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FR3111948B1 - relief valve for taking fluid circulating in a stream of a turbomachine - Google Patents

relief valve for taking fluid circulating in a stream of a turbomachine Download PDF

Info

Publication number
FR3111948B1
FR3111948B1 FR2006888A FR2006888A FR3111948B1 FR 3111948 B1 FR3111948 B1 FR 3111948B1 FR 2006888 A FR2006888 A FR 2006888A FR 2006888 A FR2006888 A FR 2006888A FR 3111948 B1 FR3111948 B1 FR 3111948B1
Authority
FR
France
Prior art keywords
leaf
orifice
turbomachine
stream
relief 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
FR2006888A
Other languages
French (fr)
Other versions
FR3111948A1 (en
Inventor
Romain Nicolas Lagarde
Baptiste René Roger Batonnet
Lilian Yann Dumas
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
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 filed Critical Safran Aircraft Engines SAS
Priority to FR2006888A priority Critical patent/FR3111948B1/en
Publication of FR3111948A1 publication Critical patent/FR3111948A1/en
Application granted granted Critical
Publication of FR3111948B1 publication Critical patent/FR3111948B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
    • 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
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02—Surge control
    • F04D27/0207—Surge control by bleeding, bypassing or recycling fluids
    • F04D27/0215—Arrangements therefor, e.g. bleed or by-pass valves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/54—Fluid-guiding means, e.g. diffusers
    • F04D29/541—Specially adapted for elastic fluid pumps
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/321—Application in turbines in gas turbines for a special turbine stage
    • F05D2220/3216—Application in turbines in gas turbines for a special turbine stage for a special compressor stage
    • F05D2220/3219—Application in turbines in gas turbines for a special turbine stage for a special compressor stage for the last stage of a compressor or a high pressure compressor

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Safety Valves (AREA)
  • Lift Valve (AREA)

Abstract

Carter comprenant une paroi (2) définissant un orifice (3) débouchant dans une veine et une vanne de décharge comprenant une porte comprenant un premier battant (10) mobile par rapport à la paroi, et un deuxième battant (20) mobile par rapport au premier battant (10), la porte étant configurable dans :- une configuration fermée dans laquelle le premier battant (10) obstrue une première portion (13) de l’orifice et le deuxième battant obstrue simultanément une deuxième portion (23) de l’orifice,- une configuration intermédiaire dans laquelle le premier battant (10) dévoile la première portion de l’orifice (13) pour permettre le passage de fluide, et le deuxième battant (20) obstrue la deuxième portion (23) de l’orifice, et - une configuration ouverte dans laquelle le premier battant (10) dévoile la première portion (13) de l’orifice, et le deuxième battant (20) dévoile simultanément la deuxième portion (23) de l’orifice. Figure pour l’abrégé : Fig. 2Housing comprising a wall (2) defining an orifice (3) opening into a vein and a discharge valve comprising a door comprising a first leaf (10) movable relative to the wall, and a second leaf (20) movable relative to the first leaf (10), the door being configurable in:- a closed configuration in which the first leaf (10) obstructs a first portion (13) of the orifice and the second leaf simultaneously obstructs a second portion (23) of the orifice, - an intermediate configuration in which the first leaf (10) reveals the first portion of the orifice (13) to allow the passage of fluid, and the second leaf (20) obstructs the second portion (23) of the orifice , and - an open configuration in which the first leaf (10) reveals the first portion (13) of the orifice, and the second leaf (20) simultaneously reveals the second portion (23) of the orifice. Figure for the abstract: Fig. 2

FR2006888A 2020-06-30 2020-06-30 relief valve for taking fluid circulating in a stream of a turbomachine Active FR3111948B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2006888A FR3111948B1 (en) 2020-06-30 2020-06-30 relief valve for taking fluid circulating in a stream of a turbomachine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2006888 2020-06-30
FR2006888A FR3111948B1 (en) 2020-06-30 2020-06-30 relief valve for taking fluid circulating in a stream of a turbomachine

Publications (2)

Publication Number Publication Date
FR3111948A1 FR3111948A1 (en) 2021-12-31
FR3111948B1 true FR3111948B1 (en) 2022-07-29

Family

ID=72885692

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2006888A Active FR3111948B1 (en) 2020-06-30 2020-06-30 relief valve for taking fluid circulating in a stream of a turbomachine

Country Status (1)

Country Link
FR (1) FR3111948B1 (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2640685B1 (en) * 1988-12-15 1991-02-08 Snecma TURBOREACTOR COMPRESSOR DISCHARGE VALVE
FR2983911B1 (en) * 2011-12-08 2014-02-07 Snecma LOW PRESSURE COMPRESSOR DISCHARGE DOORS OF A GAS TURBINE ENGINE.
US9399951B2 (en) * 2012-04-17 2016-07-26 General Electric Company Modular louver system
US10077740B2 (en) * 2015-10-16 2018-09-18 The Boeing Company Folding door thrust reversers for aircraft engines

Also Published As

Publication number Publication date
FR3111948A1 (en) 2021-12-31

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