FR1073487A - Improvements to combustion equipment for gas turbine engines - Google Patents

Improvements to combustion equipment for gas turbine engines

Info

Publication number
FR1073487A
FR1073487A FR1073487DA FR1073487A FR 1073487 A FR1073487 A FR 1073487A FR 1073487D A FR1073487D A FR 1073487DA FR 1073487 A FR1073487 A FR 1073487A
Authority
FR
France
Prior art keywords
gas turbine
turbine engines
combustion equipment
combustion
equipment
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
Other languages
French (fr)
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 FR1073487A publication Critical patent/FR1073487A/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)
FR1073487D 1952-01-08 1953-01-06 Improvements to combustion equipment for gas turbine engines Expired FR1073487A (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
FR1073487A true FR1073487A (en) 1954-09-27

Family

ID=26239529

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1073487D Expired FR1073487A (en) 1952-01-08 1953-01-06 Improvements to combustion equipment for gas turbine engines

Country Status (4)

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

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1060667B (en) * 1955-10-15 1959-07-02 Stroemungsmasch Anst Combustion device for gas turbines
US2930193A (en) * 1955-08-29 1960-03-29 Gen Electric Cowled dome liner for combustors
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

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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 (en) * 1959-03-11 1964-11-05 Rolls Royce Combustion chamber for gas turbine jet engines
FR2673454B1 (en) * 1991-02-28 1995-01-13 Snecma COMBUSTION CHAMBER COMPRISING A BOTTOM WALL COMPRISING A PLURALITY OF PARTIAL CONE TRUNKS.
EP2966356B1 (en) 2014-07-10 2020-01-08 Ansaldo Energia Switzerland AG Sequential combustor arrangement with a mixer

Cited By (3)

* 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 (en) * 1955-10-15 1959-07-02 Stroemungsmasch Anst Combustion device for gas turbines
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

Also Published As

Publication number Publication date
CH313233A (en) 1956-03-31
BE516800A (en)
GB744593A (en) 1956-02-08

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