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FR3091723B1 - Aube ou Pale d'hélice composite pour aéronef intégrant une pièce de conformation - Google Patents

Aube ou Pale d'hélice composite pour aéronef intégrant une pièce de conformation Download PDF

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Publication number
FR3091723B1
FR3091723B1 FR1900348A FR1900348A FR3091723B1 FR 3091723 B1 FR3091723 B1 FR 3091723B1 FR 1900348 A FR1900348 A FR 1900348A FR 1900348 A FR1900348 A FR 1900348A FR 3091723 B1 FR3091723 B1 FR 3091723B1
Authority
FR
France
Prior art keywords
blade
unbinding
fibrous reinforcement
reinforcement
airfoil
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
FR1900348A
Other languages
English (en)
Other versions
FR3091723A1 (fr
Inventor
Vivien Mickaël Courtier
Dominique Gerhardt Mayhew
Adrien Jacques Philippe Fabre
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 FR1900348A priority Critical patent/FR3091723B1/fr
Priority to US16/743,320 priority patent/US11208198B2/en
Priority to GB2000599.7A priority patent/GB2588252B/en
Publication of FR3091723A1 publication Critical patent/FR3091723A1/fr
Application granted granted Critical
Publication of FR3091723B1 publication Critical patent/FR3091723B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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
    • B64C11/16—Blades
    • B64C11/20—Constructional features
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06—Fibrous reinforcements only
    • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/24—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/0025—Producing blades or the like, e.g. blades for turbines, propellers, or wings
    • 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
    • B64C11/16—Blades
    • B64C11/20—Constructional features
    • B64C11/26—Fabricated blades
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D1/00—Woven fabrics designed to make specified articles
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D13/00—Woven fabrics characterised by the special disposition of the warp or weft threads, e.g. with curved weft threads, with discontinuous warp threads, with diagonal warp or weft
    • D03D13/004—Woven fabrics characterised by the special disposition of the warp or weft threads, e.g. with curved weft threads, with discontinuous warp threads, with diagonal warp or weft with weave pattern being non-standard or providing special effects
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D25/00—Woven fabrics not otherwise provided for
    • D03D25/005—Three-dimensional woven fabrics
    • 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
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
    • 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
    • F04D29/38—Blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B11/00—Making preforms
    • B29B11/14—Making preforms characterised by structure or composition
    • B29B11/16—Making preforms characterised by structure or composition comprising fillers or reinforcement
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
    • B29L2031/087—Propellers
    • D—TEXTILES; PAPER
    • D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2505/00—Industrial
    • D10B2505/02—Reinforcing materials; Prepregs
    • D—TEXTILES; PAPER
    • D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2505/00—Industrial
    • D10B2505/12—Vehicles
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/50—Building or constructing in particular ways
    • 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)
  • Textile Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Composite Materials (AREA)
  • General Engineering & Computer Science (AREA)
  • Woven Fabrics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Aube ou Pale d'hélice composite pour aéronef intégrant une pièce de conformation Une aube comprend un renfort fibreux (200) présentant un tissage tridimensionnel densifié par une matrice, le renfort fibreux (200) comprenant en une seule pièce tissée une partie de pied (212) et une partie de profil aérodynamique (211) s’étendant suivant une direction longitudinale (DL) entre la partie de pied et une portion de sommet d’aube (211d) et suivant une direction transversale (DT) entre une portion de bord d’attaque (211a) et une portion de bord de fuite (211b). La partie de profil aérodynamique (211) comporte des première et deuxième faces d’extrados et d’intrados (211e, 211f). Le renfort fibreux comporte une déliaison (103) formant un logement (206) à l’intérieur du renfort fibreux, une pièce de conformation (50) étant présente dans le logement. La déliaison (103) s’étend sur une zone de déliaison à l’intérieur de la partie de profil aérodynamique (211) du renfort fibreux (200) comprise entre la partie de pied (212) et la portion de sommet d’aube (211d) dans la direction longitudinale et entre la portion de bord d’attaque (211a) et la portion de bord de fuite (211b) dans la direction transversale, la déliaison (103) débouchant en outre à l’extérieur de la partie de profil aérodynamique du renfort fibreux. Figure pour l’abrégé : Fig. 8.
FR1900348A 2019-01-15 2019-01-15 Aube ou Pale d'hélice composite pour aéronef intégrant une pièce de conformation Active FR3091723B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1900348A FR3091723B1 (fr) 2019-01-15 2019-01-15 Aube ou Pale d'hélice composite pour aéronef intégrant une pièce de conformation
US16/743,320 US11208198B2 (en) 2019-01-15 2020-01-15 Composite propeller vane or blade for aircraft integrating a conformation part
GB2000599.7A GB2588252B (en) 2019-01-15 2020-01-15 Composite propeller vane or blade for aircraft integrating a conformation part

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1900348A FR3091723B1 (fr) 2019-01-15 2019-01-15 Aube ou Pale d'hélice composite pour aéronef intégrant une pièce de conformation
FR1900348 2019-01-15

Publications (2)

Publication Number Publication Date
FR3091723A1 FR3091723A1 (fr) 2020-07-17
FR3091723B1 true FR3091723B1 (fr) 2021-04-02

Family

ID=66867380

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1900348A Active FR3091723B1 (fr) 2019-01-15 2019-01-15 Aube ou Pale d'hélice composite pour aéronef intégrant une pièce de conformation

Country Status (3)

Country Link
US (1) US11208198B2 (fr)
FR (1) FR3091723B1 (fr)
GB (1) GB2588252B (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3107719B1 (fr) * 2020-03-02 2023-02-10 Safran Aircraft Engines Texture fibreuse pour aube de turbomachine en matériau composite
US11346228B1 (en) * 2021-02-23 2022-05-31 Raytheon Technologies Corporation Airfoil with flange formed of wishbone-shaped fiber layer structure
FR3120249B1 (fr) * 2021-03-01 2023-12-29 Safran Aircraft Engines Aube comprenant une structure en matériau composite et procédé de fabrication associé
CN113547772B (zh) * 2021-06-08 2022-09-16 南京玻璃纤维研究设计院有限公司 一种混合结构风扇叶片制备方法
FR3125977B1 (fr) * 2021-08-09 2023-08-04 Safran Aircraft Engines Preforme d’aube composite, procede de mise en forme d’une telle preforme et aube ainsi mise en forme
FR3132321B1 (fr) * 2022-02-02 2024-03-22 Safran Aircraft Engines Aube hybride métal/composite à orientation textile adaptée aux sollicitations mécaniques
US11719103B1 (en) 2022-04-07 2023-08-08 General Electric Company Components having composite laminate with co-cured chopped fibers
FR3136189A1 (fr) * 2022-06-02 2023-12-08 Safran Aircraft Engines Pièce en matériau composite à capacité d’absorption des chocs améliorée, et procédé de fabrication d’une telle pièce
FR3145772B1 (fr) * 2023-02-14 2025-02-21 Safran Aircraft Engines Aube en matériau composite à calage variable pour soufflante non-carénée d’aéronef

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5049036A (en) * 1988-09-09 1991-09-17 Airfoil Textron Inc Composite blade with divergent root and method for making same
US5340280A (en) * 1991-09-30 1994-08-23 General Electric Company Dovetail attachment for composite blade and method for making
US5279892A (en) * 1992-06-26 1994-01-18 General Electric Company Composite airfoil with woven insert
FR2861143B1 (fr) 2003-10-20 2006-01-20 Snecma Moteurs Aube de turbomachine, notamment aube de soufflante et son procede de fabrication
FR2887601B1 (fr) 2005-06-24 2007-10-05 Snecma Moteurs Sa Piece mecanique et procede de fabrication d'une telle piece
FR2954271B1 (fr) 2009-12-21 2012-02-17 Snecma Pale d'helice d'aeronef
FR2962175B1 (fr) * 2010-07-02 2012-08-10 Snecma Aube a longeron composite integre
FR2964426B1 (fr) * 2010-09-06 2014-02-14 Snecma Aube mobile en materiau composite
US8387504B2 (en) * 2011-01-06 2013-03-05 General Electric Company Fiber-reinforced Al-Li compressor airfoil and method of fabricating
US20130052004A1 (en) * 2011-08-25 2013-02-28 Nicholas D. Stilin Structural composite fan exit guide vane for a turbomachine
JP6174839B2 (ja) * 2011-10-14 2017-08-02 株式会社Ihi セラミックス基複合部材およびその製造方法
CA2862685C (fr) * 2012-01-09 2020-03-10 Snecma Preforme fibreuse d'une aube de turbomachine en materiau composite a plate-forme integree, et son procede de realisation
US10414487B2 (en) * 2013-07-08 2019-09-17 Safran Aircraft Engines Composite propeller blade for an aircraft
US10577939B2 (en) * 2016-11-01 2020-03-03 Rolls-Royce Corporation Turbine blade with three-dimensional CMC construction elements
FR3076814B1 (fr) * 2018-01-12 2020-01-31 Safran Aircraft Engines Aube ou pale d'helice composite avec longeron integre pour aeronef
FR3080322B1 (fr) * 2018-04-20 2020-03-27 Safran Aircraft Engines Aube comprenant une structure en materiau composite et procede de fabrication associe

Also Published As

Publication number Publication date
FR3091723A1 (fr) 2020-07-17
GB2588252B (en) 2022-10-26
US20200223531A1 (en) 2020-07-16
US11208198B2 (en) 2021-12-28
GB2588252A (en) 2021-04-21
GB202000599D0 (en) 2020-02-26

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