ATE513678T1 - Auflegen von verbundschichten mit elektronischen identifikationsetiketten - Google Patents

Auflegen von verbundschichten mit elektronischen identifikationsetiketten

Info

Publication number
ATE513678T1
ATE513678T1 AT06254073T AT06254073T ATE513678T1 AT E513678 T1 ATE513678 T1 AT E513678T1 AT 06254073 T AT06254073 T AT 06254073T AT 06254073 T AT06254073 T AT 06254073T AT E513678 T1 ATE513678 T1 AT E513678T1
Authority
AT
Austria
Prior art keywords
composite layers
electronic identification
identification labels
applying composite
plies
Prior art date
Application number
AT06254073T
Other languages
English (en)
Inventor
Craig B Green
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
Application filed by Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of ATE513678T1 publication Critical patent/ATE513678T1/de

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
    • B29C70/543—Fixing the position or configuration of fibrous reinforcements before or during moulding
    • 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
    • B29C70/28—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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Radar Systems Or Details Thereof (AREA)
AT06254073T 2005-08-03 2006-08-03 Auflegen von verbundschichten mit elektronischen identifikationsetiketten ATE513678T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/196,195 US7423523B2 (en) 2005-08-03 2005-08-03 Composite ply layup using electronically identifiable tags

Publications (1)

Publication Number Publication Date
ATE513678T1 true ATE513678T1 (de) 2011-07-15

Family

ID=37428599

Family Applications (1)

Application Number Title Priority Date Filing Date
AT06254073T ATE513678T1 (de) 2005-08-03 2006-08-03 Auflegen von verbundschichten mit elektronischen identifikationsetiketten

Country Status (3)

Country Link
US (1) US7423523B2 (de)
EP (1) EP1749642B1 (de)
AT (1) ATE513678T1 (de)

Families Citing this family (34)

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US8285407B2 (en) * 2007-10-25 2012-10-09 The Boeing Company Method and apparatus for composite part data extraction
US8321180B2 (en) * 2007-10-25 2012-11-27 The Boeing Company Method and apparatus for composite part data extraction
US8442804B2 (en) 2007-10-25 2013-05-14 The Boeing Company Method and apparatus for composite part data extraction
BRPI0922036B1 (pt) * 2008-11-12 2020-01-28 Lm Glasfiber As método de fabricar peças reforçadas por fibra
US20110259511A1 (en) * 2008-11-12 2011-10-27 Lm Glasfiber A/S Method and system for monitoring and controlling the manufacturing of parts for a wind power plant
KR101026017B1 (ko) 2008-11-20 2011-03-30 한국항공우주산업 주식회사 멀티 레이업이 적용된 자동 테이프 레이어 시스템
US8620627B2 (en) * 2009-10-13 2013-12-31 The Boeing Company Composite information display for a part
WO2011047167A1 (en) * 2009-10-16 2011-04-21 Gerber Scientific International, Inc. Methods and systems for manufacturing composite parts
US9522512B2 (en) 2010-08-17 2016-12-20 The Boeing Company Methods for making composite structures having composite-to-metal joints
US8993084B2 (en) 2010-08-17 2015-03-31 The Boeing Company Multi-layer metallic structure and composite-to-metal joint methods
US8652606B2 (en) 2010-08-17 2014-02-18 The Boeing Company Composite structures having composite-to-metal joints and method for making the same
US9111665B2 (en) 2010-12-31 2015-08-18 Eaton Corporation Conductive mesh for composite tube for fluid delivery system
US9366365B2 (en) 2010-12-31 2016-06-14 Eaton Corporation Reinforcement methods for composite tube for fluid delivery system
US9470352B2 (en) 2010-12-31 2016-10-18 Eaton Corporation RFID and product labelling integrated in knit composite tubes for fluid delivery system
US9545757B1 (en) 2012-02-08 2017-01-17 Textron Innovations, Inc. Composite lay up and method of forming
US9162436B2 (en) * 2013-01-04 2015-10-20 The Boeing Company Method and apparatus for accurate registration of composite laminates
WO2014204765A1 (en) * 2013-06-20 2014-12-24 Eaton Corporation Rfid and product labeling integrated in knit composite tubes for fluid delivery system
DE102013107214B4 (de) * 2013-07-09 2016-05-19 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren und Anlage zur Überwachung eines Autoklaven-Fertigungsprozesses
EP3057805A4 (de) * 2013-10-14 2017-07-12 United Technologies Corporation Automatisierte herstellung einer feststofflage eines laminatverbunds
JP6372195B2 (ja) * 2014-06-30 2018-08-15 東レ株式会社 プリフォームの製造方法及び繊維強化プラスチックの製造方法
DE102014111118B4 (de) * 2014-08-05 2017-07-13 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren zur Herstellung eines Faserverbundbauteils, Verfahren zum Verifizieren eines Faserverbundbauteils sowie Referenzelement
DE102014216136A1 (de) * 2014-08-13 2016-02-18 Bayerische Motoren Werke Aktiengesellschaft Verfahren für die Bestimmung eines Kernabschnitts eines Zuschnitts aus Faserverbundmaterial
CN105666893A (zh) * 2014-11-17 2016-06-15 昌河飞机工业（集团）有限责任公司 一种预浸料裁片铺贴定位方法
US10062202B2 (en) * 2014-12-22 2018-08-28 General Electric Company System and methods of generating a computer model of a composite component
US10005267B1 (en) 2015-09-22 2018-06-26 Textron Innovations, Inc. Formation of complex composite structures using laminate templates
CN106042413B (zh) * 2016-07-28 2018-04-24 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种面向手工铺贴过程控制的系统及其铺贴方法
CN108973160B (zh) * 2017-06-05 2021-10-12 中国商用飞机有限责任公司 一种复合材料热隔膜预成型的预浸料定位方法
JP7312753B2 (ja) 2017-12-29 2023-07-21 ティーピーアイ コンポジッツ，インコーポレーティッド レーザ投影システムを用いた風力タービンブレードの製作のための半自動レイアッププロセス
US11806948B2 (en) 2019-12-12 2023-11-07 The Boeing Company Method of forming flyaway stringer end caps
US11718047B2 (en) 2019-12-12 2023-08-08 The Boeing Company Flyaway stringer end caps
US20210252817A1 (en) * 2020-02-18 2021-08-19 The Boeing Company Methods for fabricating solid laminate stringers on a composite panel
EP3928965A1 (de) * 2020-06-25 2021-12-29 Siemens Gamesa Renewable Energy A/S Verfahren zur herstellung eines elements in einem giessverfahren auf harzinfusionsbasis und windturbinenschaufel
AT523962B1 (de) * 2020-07-08 2023-05-15 Gfm Gmbh Verfahren zum Bereitstellen von Zuschnitten aus einer Faserbahn
US20230113580A1 (en) * 2021-10-13 2023-04-13 The Boeing Company Printed fiducial system for accurate pick and place

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6212762B1 (en) * 1999-09-30 2001-04-10 David F. Lucier Lumber tagger
US6693512B1 (en) * 2000-07-17 2004-02-17 Armstrong World Industries, Inc. Device location and identification system
US6703935B1 (en) * 2001-05-14 2004-03-09 Amerasia International Technology, Inc. Antenna arrangement for RFID smart tags
US6829520B1 (en) 2003-06-03 2004-12-07 The Boeing Company Time-and-temperature sensitive material tracking
US6963282B1 (en) * 2003-12-05 2005-11-08 Microsoft Corporation Wireless self-describing buildings
US20060108056A1 (en) * 2004-11-24 2006-05-25 The Boeing Company Method and apparatus for foreign object detection in a composite layer fabrication process

Also Published As

Publication number Publication date
EP1749642A2 (de) 2007-02-07
US7423523B2 (en) 2008-09-09
EP1749642A3 (de) 2009-03-18
EP1749642B1 (de) 2011-06-22
US20070236354A1 (en) 2007-10-11

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