BR112016002096A2 - processo para fabricação de um compósito de fibra termoplástica e pá de ventilador de compósito de fibra termoplástica de motor de turbina a gás - Google Patents

processo para fabricação de um compósito de fibra termoplástica e pá de ventilador de compósito de fibra termoplástica de motor de turbina a gás

Info

Publication number
BR112016002096A2
BR112016002096A2 BR112016002096A BR112016002096A BR112016002096A2 BR 112016002096 A2 BR112016002096 A2 BR 112016002096A2 BR 112016002096 A BR112016002096 A BR 112016002096A BR 112016002096 A BR112016002096 A BR 112016002096A BR 112016002096 A2 BR112016002096 A2 BR 112016002096A2
Authority
BR
Brazil
Prior art keywords
fiber composite
thermoplastic fiber
manufacturing
gas turbine
turbine engine
Prior art date
Application number
BR112016002096A
Other languages
English (en)
Inventor
Duane Ward Douglas
Carl Gemeinhardt Gregory
Stephen Manicke Paul
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 BR112016002096A2 publication Critical patent/BR112016002096A2/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
    • B29C70/10Fibrous 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
    • B29C70/20Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel 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
    • 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
    • B29C70/30Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/38Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • 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
    • 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
    • F01D5/14Form or construction
    • 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/325Rotors specially for elastic fluids for axial flow pumps for axial flow fans
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/38Blades
    • F04D29/388Blades characterised by construction
    • 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
    • B29C70/30Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/302Details of the edges of fibre composites, e.g. edge finishing or means to avoid delamination
    • 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
    • B29K2071/00Use of polyethers, e.g. PEEK, i.e. polyether-etherketone or PEK, i.e. polyetherketone 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
    • 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
    • B29K2309/00Use of inorganic materials not provided for in groups B29K2303/00 - B29K2307/00, as reinforcement
    • B29K2309/08Glass
    • 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
    • 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

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

Abstract

trata-se de um processo para fabricação de um compósito de fibra termoplástica que inclui aquecer uma resina termoplástica para um estado líquido, orientar unidirecionalmente as fibras, impregnar as fibras com a resina termoplástica no estado líquido para produzir lâminas compósitas, e operar um processo de laminação automatizado por máquina para produzir um laminado compósito que compreende uma pluralidade das lâminas compósita.
BR112016002096A 2013-08-01 2014-07-28 processo para fabricação de um compósito de fibra termoplástica e pá de ventilador de compósito de fibra termoplástica de motor de turbina a gás BR112016002096A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201361860990P 2013-08-01 2013-08-01
PCT/US2014/048428 WO2015060917A2 (en) 2013-08-01 2014-07-28 Process of producing a thermoplastic-fiber composite and fan blades formed therefrom

Publications (1)

Publication Number Publication Date
BR112016002096A2 true BR112016002096A2 (pt) 2017-08-01

Family

ID=52474058

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112016002096A BR112016002096A2 (pt) 2013-08-01 2014-07-28 processo para fabricação de um compósito de fibra termoplástica e pá de ventilador de compósito de fibra termoplástica de motor de turbina a gás

Country Status (7)

Country Link
US (1) US20160186774A1 (pt)
EP (1) EP3027371A2 (pt)
JP (1) JP2016528345A (pt)
CN (1) CN105408079B (pt)
BR (1) BR112016002096A2 (pt)
CA (1) CA2919123A1 (pt)
WO (1) WO2015060917A2 (pt)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9909505B2 (en) * 2011-07-05 2018-03-06 United Technologies Corporation Efficient, low pressure ratio propulsor for gas turbine engines
USD804647S1 (en) * 2016-02-02 2017-12-05 Delta Electronics, Inc. Fan blade
EP3406424B1 (en) 2017-05-22 2021-04-28 Ratier-Figeac SAS Aircraft blade and methods of forming and repairing an aircraft blade
EP3406434A1 (en) 2017-05-22 2018-11-28 Ratier-Figeac SAS Composite blade and method of manufacture
EP3406778B1 (en) 2017-05-22 2022-04-13 Ratier-Figeac SAS Method of manufacturing a composite aircraft blade
USD911512S1 (en) 2018-01-31 2021-02-23 Carrier Corporation Axial flow fan
EP3957687A4 (en) * 2019-04-19 2022-06-22 Teijin Limited PREPREGNATED WITH THERMOPLASTIC RESIN, METHOD FOR PRODUCTION THEREOF, AND FIBER REINFORCED COMPOSITE MATERIAL
CN111927800A (zh) * 2020-08-13 2020-11-13 马宁疆 一种风扇用芳香防尘材料及其制备方法

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1328167A (en) * 1971-06-18 1973-08-30 Rolls Royce Rotor blade for a gas turbine engine
JPH03286841A (ja) * 1990-04-02 1991-12-17 Mitsubishi Heavy Ind Ltd 複合材構造物の製造方法
JPH0578943A (ja) * 1991-09-12 1993-03-30 Honda Motor Co Ltd 熱可塑性複合素材及び熱可塑性複合体
FR2684719B1 (fr) * 1991-12-04 1994-02-11 Snecma Aube de turbomachine comprenant des nappes de materiau composite.
EP0810081B1 (en) * 1995-12-04 2003-03-26 Toray Industries, Inc. Pressure vessel and method of manufacturing same
US6558146B1 (en) * 2000-10-10 2003-05-06 Delphi Technologies, Inc. Extrusion deposition molding with in-line compounding of reinforcing fibers
AU2002239847A1 (en) * 2002-01-11 2003-07-30 S.D. Warren Services Company Composite doctor blades
DE102006025280A1 (de) * 2005-06-01 2006-12-14 Institut Für Verbundwerkstoffe Gmbh Verfahren zur Herstellung eines faserverstärkten Bauteils und Vorrichtung dazu
GB0619401D0 (en) * 2006-10-02 2006-11-08 Hexcel Composites Ltd Composite materials with improved performance
JP4862913B2 (ja) * 2009-03-31 2012-01-25 東レ株式会社 プリプレグおよびプリフォーム
GB0908707D0 (en) * 2009-05-21 2009-07-01 Rolls Royce Plc Reinforced composite aerofoil blade
JP5660563B2 (ja) * 2010-03-31 2015-01-28 広島県 繊維強化熱可塑性樹脂プリプレグの積層方法
US20120087801A1 (en) * 2010-10-12 2012-04-12 General Electric Company Composite components and processes therefor
EP2472063B1 (fr) * 2010-12-30 2015-02-11 Techspace Aero S.A. Aube en matériau composite
JP2012167252A (ja) * 2011-01-27 2012-09-06 Toray Ind Inc 細幅プリプレグの製造方法、および繊維強化プラスチック
CN102729483A (zh) * 2011-04-15 2012-10-17 中国海洋石油总公司 连续长纤维增强热塑性树脂及其制备方法与成型设备
DE102011050780B4 (de) * 2011-05-31 2015-04-16 Reis Group Holding Gmbh & Co. Kg Verfahren und Anordnung zum Aufbringen einer Endlosfaser auf ein Objekt
JP5751415B2 (ja) * 2011-07-13 2015-07-22 株式会社Ihi ガスタービンエンジン用ブレードの製造方法
JP2013117014A (ja) * 2011-10-31 2013-06-13 Toray Ind Inc 炭素繊維強化成形品の製造方法および炭素繊維強化成形品
EP2599614B1 (fr) * 2011-12-01 2016-03-02 Techspace Aero S.A. Procédé de réalisation d'une préforme et son utilisation dans la fabrication d'une pièce composite

Also Published As

Publication number Publication date
EP3027371A2 (en) 2016-06-08
JP2016528345A (ja) 2016-09-15
CN105408079A (zh) 2016-03-16
WO2015060917A3 (en) 2015-06-18
CA2919123A1 (en) 2015-04-30
US20160186774A1 (en) 2016-06-30
WO2015060917A2 (en) 2015-04-30
CN105408079B (zh) 2018-06-22

Similar Documents

Publication Publication Date Title
BR112016002096A2 (pt) processo para fabricação de um compósito de fibra termoplástica e pá de ventilador de compósito de fibra termoplástica de motor de turbina a gás
FR2962175B1 (fr) Aube a longeron composite integre
BR102015018910A8 (pt) método de fabricação de uma pá de rotor de uma turbina eólica, pá de rotor de uma turbina eólica e método de fabricação de uma pá de rotor de uma turbina eólica
BR112014027013A2 (pt) reforço estrutural, pá de motor de turbina, e, motor de turbina
BR112015032418A8 (pt) método de produzir uma formação de camadas de laminado compósito com um padrão de furos no mesmo, e, laminado compósito
BR112015023361A2 (pt) ligações de via férrea compositas e métodos de produção e uso das mesmas
ES2598778T3 (es) Procedimiento, producto semiacabado para la fabricación de un componente reforzado con fibras de una turbina eólica y uso del producto semiacabado
BR112014030596A2 (pt) "estrutura compósita, pá de ventilador e método para produzir uma estrutura compósita
BR112014019838A8 (pt) Colmeia unida, nacela de motor, motor a jato, método para unir seções de colmeia, método para criar uma nacela de motor e método para criar um motor a jato
BR112018001278A2 (pt) ?produto de madeira fabricado e processo de produzir um produto de madeira fabricado?
BR112018009470A2 (pt) ?véu híbrido, laminado compósito, pré-forma fibrosa, pré-impregnado, fita de pré-impregnado, fita fibrosa, tecido, estrutura compósita polimérica reforçada com fibra, e, métodos para fabricar um pré-impregnado modificado e para fabricar uma estrutura compósita?
BR112014013054A2 (pt) base de aro com flange integrado, feita de materiais compostos de fibras, bem como um processo para sua produção
BR112016014911A8 (pt) fibra inorgânica com encolhimento e resistência aumentados
BR112015013093A2 (pt) processo para produzir um material compósito reforçado com fibra, com uma matriz de poliamida e material compósito reforçado com fibra.
CL2013000505A1 (es) Estructura fibrosa fijada y/o estabilizada de un material fibroso asi como un agente para su fijacion y estabilizacion, donde dicho agente es al menos un copoliester estadistico formado por: acido tereftalico, acido isoftalico, butanodiol, dietilenglicol, trietilenglicol; metodo de fabricacion; material compuesto de resina-fibra; y uso de dicha estructura.
BR112015016624A2 (pt) laminado composto reforçado com fibra triaxial
BR112018067675A2 (pt) composição curável, processos para produzir uma composição curável e um artigo de compósito e para preparar um artigo curado, e, artigo de compósito
BR112018000845A2 (pt) lâmina de turbina eólica com locais de ancoragem
BR112015001029A2 (pt) processos para produzir um material compreendendo poliisocianurato intermediário, estável e adicionalmente curável, e para adicionalmente curar o material compreendendo poliisocianurato intermediário, e, material compreendendo poliisocianurato intermediário, estável e adicionalmente curável
AR086139A1 (es) Instalacion de energia eolica
BR112012008976A2 (pt) sistema para fazer variar a incidência das pás de uma hélice de turbomáquina para aeronave, hélice para turbomáquina de aeronave, turbomáquina para aeronave, e, processo de comando da incidência das pás de uma hélice de turbomáquina para aeronave
BR112016002428A2 (pt) método para fabricação de uma moldagem compósita, moldagem compósita, componente em sanduíche, elemento de pá de rotor, e, usina de energia eólica
WO2015142395A3 (en) Compressed chopped fiber composite fan blade platform
GB2519845B (en) Blisk with low stresses at blade root, preferably for an aircraft turbine engine fan
BR112013021601A2 (pt) uso de estruturas em camadas para centrais de energia eólica

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 5A ANUIDADE.

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

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2524 DE 21-05-2019 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.