ES262327A1 - Una instalaciën de combustiën para un motor de turbina de gas - Google Patents

Una instalaciën de combustiën para un motor de turbina de gas

Info

Publication number
ES262327A1
ES262327A1 ES0262327A ES262327A ES262327A1 ES 262327 A1 ES262327 A1 ES 262327A1 ES 0262327 A ES0262327 A ES 0262327A ES 262327 A ES262327 A ES 262327A ES 262327 A1 ES262327 A1 ES 262327A1
Authority
ES
Spain
Prior art keywords
gas turbine
turbine engine
space
air
flame tube
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
ES0262327A
Other languages
English (en)
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 ES262327A1 publication Critical patent/ES262327A1/es
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
    • F23R3/06—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)

Abstract

Una instalación de combustión para un motor de turbina de gas, que comprende una caja de aire y un tubo de llamas montado en ella con un espacio entre ellos, comprendiendo dicho tubo de llamas al menos dos partes axialmente consecutivas entre las cuales está dispuesto un miembro para transmisión de aire, de enfriamiento, a través del cual puede pasar aire desde dicho espacio y por encima de la superficie interna del tubo de llamas de manera que lo enfríe, estando dicho miembro de transmisión del aire de enfriamiento formado para transmitir aire de enfriamiento más fácilmente en al menos una zona localizada en la que hay un paso restringido de aire desde dicho espacio.
ES0262327A 1959-11-20 1960-11-10 Una instalaciën de combustiën para un motor de turbina de gas Expired ES262327A1 (es)

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
ES262327A1 true ES262327A1 (es) 1961-01-16

Family

ID=10410157

Family Applications (1)

Application Number Title Priority Date Filing Date
ES0262327A Expired ES262327A1 (es) 1959-11-20 1960-11-10 Una instalaciën de combustiën para un motor de turbina de gas

Country Status (6)

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

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 (es) * 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
DE830267C (de) * 1947-12-23 1952-02-04 Lucas Ltd Joseph Verbrennungskammer fuer Rueckstossmotoren u. dgl. Kraftmaschinen
US2658337A (en) * 1947-12-23 1953-11-10 Lucas Ltd Joseph Combustion chamber for 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 (fr) * 1956-11-21 1959-09-24 Rolls Royce Perfectionnements aux appareillages de combustion des moteurs à turbine à gaz
DE1066385B (de) * 1956-11-21 1959-10-01 Rolls-Royce Limited, Derby (Großbritannien) Brennanlage von Gastufbmenaggregaten
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
US3113431A (en) 1963-12-10
GB887639A (en) 1962-01-24
NL127178C (es)
BE597174A (fr) 1961-03-15
DE1155940B (de) 1963-10-17
NL257968A (es)

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