FR2948749B1 - Systeme d'injection de carburant pour une chambre de combustion de turbomachine - Google Patents

Systeme d'injection de carburant pour une chambre de combustion de turbomachine

Info

Publication number
FR2948749B1
FR2948749B1 FR0903733A FR0903733A FR2948749B1 FR 2948749 B1 FR2948749 B1 FR 2948749B1 FR 0903733 A FR0903733 A FR 0903733A FR 0903733 A FR0903733 A FR 0903733A FR 2948749 B1 FR2948749 B1 FR 2948749B1
Authority
FR
France
Prior art keywords
combustion chamber
fuel injection
injection system
turbomachine combustion
turbomachine
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.)
Active
Application number
FR0903733A
Other languages
English (en)
Other versions
FR2948749A1 (fr
Inventor
Sebastien Alain Christophe Bourgois
Didier Hippolyte Hernandez
Lorenzo Hernandez
Christophe Nicolas Henri Viguier
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
Safran Helicopter Engines SAS
Original Assignee
Turbomeca SA
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 Turbomeca SA, SNECMA SAS filed Critical Turbomeca SA
Priority to FR0903733A priority Critical patent/FR2948749B1/fr
Publication of FR2948749A1 publication Critical patent/FR2948749A1/fr
Application granted granted Critical
Publication of FR2948749B1 publication Critical patent/FR2948749B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • 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
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00018—Manufacturing combustion chamber liners or subparts
FR0903733A 2009-07-29 2009-07-29 Systeme d'injection de carburant pour une chambre de combustion de turbomachine Active FR2948749B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0903733A FR2948749B1 (fr) 2009-07-29 2009-07-29 Systeme d'injection de carburant pour une chambre de combustion de turbomachine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0903733A FR2948749B1 (fr) 2009-07-29 2009-07-29 Systeme d'injection de carburant pour une chambre de combustion de turbomachine

Publications (2)

Publication Number Publication Date
FR2948749A1 FR2948749A1 (fr) 2011-02-04
FR2948749B1 true FR2948749B1 (fr) 2011-09-09

Family

ID=41814653

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0903733A Active FR2948749B1 (fr) 2009-07-29 2009-07-29 Systeme d'injection de carburant pour une chambre de combustion de turbomachine

Country Status (1)

Country Link
FR (1) FR2948749B1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2976649B1 (fr) * 2011-06-20 2015-01-23 Turbomeca Procede d'injection de carburant dans une chambre de combustion d'une turbine a gaz et systeme d'injection pour sa mise en oeuvre
US9447974B2 (en) 2012-09-13 2016-09-20 United Technologies Corporation Light weight swirler for gas turbine engine combustor and a method for lightening a swirler for a gas turbine engine
GB201617369D0 (en) * 2016-10-13 2016-11-30 Rolls Royce Plc A combustion chamber and a combustion chamber fuel injector seal
FR3091574B1 (fr) * 2019-01-08 2020-12-11 Safran Aircraft Engines Systeme d’injection pour turbomachine, comprenant une vrille et des trous tourbillonnaires de bol melangeur

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3570242A (en) * 1970-04-20 1971-03-16 United Aircraft Corp Fuel premixing for smokeless jet engine main burner
US6289676B1 (en) * 1998-06-26 2001-09-18 Pratt & Whitney Canada Corp. Simplex and duplex injector having primary and secondary annular lud channels and primary and secondary lud nozzles
US6863228B2 (en) * 2002-09-30 2005-03-08 Delavan Inc. Discrete jet atomizer
US7117678B2 (en) * 2004-04-02 2006-10-10 Pratt & Whitney Canada Corp. Fuel injector head
US7013649B2 (en) * 2004-05-25 2006-03-21 General Electric Company Gas turbine engine combustor mixer
US7237730B2 (en) * 2005-03-17 2007-07-03 Pratt & Whitney Canada Corp. Modular fuel nozzle and method of making
FR2896031B1 (fr) * 2006-01-09 2008-04-18 Snecma Sa Dispositif d'injection multimode pour chambre de combustion, notamment d'un turboreacteur

Also Published As

Publication number Publication date
FR2948749A1 (fr) 2011-02-04

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Owner name: SNECMA, FR

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Owner name: SAFRAN HELICOPTER ENGINES, FR

Effective date: 20170727

CD Change of name or company name

Owner name: SNECMA, FR

Effective date: 20170713

Owner name: SAFRAN HELICOPTER ENGINES, FR

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