GB0806898D0 - A combustion chamber cooling method and system - Google Patents

A combustion chamber cooling method and system

Info

Publication number
GB0806898D0
GB0806898D0 GBGB0806898.3A GB0806898A GB0806898D0 GB 0806898 D0 GB0806898 D0 GB 0806898D0 GB 0806898 A GB0806898 A GB 0806898A GB 0806898 D0 GB0806898 D0 GB 0806898D0
Authority
GB
United Kingdom
Prior art keywords
combustion chamber
cooling method
chamber cooling
combustion
cooling
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.)
Ceased
Application number
GBGB0806898.3A
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.)
TURBINE DEVELOPMENTS NI Ltd
Original Assignee
TURBINE DEVELOPMENTS NI Ltd
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 TURBINE DEVELOPMENTS NI Ltd filed Critical TURBINE DEVELOPMENTS NI Ltd
Priority to GBGB0806898.3A priority Critical patent/GB0806898D0/en
Publication of GB0806898D0 publication Critical patent/GB0806898D0/en
Priority to GB0906077.3A priority patent/GB2459177B/en
Ceased legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • 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
    • F23R3/02—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
    • 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
    • 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
    • F23R2900/03042—Film 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)
GBGB0806898.3A 2008-04-16 2008-04-16 A combustion chamber cooling method and system Ceased GB0806898D0 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GBGB0806898.3A GB0806898D0 (en) 2008-04-16 2008-04-16 A combustion chamber cooling method and system
GB0906077.3A GB2459177B (en) 2008-04-16 2009-04-08 A combustion chamber cooling method and system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB0806898.3A GB0806898D0 (en) 2008-04-16 2008-04-16 A combustion chamber cooling method and system

Publications (1)

Publication Number Publication Date
GB0806898D0 true GB0806898D0 (en) 2008-05-21

Family

ID=39472178

Family Applications (2)

Application Number Title Priority Date Filing Date
GBGB0806898.3A Ceased GB0806898D0 (en) 2008-04-16 2008-04-16 A combustion chamber cooling method and system
GB0906077.3A Expired - Fee Related GB2459177B (en) 2008-04-16 2009-04-08 A combustion chamber cooling method and system

Family Applications After (1)

Application Number Title Priority Date Filing Date
GB0906077.3A Expired - Fee Related GB2459177B (en) 2008-04-16 2009-04-08 A combustion chamber cooling method and system

Country Status (1)

Country Link
GB (2) GB0806898D0 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105716121B (en) * 2014-12-04 2018-06-22 中国航空工业集团公司沈阳发动机设计研究所 Novel flame tube structure

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19547703C2 (en) * 1995-12-20 1999-02-18 Mtu Muenchen Gmbh Combustion chamber, in particular ring combustion chamber, for gas turbine engines
US6098397A (en) * 1998-06-08 2000-08-08 Caterpillar Inc. Combustor for a low-emissions gas turbine engine
FR2842564B1 (en) * 2002-07-17 2006-01-21 Snecma Moteurs ASSISTANCE AND RELIEF FOR THE ELECTRICAL DRIVING OF ACCESSORIES IN A TURBOMOTEUR
US7617684B2 (en) * 2007-11-13 2009-11-17 Opra Technologies B.V. Impingement cooled can combustor

Also Published As

Publication number Publication date
GB2459177A (en) 2009-10-21
GB0906077D0 (en) 2009-05-20
GB2459177B (en) 2012-06-06

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Legal Events

Date Code Title Description
AT Applications terminated before publication under section 16(1)