CH313233A - Combustion device in gas turbine plants - Google Patents

Combustion device in gas turbine plants

Info

Publication number
CH313233A
CH313233A CH313233DA CH313233A CH 313233 A CH313233 A CH 313233A CH 313233D A CH313233D A CH 313233DA CH 313233 A CH313233 A CH 313233A
Authority
CH
Switzerland
Prior art keywords
gas turbine
combustion device
turbine plants
plants
combustion
Prior art date
Application number
Other languages
German (de)
Inventor
Janes Ralph
Greenhough Vernon Wallace
Original Assignee
Rolls Royce
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 filed Critical Rolls Royce
Publication of CH313233A publication Critical patent/CH313233A/en

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)
CH313233D 1952-01-08 1953-01-08 Combustion device in gas turbine plants CH313233A (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
CH313233A true CH313233A (en) 1956-03-31

Family

ID=26239529

Family Applications (1)

Application Number Title Priority Date Filing Date
CH313233D CH313233A (en) 1952-01-08 1953-01-08 Combustion device in gas turbine plants

Country Status (4)

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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1181004B (en) * 1959-03-11 1964-11-05 Rolls Royce Combustion chamber for gas turbine jet engines

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 (en) * 1955-10-15 1959-07-02 Stroemungsmasch Anst Combustion device for gas turbines
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
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 (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 (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1181004B (en) * 1959-03-11 1964-11-05 Rolls Royce Combustion chamber for gas turbine jet engines

Also Published As

Publication number Publication date
FR1073487A (en) 1954-09-27
BE516800A (en)
GB744593A (en) 1956-02-08

Similar Documents

Publication Publication Date Title
CH309297A (en) Combustion device in gas turbine plants.
CH265007A (en) Combustion device for gas turbine plants.
CH335302A (en) Aircraft gas turbine plant
CH322023A (en) Gas turbine plant
CH364145A (en) Gas turbine engine
CH324501A (en) Gas turbine jet engine
CH336645A (en) Gas turbine plant
CH311370A (en) Gas turbine rotor.
CH368974A (en) Gas turbine engine
CH319835A (en) Airplane with gas turbine engine
CH310039A (en) Combustion device in gas turbine plants.
CH313233A (en) Combustion device in gas turbine plants
FR1080357A (en) Improvements to anti-detonating fuels
CH313856A (en) Heating unit for internal combustion turbines
CH342036A (en) Exhaust gas turbine
CH316253A (en) Fuel supply device in gas turbine systems
FR1084493A (en) Turbo-machine with adjustable guide vanes
CH304500A (en) Gas turbine plant.
CH318027A (en) Gas turbine plant
CH313030A (en) Combustion device in gas turbine plants
CH343180A (en) Gas turbine plant
FR1058863A (en) advanced wind turbine
AT170528B (en) Gas turbine
FR1082680A (en) Fuel injector
CH318576A (en) Gas turbine plant