GB744593A - Improvements in or relating to combustion equipment of gas turbine engines - Google Patents

Improvements in or relating to combustion equipment of gas turbine engines

Info

Publication number
GB744593A
GB744593A GB627/52A GB62752A GB744593A GB 744593 A GB744593 A GB 744593A GB 627/52 A GB627/52 A GB 627/52A GB 62752 A GB62752 A GB 62752A GB 744593 A GB744593 A GB 744593A
Authority
GB
United Kingdom
Prior art keywords
air
apertures
ring
flame tube
walls
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
Application number
GB627/52A
Other languages
English (en)
Inventor
Ralph Janes
Vernon Wallace Greenhough
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
Publication of GB744593A publication Critical patent/GB744593A/en
Expired 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
    • F23R3/045—Air inlet arrangements using pipes
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
GB627/52A 1952-01-08 1952-01-08 Improvements in or relating to combustion equipment of gas turbine engines Expired GB744593A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB313233X 1952-01-08
GB50153X 1953-01-05

Publications (1)

Publication Number Publication Date
GB744593A true GB744593A (en) 1956-02-08

Family

ID=26239529

Family Applications (1)

Application Number Title Priority Date Filing Date
GB627/52A Expired GB744593A (en) 1952-01-08 1952-01-08 Improvements in or relating to combustion equipment of gas turbine engines

Country Status (4)

Country Link
BE (1) BE516800A (zh)
CH (1) CH313233A (zh)
FR (1) FR1073487A (zh)
GB (1) GB744593A (zh)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2966356A1 (en) * 2014-07-10 2016-01-13 Alstom Technology Ltd Sequential combustor arrangement with a mixer

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2930193A (en) * 1955-08-29 1960-03-29 Gen Electric Cowled dome liner for combustors
DE1060667B (de) * 1955-10-15 1959-07-02 Stroemungsmasch Anst Verbrennungseinrichtung fuer Gasturbinen
US2930194A (en) * 1956-11-19 1960-03-29 Bendix Aviat Corp Combustor having high turbulent mixing for turbine-type starter
US2979898A (en) * 1958-04-25 1961-04-18 United Aircraft Corp Hooded crossover tube
DE1181004B (de) * 1959-03-11 1964-11-05 Rolls Royce Brennkammer fuer Gasturbinenstrahltriebwerke
FR2222124A1 (en) * 1973-03-23 1974-10-18 Pillard Chauffage Combustion gases homogenizing equipment - ensures uniform temperatures for drying plants, gas turbines and jet engines
FR2673454B1 (fr) * 1991-02-28 1995-01-13 Snecma Chambre de combustion comportant une paroi de fond comprenant une pluralite de troncs de cones partiels.

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2966356A1 (en) * 2014-07-10 2016-01-13 Alstom Technology Ltd Sequential combustor arrangement with a mixer
CN105258157A (zh) * 2014-07-10 2016-01-20 阿尔斯通技术有限公司 带有混合器的顺序燃烧器组件
US10215417B2 (en) 2014-07-10 2019-02-26 Ansaldo Energia Switzerland AG Sequential combustor arrangement with a mixer
CN105258157B (zh) * 2014-07-10 2019-11-05 安萨尔多能源瑞士股份公司 带有混合器的顺序燃烧器组件

Also Published As

Publication number Publication date
CH313233A (de) 1956-03-31
FR1073487A (fr) 1954-09-27
BE516800A (zh)

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