FR3134599B1 - Module pour une turbomachine d’aeronef - Google Patents

Module pour une turbomachine d’aeronef Download PDF

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Publication number
FR3134599B1
FR3134599B1 FR2203561A FR2203561A FR3134599B1 FR 3134599 B1 FR3134599 B1 FR 3134599B1 FR 2203561 A FR2203561 A FR 2203561A FR 2203561 A FR2203561 A FR 2203561A FR 3134599 B1 FR3134599 B1 FR 3134599B1
Authority
FR
France
Prior art keywords
longitudinal axis
axial pistons
module
hydraulic actuator
main plate
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
FR2203561A
Other languages
English (en)
Other versions
FR3134599A1 (fr
Inventor
Jean Charles Olivier Roda
Didier René André Escure
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 FR2203561A priority Critical patent/FR3134599B1/fr
Priority to EP23722624.6A priority patent/EP4508336A1/fr
Priority to US18/856,838 priority patent/US12428131B2/en
Priority to CN202380040040.6A priority patent/CN119173696A/zh
Priority to PCT/FR2023/050521 priority patent/WO2023198987A1/fr
Publication of FR3134599A1 publication Critical patent/FR3134599A1/fr
Application granted granted Critical
Publication of FR3134599B1 publication Critical patent/FR3134599B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • F04D29/322—Blade mountings
    • F04D29/323—Blade mountings adjustable
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/30—Blade pitch-changing mechanisms
    • B64C11/38—Blade pitch-changing mechanisms fluid, e.g. hydraulic
    • 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
    • F01D7/00—Rotors with blades adjustable in operation; Control thereof
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B1/00—Multi-cylinder machines or pumps characterised by number or arrangement of cylinders
    • F04B1/12—Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinder axes coaxial with, or parallel or inclined to, main shaft axis
    • F04B1/26—Control
    • F04B1/30—Control of machines or pumps with rotary cylinder blocks
    • F04B1/32—Control of machines or pumps with rotary cylinder blocks by varying the relative positions of a swash plate and a cylinder block
    • F04B1/324—Control of machines or pumps with rotary cylinder blocks by varying the relative positions of a swash plate and a cylinder block by changing the inclination of the swash plate
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D2027/005—Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR]
    • 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
    • F05D2220/323—Application in turbines in gas turbines for aircraft propulsion, e.g. jet engines
    • 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
    • F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
    • F05D2260/74—Adjusting of angle of incidence or attack of rotating blades by turning around an axis perpendicular the rotor centre line
    • 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
    • F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
    • F05D2260/79—Bearing, support or actuation arrangements therefor
    • 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
    • F05D2270/60—Control system actuates means
    • F05D2270/64—Hydraulic actuators

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Transmission Devices (AREA)
  • Reciprocating Pumps (AREA)
  • Actuator (AREA)

Abstract

L’invention concerne un module (3) d’axe longitudinal (X) et comprenant un actionneur hydraulique (46), et une pompe (54) d’alimentation en fluide de l’actionneur hydraulique (46) comprenant des pistons axiaux (54c) destinés à être mobiles en rotation autour de l’axe longitudinal (X) et configurés pour transférer le fluide à l’actionneur hydraulique (46), un plateau de liaison (54g) relié aux pistons axiaux (54c) et coopérant avec un plateau principal (54e) annulaire centré sur l’axe longitudinal (X), destiné à être fixe en rotation autour de l’axe longitudinal (X) et inclinable par rapport à l’axe longitudinal (X), le plateau de liaison (54g) étant agencé entre le plateau principal (54e) et les pistons axiaux (54c), les pistons axiaux (54c) étant mobiles en translation selon une direction (D) parallèle à l’axe longitudinal (X), l’inclinaison du plateau principal (54e) entraînant un déplacement des pistons axiaux (54c) selon la direction (D). Figure n° 3a
FR2203561A 2022-04-15 2022-04-15 Module pour une turbomachine d’aeronef Active FR3134599B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR2203561A FR3134599B1 (fr) 2022-04-15 2022-04-15 Module pour une turbomachine d’aeronef
EP23722624.6A EP4508336A1 (fr) 2022-04-15 2023-04-11 Module pour une turbomachine d'aeronef
US18/856,838 US12428131B2 (en) 2022-04-15 2023-04-11 Module for an aircraft turbine engine
CN202380040040.6A CN119173696A (zh) 2022-04-15 2023-04-11 用于飞行器涡轮发动机的模块
PCT/FR2023/050521 WO2023198987A1 (fr) 2022-04-15 2023-04-11 Module pour une turbomachine d'aeronef

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2203561A FR3134599B1 (fr) 2022-04-15 2022-04-15 Module pour une turbomachine d’aeronef
FR2203561 2022-04-15

Publications (2)

Publication Number Publication Date
FR3134599A1 FR3134599A1 (fr) 2023-10-20
FR3134599B1 true FR3134599B1 (fr) 2025-05-02

Family

ID=82196655

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2203561A Active FR3134599B1 (fr) 2022-04-15 2022-04-15 Module pour une turbomachine d’aeronef

Country Status (5)

Country Link
US (1) US12428131B2 (fr)
EP (1) EP4508336A1 (fr)
CN (1) CN119173696A (fr)
FR (1) FR3134599B1 (fr)
WO (1) WO2023198987A1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12428972B2 (en) * 2022-05-26 2025-09-30 Ge Infrastructure Technology Llc System and method for hydraulically actuating main and bypass valves of a steam turbine
US20260049604A1 (en) * 2024-08-15 2026-02-19 The Boeing Company Accumulator for Prevention of Hydraulic Pump Cavitation

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR948952A (fr) * 1946-06-26 1949-08-17 United Aircraft Corp Perfectionnements aux hélices
FR969611A (fr) * 1948-07-16 1950-12-22 Dispositif de commande hydraulique pour mécanismes de changement de pas d'hélices aériennes
CH514790A (de) * 1970-07-09 1971-10-31 Rostock Dieselmotoren Vorrichtung zur Erzeugung eines Druckmittelstromes zur Betätigung eines sich mit einer Welle drehenden hydraulischen Servomotors
GB1420625A (en) * 1972-08-10 1976-01-07 Rolls Royce Pitch varying mechanism for a variable pitch fan or propeller
FR3087232B1 (fr) 2018-10-12 2021-06-25 Safran Aircraft Engines Turbomachine comprenant un rotor portant des pales a calage variable
FR3101664B1 (fr) * 2019-10-02 2021-09-03 Safran Aircraft Engines Système de commande de calage cyclique de pales
US11970956B2 (en) * 2022-08-26 2024-04-30 General Electric Company Pitch change mechanism for a fan of a gas turbine engine

Also Published As

Publication number Publication date
CN119173696A (zh) 2024-12-20
FR3134599A1 (fr) 2023-10-20
WO2023198987A1 (fr) 2023-10-19
US12428131B2 (en) 2025-09-30
US20250256835A1 (en) 2025-08-14
EP4508336A1 (fr) 2025-02-19

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