Of The Navy Means for cooling exhaust nozzle sidewalls
US4653279A (en) * 1985-01-07 1987-03-31 United Technologies Corporation Integral refilmer lip for floatwall panels
US4751962A (en) * 1986-02-10 1988-06-21 General Motors Corporation Temperature responsive laminated porous metal panel
US4773593A (en) * 1987-05-04 1988-09-27 United Technologies Corporation Coolable thin metal sheet
GB2298266A (en) * 1995-02-23 1996-08-28 Rolls Royce Plc A cooling arrangement for heat resistant tiles in a gas turbine engine combustor

Also Published As

Publication number Publication date
GB2356042A (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)