BR102016005933B1 - Sistema configurado para fabricação de uma parte compósita, e, método para formação de uma parte compósita - Google Patents

Sistema configurado para fabricação de uma parte compósita, e, método para formação de uma parte compósita Download PDF

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Publication number
BR102016005933B1
BR102016005933B1 BR102016005933-0A BR102016005933A BR102016005933B1 BR 102016005933 B1 BR102016005933 B1 BR 102016005933B1 BR 102016005933 A BR102016005933 A BR 102016005933A BR 102016005933 B1 BR102016005933 B1 BR 102016005933B1
Authority
BR
Brazil
Prior art keywords
tool
composite material
flange
composite
material receiving
Prior art date
Application number
BR102016005933-0A
Other languages
English (en)
Portuguese (pt)
Other versions
BR102016005933A2 (pt
Inventor
Michael P. Thompson
Otis Franklin Layton
Original Assignee
The Boeing Company
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 The Boeing Company filed Critical The Boeing Company
Publication of BR102016005933A2 publication Critical patent/BR102016005933A2/pt
Publication of BR102016005933B1 publication Critical patent/BR102016005933B1/pt

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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
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • B29C70/443—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding and impregnating by vacuum or injection
    • 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
    • B29C70/549—Details of caul plates, e.g. materials or shape
    • 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
    • B29C70/34—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 and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
    • B29C70/342—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 and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using isostatic pressure
    • 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
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • B29C70/446—Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
    • 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
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • 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
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)
BR102016005933-0A 2015-04-22 2016-03-17 Sistema configurado para fabricação de uma parte compósita, e, método para formação de uma parte compósita BR102016005933B1 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US14/693,363 US9895848B2 (en) 2015-04-22 2015-04-22 Systems and tooling for manufacturing composite parts and related methods
US14/693,363 2015-04-22

Publications (2)

Publication Number Publication Date
BR102016005933A2 BR102016005933A2 (pt) 2016-11-29
BR102016005933B1 true BR102016005933B1 (pt) 2021-06-01

Family

ID=57147285

Family Applications (1)

Application Number Title Priority Date Filing Date
BR102016005933-0A BR102016005933B1 (pt) 2015-04-22 2016-03-17 Sistema configurado para fabricação de uma parte compósita, e, método para formação de uma parte compósita

Country Status (5)

Country Link
US (1) US9895848B2 (enExample)
JP (1) JP6807654B2 (enExample)
CN (1) CN106064485B (enExample)
AU (1) AU2016200777B2 (enExample)
BR (1) BR102016005933B1 (enExample)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SG10202108219QA (en) 2017-01-27 2021-08-30 A Clip Institute Co Prophylactic and/or therapeutic agent of infectious disease or inflammatory disease
US10654208B2 (en) * 2017-09-20 2020-05-19 Bell Helicopter Textron Inc. Assembly fixture with anisotropic thermal properties
JP2022080870A (ja) * 2020-11-18 2022-05-30 ザ・ボーイング・カンパニー 複合構造を処理するための装置及び方法

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4406422A (en) * 1981-08-27 1983-09-27 Jonathan Temple & Co., Inc. Spool assembly
JPH0517296U (ja) * 1991-08-21 1993-03-05 積水化学工業株式会社 管継手
JP2585008Y2 (ja) * 1991-10-29 1998-11-11 積水化学工業株式会社 管継手
FR2691922B1 (fr) * 1992-06-03 1994-07-22 Snecma Procede et dispositif de moulage de piece en materiau composite constituee de deux secteurs.
TW298574B (enExample) * 1994-03-08 1997-02-21 Syfal Srl
US5876540A (en) * 1996-05-31 1999-03-02 The Boeing Company Joining composites using Z-pinned precured strips
US7534387B2 (en) 2004-02-25 2009-05-19 The Boeing Company Apparatus and methods for processing composite components using an elastomeric caul
US7335012B2 (en) * 2004-12-22 2008-02-26 General Electric Company Apparatus for fabricating reinforced composite materials
US8449709B2 (en) * 2007-05-25 2013-05-28 The Boeing Company Method of fabricating fiber reinforced composite structure having stepped surface
US8951375B2 (en) * 2010-11-11 2015-02-10 Spirit Aerosystems, Inc. Methods and systems for co-bonding or co-curing composite parts using a rigid/malleable SMP apparatus
US9120276B2 (en) * 2012-07-25 2015-09-01 The Boeing Company Laminated composite bending and stiffening members with reinforcement by inter-laminar metal sheets
US9259865B2 (en) * 2013-03-17 2016-02-16 The Boeing Company Seal molding system and method

Also Published As

Publication number Publication date
US20160311176A1 (en) 2016-10-27
CN106064485A (zh) 2016-11-02
AU2016200777B2 (en) 2021-01-21
US9895848B2 (en) 2018-02-20
JP2017013486A (ja) 2017-01-19
BR102016005933A2 (pt) 2016-11-29
CN106064485B (zh) 2020-01-31
AU2016200777A1 (en) 2016-11-10
JP6807654B2 (ja) 2021-01-06

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Legal Events

Date Code Title Description
B03A Publication of a patent application or of a certificate of addition of invention [chapter 3.1 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 17/03/2016, OBSERVADAS AS CONDICOES LEGAIS.