FR2122308B1 - - Google Patents

Info

Publication number
FR2122308B1
FR2122308B1 FR7101683A FR7101683A FR2122308B1 FR 2122308 B1 FR2122308 B1 FR 2122308B1 FR 7101683 A FR7101683 A FR 7101683A FR 7101683 A FR7101683 A FR 7101683A FR 2122308 B1 FR2122308 B1 FR 2122308B1
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
FR7101683A
Other languages
French (fr)
Other versions
FR2122308A1 (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.)
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 FR7101683A priority Critical patent/FR2122308B1/fr
Priority to GB215372A priority patent/GB1329944A/en
Priority to US00218811A priority patent/US3768251A/en
Priority to DE2202508A priority patent/DE2202508C3/en
Publication of FR2122308A1 publication Critical patent/FR2122308A1/fr
Application granted granted Critical
Publication of FR2122308B1 publication Critical patent/FR2122308B1/fr
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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F02C7/222—Fuel flow conduits, e.g. manifolds

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
FR7101683A 1971-01-19 1971-01-19 Expired FR2122308B1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR7101683A FR2122308B1 (en) 1971-01-19 1971-01-19
GB215372A GB1329944A (en) 1971-01-19 1972-01-17 Mounting of fuel injection manifolds in combustion chambers
US00218811A US3768251A (en) 1971-01-19 1972-01-18 Fixing of fuel injection manifolds into combustion chambers
DE2202508A DE2202508C3 (en) 1971-01-19 1972-01-19 Arrangement for fastening an injection nozzle ring line in a combustion chamber

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7101683A FR2122308B1 (en) 1971-01-19 1971-01-19

Publications (2)

Publication Number Publication Date
FR2122308A1 FR2122308A1 (en) 1972-09-01
FR2122308B1 true FR2122308B1 (en) 1976-03-05

Family

ID=9070516

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7101683A Expired FR2122308B1 (en) 1971-01-19 1971-01-19

Country Status (4)

Country Link
US (1) US3768251A (en)
DE (1) DE2202508C3 (en)
FR (1) FR2122308B1 (en)
GB (1) GB1329944A (en)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4064691A (en) * 1975-11-04 1977-12-27 General Electric Company Cooling of fastener means for a removable flameholder
FR2586792B1 (en) * 1985-09-03 1989-06-16 Snecma CONNECTION DEVICE BETWEEN A BURNER RING OR FLAME HANGER OF COMPOSITE MATERIAL AND A POST-COMBUSTION CHAMBER CHANNEL OF A TURBOREACTOR
US5001897A (en) * 1989-12-20 1991-03-26 United Technologies Corporation Augmentor spray ring mount
US5127224A (en) * 1991-03-25 1992-07-07 United Technologies Corporation Spray-ring mounting assembly
US5271218A (en) * 1992-05-28 1993-12-21 Gerneral Electric Company Off-engine mounting system for steam and gaseous fuel manifolds of marine and industrial gas turbine engines
GB2298916B (en) * 1995-03-15 1998-11-04 Rolls Royce Plc Annular combustor
US6367240B1 (en) * 1998-06-22 2002-04-09 General Electric Company Air manifold system
US7654088B2 (en) * 2004-02-27 2010-02-02 Pratt & Whitney Canada Corp. Dual conduit fuel manifold for gas turbine engine
US20060156733A1 (en) * 2005-01-14 2006-07-20 Pratt & Whitney Canada Corp. Integral heater for fuel conveying member
US7540157B2 (en) * 2005-06-14 2009-06-02 Pratt & Whitney Canada Corp. Internally mounted fuel manifold with support pins
US8171738B2 (en) * 2006-10-24 2012-05-08 Pratt & Whitney Canada Corp. Gas turbine internal manifold mounting arrangement
US8418468B2 (en) 2010-04-06 2013-04-16 General Electric Company Segmented annular ring-manifold quaternary fuel distributor
US8438852B2 (en) 2010-04-06 2013-05-14 General Electric Company Annular ring-manifold quaternary fuel distributor
US20130180253A1 (en) * 2012-01-13 2013-07-18 General Electric Company System and method for supplying a working fluid to a combustor
US9267436B2 (en) * 2013-03-18 2016-02-23 General Electric Company Fuel distribution manifold for a combustor of a gas turbine
JP6210810B2 (en) * 2013-09-20 2017-10-11 三菱日立パワーシステムズ株式会社 Dual fuel fired gas turbine combustor
US11156162B2 (en) * 2018-05-23 2021-10-26 General Electric Company Fluid manifold damper for gas turbine engine
CN114165813B (en) * 2021-12-03 2022-08-30 北京航空航天大学 Pneumatic auxiliary integrated support plate stabilizer with double oil way oil supply
CN114412646B (en) * 2022-02-18 2024-03-19 中国航发贵阳发动机设计研究所 Fixing structure of stress application outer ring main pipe
CN114876646B (en) * 2022-07-11 2022-09-30 成都中科翼能科技有限公司 Supporting structure of gas turbine fuel main pipe and fuel main pipe assembly

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB821286A (en) * 1956-06-05 1959-10-07 Rolls Royce Improvements in or relating to reheat combustion equipment of jet-propulsion engines
US3102392A (en) * 1959-04-21 1963-09-03 Snecma Combustion equipment for jet propulsion units
US3056261A (en) * 1959-09-01 1962-10-02 Gen Electric Flameholder configuration
FR1477974A (en) * 1966-04-28 1967-04-21 United Aircraft Corp Improvements to post-combustion flame-holder devices for jet engines
US3646763A (en) * 1970-05-25 1972-03-07 Gen Electric Gas turbine engine with improved afterburner

Also Published As

Publication number Publication date
DE2202508B2 (en) 1980-07-10
US3768251A (en) 1973-10-30
DE2202508C3 (en) 1981-06-04
DE2202508A1 (en) 1972-07-27
GB1329944A (en) 1973-09-12
FR2122308A1 (en) 1972-09-01

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Legal Events

Date Code Title Description
ST Notification of lapse