FR2661714B1 - Dispositif d'alimentation en comburant d'une turbine a gaz. - Google Patents

Dispositif d'alimentation en comburant d'une turbine a gaz.

Info

Publication number
FR2661714B1
FR2661714B1 FR909005556A FR9005556A FR2661714B1 FR 2661714 B1 FR2661714 B1 FR 2661714B1 FR 909005556 A FR909005556 A FR 909005556A FR 9005556 A FR9005556 A FR 9005556A FR 2661714 B1 FR2661714 B1 FR 2661714B1
Authority
FR
France
Prior art keywords
gas turbine
supplying fuel
fuel
supplying
turbine
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 - Fee Related
Application number
FR909005556A
Other languages
English (en)
Other versions
FR2661714A1 (fr
Inventor
Forestier Alexandre
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 FR909005556A priority Critical patent/FR2661714B1/fr
Priority to US07/694,256 priority patent/US5159807A/en
Priority to DE91401167T priority patent/DE69100735T2/de
Priority to EP91401167A priority patent/EP0455559B1/fr
Publication of FR2661714A1 publication Critical patent/FR2661714A1/fr
Application granted granted Critical
Publication of FR2661714B1 publication Critical patent/FR2661714B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F23R3/26—Controlling the air flow
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2250/00—Geometry
    • F05B2250/40—Movement of component
    • F05B2250/41—Movement of component with one degree of freedom
    • F05B2250/411—Movement of component with one degree of freedom in rotation

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanically-Actuated Valves (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Actuator (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
FR909005556A 1990-05-03 1990-05-03 Dispositif d'alimentation en comburant d'une turbine a gaz. Expired - Fee Related FR2661714B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR909005556A FR2661714B1 (fr) 1990-05-03 1990-05-03 Dispositif d'alimentation en comburant d'une turbine a gaz.
US07/694,256 US5159807A (en) 1990-05-03 1991-05-01 Control system for oxidizer intake diaphragms
DE91401167T DE69100735T2 (de) 1990-05-03 1991-05-03 Verbrennungsluftzufuhreinrichtung für Gasturbine.
EP91401167A EP0455559B1 (fr) 1990-05-03 1991-05-03 Dispositif d'alimentation en comburant d'une turbine à gaz

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR909005556A FR2661714B1 (fr) 1990-05-03 1990-05-03 Dispositif d'alimentation en comburant d'une turbine a gaz.

Publications (2)

Publication Number Publication Date
FR2661714A1 FR2661714A1 (fr) 1991-11-08
FR2661714B1 true FR2661714B1 (fr) 1994-06-17

Family

ID=9396273

Family Applications (1)

Application Number Title Priority Date Filing Date
FR909005556A Expired - Fee Related FR2661714B1 (fr) 1990-05-03 1990-05-03 Dispositif d'alimentation en comburant d'une turbine a gaz.

Country Status (4)

Country Link
US (1) US5159807A (fr)
EP (1) EP0455559B1 (fr)
DE (1) DE69100735T2 (fr)
FR (1) FR2661714B1 (fr)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2676529B1 (fr) * 1991-05-16 1994-11-25 Snecma Dispositif d'alimentation en comburant d'une turbine a gaz comprenant des diaphragmes de reglage du debit.
DE4220060C2 (de) * 1992-06-19 1996-10-17 Mtu Muenchen Gmbh Einrichtung zur Betätigung einer den Durchsatz von Verbrennungsluft steuernden Dralleinrichtung eines Brenners für Gasturbinentriebwerke
FR2704628B1 (fr) * 1993-04-29 1995-06-09 Snecma Chambre de combustion comportant un système d'injection de comburant à géométrie variable.
FR2748553B1 (fr) * 1996-05-09 1998-06-19 Snecma Systeme d'injection a geometrie variable adoptant un debit d'air en fonction du regime moteur
FR2754590B1 (fr) * 1996-10-16 1998-11-20 Snecma Dispositif d'alimentation en comburant d'une turbine a gaz comprenant des diaphragmes de reglage du debit commandes par paires
FR2779807B1 (fr) * 1998-06-11 2000-07-13 Inst Francais Du Petrole Chambre de combustion de turbine a gaz a geometrie variable
EP1312865A1 (fr) * 2001-11-15 2003-05-21 Siemens Aktiengesellschaft Chambre de combustion annulaire de turbine à gaz
US7000396B1 (en) * 2004-09-02 2006-02-21 General Electric Company Concentric fixed dilution and variable bypass air injection for a combustor
FR2939171B1 (fr) * 2008-11-28 2010-12-31 Snecma Turbomachine a systemes d'injection de carburant distincts, utilisant des joints d'etancheite identiques.
US8276386B2 (en) * 2010-09-24 2012-10-02 General Electric Company Apparatus and method for a combustor
US9709279B2 (en) 2014-02-27 2017-07-18 General Electric Company System and method for control of combustion dynamics in combustion system
US9709278B2 (en) 2014-03-12 2017-07-18 General Electric Company System and method for control of combustion dynamics in combustion system
US9644846B2 (en) 2014-04-08 2017-05-09 General Electric Company Systems and methods for control of combustion dynamics and modal coupling in gas turbine engine
US9845956B2 (en) 2014-04-09 2017-12-19 General Electric Company System and method for control of combustion dynamics in combustion system
US9845732B2 (en) 2014-05-28 2017-12-19 General Electric Company Systems and methods for variation of injectors for coherence reduction in combustion system
US9551283B2 (en) * 2014-06-26 2017-01-24 General Electric Company Systems and methods for a fuel pressure oscillation device for reduction of coherence
US10113747B2 (en) 2015-04-15 2018-10-30 General Electric Company Systems and methods for control of combustion dynamics in combustion system

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2020416A1 (de) * 1970-04-27 1971-11-11 Motoren Turbinen Union Brennkammer fuer Gasturbinentriebwerke
FR2174672B1 (fr) * 1972-03-06 1975-06-13 Snecma
US3941313A (en) * 1972-03-06 1976-03-02 Societe Nationale D'etude Et De Construction De Moteurs D'aviation Jet engine nacelle with drag augmenter auxiliary for thrust-reverser system
US3869246A (en) * 1973-12-26 1975-03-04 Gen Motors Corp Variable configuration combustion apparatus
US3902316A (en) * 1974-10-15 1975-09-02 Gen Motors Corp Deceleration detector
FR2471480A1 (fr) * 1979-12-13 1981-06-19 Snecma Dispositif d'injection pour chambre a combustion de moteur a turbine
GB2085146B (en) * 1980-10-01 1985-06-12 Gen Electric Flow modifying device
FR2572463B1 (fr) * 1984-10-30 1989-01-20 Snecma Systeme d'injection a geometrie variable.
JPS61195214A (ja) * 1985-02-22 1986-08-29 Hitachi Ltd ガスタ−ビン燃焼器の空気流量調整機構
FR2585770B1 (fr) * 1985-08-02 1989-07-13 Snecma Dispositif d'injection a bol elargi pour chambre de combustion de turbomachine
FR2596102B1 (fr) * 1986-03-20 1988-05-27 Snecma Dispositif d'injection a vrille axialo-centripete

Also Published As

Publication number Publication date
US5159807A (en) 1992-11-03
DE69100735T2 (de) 1994-04-28
EP0455559A1 (fr) 1991-11-06
EP0455559B1 (fr) 1993-12-08
DE69100735D1 (de) 1994-01-20
FR2661714A1 (fr) 1991-11-08

Similar Documents

Publication Publication Date Title
FR2504195B1 (fr) Systeme d'alimentation en combustible des turbines a gaz
FR2661714B1 (fr) Dispositif d'alimentation en comburant d'une turbine a gaz.
FR2546571B1 (fr) Dispositif d'alimentation en carburant
GB2247522B (en) Gas turbine engine combustor
GB9112324D0 (en) Gas turbine engine combustor
GB9018014D0 (en) Gas turbine engine combustor
GB9018013D0 (en) Gas turbine engine combustor
GB2270974B (en) Burner for gas turbine engines
FR2589990B1 (fr) Module d'alimentation en carburant pour dispositif a chalumeau fonctionnant avec un carburant gazeux
FR2579678B1 (fr) Dispositif d'alimentation en carburant
FR2632015B1 (fr) Syste me d'injecteurs pour moteur a turbine a gaz
GB9022387D0 (en) Fuel control system for a gas turbine engine
FR2583459B1 (fr) Dispositif de regulation de carburant pour un moteur a turbine a gaz.
GB9106085D0 (en) Gas turbine engine combustor
FR2676000B1 (fr) Dispositif d'alimentation en gaz respiratoire.
EP0350795A3 (en) Gas engine including fuel supply system
FR2677404B1 (fr) Dispositif pour l'assemblage d'un moteur a turbine a gaz avec un echangeur-recuperateur de chaleur.
GB9220937D0 (en) Gas turbine engine combustor
GB2262802B (en) Fuel injection device for a turbomachine
GB9115670D0 (en) Gas turbine combustion system
GB2270973B (en) Burner for gas turbine engines
FR2670829B1 (fr) Generateur d'allumage haute energie notamment pour turbine a gaz.
GB9120372D0 (en) A fuel supply device particularly for heat engines
FR2563739B1 (fr) Soupape compensee pour dispositif d'alimentation en gaz respiratoire
FR2720442B1 (fr) Installation d'alimentation en carburant d'un turboréacteur.

Legal Events

Date Code Title Description
ST Notification of lapse
ST Notification of lapse