FR2982319B1 - Systeme de commande d'une vanne pneumatique de turbomachine - Google Patents

Systeme de commande d'une vanne pneumatique de turbomachine

Info

Publication number
FR2982319B1
FR2982319B1 FR1160121A FR1160121A FR2982319B1 FR 2982319 B1 FR2982319 B1 FR 2982319B1 FR 1160121 A FR1160121 A FR 1160121A FR 1160121 A FR1160121 A FR 1160121A FR 2982319 B1 FR2982319 B1 FR 2982319B1
Authority
FR
France
Prior art keywords
turbomachine
controlling
pressure
valve
pneumatic valve
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
FR1160121A
Other languages
English (en)
Other versions
FR2982319A1 (fr
Inventor
Lauranne Sophie Mottet
Marie Gentilhomme
Nicolas Potel
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 FR1160121A priority Critical patent/FR2982319B1/fr
Priority to GB1219325.6A priority patent/GB2496292A/en
Priority to US13/669,999 priority patent/US20130115055A1/en
Publication of FR2982319A1 publication Critical patent/FR2982319A1/fr
Application granted granted Critical
Publication of FR2982319B1 publication Critical patent/FR2982319B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/105—Final actuators by passing part of the fluid
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/20—Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted
    • F01D17/22—Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted the operation or power assistance being predominantly non-mechanical
    • F01D17/24—Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted the operation or power assistance being predominantly non-mechanical electrical
    • 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
    • F02C9/16—Control of working fluid flow
    • 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
    • F02C9/16—Control of working fluid flow
    • F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
    • F16K31/00—Actuating devices; Operating means; Releasing devices
    • F16K31/12—Actuating devices; Operating means; Releasing devices actuated by fluid
    • 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
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/7722—Line condition change responsive valves
    • Y10T137/7758—Pilot or servo controlled
    • Y10T137/7761—Electrically actuated valve

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Fluid-Driven Valves (AREA)
  • Supercharger (AREA)
  • Control Of Turbines (AREA)

Abstract

Système (110) de commande d'une vanne pneumatique (112) de turbomachine, telle qu'une vanne de décharge, comprenant un distributeur 140) d'air sous pression monté entre la vanne (112) à commander, une électrovalve de commande (118) et des moyens (144) de prélèvement d'air à une pression P1, l'électrovalve comportant en outre une première entrée (132) reliée à une source de fluide à une pression P2 qui est indépendante de P1, l'ouverture et la fermeture de la vanne étant commandées par le débit d'air à pression P1 fourni par le distributeur commandé par le fluide à pression P2 fourni par l'électrovalve.
FR1160121A 2011-11-07 2011-11-07 Systeme de commande d'une vanne pneumatique de turbomachine Active FR2982319B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1160121A FR2982319B1 (fr) 2011-11-07 2011-11-07 Systeme de commande d'une vanne pneumatique de turbomachine
GB1219325.6A GB2496292A (en) 2011-11-07 2012-10-26 A system for controlling a gas turbine engine pneumatic valve
US13/669,999 US20130115055A1 (en) 2011-11-07 2012-11-06 System for controlling a pneumatic valve of a turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1160121A FR2982319B1 (fr) 2011-11-07 2011-11-07 Systeme de commande d'une vanne pneumatique de turbomachine

Publications (2)

Publication Number Publication Date
FR2982319A1 FR2982319A1 (fr) 2013-05-10
FR2982319B1 true FR2982319B1 (fr) 2016-05-13

Family

ID=47358728

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1160121A Active FR2982319B1 (fr) 2011-11-07 2011-11-07 Systeme de commande d'une vanne pneumatique de turbomachine

Country Status (3)

Country Link
US (1) US20130115055A1 (fr)
FR (1) FR2982319B1 (fr)
GB (1) GB2496292A (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9822900B2 (en) 2015-07-16 2017-11-21 Honeywell International Inc Pneumatic mixing valve
FR3050760B1 (fr) * 2016-04-28 2019-12-20 Safran Aircraft Engines Systeme de vanne de decharge pour une turbomachine d'aeronef
EP3323726A1 (fr) * 2016-11-22 2018-05-23 Airbus Defence and Space SA Aéronef équipé de moteurs turbopropulseurs ayant des moyens actifs pour éviter les dégâts causés par les impacts de glace
FR3074533B1 (fr) * 2017-12-06 2020-11-06 Safran Aircraft Engines Circuit de commande hydraulique et pneumatique pour turboreacteur a echangeur de chaleur carburant/air
FR3075172B1 (fr) 2017-12-19 2019-12-27 Safran Aircraft Engines Circuit pneumatique pour l'alimentation en air d'au moins une vanne de decharge et d'au moins un dispositif de depressurisation d'une enceinte huile d'une turbomachine
FR3079888B1 (fr) 2018-04-04 2021-07-30 Safran Aircraft Engines Controleur pneumatique pour la commande d'une vanne de decharge
FR3079879B1 (fr) * 2018-04-05 2020-05-08 Safran Aircraft Engines Vanne de decharge a ouverture regulee

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3376893A (en) * 1964-10-22 1968-04-09 Bendix Corp Emergency fuel shutoff valve
CH502513A (de) * 1969-01-08 1971-01-31 Sulzer Ag Zwischen Dampferzeuger und Verbraucher angeordnetes Überströmventil
CH523456A (de) * 1970-05-15 1972-05-31 Sulzer Ag Ventil, insbesondere Absperrventil
CH589815A5 (fr) * 1975-03-20 1977-07-15 Sulzer Ag
DE2519600A1 (de) * 1975-05-02 1976-11-11 Bbc Brown Boveri & Cie Verfahren und einrichtung zum verstellen eines eine vorsteuerung aufweisenden turbomaschinen-regelventils
US4791955A (en) * 1983-09-22 1988-12-20 Dresser Industries, Inc. Modulating pressure operated pilot relief valve
US6739293B2 (en) * 2000-12-04 2004-05-25 Sturman Industries, Inc. Hydraulic valve actuation systems and methods
US6910851B2 (en) * 2003-05-30 2005-06-28 Honeywell International, Inc. Turbofan jet engine having a turbine case cooling valve
US6981842B2 (en) * 2003-07-22 2006-01-03 Honeywell International, Inc. Bleed valve system
US7147430B2 (en) * 2004-06-10 2006-12-12 Honeywell International, Inc. Pneumatic valve control using downstream pressure feedback and an air turbine starter incorporating the same
US20090101230A1 (en) * 2007-10-19 2009-04-23 Anstead Duane H Apparatus for filling an oil tank
US8616827B2 (en) * 2008-02-20 2013-12-31 Rolls-Royce Corporation Turbine blade tip clearance system
US8011382B2 (en) * 2008-10-06 2011-09-06 Honeywell International Inc. Bi-modal bleed valve assembly for gas turbine engine
US8419345B2 (en) * 2008-12-30 2013-04-16 Rolls-Royce Corporation Actuator

Also Published As

Publication number Publication date
US20130115055A1 (en) 2013-05-09
FR2982319A1 (fr) 2013-05-10
GB2496292A (en) 2013-05-08
GB201219325D0 (en) 2012-12-12

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