GB0426214D0 - Combustor - Google Patents

Combustor

Info

Publication number
GB0426214D0
GB0426214D0 GBGB0426214.3A GB0426214A GB0426214D0 GB 0426214 D0 GB0426214 D0 GB 0426214D0 GB 0426214 A GB0426214 A GB 0426214A GB 0426214 D0 GB0426214 D0 GB 0426214D0
Authority
GB
United Kingdom
Prior art keywords
combustor
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
GBGB0426214.3A
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.)
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 GBGB0426214.3A priority Critical patent/GB0426214D0/en
Publication of GB0426214D0 publication Critical patent/GB0426214D0/en
Priority to EP05256724A priority patent/EP1662203B1/en
Priority to DE602005008688T priority patent/DE602005008688D1/en
Priority to US11/262,771 priority patent/US20060213203A1/en
Ceased 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means
    • 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
    • F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing

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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GBGB0426214.3A 2004-11-30 2004-11-30 Combustor Ceased GB0426214D0 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
GBGB0426214.3A GB0426214D0 (en) 2004-11-30 2004-11-30 Combustor
EP05256724A EP1662203B1 (en) 2004-11-30 2005-10-31 Combustor
DE602005008688T DE602005008688D1 (en) 2004-11-30 2005-10-31 combustion chamber
US11/262,771 US20060213203A1 (en) 2004-11-30 2005-11-01 Combustor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB0426214.3A GB0426214D0 (en) 2004-11-30 2004-11-30 Combustor

Publications (1)

Publication Number Publication Date
GB0426214D0 true GB0426214D0 (en) 2004-12-29

Family

ID=33561542

Family Applications (1)

Application Number Title Priority Date Filing Date
GBGB0426214.3A Ceased GB0426214D0 (en) 2004-11-30 2004-11-30 Combustor

Country Status (4)

Country Link
US (1) US20060213203A1 (en)
EP (1) EP1662203B1 (en)
DE (1) DE602005008688D1 (en)
GB (1) GB0426214D0 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9181812B1 (en) * 2009-05-05 2015-11-10 Majed Toqan Can-annular combustor with premixed tangential fuel-air nozzles for use on gas turbine engines

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2543755A (en) * 1946-07-25 1951-03-06 Westinghouse Electric Corp Air inlet opening arrangement for combustion chambers
US2513325A (en) * 1946-08-29 1950-07-04 Westinghouse Electric Corp Combustion apparatus
US2488911A (en) * 1946-11-09 1949-11-22 Surface Combustion Corp Combustion apparatus for use with turbines
US2782597A (en) * 1952-03-15 1957-02-26 Gen Electric Combustion chamber having improved air inlet means
US2952126A (en) * 1955-05-10 1960-09-13 Midland Ross Corp Combustion unit for supplying hot gas for jet aircraft
DE1066385B (en) * 1956-11-21 1959-10-01 Rolls-Royce Limited, Derby (Großbritannien) Burning plant of gas tank aggregates
JPS60194234A (en) * 1984-03-16 1985-10-02 Hitachi Ltd Combustor for gas turbine
US6681577B2 (en) * 2002-01-16 2004-01-27 General Electric Company Method and apparatus for relieving stress in a combustion case in a gas turbine engine

Also Published As

Publication number Publication date
EP1662203B1 (en) 2008-08-06
DE602005008688D1 (en) 2008-09-18
US20060213203A1 (en) 2006-09-28
EP1662203A1 (en) 2006-05-31

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Legal Events

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