FR2410138B2 - - Google Patents

Info

Publication number
FR2410138B2
FR2410138B2 FR7735875A FR7735875A FR2410138B2 FR 2410138 B2 FR2410138 B2 FR 2410138B2 FR 7735875 A FR7735875 A FR 7735875A FR 7735875 A FR7735875 A FR 7735875A FR 2410138 B2 FR2410138 B2 FR 2410138B2
Authority
FR
France
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
FR7735875A
Other languages
French (fr)
Other versions
FR2410138A2 (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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR7735875A priority Critical patent/FR2410138A2/fr
Priority to US05/964,427 priority patent/US4241586A/en
Priority to GB7846282A priority patent/GB2008683B/en
Priority to DE19782851666 priority patent/DE2851666A1/de
Publication of FR2410138A2 publication Critical patent/FR2410138A2/fr
Application granted granted Critical
Publication of FR2410138B2 publication Critical patent/FR2410138B2/fr
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/10Air inlet arrangements for primary air
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002Wall structures
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00Function
    • F05B2260/20Heat transfer, e.g. cooling
    • F05B2260/201Heat transfer, e.g. cooling by impingement of a fluid
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00Function
    • F05B2260/20Heat transfer, e.g. cooling
    • F05B2260/202Heat transfer, e.g. cooling by film cooling
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spray-Type Burners (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
FR7735875A 1977-11-29 1977-11-29 Perfectionnements aux chambres de combustion pour moteur a turbine a gaz Granted FR2410138A2 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR7735875A FR2410138A2 (fr) 1977-11-29 1977-11-29 Perfectionnements aux chambres de combustion pour moteur a turbine a gaz
US05/964,427 US4241586A (en) 1977-11-29 1978-11-28 Combustion chamber of gas turbine engines
GB7846282A GB2008683B (en) 1977-11-29 1978-11-28 Gas turbine combusition chamber
DE19782851666 DE2851666A1 (de) 1977-11-29 1978-11-29 Brennkammer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7735875A FR2410138A2 (fr) 1977-11-29 1977-11-29 Perfectionnements aux chambres de combustion pour moteur a turbine a gaz

Publications (2)

Publication Number Publication Date
FR2410138A2 FR2410138A2 (fr) 1979-06-22
FR2410138B2 true FR2410138B2 (US20110009641A1-20110113-C00116.png) 1980-08-22

Family

ID=9198195

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7735875A Granted FR2410138A2 (fr) 1977-11-29 1977-11-29 Perfectionnements aux chambres de combustion pour moteur a turbine a gaz

Country Status (4)

Country Link
US (1) US4241586A (US20110009641A1-20110113-C00116.png)
DE (1) DE2851666A1 (US20110009641A1-20110113-C00116.png)
FR (1) FR2410138A2 (US20110009641A1-20110113-C00116.png)
GB (1) GB2008683B (US20110009641A1-20110113-C00116.png)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2044912B (en) * 1979-03-22 1983-02-23 Rolls Royce Gas turbine combustion chamber
GB9018013D0 (en) * 1990-08-16 1990-10-03 Rolls Royce Plc Gas turbine engine combustor
US5307637A (en) * 1992-07-09 1994-05-03 General Electric Company Angled multi-hole film cooled single wall combustor dome plate
US5331805A (en) * 1993-04-22 1994-07-26 Alliedsignal Inc. Reduced diameter annular combustor
US5444982A (en) * 1994-01-12 1995-08-29 General Electric Company Cyclonic prechamber with a centerbody
FR2733582B1 (fr) * 1995-04-26 1997-06-06 Snecma Chambre de combustion comportant une multiperforation d'inclinaison axiale et tangentielle variable
US6751961B2 (en) * 2002-05-14 2004-06-22 United Technologies Corporation Bulkhead panel for use in a combustion chamber of a gas turbine engine
US7093439B2 (en) * 2002-05-16 2006-08-22 United Technologies Corporation Heat shield panels for use in a combustor for a gas turbine engine
US6792757B2 (en) 2002-11-05 2004-09-21 Honeywell International Inc. Gas turbine combustor heat shield impingement cooling baffle
FR2897107B1 (fr) * 2006-02-09 2013-01-18 Snecma Paroi transversale de chambre de combustion munie de trous de multiperforation
US7762070B2 (en) * 2006-05-11 2010-07-27 Siemens Energy, Inc. Pilot nozzle heat shield having internal turbulators
US20100050640A1 (en) * 2008-08-29 2010-03-04 General Electric Company Thermally compliant combustion cap device and system
US10378775B2 (en) * 2012-03-23 2019-08-13 Pratt & Whitney Canada Corp. Combustor heat shield
EP2986916A1 (de) * 2013-05-21 2016-02-24 Siemens Aktiengesellschaft Hitzeschildkachel für einen hitzeschild einer brennkammer
GB201715366D0 (en) * 2017-09-22 2017-11-08 Rolls Royce Plc A combustion chamber
US11739935B1 (en) * 2022-03-23 2023-08-29 General Electric Company Dome structure providing a dome-deflector cavity with counter-swirled airflow

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE892096C (de) * 1950-12-02 1953-08-20 Armstrong Siddeley'Motors Limited, Coventry, Warwickshire (Großbritannien) Brennkammer für flüssigen Kraftstoff
GB798474A (en) * 1955-03-16 1958-07-23 Bristol Aero Engines Ltd Improvements in or relating to combustion chambers
US2956404A (en) * 1956-10-02 1960-10-18 Avco Mfg Corp Fuel vaporizer
GB943250A (en) * 1962-02-01 1963-12-04 Rolls Royce Improvements in or relating to gas turbine combustion chambers
GB1429677A (en) * 1973-03-20 1976-03-24 Rolls Royce Gas turbine engine combustion equipment
FR2312654A1 (fr) * 1975-05-28 1976-12-24 Snecma Perfectionnements aux chambres de combustion pour moteurs a turbine a gaz

Also Published As

Publication number Publication date
GB2008683A (en) 1979-06-06
DE2851666A1 (de) 1979-05-31
GB2008683B (en) 1982-04-28
US4241586A (en) 1980-12-30
FR2410138A2 (fr) 1979-06-22
DE2851666C2 (US20110009641A1-20110113-C00116.png) 1987-01-22

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