MX2015008509A - Metodo de fabricacion de estructura compuesta curveada utilizando cinta compuesta de prepeg. - Google Patents

Metodo de fabricacion de estructura compuesta curveada utilizando cinta compuesta de prepeg.

Info

Publication number
MX2015008509A
MX2015008509A MX2015008509A MX2015008509A MX2015008509A MX 2015008509 A MX2015008509 A MX 2015008509A MX 2015008509 A MX2015008509 A MX 2015008509A MX 2015008509 A MX2015008509 A MX 2015008509A MX 2015008509 A MX2015008509 A MX 2015008509A
Authority
MX
Mexico
Prior art keywords
curved
fabricating
composite
prepreg tape
carrier
Prior art date
Application number
MX2015008509A
Other languages
English (en)
Other versions
MX371351B (es
Inventor
Daniel Richard Smith Jr
Andrew E Modin
Edoardo Depase
Donald Chester Darrow
Mark Klewiada
Original Assignee
Boeing Co
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
Priority claimed from US13/736,021 external-priority patent/US9387657B2/en
Application filed by Boeing Co filed Critical Boeing Co
Publication of MX2015008509A publication Critical patent/MX2015008509A/es
Publication of MX371351B publication Critical patent/MX371351B/es

Links

Classifications

    • 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
    • B29C70/28—Shaping operations therefor
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • 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
    • B29C70/28—Shaping operations therefor
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/541—Positioning reinforcements in a mould, e.g. using clamping means for the 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
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping 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
    • 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
    • B29C70/20—Fibrous 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
    • 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
    • B29D99/0003—Producing profiled members, e.g. beams
    • 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
    • B29L2031/001—Profiled members, e.g. beams, sections
    • B29L2031/003—Profiled members, e.g. beams, sections having a profiled transverse cross-section
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/064—Stringers; Longerons
    • 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
    • Y02T50/40—Weight reduction

Abstract

Es proporcionado un método de fabricación de un refuerzo compuesto que tiene un alma curveada y al menos una pestaña curveada. Una longitud sustancialmente recta de cinta unidireccional de prepreg (30) es colocada sobre un portador (32). Al menos la pestaña curveada es formada al utilizar el portador para orientar una primera porción de la cinta sobre una primera superficie de herramienta curveada. El alma curveada es formada al utilizar el portador para formar una segunda porción de la cinta sobre una segunda superficie de herramienta curveada.
MX2015008509A 2013-01-07 2013-11-20 Metodo de fabricacion de estructura compuesta curveada utilizando cinta compuesta de prepeg. MX371351B (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/736,021 US9387657B2 (en) 2010-11-12 2013-01-07 Method of fabricating a curved composite structure using composite prepreg tape
PCT/US2013/070918 WO2014107241A1 (en) 2013-01-07 2013-11-20 Method of fabricating a curved composite structure using composite prepreg tape

Publications (2)

Publication Number Publication Date
MX2015008509A true MX2015008509A (es) 2016-01-20
MX371351B MX371351B (es) 2020-01-27

Family

ID=49684099

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2015008509A MX371351B (es) 2013-01-07 2013-11-20 Metodo de fabricacion de estructura compuesta curveada utilizando cinta compuesta de prepeg.

Country Status (9)

Country Link
EP (1) EP2941345B1 (es)
JP (1) JP6353465B2 (es)
KR (1) KR102143668B1 (es)
CN (1) CN104903081B (es)
BR (1) BR112015013772B1 (es)
CA (1) CA2890761C (es)
MX (1) MX371351B (es)
RU (1) RU2631296C2 (es)
WO (1) WO2014107241A1 (es)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9387657B2 (en) 2010-11-12 2016-07-12 The Boeing Company Method of fabricating a curved composite structure using composite prepreg tape
US9701067B2 (en) 2010-11-12 2017-07-11 The Boeing Company Method of laying up prepreg plies on contoured tools using a deformable carrier film
WO2015053869A1 (en) * 2013-10-07 2015-04-16 The Boeing Company Method of laying up prepreg plies on contoured tools using a deformable carrier film
US10800111B2 (en) * 2015-06-16 2020-10-13 The Boeing Company Composite structure fabrication systems and methods
WO2021200047A1 (ja) * 2020-03-31 2021-10-07 川崎重工業株式会社 航空機部品の中間生成品の製造方法および航空機部品
WO2022058703A1 (en) * 2020-09-17 2022-03-24 Icomat Limited A tape laying head
CN113334764B (zh) * 2021-07-08 2023-07-04 上海交通大学 一种纤维横向铺带3d打印方法

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0773886B2 (ja) * 1986-07-03 1995-08-09 東芝ケミカル株式会社 繊維強化プラスチック積層板からなるスペーサの製造方法
GB8629267D0 (en) * 1986-12-08 1987-02-11 Westland Plc Laying pre-impregnated fibre reinforced material on surface
US4961700A (en) * 1988-12-15 1990-10-09 Owens-Corning Fiberglas Corporation Shaping means for the production of fiber-reinforced preform articles
SU1805605A1 (ru) * 1991-02-25 1996-07-20 Киевский механический завод им.О.К.Антонова Способ формования листовых деталей из композитов с синусоидальными гофрами
JPH11158764A (ja) * 1997-11-27 1999-06-15 Nippon Resibon Corp 強化繊維シート
US8632653B2 (en) * 2005-05-03 2014-01-21 The Boeing Company Method of manufacturing curved composite structural elements
US7943076B1 (en) * 2005-05-03 2011-05-17 The Boeing Company Method of manufacturing curved composite structural elements
DE102005044823B3 (de) * 2005-09-20 2007-05-16 Airbus Gmbh Verfahren und Vorrichtung zum Aufbringen dünner Materiallagen auf eine Reliefform
US7968169B2 (en) * 2007-08-07 2011-06-28 The Boeing Company Compound contoured composite beams and fabrication methods
JP5324788B2 (ja) * 2008-01-09 2013-10-23 有限会社アズモ技研 繊維強化プラスチック、その製造方法、およびその製造キット
JP2009221390A (ja) * 2008-03-18 2009-10-01 Jamco Corp 複合材連続成形用プリプレグピールプライ
US8932423B2 (en) * 2008-04-17 2015-01-13 The Boeing Company Method for producing contoured composite structures and structures produced thereby
US9278484B2 (en) * 2008-04-17 2016-03-08 The Boeing Company Method and apparatus for producing contoured composite structures and structures produced thereby
US8709576B2 (en) 2008-11-21 2014-04-29 Airbus Operations (Sas) Curved structural part made of composite material and a process for manufacturing such a part
US8551380B2 (en) * 2010-11-12 2013-10-08 The Boeing Company Method of laying up prepreg plies on contoured tools using a deformable carrier film

Also Published As

Publication number Publication date
KR20150104085A (ko) 2015-09-14
RU2015117413A (ru) 2017-02-09
KR102143668B1 (ko) 2020-08-12
BR112015013772A2 (pt) 2017-07-11
EP2941345A1 (en) 2015-11-11
EP2941345B1 (en) 2021-10-20
CA2890761C (en) 2017-08-22
BR112015013772B1 (pt) 2021-06-08
WO2014107241A1 (en) 2014-07-10
RU2631296C2 (ru) 2017-09-20
MX371351B (es) 2020-01-27
CN104903081B (zh) 2018-03-13
CA2890761A1 (en) 2014-07-10
JP2016501756A (ja) 2016-01-21
CN104903081A (zh) 2015-09-09
JP6353465B2 (ja) 2018-07-04

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