BR112016007445A2 - montagem de compactação e método para fabricar uma pá compósita de turbomáquina - Google Patents

montagem de compactação e método para fabricar uma pá compósita de turbomáquina

Info

Publication number
BR112016007445A2
BR112016007445A2 BR112016007445A BR112016007445A BR112016007445A2 BR 112016007445 A2 BR112016007445 A2 BR 112016007445A2 BR 112016007445 A BR112016007445 A BR 112016007445A BR 112016007445 A BR112016007445 A BR 112016007445A BR 112016007445 A2 BR112016007445 A2 BR 112016007445A2
Authority
BR
Brazil
Prior art keywords
compaction
turbocharger
fabricating
compaction assembly
assembly
Prior art date
Application number
BR112016007445A
Other languages
English (en)
Other versions
BR112016007445B1 (pt
Inventor
Gimat Matthieu
Marchal Yann
Original Assignee
Snecma
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 filed Critical Snecma
Publication of BR112016007445A2 publication Critical patent/BR112016007445A2/pt
Publication of BR112016007445B1 publication Critical patent/BR112016007445B1/pt

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00Subject matter not provided for in other groups of this subclass
    • B29D99/0025Producing blades or the like, e.g. blades for turbines, propellers, or wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29BPREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B11/00Making preforms
    • B29B11/14Making preforms characterised by structure or composition
    • B29B11/16Making preforms characterised by structure or composition comprising fillers or reinforcement
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/006Pressing and sintering powders, granules or fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C45/00Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
    • B29C45/0005Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor using fibre reinforcements
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06Fibrous reinforcements only
    • B29C70/10Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/24Fibrous 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
    • B29C70/48Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00Subject matter not provided for in other groups of this subclass
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282Selecting composite materials, e.g. blades with reinforcing filaments
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/08Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/36Application in turbines specially adapted for the fan of turbofan engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/20Manufacture essentially without removing material
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/20Rotors
    • F05D2240/30Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/60Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603Composites; e.g. fibre-reinforced
    • F05D2300/6034Orientation of fibres, weaving, ply angle

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Textile Engineering (AREA)
  • Materials Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • General Engineering & Computer Science (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Woven Fabrics (AREA)

Abstract

trata-se de uma montagem de compactação que compreende um molde modelador (24) que delimita um alojamento aberto no topo com capacidade para receber uma pré-forma tecida (10a) pré-cortada e uma ferramenta de compactação (128) que tem capacidade para se mover verticalmente e que forma, junto com o molde modelador (24), uma montagem de compactação para compactar a dita pré-forma colocada anteriormente no alojamento. a ferramenta de compactação (128) compreende pelo menos uma porção de raiz (128a). a invenção é aplicável para fabricar pás compósitas de turbomáquina.
BR112016007445-9A 2013-10-04 2014-10-03 Montagem de compactação para compactar uma pré-forma tecida, método para fabricar uma pá compósita de turbomáquina, pá compósita de turbomáquina, e, turbomáquina BR112016007445B1 (pt)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US201361886725P 2013-10-04 2013-10-04
US61/886,725 2013-10-04
FR1456021A FR3022829B1 (fr) 2014-06-27 2014-06-27 Ensemble de compactage et procede de fabrication d'une aube composite de turbomachine
FR1456021 2014-06-27
PCT/FR2014/052515 WO2015049475A1 (fr) 2013-10-04 2014-10-03 Ensemble de compactage et procede de fabrication d'une aube composite de turbomachine

Publications (2)

Publication Number Publication Date
BR112016007445A2 true BR112016007445A2 (pt) 2017-08-01
BR112016007445B1 BR112016007445B1 (pt) 2021-12-14

Family

ID=51261167

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112016007445-9A BR112016007445B1 (pt) 2013-10-04 2014-10-03 Montagem de compactação para compactar uma pré-forma tecida, método para fabricar uma pá compósita de turbomáquina, pá compósita de turbomáquina, e, turbomáquina

Country Status (9)

Country Link
US (1) US10569489B2 (pt)
EP (1) EP3052286B1 (pt)
JP (1) JP6397006B2 (pt)
CN (1) CN105592995B (pt)
BR (1) BR112016007445B1 (pt)
CA (1) CA2926069C (pt)
FR (1) FR3022829B1 (pt)
RU (1) RU2671736C2 (pt)
WO (1) WO2015049475A1 (pt)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3029134B1 (fr) * 2014-12-02 2017-10-06 Snecma Procede de controle de position d'une preforme d'aube composite de turbomachine dans un moule
CN107839258B (zh) * 2016-09-20 2019-09-10 江苏亨睿碳纤维科技有限公司 半自动膜辅助压缩成型工艺
FR3060179B1 (fr) * 2016-12-08 2020-04-03 Safran Procede et dispositif de determination des orientations d'elements de fibres dans une piece en materiau composite
US10391723B2 (en) * 2017-08-31 2019-08-27 The Boeing Company Rotary compaction tool
FR3089857B1 (fr) 2018-12-13 2022-02-18 Safran Aircraft Engines Réparation de pièces en matériau composite à matrice organique
FR3096375B1 (fr) * 2019-05-21 2021-04-30 Safran Ceram Texture fibreuse comprenant un fil de marquage et son procédé d’obtention
EP3854560A1 (en) * 2020-01-27 2021-07-28 Siemens Gamesa Renewable Energy A/S Method for fabricating a wind turbine shell, wind turbine blade, wind turbine and method for repair of a wind turbine blade shell
US11352891B2 (en) 2020-10-19 2022-06-07 Pratt & Whitney Canada Corp. Method for manufacturing a composite guide vane having a metallic leading edge
FR3118030B1 (fr) * 2020-12-18 2023-09-01 Safran Ceram Procédé de fabrication d’une pièce en matériau composite à matrice céramique
US20220297391A1 (en) * 2021-03-19 2022-09-22 Safran Tracer strand for weaving a composite material part reinforcement
FR3121624B1 (fr) * 2021-04-07 2023-11-17 Safran Aircraft Engines Ajustement du torsadage pour optimiser les moules et la mise en forme des architectures textiles
FR3130672B1 (fr) * 2021-12-16 2023-11-03 Safran Aircraft Engines Dispositif de mise en forme d’une preforme fibreuse pour la realisation d’une piece aubagee de turbomachine
WO2022229548A1 (fr) * 2021-04-28 2022-11-03 Safran Aircraft Engines Dispositif de mise en forme d'une preforme fibreuse pour la realisation d'une piece aubagee de turbomachine
WO2023275458A1 (fr) 2021-06-29 2023-01-05 Safran Aircraft Engines Mise en forme reproductible d'une ebauche fibreuse
FR3134338A1 (fr) 2022-04-12 2023-10-13 Safran Aircraft Engines Mise en forme reproductible d’une ébauche fibreuse
US20240084707A1 (en) * 2022-09-13 2024-03-14 BladeX Technologies, LLC Fiber Reinforced Polymer Blade
FR3139493A1 (fr) * 2022-09-14 2024-03-15 Safran Aircraft Engines Texture fibreuse de pied d’aube ou d’helice
CN117464891A (zh) * 2023-10-23 2024-01-30 台春节能新材料(苏州)有限公司 一种用于高热阻性xps挤塑保温板生产的挤出装置

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2746514A (en) * 1950-04-06 1956-05-22 Cincinnati Testing And Res Lab Machine for making compressor blades
DE2701480C3 (de) 1977-01-12 1986-01-02 Lignotock Verfahrenstechnik Gmbh, 1000 Berlin Schrittweise arbeitende Vorrichtung zum Herstellen von Vorformkörpern
US5013216A (en) 1988-09-09 1991-05-07 Airfoil Textron Inc. Composite blade perform with divergent root
FR2732406B1 (fr) 1995-03-29 1997-08-29 Snecma Aube de turbomachine en materiau composite
FR2861143B1 (fr) 2003-10-20 2006-01-20 Snecma Moteurs Aube de turbomachine, notamment aube de soufflante et son procede de fabrication
FR2892339B1 (fr) * 2005-10-21 2009-08-21 Snecma Sa Procede de fabrication d'une aube de turbomachine composite, et aube obtenue par ce procede
FR2933634B1 (fr) * 2008-07-10 2010-08-27 Snecma Aube redresseur de soufflante en composite 3d
FR2939129B1 (fr) * 2008-11-28 2014-08-22 Snecma Propulsion Solide Aube de turbomachine en materiau composite et procede pour sa fabrication.
FR2949710B1 (fr) * 2009-09-04 2011-11-25 Lorraine Construction Aeronautique Dispositif de moulage destine a recevoir des fibres et une resine par injection.
FR2950286B1 (fr) 2009-09-24 2013-08-09 Snecma Procede de fabrication d'une aube de turbomachine en materiau composite
FR2974752B1 (fr) * 2011-05-06 2013-04-19 Snecma Procede de moulage par injection d'une piece en materiau composite
US20140203468A1 (en) * 2012-01-26 2014-07-24 Weir Minerals Australia Ltd Polymer Composites

Also Published As

Publication number Publication date
EP3052286B1 (fr) 2020-07-15
WO2015049475A1 (fr) 2015-04-09
EP3052286A1 (fr) 2016-08-10
US10569489B2 (en) 2020-02-25
RU2671736C2 (ru) 2018-11-06
FR3022829B1 (fr) 2017-02-24
CA2926069A1 (fr) 2015-04-09
CA2926069C (fr) 2021-08-31
JP6397006B2 (ja) 2018-09-26
RU2016117170A (ru) 2017-11-10
BR112016007445B1 (pt) 2021-12-14
JP2016539819A (ja) 2016-12-22
FR3022829A1 (fr) 2016-01-01
RU2016117170A3 (pt) 2018-05-17
US20160243777A1 (en) 2016-08-25
CN105592995B (zh) 2018-08-10
CN105592995A (zh) 2016-05-18

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Legal Events

Date Code Title Description
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B06A Patent application procedure suspended [chapter 6.1 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 03/10/2014, OBSERVADAS AS CONDICOES LEGAIS.