FR3027948B1 - Anneau d'helice en materiau composite pour une turbomachine - Google Patents

Anneau d'helice en materiau composite pour une turbomachine Download PDF

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Publication number
FR3027948B1
FR3027948B1 FR1460505A FR1460505A FR3027948B1 FR 3027948 B1 FR3027948 B1 FR 3027948B1 FR 1460505 A FR1460505 A FR 1460505A FR 1460505 A FR1460505 A FR 1460505A FR 3027948 B1 FR3027948 B1 FR 3027948B1
Authority
FR
France
Prior art keywords
composite material
annular body
turbomachine
propeller ring
root
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
FR1460505A
Other languages
English (en)
Other versions
FR3027948A1 (fr
Inventor
Sebastien Emile Philippe Tajan
Charles-Henri Michel Marie Derrez
Anthony Lafitte
Pecheur Cyril Roger Yves Le
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 FR1460505A priority Critical patent/FR3027948B1/fr
Priority to GB1519267.7A priority patent/GB2534445B/en
Priority to US14/927,672 priority patent/US10378368B2/en
Publication of FR3027948A1 publication Critical patent/FR3027948A1/fr
Application granted granted Critical
Publication of FR3027948B1 publication Critical patent/FR3027948B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F01D7/00—Rotors with blades adjustable in operation; Control thereof
    • 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
    • B64C11/02—Hub construction
    • 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
    • B64C11/02—Hub construction
    • B64C11/04—Blade mountings
    • 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
    • B64C11/02—Hub construction
    • B64C11/04—Blade mountings
    • B64C11/06—Blade mountings for variable-pitch blades
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3023—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
    • 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
    • B64C11/306—Blade pitch-changing mechanisms specially adapted for contrarotating propellers
    • 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
    • F05D2240/00—Components
    • F05D2240/20—Rotors
    • 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
    • F05D2240/00—Components
    • F05D2240/50—Bearings
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

L'invention concerne un anneau d'hélice (10) de turbomachine comprenant un corps annulaire (11) sensiblement coaxial avec un axe principal (A) et une pluralité de logements radiaux (12) uniformément répartis autour de l'axe principal (A), chaque logement radial (12) étant configuré pour recevoir un pied (14) d'une pale (P), le corps annulaire (11) étant réalisé dans un matériau composite comprenant un renfort fibreux densifié par une matrice polymère et comportant en outre une pluralité d'inserts métalliques (20) configurés pour recevoir chacun le pied (14) d'une pale (P), lesdits inserts métalliques (20) étant ancrés dans le matériau composite du corps annulaire (11).
FR1460505A 2014-10-31 2014-10-31 Anneau d'helice en materiau composite pour une turbomachine Active FR3027948B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1460505A FR3027948B1 (fr) 2014-10-31 2014-10-31 Anneau d'helice en materiau composite pour une turbomachine
GB1519267.7A GB2534445B (en) 2014-10-31 2015-10-30 Propeller ring made of composite material for a turbomachine
US14/927,672 US10378368B2 (en) 2014-10-31 2015-10-30 Propeller ring made of composite material for a turbomachine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1460505A FR3027948B1 (fr) 2014-10-31 2014-10-31 Anneau d'helice en materiau composite pour une turbomachine

Publications (2)

Publication Number Publication Date
FR3027948A1 FR3027948A1 (fr) 2016-05-06
FR3027948B1 true FR3027948B1 (fr) 2020-10-16

Family

ID=52345337

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1460505A Active FR3027948B1 (fr) 2014-10-31 2014-10-31 Anneau d'helice en materiau composite pour une turbomachine

Country Status (3)

Country Link
US (1) US10378368B2 (fr)
FR (1) FR3027948B1 (fr)
GB (1) GB2534445B (fr)

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2453294A1 (fr) * 1979-04-04 1980-10-31 Snecma Dispositif de fixation d'aubes sur un rotor de compresseur pour turbo-reacteur
US4524499A (en) * 1981-11-16 1985-06-25 Trw Inc. Method of fabricating an aircraft propeller assembly with composite blades
GB2161108B (en) * 1984-07-07 1988-03-23 Rolls Royce A compressor rotor assembly and a method of manufacture of such an assembly
FR2605586B1 (fr) 1986-10-22 1990-11-30 Snecma Anneau porte-pales pour aubage d'helice de grande dimension
JPH02246897A (ja) * 1988-12-29 1990-10-02 General Electric Co <Ge> 航空機推進装置及び方法
US8182222B2 (en) * 2009-02-12 2012-05-22 Hamilton Sundstrand Corporation Thermal protection of rotor blades
EP2413205B1 (fr) * 2009-03-27 2014-04-09 Honda Motor Co., Ltd. Dispositif de commande pour une installation
FR2943985B1 (fr) * 2009-04-07 2011-05-13 Airbus France Helice pour turbomachine d'aeronef comprenant un anneau de retention d'aubes monte autour du moyeu.
FR2951435B1 (fr) 2009-10-15 2012-02-03 Snecma Dispositif adapte pour etre pourvu de pales d'helice
EP2509860B1 (fr) * 2009-12-07 2017-07-19 Safran Aircraft Engines Moyeu d'hélice à anneau polygonal renforce et turbomachine équipée d'un tel moyeu
FR2962175B1 (fr) * 2010-07-02 2012-08-10 Snecma Aube a longeron composite integre
FR2963054B1 (fr) * 2010-07-22 2012-07-27 Snecma Anneau de retention
JP5676961B2 (ja) * 2010-07-30 2015-02-25 スパンション エルエルシー 電源の制御回路、電子機器及び電源の制御方法
GB201020857D0 (en) * 2010-12-09 2011-01-26 Rolls Royce Plc Annulus filler
US9045990B2 (en) * 2011-05-26 2015-06-02 United Technologies Corporation Integrated ceramic matrix composite rotor disk geometry for a gas turbine engine
GB201118386D0 (en) 2011-10-25 2011-12-07 Rolls Royce Plc A support ring for a rotary assembly
FR2992677B1 (fr) * 2012-07-02 2016-03-18 Snecma Moyeu pour logement radial d'anneau d'helice de turbomachine a pales a calage variable et assemblage comportant un tel moyeu
JP2015048783A (ja) * 2013-09-02 2015-03-16 株式会社東芝 回転機器ロータおよび回転機器

Also Published As

Publication number Publication date
GB201519267D0 (en) 2015-12-16
FR3027948A1 (fr) 2016-05-06
GB2534445A (en) 2016-07-27
US10378368B2 (en) 2019-08-13
US20160123162A1 (en) 2016-05-05
GB2534445B (en) 2020-09-09

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