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BR112014030596A2 - "estrutura compósita, pá de ventilador e método para produzir uma estrutura compósita - Google Patents

"estrutura compósita, pá de ventilador e método para produzir uma estrutura compósita

Info

Publication number
BR112014030596A2
BR112014030596A2 BR112014030596A BR112014030596A BR112014030596A2 BR 112014030596 A2 BR112014030596 A2 BR 112014030596A2 BR 112014030596 A BR112014030596 A BR 112014030596A BR 112014030596 A BR112014030596 A BR 112014030596A BR 112014030596 A2 BR112014030596 A2 BR 112014030596A2
Authority
BR
Brazil
Prior art keywords
composite structure
producing
fan blade
composite
fan
Prior art date
Application number
BR112014030596A
Other languages
English (en)
Inventor
Shim Dong-Jin
Joseph Kray Nicholas
Spoonire Ross
Wen-Ling Lin Wendy
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of BR112014030596A2 publication Critical patent/BR112014030596A2/pt

Links

Classifications

    • 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
    • B29C70/08Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
    • 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
    • B29C70/08Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
    • B29C70/086Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers and with one or more layers of pure plastics material, e.g. foam layers
    • 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
    • B29C70/68Shaping 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
    • B29C70/86Incorporated in coherent impregnated reinforcing layers, e.g. by winding
    • B29C70/865Incorporated in coherent impregnated reinforcing layers, e.g. by winding completely encapsulated
    • 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
    • B29D99/001Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
    • B29D99/0021Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with plain or filled structures, e.g. cores, placed between two or more plates or sheets, e.g. in a matrix
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • B32B5/06Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer characterised by a fibrous or filamentary layer mechanically connected, e.g. by needling to another layer, e.g. of fibres, of paper
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2063/00Use of EP, i.e. epoxy resins or derivatives thereof, as moulding material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2307/00Use of elements other than metals as reinforcement
    • B29K2307/04Carbon
    • 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
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/23Sheet including cover or casing
    • Y10T428/233Foamed or expanded material encased
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/23Sheet including cover or casing
    • Y10T428/239Complete cover or casing

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Textile Engineering (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
BR112014030596A 2012-06-06 2013-05-31 "estrutura compósita, pá de ventilador e método para produzir uma estrutura compósita BR112014030596A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/490,235 US20130330496A1 (en) 2012-06-06 2012-06-06 Composite structure with low density core and composite stitching reinforcement
PCT/US2013/043510 WO2013184491A1 (en) 2012-06-06 2013-05-31 Composite structure with low density core and composite stitching reinforcement

Publications (1)

Publication Number Publication Date
BR112014030596A2 true BR112014030596A2 (pt) 2017-06-27

Family

ID=48626642

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112014030596A BR112014030596A2 (pt) 2012-06-06 2013-05-31 "estrutura compósita, pá de ventilador e método para produzir uma estrutura compósita

Country Status (7)

Country Link
US (1) US20130330496A1 (pt)
EP (1) EP2858810A1 (pt)
JP (1) JP2015525155A (pt)
CN (1) CN104349888A (pt)
BR (1) BR112014030596A2 (pt)
CA (1) CA2875029A1 (pt)
WO (1) WO2013184491A1 (pt)

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US20140248156A1 (en) * 2012-12-21 2014-09-04 United Technologies Corporation Composite Articles and Methods
US9835112B2 (en) * 2014-02-10 2017-12-05 MRA Systems Inc. Thrust reverser cascade
CN106460865B (zh) 2014-05-05 2019-04-12 霍顿公司 复合物风扇
DE102014015976A1 (de) * 2014-10-31 2016-05-04 Airbus Defence and Space GmbH Verbundkonstruktion für eine erhöhte Lebensdauer
CN107278217B (zh) * 2014-12-22 2021-04-09 巴斯夫欧洲公司 由膨胀的珠粒泡沫制得的纤维增强的模制品
US9828862B2 (en) 2015-01-14 2017-11-28 General Electric Company Frangible airfoil
US10449737B2 (en) 2015-03-04 2019-10-22 Ebert Composites Corporation 3D thermoplastic composite pultrusion system and method
US9616623B2 (en) 2015-03-04 2017-04-11 Ebert Composites Corporation 3D thermoplastic composite pultrusion system and method
US10124546B2 (en) 2015-03-04 2018-11-13 Ebert Composites Corporation 3D thermoplastic composite pultrusion system and method
US9963978B2 (en) 2015-06-09 2018-05-08 Ebert Composites Corporation 3D thermoplastic composite pultrusion system and method
CN106945302A (zh) * 2016-01-07 2017-07-14 中航商用航空发动机有限责任公司 纤维增强复合风扇叶片及其制造方法
JP6672233B2 (ja) * 2017-09-25 2020-03-25 三菱重工業株式会社 複合材翼の成形方法、複合材翼及び複合材翼の成形型
US11931981B2 (en) 2018-01-29 2024-03-19 General Electric Company Reinforced composite blade and method of making a blade
JP6738850B2 (ja) 2018-03-29 2020-08-12 三菱重工業株式会社 複合材料翼および複合材料翼の製造方法
DE102018120905A1 (de) * 2018-08-27 2020-02-27 Wobben Properties Gmbh Faserverbundhalbzeug, Faserverbundbauteil, Rotorblattelement, Rotorblatt und Windenergieanlage sowie Verfahren zum Herstellen eines Faserverbundhalbzeugs und Verfahren zum Herstellen eines Faserverbundbauteils
AU2021204709A1 (en) * 2020-07-29 2022-02-17 The Boeing Company Composite thin wingbox architecture for supersonic business jets
US20240280027A1 (en) * 2023-02-21 2024-08-22 General Electric Company Turbine engine airfoil with a woven core and woven layer

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1411379A (en) * 1971-12-21 1975-10-22 Rolls Royce Fibre reinforced composite structures
JPH01110944A (ja) * 1987-10-26 1989-04-27 Toyota Motor Corp Frp構造体
FR2684719B1 (fr) * 1991-12-04 1994-02-11 Snecma Aube de turbomachine comprenant des nappes de materiau composite.
US5279892A (en) * 1992-06-26 1994-01-18 General Electric Company Composite airfoil with woven insert
AU7470394A (en) * 1993-05-04 1995-02-20 Foster-Miller Inc. Truss reinforced foam core sandwich structure
US6431837B1 (en) * 1999-06-01 2002-08-13 Alexander Velicki Stitched composite fan blade
US20050025948A1 (en) * 2001-04-06 2005-02-03 Johnson David W. Composite laminate reinforced with curvilinear 3-D fiber and method of making the same
US6645333B2 (en) * 2001-04-06 2003-11-11 Ebert Composites Corporation Method of inserting z-axis reinforcing fibers into a composite laminate
US7105071B2 (en) * 2001-04-06 2006-09-12 Ebert Composites Corporation Method of inserting z-axis reinforcing fibers into a composite laminate
CA2456017C (en) * 2001-08-02 2009-12-08 Ebert Composites Corporation Method of clinching top and bottom ends of z-axis fibers into the respective top and bottom surfaces of a composite laminate
US6884507B2 (en) * 2001-10-05 2005-04-26 General Electric Company Use of high modulus, impact resistant foams for structural components
GB0428201D0 (en) * 2004-12-22 2005-01-26 Rolls Royce Plc A composite blade
JP4615398B2 (ja) * 2005-08-26 2011-01-19 本田技研工業株式会社 炭素繊維複合材料成形体
US8357323B2 (en) * 2008-07-16 2013-01-22 Siemens Energy, Inc. Ceramic matrix composite wall with post laminate stitching

Also Published As

Publication number Publication date
WO2013184491A1 (en) 2013-12-12
CN104349888A (zh) 2015-02-11
EP2858810A1 (en) 2015-04-15
US20130330496A1 (en) 2013-12-12
JP2015525155A (ja) 2015-09-03
CA2875029A1 (en) 2013-12-12

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 4A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]