FR3053396B1 - Dispositif de dosage de carburant et procede associe - Google Patents

Dispositif de dosage de carburant et procede associe Download PDF

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Publication number
FR3053396B1
FR3053396B1 FR1656177A FR1656177A FR3053396B1 FR 3053396 B1 FR3053396 B1 FR 3053396B1 FR 1656177 A FR1656177 A FR 1656177A FR 1656177 A FR1656177 A FR 1656177A FR 3053396 B1 FR3053396 B1 FR 3053396B1
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FR
France
Prior art keywords
temperature
function
valve
regulation
flow
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
FR1656177A
Other languages
English (en)
Other versions
FR3053396A1 (fr
Inventor
Arnaud Bernard Clement Thomas Joudareff
Thomas LEPAGE
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
Safran Aircraft Engines SAS
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 Safran Aircraft Engines SAS, SNECMA SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1656177A priority Critical patent/FR3053396B1/fr
Publication of FR3053396A1 publication Critical patent/FR3053396A1/fr
Application granted granted Critical
Publication of FR3053396B1 publication Critical patent/FR3053396B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/263—Control of fuel supply by means of fuel metering valves
    • 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
    • F02C7/232—Fuel valves; Draining valves or systems
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
    • G01F1/00—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow
    • G01F1/76—Devices for measuring mass flow of a fluid or a fluent solid material
    • G01F1/86—Indirect mass flowmeters, e.g. measuring volume flow and density, temperature or pressure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/07—Purpose of the control system to improve fuel economy
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/301—Pressure
    • F05D2270/3015—Pressure differential pressure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/303—Temperature
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/306—Mass flow

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Physics & Mathematics (AREA)
  • Measuring Volume Flow (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Flow Control (AREA)

Abstract

L'invention concerne un procédé de détermination d'un débit reconstruit, pour régulation étant mise en œuvre à l'aide d'un dispositif de régulation comprenant un bloc hydraulique (100) comprenant une valve de dosage (130) et une soupape de régulation (140), un capteur de température (160), un débitmètre (150), un module de mémoire (120), une unité de calcul (200), caractérisé en ce que le procédé comprend les étapes suivantes : - (E1) mesure de la température et/ou de la position de la pièce mobile (138), et/ou du débit, - (E2) récupération de données relatives à un écart de pression (ΔP) maintenu aux bornes de la valve de dosage (130) par la soupape de régulation (140) en fonction de la température (T) et/ou de données relatives à des caractéristiques mécaniques propres à la valve de dosage (130) en fonction de la position de la pièce mobile (138) de dosage, et/ou relatives au débit massique corrigé en fonction de la température et/ou du débit massique mesuré, lesdites données étant stockées dans le module de mémoire (120),
FR1656177A 2016-06-30 2016-06-30 Dispositif de dosage de carburant et procede associe Active FR3053396B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1656177A FR3053396B1 (fr) 2016-06-30 2016-06-30 Dispositif de dosage de carburant et procede associe

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1656177A FR3053396B1 (fr) 2016-06-30 2016-06-30 Dispositif de dosage de carburant et procede associe
FR1656177 2016-06-30

Publications (2)

Publication Number Publication Date
FR3053396A1 FR3053396A1 (fr) 2018-01-05
FR3053396B1 true FR3053396B1 (fr) 2020-02-21

Family

ID=56684102

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1656177A Active FR3053396B1 (fr) 2016-06-30 2016-06-30 Dispositif de dosage de carburant et procede associe

Country Status (1)

Country Link
FR (1) FR3053396B1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3088365B1 (fr) 2018-11-13 2020-12-25 Safran Aircraft Engines Unite de dosage de carburant pour un moteur d’aeronef
FR3094086B1 (fr) * 2019-03-19 2021-03-19 Safran Aircraft Engines Procédé de surveillance de l’état de fonctionnement d’un bloc hydromécanique
FR3098255B1 (fr) * 2019-07-03 2021-06-04 Safran Aircraft Engines Détermination de densité de carburant pour dosage de carburant dans un circuit d’alimentation en carburant d’un moteur d’aéronef
US11713718B2 (en) 2021-09-30 2023-08-01 Hamilton Sundstrand Corporation Dual valve fluid metering system
GB202205350D0 (en) * 2022-04-12 2022-05-25 Rolls Royce Plc Fuel delivery
FR3140163A1 (fr) * 2022-09-22 2024-03-29 Vitesco Technologies Procédé de détermination d’un débit de fluide dans un système de motorisation de véhicule

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5259186A (en) * 1991-03-08 1993-11-09 General Electric Company Gas turbine fuel control
JP4119908B2 (ja) * 2005-09-14 2008-07-16 三菱重工業株式会社 ガスタービンの燃焼制御装置
FR2945075B1 (fr) * 2009-04-29 2015-06-05 Snecma Procede et dispositif pour alimenter une chambre de turbomachine avec un debit de carburant regule

Also Published As

Publication number Publication date
FR3053396A1 (fr) 2018-01-05

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