FR3050766B1 - Turboreacteur double flux dote d'un prelevement de debit permettant une calibration reglable du taux de dilution a la confluence - Google Patents

Turboreacteur double flux dote d'un prelevement de debit permettant une calibration reglable du taux de dilution a la confluence Download PDF

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Publication number
FR3050766B1
FR3050766B1 FR1653898A FR1653898A FR3050766B1 FR 3050766 B1 FR3050766 B1 FR 3050766B1 FR 1653898 A FR1653898 A FR 1653898A FR 1653898 A FR1653898 A FR 1653898A FR 3050766 B1 FR3050766 B1 FR 3050766B1
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FR
France
Prior art keywords
flow
air flow
confluence
rate
dilution
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
FR1653898A
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English (en)
Other versions
FR3050766A1 (fr
Inventor
Sebastien Alain Christophe Bourgois
Mario Antoine Lambey
Brice Marie Yves Emile LE PANNERER
Christophe Pieussergues
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 FR1653898A priority Critical patent/FR3050766B1/fr
Publication of FR3050766A1 publication Critical patent/FR3050766A1/fr
Application granted granted Critical
Publication of FR3050766B1 publication Critical patent/FR3050766B1/fr
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/38—Introducing air inside the jet
    • F02K1/386—Introducing air inside the jet mixing devices in the jet pipe, e.g. for mixing primary and secondary 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/10—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the 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
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • 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
    • F05D2220/324—Application in turbines in gas turbines to drive unshrouded, low solidity propeller
    • 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
    • F05D2220/325—Application in turbines in gas turbines to drive unshrouded, high solidity propeller

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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Exhaust Gas After Treatment (AREA)

Abstract

Un turboréacteur (1) à double flux comprenant un compresseur basse pression (3) apte à prélever un flux d'air destiné à être divisé en un flux d'air primaire (F1) et un flux d'air secondaire (F2) distincts, un canal primaire (10) apte à acheminer le flux d'air primaire (F1) depuis le compresseur basse pression (3) jusqu'à une zone de confluence (12) des flux d'air primaire et secondaire (F1 et F2) permettant la dilution du flux d'air secondaire (F2) dans le flux d'air primaire (F1), un canal secondaire (11) apte à acheminer le flux d'air secondaire depuis le compresseur basse pression (3) jusqu'à la zone de confluence (12). Le turboréacteur (1) comprend un dispositif (20) de régulation du débit d'air du flux secondaire (F2) comportant des moyens de prélèvement d'une portion d'air dans le flux secondaire (F2) en amont de la zone de confluence (12).
FR1653898A 2016-04-29 2016-04-29 Turboreacteur double flux dote d'un prelevement de debit permettant une calibration reglable du taux de dilution a la confluence Active FR3050766B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1653898A FR3050766B1 (fr) 2016-04-29 2016-04-29 Turboreacteur double flux dote d'un prelevement de debit permettant une calibration reglable du taux de dilution a la confluence

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1653898A FR3050766B1 (fr) 2016-04-29 2016-04-29 Turboreacteur double flux dote d'un prelevement de debit permettant une calibration reglable du taux de dilution a la confluence
FR1653898 2016-04-29

Publications (2)

Publication Number Publication Date
FR3050766A1 FR3050766A1 (fr) 2017-11-03
FR3050766B1 true FR3050766B1 (fr) 2020-02-14

Family

ID=57113431

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1653898A Active FR3050766B1 (fr) 2016-04-29 2016-04-29 Turboreacteur double flux dote d'un prelevement de debit permettant une calibration reglable du taux de dilution a la confluence

Country Status (1)

Country Link
FR (1) FR3050766B1 (fr)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7134271B2 (en) * 2004-11-05 2006-11-14 General Electric Company Thrust vectoring aft FLADE engine
US7475532B2 (en) * 2005-08-29 2009-01-13 General Electric Company Valve assembly for a gas turbine engine
DE102010009477A1 (de) * 2010-02-26 2011-09-01 Rolls-Royce Deutschland Ltd & Co Kg Fluggasturbinenantrieb
US9341075B2 (en) * 2012-06-25 2016-05-17 United Technologies Corporation Pre-turbine engine case variable area mixing plane

Also Published As

Publication number Publication date
FR3050766A1 (fr) 2017-11-03

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