BR112014016858A2 - peça de reforço com seção em tt feita de material compósito, notadamente plataforma de ventoinha de turbomáquina, e seu processo de fabricação - Google Patents

peça de reforço com seção em tt feita de material compósito, notadamente plataforma de ventoinha de turbomáquina, e seu processo de fabricação

Info

Publication number
BR112014016858A2
BR112014016858A2 BR112014016858A BR112014016858A BR112014016858A2 BR 112014016858 A2 BR112014016858 A2 BR 112014016858A2 BR 112014016858 A BR112014016858 A BR 112014016858A BR 112014016858 A BR112014016858 A BR 112014016858A BR 112014016858 A2 BR112014016858 A2 BR 112014016858A2
Authority
BR
Brazil
Prior art keywords
preform
composite material
manufacturing process
fibrous
yarns
Prior art date
Application number
BR112014016858A
Other languages
English (en)
Other versions
BR112014016858B1 (pt
BR112014016858A8 (pt
Inventor
Mahieu Jean-Noël
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 BR112014016858A2 publication Critical patent/BR112014016858A2/pt
Publication of BR112014016858A8 publication Critical patent/BR112014016858A8/pt
Publication of BR112014016858B1 publication Critical patent/BR112014016858B1/pt

Links

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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements
    • F01D11/006—Sealing the gap between rotor blades or blades and rotor
    • F01D11/008—Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
    • 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
    • B29C70/22—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 two directions forming a two dimensional structure
    • B29C70/222—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 two directions forming a two dimensional structure the structure being shaped to form a three dimensional configuration
    • 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
    • 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
    • B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/681—Component parts, details or accessories; Auxiliary operations
    • B29C70/682—Preformed parts characterised by their structure, e.g. form
    • 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
    • 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
    • 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
    • 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
    • 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
    • F05D2300/40—Organic materials
    • F05D2300/44—Resins
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24628—Nonplanar uniform thickness material
    • Y10T428/24636—Embodying mechanically interengaged strand[s], strand-portion[s] or strand-like strip[s] [e.g., weave, knit, etc.]

Landscapes

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

Abstract

1/1 resumo “peça de reforço com seção em . feita de material compósito, notadamente plataforma de ventoinha de turbomáquina, e seu processo de fabricação” a invenção se refere a um processo de fabricação de uma peça de reforço (10) com seção em . feita de material compósito, o processo compreendendo a realização por tecedura tridimensional de um primeiro conjunto de camadas de fios ligadas entre si para formar uma primeira parte de esboço fibroso (102) destinada a formar uma preforma de base, a realização por tecedura tridimensional de um segundo conjunto de camadas de fios ligadas entre si para formar uma segunda parte de esboço fibroso (104) destinada a formar uma preforma de enrijecedor, fios do segundo conjunto sendo ligados por tecedura aos fios do primeiro conjunto em uma tira central de separação (106) que se alarga na direção das bordas laterais (102a) da primeira parte de esboço fibroso ao nível de uma zona (108, 110) que corresponde ao degrau da base, a conformação das duas partes de esboço fibroso para obter uma preforma fibrosa (100) feita de uma só peça que tem uma parte que forma preforma de base e uma parte que forma preforma de enrijecedor, e a colocação de uma resina na preforma fibrosa por uma matriz. a invenção se refere também a uma peça de reforço com seção em . obtida pelo processo.
BR112014016858-0A 2012-01-09 2013-01-07 processo de fabricação de peça de reforço, peça de reforço e turbomáquina BR112014016858B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201261584422P 2012-01-09 2012-01-09
US61/584,422 2012-01-09
PCT/FR2013/050027 WO2013104853A2 (fr) 2012-01-09 2013-01-07 Piece de renfort a section en pi en materiau composite, notamment plate-forme de soufflante de turbomachine, et son procede de fabrication

Publications (3)

Publication Number Publication Date
BR112014016858A2 true BR112014016858A2 (pt) 2017-06-13
BR112014016858A8 BR112014016858A8 (pt) 2017-07-04
BR112014016858B1 BR112014016858B1 (pt) 2021-05-25

Family

ID=47748664

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112014016858-0A BR112014016858B1 (pt) 2012-01-09 2013-01-07 processo de fabricação de peça de reforço, peça de reforço e turbomáquina

Country Status (8)

Country Link
US (1) US9657583B2 (pt)
EP (1) EP2802702B1 (pt)
JP (1) JP6165774B2 (pt)
CN (1) CN104040057B (pt)
BR (1) BR112014016858B1 (pt)
CA (1) CA2860379C (pt)
RU (1) RU2612993C2 (pt)
WO (1) WO2013104853A2 (pt)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3018473B1 (fr) 2014-03-17 2016-04-08 Snecma Procede de fabrication d'une plate-forme d'aube en materiau composite a joints integres pour soufflante de turbomachine
US10156151B2 (en) * 2014-10-23 2018-12-18 Rolls-Royce North American Technologies Inc. Composite annulus filler
FR3037097B1 (fr) * 2015-06-03 2017-06-23 Snecma Aube composite comprenant une plateforme munie d'un raidisseur
US10081154B2 (en) * 2015-05-06 2018-09-25 Li-Ju TSAI Integrated open box-like woven fabric
US10605117B2 (en) 2015-10-08 2020-03-31 General Electric Company Fan platform for a gas turbine engine
FR3107077B1 (fr) * 2020-02-12 2022-12-23 Safran Aircraft Engines Plateforme de turbomachine rigidifiee
FR3107915B1 (fr) * 2020-03-03 2022-02-04 Safran Aircraft Engines Procede de fabrication d’une plateforme composite pour une soufflante de turbomachine d’aeronef
US11766828B2 (en) * 2020-07-15 2023-09-26 Spirit Aerosystems, Inc. Method of manufacturing folded structure with additive features
CN112538680B (zh) * 2020-11-02 2022-07-12 南京玻璃纤维研究设计院有限公司 中空盒状纤维增强体及其制备方法、中空盒的制备方法
CN112626680B (zh) * 2020-12-10 2022-04-22 南京玻璃纤维研究设计院有限公司 一种三维机织封闭式空腔结构的制备方法及其预制件
CN114635217B (zh) * 2022-03-09 2023-05-09 南京玻璃纤维研究设计院有限公司 一种三维机织复合材料风扇流道平台预制件及其制备方法
FR3141872A1 (fr) * 2022-11-10 2024-05-17 Safran Aircraft Engines Texture fibreuse comprenant deux portions de déploiement
FR3141873A1 (fr) * 2022-11-10 2024-05-17 Safran Aircraft Engines Texture fibreuse comprenant deux portions de déploiement

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3812909A1 (de) * 1987-09-26 1989-04-13 Vorwerk Co Interholding Aus mehrlagengewebe bestehender vor-formling
JPH03119138A (ja) * 1989-09-29 1991-05-21 Shikishima Kanbasu Kk 繊維補強複合材
US6446675B1 (en) * 2001-07-05 2002-09-10 Albany International Techniweave, Inc. Minimum distortion 3D woven preforms
US6874543B2 (en) * 2001-09-12 2005-04-05 Lockheed Martin Corporation Woven preform for structural joints
US8440276B2 (en) * 2008-02-11 2013-05-14 Albany Engineered Composites, Inc. Multidirectionally reinforced shape woven preforms for composite structures
US7712488B2 (en) * 2008-03-31 2010-05-11 Albany Engineered Composites, Inc. Fiber architecture for Pi-preforms
US8127802B2 (en) * 2008-10-29 2012-03-06 Albany Engineered Composites, Inc. Pi-preform with variable width clevis
US8079387B2 (en) * 2008-10-29 2011-12-20 Albany Engineered Composites, Inc. Pi-shaped preform
FR2939129B1 (fr) * 2008-11-28 2014-08-22 Snecma Propulsion Solide Aube de turbomachine en materiau composite et procede pour sa fabrication.
US8846553B2 (en) * 2008-12-30 2014-09-30 Albany Engineered Composites, Inc. Woven preform with integral off axis stiffeners
FR2943942B1 (fr) * 2009-04-06 2016-01-29 Snecma Procede de fabrication d'une aube de turbomachine en materiau composite
FR2954271B1 (fr) * 2009-12-21 2012-02-17 Snecma Pale d'helice d'aeronef
FR2961846B1 (fr) * 2010-06-28 2012-08-03 Snecma Propulsion Solide Aube de turbomachine a geometrie asymetrique complementaire

Also Published As

Publication number Publication date
WO2013104853A3 (fr) 2014-02-20
CN104040057B (zh) 2016-03-02
EP2802702A2 (fr) 2014-11-19
JP2015509053A (ja) 2015-03-26
RU2612993C2 (ru) 2017-03-14
US20140363299A1 (en) 2014-12-11
CA2860379A1 (fr) 2013-07-18
JP6165774B2 (ja) 2017-07-19
BR112014016858B1 (pt) 2021-05-25
CA2860379C (fr) 2019-06-04
US9657583B2 (en) 2017-05-23
RU2014132891A (ru) 2016-02-27
CN104040057A (zh) 2014-09-10
EP2802702B1 (fr) 2018-12-26
BR112014016858A8 (pt) 2017-07-04
WO2013104853A2 (fr) 2013-07-18

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
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 07/01/2013, OBSERVADAS AS CONDICOES LEGAIS.