FR2333126A1 - Dispositif de refrigeration pour chambre de combustion de moteur a turbine a gaz - Google Patents

Dispositif de refrigeration pour chambre de combustion de moteur a turbine a gaz

Info

Publication number
FR2333126A1
FR2333126A1 FR7635735A FR7635735A FR2333126A1 FR 2333126 A1 FR2333126 A1 FR 2333126A1 FR 7635735 A FR7635735 A FR 7635735A FR 7635735 A FR7635735 A FR 7635735A FR 2333126 A1 FR2333126 A1 FR 2333126A1
Authority
FR
France
Prior art keywords
combustion chamber
gas turbine
turbine engine
refrigeration device
engine combustion
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.)
Granted
Application number
FR7635735A
Other languages
English (en)
French (fr)
Other versions
FR2333126B1 (cg-RX-API-DMAC7.html
Inventor
Sidney Edward Slattery
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 FR2333126A1 publication Critical patent/FR2333126A1/fr
Application granted granted Critical
Publication of FR2333126B1 publication Critical patent/FR2333126B1/fr
Granted 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
    • F23R3/002—Wall structures
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
FR7635735A 1975-11-29 1976-11-26 Dispositif de refrigeration pour chambre de combustion de moteur a turbine a gaz Granted FR2333126A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB49138/75A GB1552132A (en) 1975-11-29 1975-11-29 Combustion chambers for gas turbine engines

Publications (2)

Publication Number Publication Date
FR2333126A1 true FR2333126A1 (fr) 1977-06-24
FR2333126B1 FR2333126B1 (cg-RX-API-DMAC7.html) 1982-07-16

Family

ID=10451306

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7635735A Granted FR2333126A1 (fr) 1975-11-29 1976-11-26 Dispositif de refrigeration pour chambre de combustion de moteur a turbine a gaz

Country Status (6)

Country Link
US (1) US4085580A (cg-RX-API-DMAC7.html)
JP (1) JPS5274713A (cg-RX-API-DMAC7.html)
DE (1) DE2653410C2 (cg-RX-API-DMAC7.html)
FR (1) FR2333126A1 (cg-RX-API-DMAC7.html)
GB (1) GB1552132A (cg-RX-API-DMAC7.html)
IT (1) IT1064440B (cg-RX-API-DMAC7.html)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2431096A1 (fr) * 1978-08-14 1980-02-08 Gen Electric Dome de chambre de combustion de moteur a turbine a gaz
FR2451998A1 (fr) * 1979-03-22 1980-10-17 Rolls Royce Chambre de combustion pour moteur a turbine a gaz a paroi amont specialement refrigeree
FR2479951A1 (fr) * 1980-04-02 1981-10-09 United Technologies Corp Garniture interieure de chambre de combustion
WO1992016798A1 (en) * 1991-03-22 1992-10-01 Rolls-Royce Plc Gas turbine engine combustor
US5435139A (en) * 1991-03-22 1995-07-25 Rolls-Royce Plc Removable combustor liner for gas turbine engine combustor

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4192138A (en) * 1977-08-29 1980-03-11 Westinghouse Electric Corp. Gas turbine combustor air inlet
DE3664374D1 (en) * 1985-12-02 1989-08-17 Siemens Ag Heat shield arrangement, especially for the structural components of a gas turbine plant
US4686823A (en) * 1986-04-28 1987-08-18 United Technologies Corporation Sliding joint for an annular combustor
US5265425A (en) * 1991-09-23 1993-11-30 General Electric Company Aero-slinger combustor
US5329772A (en) * 1992-12-09 1994-07-19 General Electric Company Cast slot-cooled single nozzle combustion liner cap
DE19516798A1 (de) * 1995-05-08 1996-11-14 Abb Management Ag Vormischbrenner mit axialer oder radialer Luftzuströmung
US6164074A (en) * 1997-12-12 2000-12-26 United Technologies Corporation Combustor bulkhead with improved cooling and air recirculation zone
US6711900B1 (en) * 2003-02-04 2004-03-30 Pratt & Whitney Canada Corp. Combustor liner V-band design
GB0913580D0 (en) * 2009-08-05 2009-09-16 Rolls Royce Plc Combustor tile
JP2013100765A (ja) * 2011-11-08 2013-05-23 Ihi Corp インピンジ冷却機構、タービン翼及び燃焼器
US20130298564A1 (en) * 2012-05-14 2013-11-14 General Electric Company Cooling system and method for turbine system
DE102012016493A1 (de) * 2012-08-21 2014-02-27 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenbrennkammer mit prallgekühlten Bolzen der Brennkammerschindeln
DE102012023297A1 (de) * 2012-11-28 2014-06-12 Rolls-Royce Deutschland Ltd & Co Kg Schindelbefestigungsanordnung einer Gasturbinenbrennkammer
GB201322838D0 (en) 2013-12-23 2014-02-12 Rolls Royce Plc A combustion chamber
KR20160004639A (ko) * 2014-07-03 2016-01-13 한화테크윈 주식회사 연소기 어셈블리
GB201413194D0 (en) 2014-07-25 2014-09-10 Rolls Royce Plc A liner element for a combustor, and a related method
US12129799B2 (en) 2022-12-29 2024-10-29 Ge Infrastructure Technology Llc Thermal radiation shield for a gaseous fuel circuit
US12305576B2 (en) 2022-12-29 2025-05-20 Ge Vernova Infrastructure Technology Llc Radiation shield for a gaseous fuel circuit

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB621238A (en) * 1947-02-10 1949-04-06 Lucas Ltd Joseph Improvements relating to liquid fuel combustion chambers
US2510645A (en) * 1946-10-26 1950-06-06 Gen Electric Air nozzle and porting for combustion chamber liners
US2547619A (en) * 1948-11-27 1951-04-03 Gen Electric Combustor with sectional housing and liner
US3656298A (en) * 1970-11-27 1972-04-18 Gen Motors Corp Combustion apparatus
FR2194881A1 (cg-RX-API-DMAC7.html) * 1972-08-02 1974-03-01 Gen Electric
FR2241055A1 (cg-RX-API-DMAC7.html) * 1973-08-16 1975-03-14 Rolls Royce

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL74196C (cg-RX-API-DMAC7.html) * 1947-08-11
US2657531A (en) * 1948-01-22 1953-11-03 Gen Electric Wall cooling arrangement for combustion devices
US2699648A (en) * 1950-10-03 1955-01-18 Gen Electric Combustor sectional liner structure with annular inlet nozzles
US2651912A (en) * 1950-10-31 1953-09-15 Gen Electric Combustor and cooling means therefor
BE535497A (cg-RX-API-DMAC7.html) * 1954-02-26
US3064424A (en) * 1959-09-30 1962-11-20 Gen Motors Corp Flame tube
US3064425A (en) * 1959-10-05 1962-11-20 Gen Motors Corp Combustion liner
GB1136543A (en) * 1966-02-21 1968-12-11 Rolls Royce Liquid fuel combustion apparatus for gas turbine engines
FR2152465B1 (cg-RX-API-DMAC7.html) * 1971-09-16 1975-02-21 Snecma
GB1424197A (en) * 1972-06-09 1976-02-11 Lucas Industries Ltd Combustion chambers for gas turbine engines
GB1429677A (en) * 1973-03-20 1976-03-24 Rolls Royce Gas turbine engine combustion equipment

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2510645A (en) * 1946-10-26 1950-06-06 Gen Electric Air nozzle and porting for combustion chamber liners
GB621238A (en) * 1947-02-10 1949-04-06 Lucas Ltd Joseph Improvements relating to liquid fuel combustion chambers
US2547619A (en) * 1948-11-27 1951-04-03 Gen Electric Combustor with sectional housing and liner
US3656298A (en) * 1970-11-27 1972-04-18 Gen Motors Corp Combustion apparatus
FR2194881A1 (cg-RX-API-DMAC7.html) * 1972-08-02 1974-03-01 Gen Electric
FR2241055A1 (cg-RX-API-DMAC7.html) * 1973-08-16 1975-03-14 Rolls Royce

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2431096A1 (fr) * 1978-08-14 1980-02-08 Gen Electric Dome de chambre de combustion de moteur a turbine a gaz
FR2451998A1 (fr) * 1979-03-22 1980-10-17 Rolls Royce Chambre de combustion pour moteur a turbine a gaz a paroi amont specialement refrigeree
FR2479951A1 (fr) * 1980-04-02 1981-10-09 United Technologies Corp Garniture interieure de chambre de combustion
WO1992016798A1 (en) * 1991-03-22 1992-10-01 Rolls-Royce Plc Gas turbine engine combustor
US5435139A (en) * 1991-03-22 1995-07-25 Rolls-Royce Plc Removable combustor liner for gas turbine engine combustor

Also Published As

Publication number Publication date
JPS5274713A (en) 1977-06-23
DE2653410A1 (de) 1977-06-08
FR2333126B1 (cg-RX-API-DMAC7.html) 1982-07-16
GB1552132A (en) 1979-09-12
US4085580A (en) 1978-04-25
DE2653410C2 (de) 1983-05-11
IT1064440B (it) 1985-02-18

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Legal Events

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CD Change of name or company name
ST Notification of lapse