BR112014014540A2 - estrutura de reforço fibroso para parte de material compósito que tem uma porção de espessura reduzida - Google Patents

estrutura de reforço fibroso para parte de material compósito que tem uma porção de espessura reduzida

Info

Publication number
BR112014014540A2
BR112014014540A2 BR112014014540A BR112014014540A BR112014014540A2 BR 112014014540 A2 BR112014014540 A2 BR 112014014540A2 BR 112014014540 A BR112014014540 A BR 112014014540A BR 112014014540 A BR112014014540 A BR 112014014540A BR 112014014540 A2 BR112014014540 A2 BR 112014014540A2
Authority
BR
Brazil
Prior art keywords
yarns
layers
yarn
layer
composite material
Prior art date
Application number
BR112014014540A
Other languages
English (en)
Other versions
BR112014014540B1 (pt
Inventor
Jacques Gérard Dambrine Bruno
Coupe Dominique
Mahieu Jean-Noël
Goering Jonathan
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 BR112014014540A2 publication Critical patent/BR112014014540A2/pt
Publication of BR112014014540B1 publication Critical patent/BR112014014540B1/pt

Links

Classifications

    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D25/00—Woven fabrics not otherwise provided for
    • 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
    • F01D5/14—Form or construction
    • F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow 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
    • 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
    • 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
    • F01D5/286—Particular treatment of blades, e.g. to increase durability or resistance against corrosion or erosion
    • 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
    • F01D5/288—Protective coatings for 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
    • F01D5/3092—Protective layers between blade root and rotor disc surfaces, e.g. anti-friction layers
    • 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
    • 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)
  • Chemical & Material Sciences (AREA)
  • Textile Engineering (AREA)
  • Materials Engineering (AREA)
  • Composite Materials (AREA)
  • Architecture (AREA)
  • Woven Fabrics (AREA)

Abstract

1/1 resumo “estrutura de reforço fibroso para parte de material compósito que tem uma porção de espessura reduzida” a invenção se refere a uma estrutura de fibra (200) para reforçar uma parte de material compósito tecida como uma peça única por meio de tecelagem de múltiplas camadas entre uma primeira pluralidade de camadas de fios (c1-c10) e uma segunda pluralidade de camadas de fios (t1-t10). a estrutura de fibra inclui uma porção (204) que tem uma espessura decrescente e tem uma pluralidade de porções de retrocesso de fios de continuidade superficial (210, 211, 212) na dita porção, em que cada porção tem fios (f; f; f) de uma camada de fios (c, c; c3c8c438 c4) da primeira pluralidade de camadas de fios (c1; c10) da primeira pluralidade de camadas de fios subjacente à camada de fios da primeira pluralidade de camadas de fios e várias porções de retrocesso de fios de descontinuidade superficial situada sobre a superfície da estrutura, que são interrompidos. cada fio interrompido (fc1; f) é substituído, na superfície da estrutura, por um fio (f; f) de uma camada c10c2c9 de fios (c2; c9) subjacente à primeira pluralidade de camadas de fios. os fios das camadas da segunda pluralidade de camadas de fios (t1-t10) situada na superfície da estrutura de fibra são contínuos sobre pelo menos toda a porção (204) de espessura decrescente.
BR112014014540-7A 2011-12-14 2012-12-10 estrutura de fibra para reforçar uma peça de material compósito, peça de material compósito, turbopropulsor, aeronave e método de fabricação de um estrutura de fibra BR112014014540B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201161570379P 2011-12-14 2011-12-14
US61/570,379 2011-12-14
PCT/FR2012/052851 WO2013088038A2 (fr) 2011-12-14 2012-12-10 Structure fibreuse de renfort de pieces en materiau composite a portion d'epaisseur reduite

Publications (2)

Publication Number Publication Date
BR112014014540A2 true BR112014014540A2 (pt) 2017-06-13
BR112014014540B1 BR112014014540B1 (pt) 2021-03-09

Family

ID=47666411

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112014014540-7A BR112014014540B1 (pt) 2011-12-14 2012-12-10 estrutura de fibra para reforçar uma peça de material compósito, peça de material compósito, turbopropulsor, aeronave e método de fabricação de um estrutura de fibra

Country Status (8)

Country Link
US (1) US9617858B2 (pt)
EP (1) EP2791405B1 (pt)
JP (1) JP6254532B2 (pt)
CN (1) CN103998663B (pt)
BR (1) BR112014014540B1 (pt)
CA (1) CA2858790C (pt)
RU (1) RU2617298C2 (pt)
WO (1) WO2013088038A2 (pt)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2970715B1 (fr) * 2011-01-21 2014-10-17 Snecma Structure fibreuse tissee multicouches ayant une partie tubulaire creuse, procede de fabrication et piece composite la comportant
WO2013088037A2 (fr) * 2011-12-14 2013-06-20 Snecma Metier a tisser avec contexture en chaine optimisee
FR3011253B1 (fr) * 2013-10-01 2016-06-10 Snecma Structure fibreuse avec regroupement des flottes
KR20180044416A (ko) * 2015-09-02 2018-05-02 알바니 엔지니어드 콤포짓스, 인크. 내충돌성을 위한 3차원 제직 복합체 차량 성분
FR3040909B1 (fr) * 2015-09-16 2018-03-16 Safran Aircraft Engines Preforme fibreuse pour aube de turbomachine en materiau composite et procede de fabrication d'une telle preforme
FR3055569B1 (fr) 2016-09-02 2019-11-22 Porcher Industries Preforme, piece d'ossature et procede de fabrication d'une telle preforme
JP6790967B2 (ja) * 2017-03-31 2020-11-25 株式会社豊田自動織機 繊維構造体及び繊維強化複合材
WO2019097147A1 (fr) 2017-11-14 2019-05-23 Safran Ceramics Structure fibreuse et piece en materiau composite incorporant une telle structure
FR3082854B1 (fr) 2018-06-25 2020-09-11 Safran Ceram Structure fibreuse et piece en materiau composite incorporant une telle structure
CN108004650B (zh) * 2017-12-11 2020-03-17 南京玻璃纤维研究设计院有限公司 大尺寸变厚度回转体预制体及其制备方法
IL259149B (en) 2018-05-03 2022-09-01 Israel Aerospace Ind Ltd Structural elements made of composite materials
FR3084088B1 (fr) * 2018-07-23 2020-10-02 Safran Texture fibreuse pour carter en materiau composite a resistance a l'impact amelioree
FR3084089B1 (fr) * 2018-07-23 2020-10-02 Safran Texture fibreuse pour carter en materiau composite a resistance au cisaillement amelioree
CN109972271B (zh) * 2019-03-27 2023-03-14 南京玻璃纤维研究设计院有限公司 一种变厚度预制体、一种复合部件以及一种变厚度预制体的减纱方法
GB201913394D0 (en) * 2019-09-17 2019-10-30 Rolls Royce Plc A vane
CN112877862B (zh) * 2021-01-04 2022-04-15 南京玻璃纤维研究设计院有限公司 回转体预制体的制备方法及回转体的制备方法
FR3132461A1 (fr) * 2022-02-10 2023-08-11 Safran Aircraft Engines Procédé de fabrication d’une plateforme inter-aubes avec bords sacrificiels

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1379716B1 (en) * 2001-09-12 2007-07-18 Lockheed Martin Corporation Woven preform for structural joints
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
US7943535B2 (en) * 2005-11-17 2011-05-17 Albany Engineered Composites, Inc. Hybrid three-dimensional woven/laminated struts for composite structural applications
US7655581B2 (en) * 2005-11-17 2010-02-02 Albany Engineered Composites, Inc. Hybrid three-dimensional woven/laminated struts for composite structural applications
FR2911644B1 (fr) 2007-01-23 2012-06-01 Snecma Turbopropulseur comportant une helice formee de pales a orientation reglable.
FR2932408B1 (fr) * 2008-06-11 2010-05-28 Aircelle Sa Preforme destinee a former une piece mecanique structurante creuse
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.
FR2939153B1 (fr) * 2008-11-28 2011-12-09 Snecma Propulsion Solide Realisation d'une structure fibreuse a epaisseur evolutive par tissage 3d
US20110176927A1 (en) 2010-01-20 2011-07-21 United Technologies Corporation Composite fan blade

Also Published As

Publication number Publication date
US20140334935A1 (en) 2014-11-13
EP2791405B1 (fr) 2020-04-15
WO2013088038A3 (fr) 2014-01-16
RU2014128619A (ru) 2016-02-10
WO2013088038A2 (fr) 2013-06-20
CA2858790A1 (fr) 2013-06-20
BR112014014540B1 (pt) 2021-03-09
EP2791405A2 (fr) 2014-10-22
CN103998663A (zh) 2014-08-20
JP6254532B2 (ja) 2017-12-27
US9617858B2 (en) 2017-04-11
RU2617298C2 (ru) 2017-04-24
CA2858790C (fr) 2020-09-29
CN103998663B (zh) 2016-11-16
JP2015504980A (ja) 2015-02-16

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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]
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 10/12/2012, OBSERVADAS AS CONDICOES LEGAIS.