FR3020404B1 - FLUID SUPPLY CIRCUIT OF VARIABLE TURBOMACHINE GEOMETRIES WITHOUT VOLUMETRIC PUMP - Google Patents

FLUID SUPPLY CIRCUIT OF VARIABLE TURBOMACHINE GEOMETRIES WITHOUT VOLUMETRIC PUMP Download PDF

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Publication number
FR3020404B1
FR3020404B1 FR1453820A FR1453820A FR3020404B1 FR 3020404 B1 FR3020404 B1 FR 3020404B1 FR 1453820 A FR1453820 A FR 1453820A FR 1453820 A FR1453820 A FR 1453820A FR 3020404 B1 FR3020404 B1 FR 3020404B1
Authority
FR
France
Prior art keywords
supply circuit
geometries
variable
turbomachine
circuit
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
FR1453820A
Other languages
French (fr)
Other versions
FR3020404A1 (en
Inventor
Sebastien CHALAUD
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
Priority to FR1453820A priority Critical patent/FR3020404B1/en
Application filed by Safran Aircraft Engines SAS, SNECMA SAS filed Critical Safran Aircraft Engines SAS
Priority to US15/306,936 priority patent/US9909498B2/en
Priority to CA2947120A priority patent/CA2947120C/en
Priority to RU2016146338A priority patent/RU2674301C2/en
Priority to PCT/FR2015/051130 priority patent/WO2015166177A1/en
Priority to BR112016024679-9A priority patent/BR112016024679B1/en
Priority to CN201580023571.XA priority patent/CN106662016B/en
Priority to EP15725804.7A priority patent/EP3137756B1/en
Publication of FR3020404A1 publication Critical patent/FR3020404A1/en
Application granted granted Critical
Publication of FR3020404B1 publication Critical patent/FR3020404B1/en
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
    • 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
    • F02C7/236—Fuel delivery systems comprising two or more 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
    • F05D2260/00—Function
    • F05D2260/40—Transmission of power
    • F05D2260/406—Transmission of power through hydraulic systems
    • 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
    • F05D2270/50—Control logic embodiments
    • F05D2270/52—Control logic embodiments by electrical means, e.g. relays or switches

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

L'invention concerne un système d'alimentation (10) de turbomachine en fluide, le système d'alimentation (10) comprenant un bloc de pompage basse pression (101) destiné à augmenter la pression du fluide s'écoulant en direction d'un circuit aval (50, 60). Selon l'invention, le circuit aval (50, 60) se subdivise à un nœud d'entrée (E) en un circuit d'alimentation (60) d'un système d'injection (62) et en un circuit d'alimentation (50) de géométries variables. Le circuit d'alimentation (50) de géométries variables est configuré pour acheminer du fluide vers des géométries variables (54) depuis le nœud d'entrée (E) jusqu'à un nœud de sortie (S) raccordant le circuit d'alimentation (50) de géométries variables au circuit amont (100). Le circuit d'alimentation (60) du système d'injection comprend une pompe volumétrique haute pression (102).The invention relates to a fluid supply system (10) for the turbomachine, the supply system (10) comprising a low pressure pumping unit (101) intended to increase the pressure of the fluid flowing towards a downstream circuit (50, 60). According to the invention, the downstream circuit (50, 60) is subdivided at an input node (E) into a supply circuit (60) of an injection system (62) and into a supply circuit (50) of variable geometries. The supply circuit (50) of variable geometries is configured to convey fluid to variable geometries (54) from the input node (E) to an output node (S) connecting the supply circuit ( 50) of variable geometries in the upstream circuit (100). The supply circuit (60) of the injection system comprises a high pressure positive displacement pump (102).

FR1453820A 2014-04-28 2014-04-28 FLUID SUPPLY CIRCUIT OF VARIABLE TURBOMACHINE GEOMETRIES WITHOUT VOLUMETRIC PUMP Active FR3020404B1 (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR1453820A FR3020404B1 (en) 2014-04-28 2014-04-28 FLUID SUPPLY CIRCUIT OF VARIABLE TURBOMACHINE GEOMETRIES WITHOUT VOLUMETRIC PUMP
CA2947120A CA2947120C (en) 2014-04-28 2015-04-27 Variable geometries fluid supply circuit for a turbomachine without volumetric pump
RU2016146338A RU2674301C2 (en) 2014-04-28 2015-04-27 Fluid flow contour with devices of variable geometry and without volumetric pump for turbomachine
PCT/FR2015/051130 WO2015166177A1 (en) 2014-04-28 2015-04-27 Variable geometries fluid supply circuit for a turbomachine without volumetric pump
US15/306,936 US9909498B2 (en) 2014-04-28 2015-04-27 Variable geometries fluid supply circuit for a turbomachine without volumetric pump
BR112016024679-9A BR112016024679B1 (en) 2014-04-28 2015-04-27 TURBOMACHINE FEEDING SYSTEM WITH FLUID AND TURBOMACHINE
CN201580023571.XA CN106662016B (en) 2014-04-28 2015-04-27 The variable-geometry body fluid supply circuit without positive displacement pump for turbine
EP15725804.7A EP3137756B1 (en) 2014-04-28 2015-04-27 Fluid supply circuit for variable geometry devices of a turbomachine without volumetric pump

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1453820 2014-04-28
FR1453820A FR3020404B1 (en) 2014-04-28 2014-04-28 FLUID SUPPLY CIRCUIT OF VARIABLE TURBOMACHINE GEOMETRIES WITHOUT VOLUMETRIC PUMP

Publications (2)

Publication Number Publication Date
FR3020404A1 FR3020404A1 (en) 2015-10-30
FR3020404B1 true FR3020404B1 (en) 2020-05-15

Family

ID=51168169

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1453820A Active FR3020404B1 (en) 2014-04-28 2014-04-28 FLUID SUPPLY CIRCUIT OF VARIABLE TURBOMACHINE GEOMETRIES WITHOUT VOLUMETRIC PUMP

Country Status (1)

Country Link
FR (1) FR3020404B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3044044B1 (en) * 2015-11-19 2021-01-29 Snecma FLUID SUPPLY SYSTEM OF AT LEAST ONE ORGAN OF AN AIRCRAFT PROPELLER ASSEMBLY

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8256222B2 (en) * 2008-02-11 2012-09-04 Honeywell International Inc. Direct metering fuel control with integral electrical metering pump and actuator servo pump
US8127548B2 (en) * 2008-02-21 2012-03-06 Honeywell International Inc. Hybrid electrical/mechanical turbine engine fuel supply system
US8286432B2 (en) * 2008-11-25 2012-10-16 Honeywell International Inc. Electric power generating turbine engine fuel supply system
FR2971548B1 (en) * 2011-02-11 2015-02-13 Snecma FUEL SUPPLY SYSTEM WITH MULTIPLE PUMPING MEANS

Also Published As

Publication number Publication date
FR3020404A1 (en) 2015-10-30

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