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FR2983910B1 - Porte de decharge de compresseur de moteur a turbine a gaz formant ecope. - Google Patents

Porte de decharge de compresseur de moteur a turbine a gaz formant ecope.

Info

Publication number
FR2983910B1
FR2983910B1 FR1161327A FR1161327A FR2983910B1 FR 2983910 B1 FR2983910 B1 FR 2983910B1 FR 1161327 A FR1161327 A FR 1161327A FR 1161327 A FR1161327 A FR 1161327A FR 2983910 B1 FR2983910 B1 FR 2983910B1
Authority
FR
France
Prior art keywords
discharge door
gas turbine
turbine engine
ecope
compressor discharge
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
FR1161327A
Other languages
English (en)
Other versions
FR2983910A1 (fr
Inventor
Sarah Ouboussad
Morgan Balland
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 FR1161327A priority Critical patent/FR2983910B1/fr
Publication of FR2983910A1 publication Critical patent/FR2983910A1/fr
Application granted granted Critical
Publication of FR2983910B1 publication Critical patent/FR2983910B1/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
    • 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
    • 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
    • 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
    • F04D27/023—Details or means for fluid extraction
    • 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
    • F05D2250/00—Geometry
    • F05D2250/40—Movement of components
    • F05D2250/41—Movement of components with one degree of freedom
    • F05D2250/411—Movement of components with one degree of freedom in rotation
    • 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
    • F05D2260/00—Function
    • F05D2260/50—Kinematic linkage, i.e. transmission of position
    • 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
    • F05D2260/00—Function
    • F05D2260/50—Kinematic linkage, i.e. transmission of position
    • F05D2260/57—Kinematic linkage, i.e. transmission of position using servos, independent actuators, etc.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

La présente invention porte sur un moteur à turbine à gaz multiflux comprenant un compresseur et au moins une porte de décharge (30) en aval du compresseur, pivotant autour d'un axe aval (31), transversal par rapport à l'axe du moteur, caractérisé par le fait que la porte de décharge (30) comprend sur un seul côté longitudinal, sur au moins une partie de la longueur de ce dernier, une portion de paroi radiale (30L), parallèle à l'axe du moteur, ledit côté étant aval par rapport à la composante tangentielle de l'écoulement sortant du compresseur.
FR1161327A 2011-12-08 2011-12-08 Porte de decharge de compresseur de moteur a turbine a gaz formant ecope. Active FR2983910B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1161327A FR2983910B1 (fr) 2011-12-08 2011-12-08 Porte de decharge de compresseur de moteur a turbine a gaz formant ecope.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1161327A FR2983910B1 (fr) 2011-12-08 2011-12-08 Porte de decharge de compresseur de moteur a turbine a gaz formant ecope.

Publications (2)

Publication Number Publication Date
FR2983910A1 FR2983910A1 (fr) 2013-06-14
FR2983910B1 true FR2983910B1 (fr) 2013-12-20

Family

ID=45563330

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1161327A Active FR2983910B1 (fr) 2011-12-08 2011-12-08 Porte de decharge de compresseur de moteur a turbine a gaz formant ecope.

Country Status (1)

Country Link
FR (1) FR2983910B1 (fr)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2640685B1 (fr) * 1988-12-15 1991-02-08 Snecma Vanne de decharge de compresseur de turboreacteur
US5123240A (en) * 1990-03-19 1992-06-23 General Electric Co. Method and apparatus for ejecting foreign matter from the primary flow path of a gas turbine engine
GB2259328B (en) * 1991-09-03 1995-07-19 Gen Electric Gas turbine engine variable bleed pivotal flow splitter
CA2133793A1 (fr) * 1994-10-06 1996-04-07 William E. Carscallen Purgeur-diffuseur annulaire a geometrie variable pour conduits jumeles de compresseur

Also Published As

Publication number Publication date
FR2983910A1 (fr) 2013-06-14

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