DE69715959T2 - Doppelzweckauflegewerkzeug - Google Patents

Doppelzweckauflegewerkzeug

Info

Publication number
DE69715959T2
DE69715959T2 DE69715959T DE69715959T DE69715959T2 DE 69715959 T2 DE69715959 T2 DE 69715959T2 DE 69715959 T DE69715959 T DE 69715959T DE 69715959 T DE69715959 T DE 69715959T DE 69715959 T2 DE69715959 T2 DE 69715959T2
Authority
DE
Germany
Prior art keywords
doppelzweckauflegewerkzeug
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Lifetime
Application number
DE69715959T
Other languages
English (en)
Other versions
DE69715959D1 (de
Inventor
Dwight L Engwall
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Spirit AeroSystems Inc
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
Publication of DE69715959D1 publication Critical patent/DE69715959D1/de
Application granted granted Critical
Publication of DE69715959T2 publication Critical patent/DE69715959T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
    • B23Q3/00—Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine
    • B23Q3/02—Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine for mounting on a work-table, tool-slide, or analogous part
    • B23Q3/06—Work-clamping means
    • B23Q3/08—Work-clamping means other than mechanically-actuated
    • B23Q3/086—Work-clamping means other than mechanically-actuated using a solidifying liquid, e.g. with freezing, setting or hardening means
    • 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
    • B29C70/305—Spray-up of reinforcing fibres with or without matrix to form a non-coherent mat in or on a mould
    • 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
    • B29C70/545—Perforating, cutting or machining during or after moulding
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T409/00—Gear cutting, milling, or planing
    • Y10T409/30—Milling
    • Y10T409/303752—Process
    • Y10T409/303808—Process including infeeding
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T409/00—Gear cutting, milling, or planing
    • Y10T409/30—Milling
    • Y10T409/304144—Means to trim edge
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T409/00—Gear cutting, milling, or planing
    • Y10T409/30—Milling
    • Y10T409/306664—Milling including means to infeed rotary cutter toward work
    • Y10T409/307448—Milling including means to infeed rotary cutter toward work with work holder
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T409/00—Gear cutting, milling, or planing
    • Y10T409/30—Milling
    • Y10T409/30868—Work support

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Laminated Bodies (AREA)
  • Milling Processes (AREA)
DE69715959T 1996-04-08 1997-04-08 Doppelzweckauflegewerkzeug Expired - Lifetime DE69715959T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/629,120 US5746553A (en) 1996-04-08 1996-04-08 Dual purpose lay-up tool

Publications (2)

Publication Number Publication Date
DE69715959D1 DE69715959D1 (de) 2002-11-07
DE69715959T2 true DE69715959T2 (de) 2003-01-30

Family

ID=24521661

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69715959T Expired - Lifetime DE69715959T2 (de) 1996-04-08 1997-04-08 Doppelzweckauflegewerkzeug

Country Status (6)

Country Link
US (1) US5746553A (de)
EP (1) EP0807504B1 (de)
KR (1) KR100469876B1 (de)
CN (1) CN1098152C (de)
CA (1) CA2201981C (de)
DE (1) DE69715959T2 (de)

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US7874936B2 (en) * 2007-12-19 2011-01-25 Taylor Made Golf Company, Inc. Composite articles and methods for making the same
US7236625B2 (en) * 2003-07-28 2007-06-26 The Boeing Company Systems and method for identifying foreign objects and debris (FOD) and defects during fabrication of a composite structure
US7080441B2 (en) * 2003-07-28 2006-07-25 The Boeing Company Composite fuselage machine and method of automated composite lay up
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US7228611B2 (en) * 2003-11-18 2007-06-12 The Boeing Company Method of transferring large uncured composite laminates
US8934702B2 (en) * 2003-12-02 2015-01-13 The Boeing Company System and method for determining cumulative tow gap width
US7289656B2 (en) 2003-12-02 2007-10-30 The Boeing Company Systems and methods for determining inconsistency characteristics of a composite structure
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US7159822B2 (en) * 2004-04-06 2007-01-09 The Boeing Company Structural panels for use in aircraft fuselages and other structures
US7527222B2 (en) * 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
US7193696B2 (en) * 2004-04-12 2007-03-20 United Technologies Corporation Systems and methods for using light to indicate defect locations on a composite structure
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US7503368B2 (en) 2004-11-24 2009-03-17 The Boeing Company Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections
US7424902B2 (en) 2004-11-24 2008-09-16 The Boeing Company In-process vision detection of flaw and FOD characteristics
US20060108048A1 (en) 2004-11-24 2006-05-25 The Boeing Company In-process vision detection of flaws and fod by back field illumination
US20060118244A1 (en) * 2004-12-02 2006-06-08 The Boeing Company Device for laying tape materials for aerospace applications
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US7889907B2 (en) * 2005-01-12 2011-02-15 The Boeing Company Apparatus and methods for inspecting tape lamination
US7278198B2 (en) * 2005-02-01 2007-10-09 The Boeing Company Mandrel segment loader
US7748119B2 (en) * 2005-06-03 2010-07-06 The Boeing Company Method for manufacturing composite components
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US7372556B2 (en) * 2005-10-31 2008-05-13 The Boeing Company Apparatus and methods for inspecting a composite structure for inconsistencies
US7435947B2 (en) * 2005-10-31 2008-10-14 The Boeing Company Apparatus and methods for integrating encoding functions in material placement machines
US7398586B2 (en) * 2005-11-01 2008-07-15 The Boeing Company Methods and systems for manufacturing a family of aircraft wings and other composite structures
DE102006021110B4 (de) * 2006-05-05 2011-04-21 Airbus Operations Gmbh Vorrichtung und Verfahren zum Herstellen eines großflächigen Faserverbund-Strukturbauteils
DE102006050432B4 (de) * 2006-08-11 2010-10-07 MV Marketing und Vertriebs-GmbH & Co. KG Wieländer + Schill Bohrvorrichtung
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US9579856B2 (en) 2007-05-11 2017-02-28 The Boeing Company Methods and apparatus for molding and joining composite parts
US8337654B2 (en) 2007-05-11 2012-12-25 The Boeing Company Configurable tooling and molding method using the same
US8388795B2 (en) * 2007-05-17 2013-03-05 The Boeing Company Nanotube-enhanced interlayers for composite structures
US20090035412A1 (en) * 2007-07-31 2009-02-05 Sobcinski Thomas J Hybrid lay-up tool
US7968021B2 (en) * 2007-07-31 2011-06-28 The Boeing Company Coefficient of thermal expansion control structure
US8042767B2 (en) * 2007-09-04 2011-10-25 The Boeing Company Composite fabric with rigid member structure
US8196452B2 (en) * 2008-03-27 2012-06-12 The Boeing Company Collection of process data using in-situ sensors
DE102008028076A1 (de) * 2008-06-13 2009-12-17 Claas Fertigungstechnik Gmbh Werkzeug, sowie Verfahren zum Herstellen eines Werkzeugs, insbesondere zur Herstellung faserverstärkter Bauteile
US8298473B2 (en) * 2009-05-15 2012-10-30 The Boeing Company Method of making a cure tool with integrated edge breather
US8961732B2 (en) 2011-01-03 2015-02-24 The Boeing Company Method and device for compressing a composite radius
US8460502B2 (en) 2011-04-14 2013-06-11 Spirit Aerosystems, Inc. Method and tooling for manufacture of co-cured composite structures
DE102011079928A1 (de) * 2011-07-27 2013-01-31 Airbus Operations Gmbh Vorrichtung zur Herstellung eines Klebebauteils mit Faserverbundkunststoffen sowie Verfahren
FR2991628A1 (fr) * 2012-06-12 2013-12-13 Aircelle Sa Ensemble d'outillage pour la fabrication d'une piece composite et procede de fabrication d'une piece composite.
EP2796373B1 (de) * 2013-04-25 2015-12-09 Airbus Operations GmbH Anordnungseinspannung zum Montieren von Plattenstrukturelementen auf einer Oberfläche einer CFRP-Platte
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US9902091B2 (en) * 2015-04-21 2018-02-27 Rohr, Inc. Composite bonding tool with high thermal conductivity and low coefficient of thermal expansion
US10513324B2 (en) * 2016-02-08 2019-12-24 Bell Helicopter Textron Inc. Composite rib assembly
US10639854B2 (en) 2016-02-08 2020-05-05 Bell Helicopter Textron Inc. Composite wing structure and methods of manufacture
CN105773991A (zh) * 2016-03-25 2016-07-20 哈尔滨飞机工业集团有限责任公司 一种小曲率蜂窝结构机翼蒙皮的胶接成型装置及方法
KR102473358B1 (ko) * 2017-03-16 2022-12-06 더 보잉 컴파니 경화된 복합재 부품을 정의하기 위해 제1 열경화성 복합재와 제2 열경화성 복합재를 일체접합하는 방법
US11701801B2 (en) * 2019-03-04 2023-07-18 The Boeing Company Caul plate with feature for separating from composite part
CN111069697B (zh) * 2019-12-26 2021-04-30 济南北方金锋锯业有限公司 一种立式锯床
CN111958886B (zh) * 2020-07-15 2022-06-07 天津爱思达航天科技有限公司 通用式、高成品率的炭泡沫复合材料模具及制备方法
CN112571835B (zh) * 2020-10-30 2022-09-27 航天材料及工艺研究所 一种适应于自动倾斜铺放的高效示教编程工艺方法
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Also Published As

Publication number Publication date
KR970069310A (ko) 1997-11-07
US5746553A (en) 1998-05-05
EP0807504B1 (de) 2002-10-02
EP0807504A1 (de) 1997-11-19
KR100469876B1 (ko) 2005-03-16
CN1168317A (zh) 1997-12-24
DE69715959D1 (de) 2002-11-07
CN1098152C (zh) 2003-01-08
CA2201981A1 (en) 1997-10-08
CA2201981C (en) 2005-11-29

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: SPIRIT AEROSYSTEMS,INC. (N.D.GES.D.STAATES DEL, US