BE597174A - Combustion equipment for a gas turbine engine. - Google Patents

Combustion equipment for a gas turbine engine.

Info

Publication number
BE597174A
BE597174A BE597174A BE597174A BE597174A BE 597174 A BE597174 A BE 597174A BE 597174 A BE597174 A BE 597174A BE 597174 A BE597174 A BE 597174A BE 597174 A BE597174 A BE 597174A
Authority
BE
Belgium
Prior art keywords
gas turbine
turbine engine
combustion equipment
combustion
equipment
Prior art date
Application number
BE597174A
Other languages
French (fr)
Inventor
Ralph James
Stewart Crichton Miller
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 BE597174A publication Critical patent/BE597174A/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
    • F23R3/06—Arrangement of apertures along the flame tube
    • F23R3/08—Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections
    • 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
    • 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
    • F23R3/06—Arrangement of apertures along the flame tube

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)
BE597174A 1959-11-20 1960-11-17 Combustion equipment for a gas turbine engine. BE597174A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB39549/59A GB887639A (en) 1959-11-20 1959-11-20 Combustion equipment for a gas turbine engine

Publications (1)

Publication Number Publication Date
BE597174A true BE597174A (en) 1961-03-15

Family

ID=10410157

Family Applications (1)

Application Number Title Priority Date Filing Date
BE597174A BE597174A (en) 1959-11-20 1960-11-17 Combustion equipment for a gas turbine engine.

Country Status (6)

Country Link
US (1) US3113431A (en)
BE (1) BE597174A (en)
DE (1) DE1155940B (en)
ES (1) ES262327A1 (en)
GB (1) GB887639A (en)
NL (2) NL257968A (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB943250A (en) * 1962-02-01 1963-12-04 Rolls Royce Improvements in or relating to gas turbine combustion chambers
US3359724A (en) * 1965-08-03 1967-12-26 Bristol Siddeley Engines Ltd Cooling means in combustors for gas turbine engines
US3369363A (en) * 1966-01-19 1968-02-20 Gen Electric Integral spacing rings for annular combustion chambers
FR2155835B1 (en) * 1971-10-08 1974-05-31 Snecma
US4132066A (en) * 1977-09-23 1979-01-02 United Technologies Corporation Combustor liner for gas turbine engine
GB2017827B (en) * 1978-04-04 1983-02-02 Gen Electric Combustor liner cooling
US5259182A (en) * 1989-12-22 1993-11-09 Hitachi, Ltd. Combustion apparatus and combustion method therein

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2537033A (en) * 1947-07-18 1951-01-09 Westinghouse Electric Corp Gas turbine combustion chamber construction
US2658337A (en) * 1947-12-23 1953-11-10 Lucas Ltd Joseph Combustion chamber for prime movers
DE830267C (en) * 1947-12-23 1952-02-04 Lucas Ltd Joseph Combustion chamber for recoil engines u. like. prime movers
GB723413A (en) * 1949-07-22 1955-02-09 Lysholm Alf Improvements in combustion chambers for gas turbines, jet propulsion plants and the like
GB762596A (en) * 1954-02-18 1956-11-28 Armstrong Siddeley Motors Ltd A combustion chamber, particularly for a gas turbine engine
US2973624A (en) * 1955-10-26 1961-03-07 Gen Electric Cowled dome liners
FR1188614A (en) * 1956-11-21 1959-09-24 Rolls Royce Improvements to combustion equipment for gas turbine engines
DE1066385B (en) * 1956-11-21 1959-10-01 Rolls-Royce Limited, Derby (Großbritannien) Burning plant of gas tank aggregates
GB845971A (en) * 1958-07-21 1960-08-24 Gen Electric Improvements relating to combustion chambers for gas turbine engines

Also Published As

Publication number Publication date
ES262327A1 (en) 1961-01-16
NL257968A (en)
NL127178C (en)
GB887639A (en) 1962-01-24
US3113431A (en) 1963-12-10
DE1155940B (en) 1963-10-17

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