DE69719671D1 - Gasturbinenbrennkammer - Google Patents

Gasturbinenbrennkammer

Info

Publication number
DE69719671D1
DE69719671D1 DE69719671T DE69719671T DE69719671D1 DE 69719671 D1 DE69719671 D1 DE 69719671D1 DE 69719671 T DE69719671 T DE 69719671T DE 69719671 T DE69719671 T DE 69719671T DE 69719671 D1 DE69719671 D1 DE 69719671D1
Authority
DE
Germany
Prior art keywords
gas turbine
turbine combustor
combustor
gas
turbine
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.)
Expired - Lifetime
Application number
DE69719671T
Other languages
English (en)
Other versions
DE69719671T2 (de
Inventor
John Guy Allen
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
Application granted granted Critical
Publication of DE69719671D1 publication Critical patent/DE69719671D1/de
Publication of DE69719671T2 publication Critical patent/DE69719671T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
    • 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
    • F23R3/10—Air inlet arrangements for primary air
    • 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)
  • Spray-Type Burners (AREA)
DE1997619671 1996-11-07 1997-10-17 Gasturbinenbrennkammer Expired - Lifetime DE69719671T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB9623195.6A GB9623195D0 (en) 1996-11-07 1996-11-07 Gas turbine engine combustor

Publications (2)

Publication Number Publication Date
DE69719671D1 true DE69719671D1 (de) 2003-04-17
DE69719671T2 DE69719671T2 (de) 2003-08-14

Family

ID=10802586

Family Applications (1)

Application Number Title Priority Date Filing Date
DE1997619671 Expired - Lifetime DE69719671T2 (de) 1996-11-07 1997-10-17 Gasturbinenbrennkammer

Country Status (3)

Country Link
EP (1) EP0841520B1 (de)
DE (1) DE69719671T2 (de)
GB (1) GB9623195D0 (de)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10048864A1 (de) * 2000-10-02 2002-04-11 Rolls Royce Deutschland Brennkammerkopf für eine Gasturbine
US6923002B2 (en) * 2003-08-28 2005-08-02 General Electric Company Combustion liner cap assembly for combustion dynamics reduction
US8312627B2 (en) * 2006-12-22 2012-11-20 General Electric Company Methods for repairing combustor liners
FR3033028B1 (fr) * 2015-02-25 2019-12-27 Safran Helicopter Engines Chambre de combustion de turbomachine comportant une piece penetrante avec ouverture
GB201701380D0 (en) 2016-12-20 2017-03-15 Rolls Royce Plc A combustion chamber and a combustion chamber fuel injector seal

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4914918A (en) * 1988-09-26 1990-04-10 United Technologies Corporation Combustor segmented deflector
US4934145A (en) * 1988-10-12 1990-06-19 United Technologies Corporation Combustor bulkhead heat shield assembly
DE4427222A1 (de) * 1994-08-01 1996-02-08 Bmw Rolls Royce Gmbh Hitzeschild für eine Gasturbinen-Brennkammer
DE19508111A1 (de) * 1995-03-08 1996-09-12 Bmw Rolls Royce Gmbh Hitzeschild-Anordnung für eine Gasturbinen-Brennkammer

Also Published As

Publication number Publication date
DE69719671T2 (de) 2003-08-14
EP0841520A2 (de) 1998-05-13
EP0841520B1 (de) 2003-03-12
GB9623195D0 (en) 1997-01-08
EP0841520A3 (de) 1999-11-03

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition