CN102431182A - 铺设筒形复合结构的方法和器械 - Google Patents

铺设筒形复合结构的方法和器械 Download PDF

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Publication number
CN102431182A
CN102431182A CN2011102820779A CN201110282077A CN102431182A CN 102431182 A CN102431182 A CN 102431182A CN 2011102820779 A CN2011102820779 A CN 2011102820779A CN 201110282077 A CN201110282077 A CN 201110282077A CN 102431182 A CN102431182 A CN 102431182A
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CN
China
Prior art keywords
mould
executor
manipulator
composite
oml
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.)
Pending
Application number
CN2011102820779A
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English (en)
Chinese (zh)
Inventor
P·J·克劳泽斯
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.)
Boeing Co
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
Priority to CN201711048190.4A priority Critical patent/CN107791538A/zh
Publication of CN102431182A publication Critical patent/CN102431182A/zh
Pending legal-status Critical Current

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    • 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
    • B29C70/30—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
    • B29C70/32—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 on a rotating mould, former or core
    • B29C70/323—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 on a rotating mould, former or core on the inner surface of a rotating 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
    • B29C70/30—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
    • B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • 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
    • B29L2031/3076—Aircrafts
    • B29L2031/3082—Fuselages
    • 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

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Robotics (AREA)
  • Moulding By Coating Moulds (AREA)
CN2011102820779A 2010-09-29 2011-09-16 铺设筒形复合结构的方法和器械 Pending CN102431182A (zh)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711048190.4A CN107791538A (zh) 2010-09-29 2011-09-16 铺设筒形复合结构的方法和器械

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/893,050 US20120073738A1 (en) 2010-09-29 2010-09-29 Method and apparatus for laying up barrel-shaped composite structures
US12/893,050 2010-09-29

Related Child Applications (1)

Application Number Title Priority Date Filing Date
CN201711048190.4A Division CN107791538A (zh) 2010-09-29 2011-09-16 铺设筒形复合结构的方法和器械

Publications (1)

Publication Number Publication Date
CN102431182A true CN102431182A (zh) 2012-05-02

Family

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Family Applications (2)

Application Number Title Priority Date Filing Date
CN2011102820779A Pending CN102431182A (zh) 2010-09-29 2011-09-16 铺设筒形复合结构的方法和器械
CN201711048190.4A Pending CN107791538A (zh) 2010-09-29 2011-09-16 铺设筒形复合结构的方法和器械

Family Applications After (1)

Application Number Title Priority Date Filing Date
CN201711048190.4A Pending CN107791538A (zh) 2010-09-29 2011-09-16 铺设筒形复合结构的方法和器械

Country Status (7)

Country Link
US (1) US20120073738A1 (enExample)
EP (1) EP2436511B1 (enExample)
JP (1) JP2012071824A (enExample)
CN (2) CN102431182A (enExample)
CA (1) CA2753615C (enExample)
ES (1) ES2621791T3 (enExample)
PT (1) PT2436511T (enExample)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104669637A (zh) * 2013-12-02 2015-06-03 昌河飞机工业（集团）有限责任公司 一种复合材料筒形件的铺贴成型方法
CN105189094A (zh) * 2013-04-19 2015-12-23 波音公司 在波状外形芯轴表面上压实未固化复合构件
US9931807B2 (en) 2011-08-08 2018-04-03 The Boeing Company Flexible compactor with reinforcing spine
CN110509575A (zh) * 2019-08-28 2019-11-29 湖北三江航天江北机械工程有限公司 碳纤维复合材料壳体精密弹翼座铺设缠绕成型方法
US10569484B2 (en) 2011-08-08 2020-02-25 The Boeing Company Device for transporting, placing and compacting composite stiffeners
CN114043749A (zh) * 2021-11-12 2022-02-15 中航西安飞机工业集团股份有限公司 一种复合材料旋转铺丝装置及使用方法
CN115214870A (zh) * 2021-04-16 2022-10-21 空中客车西班牙有限责任公司 制造复合件的装置和方法以及通过其制造的飞行器隔板

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9481158B2 (en) * 2013-07-11 2016-11-01 The Boeing Company Short course fiber placement head
CN104669650A (zh) * 2013-12-02 2015-06-03 昌河飞机工业（集团）有限责任公司 一种多束数、多定位大梁带的分块铺贴成型模具及方法
US10414042B2 (en) * 2015-02-26 2019-09-17 Khalifa University of Science and Technology Parallel mechanism based automated fiber placement system
US10926490B2 (en) * 2018-04-09 2021-02-23 The Boeing Company Composite laminate forming apparatus and method therefor
US11135783B2 (en) 2018-09-26 2021-10-05 The Boeing Company System and method for manufacturing composite structures
US11135784B2 (en) 2018-09-26 2021-10-05 The Boeing Company System and method for manufacturing composite structures
WO2022044324A1 (ja) * 2020-08-31 2022-03-03 株式会社Ｉｈｉエアロスペース Ｆｒｐ成形システムと方法
US11724467B2 (en) 2020-12-18 2023-08-15 The Boeing Company System and method for laying up composite barrel shaped structures
CN114311744B (zh) * 2021-12-22 2023-09-01 西安鑫垚陶瓷复合材料有限公司 曲面窄腔回转体模具及其制备曲面窄腔回转体零件的方法

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US20050023414A1 (en) * 2003-07-28 2005-02-03 The Boeing Company Composite fuselage machine
US20050172750A1 (en) * 2002-02-06 2005-08-11 Abb Ab Industrial robot
US20060108058A1 (en) * 2004-11-24 2006-05-25 Chapman Michael R Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections

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US4699683A (en) 1986-02-07 1987-10-13 The Boeing Company Multiroving fiber laminator
CA2057201C (en) * 1990-12-19 1998-05-19 Vernon M. Benson Multiple axes fiber placement machine
CA2277846A1 (en) 1997-01-14 1998-07-16 Asea Brown Boveri Ab A device for relative displacement of two elements
SE512931C2 (sv) 1998-04-29 2000-06-05 Abb Ab Anordning för relativ förflyttning av två element
SE517356C2 (sv) 2000-09-11 2002-05-28 Abb Ab Manipulator innefattande minst tre armar för förflyttning av en kropp i rymden
SE0100134D0 (sv) 2001-01-15 2001-01-15 Abb Ab Industrirobot
SE0201848D0 (sv) 2002-06-14 2002-06-14 Abb Ab Anordning vid industrirobot
WO2004056538A1 (en) 2002-12-20 2004-07-08 Abb Ab A parallel kinematic manipulator and a method of operating the same, including pairwise actuators
US7083698B2 (en) * 2003-08-22 2006-08-01 The Boeing Company Automated composite lay-up to an internal fuselage mandrel
US7681615B2 (en) 2005-08-04 2010-03-23 The Boeing Company Tow width adaptable placement head device and method
US20070211817A1 (en) * 2006-03-13 2007-09-13 Ren An Information Technology Co., Ltd. Computer numerical control wireless transmission System
FR2912680B1 (fr) * 2007-02-21 2009-04-24 Coriolis Composites Sa Procede et dispositif de fabrication de pieces en materiau composite, en particulier de troncons de fuselage d'avion
US8557074B2 (en) 2008-02-27 2013-10-15 The Boeing Company Reduced complexity automatic fiber placement apparatus and method
US20100200168A1 (en) * 2009-02-06 2010-08-12 Ingersoll Machine Tools, Inc. Fiber delivery apparatus and system having a creel and fiber placement head sans fiber redirect
US8308101B2 (en) 2009-03-09 2012-11-13 The Boeing Company Simplified fiber tensioning for automated fiber placement machines
US8454788B2 (en) 2009-03-13 2013-06-04 The Boeing Company Method and apparatus for placing short courses of composite tape

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US20050172750A1 (en) * 2002-02-06 2005-08-11 Abb Ab Industrial robot
US20050023414A1 (en) * 2003-07-28 2005-02-03 The Boeing Company Composite fuselage machine
US20060108058A1 (en) * 2004-11-24 2006-05-25 Chapman Michael R Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9931807B2 (en) 2011-08-08 2018-04-03 The Boeing Company Flexible compactor with reinforcing spine
US10195811B2 (en) 2011-08-08 2019-02-05 The Boeing Company Flexible compactor with reinforcing spine
US10569484B2 (en) 2011-08-08 2020-02-25 The Boeing Company Device for transporting, placing and compacting composite stiffeners
CN105189094A (zh) * 2013-04-19 2015-12-23 波音公司 在波状外形芯轴表面上压实未固化复合构件
US10315750B2 (en) 2013-04-19 2019-06-11 The Boeing Company Compacting uncured composite members on contoured mandrel surfaces
CN104669637A (zh) * 2013-12-02 2015-06-03 昌河飞机工业（集团）有限责任公司 一种复合材料筒形件的铺贴成型方法
CN110509575A (zh) * 2019-08-28 2019-11-29 湖北三江航天江北机械工程有限公司 碳纤维复合材料壳体精密弹翼座铺设缠绕成型方法
CN115214870A (zh) * 2021-04-16 2022-10-21 空中客车西班牙有限责任公司 制造复合件的装置和方法以及通过其制造的飞行器隔板
CN114043749A (zh) * 2021-11-12 2022-02-15 中航西安飞机工业集团股份有限公司 一种复合材料旋转铺丝装置及使用方法

Also Published As

Publication number Publication date
JP2012071824A (ja) 2012-04-12
CA2753615C (en) 2018-10-16
CA2753615A1 (en) 2012-03-29
ES2621791T3 (es) 2017-07-05
PT2436511T (pt) 2017-04-05
EP2436511B1 (en) 2017-03-22
US20120073738A1 (en) 2012-03-29
CN107791538A (zh) 2018-03-13
EP2436511A1 (en) 2012-04-04

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Application publication date: 20120502