JP2010527303A - ハイブリッド複合パネルシステム及び方法 - Google Patents

ハイブリッド複合パネルシステム及び方法 Download PDF

Info

Publication number
JP2010527303A
JP2010527303A JP2010508503A JP2010508503A JP2010527303A JP 2010527303 A JP2010527303 A JP 2010527303A JP 2010508503 A JP2010508503 A JP 2010508503A JP 2010508503 A JP2010508503 A JP 2010508503A JP 2010527303 A JP2010527303 A JP 2010527303A
Authority
JP
Japan
Prior art keywords
forming
composite
composite layers
assembly
reinforcing
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
JP2010508503A
Other languages
English (en)
Japanese (ja)
Other versions
JP2010527303A5 (enExample
Inventor
ジェームス， エフ． アッカーマン，
グレゴリー， アール． グリーソン，
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
Publication of JP2010527303A publication Critical patent/JP2010527303A/ja
Publication of JP2010527303A5 publication Critical patent/JP2010527303A5/ja
Pending legal-status Critical Current

Links

Images

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
    • B29C70/06—Fibrous reinforcements only
    • B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
    • B29C70/088—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers and with one or more layers of non-plastics material or non-specified material, e.g. supports
    • 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
    • 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
    • B29C70/22—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
    • 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
    • B29C70/386—Automated tape laying [ATL]
    • 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
    • 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
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Reinforced Plastic Materials (AREA)
JP2010508503A 2007-05-11 2008-05-07 ハイブリッド複合パネルシステム及び方法 Pending JP2010527303A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/747,760 US20080277531A1 (en) 2007-05-11 2007-05-11 Hybrid Composite Panel Systems and Methods
PCT/US2008/062951 WO2009023312A2 (en) 2007-05-11 2008-05-07 Hybrid composite panel systems and methods

Publications (2)

Publication Number Publication Date
JP2010527303A true JP2010527303A (ja) 2010-08-12
JP2010527303A5 JP2010527303A5 (enExample) 2011-06-16

Family

ID=39968656

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2010508503A Pending JP2010527303A (ja) 2007-05-11 2008-05-07 ハイブリッド複合パネルシステム及び方法

Country Status (5)

Country Link
US (1) US20080277531A1 (enExample)
EP (1) EP2170592A2 (enExample)
JP (1) JP2010527303A (enExample)
CN (1) CN101652240B (enExample)
WO (1) WO2009023312A2 (enExample)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105073370A (zh) * 2013-01-18 2015-11-18 三菱重工业株式会社 复合材料的制造方法
JP7606382B2 (ja) 2021-03-26 2024-12-25 株式会社Subaru 複合材構造およびその製造方法

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9586699B1 (en) 1999-08-16 2017-03-07 Smart Drilling And Completion, Inc. Methods and apparatus for monitoring and fixing holes in composite aircraft
US9625361B1 (en) 2001-08-19 2017-04-18 Smart Drilling And Completion, Inc. Methods and apparatus to prevent failures of fiber-reinforced composite materials under compressive stresses caused by fluids and gases invading microfractures in the materials
US9238335B2 (en) * 2008-07-10 2016-01-19 The Boeing Company Mandrel for autoclave curing applications
US9327467B2 (en) * 2008-07-10 2016-05-03 The Boeing Company Composite mandrel for autoclave curing applications
US20100116938A1 (en) * 2008-11-13 2010-05-13 Kline William T Method and apparatus for joining composite structural members and structural members made thereby
US9669579B2 (en) 2008-11-13 2017-06-06 The Boeing Company Aircraft skin attachment system
FR2964339B1 (fr) * 2010-09-06 2014-01-31 Messier Dowty Sa Procede de fabrication de pieces en materiaux composites, avec revetement tresse
GB201115080D0 (en) 2011-09-01 2011-10-19 Airbus Operations Ltd An aircraft structure
US9415858B2 (en) 2012-08-28 2016-08-16 The Boeing Company Bonded and tailorable composite assembly
US8851422B2 (en) 2012-08-28 2014-10-07 The Boeing Company Bonded composite aircraft wing
US9333713B2 (en) 2012-10-04 2016-05-10 The Boeing Company Method for co-curing composite skins and stiffeners in an autoclave
US11123948B2 (en) 2018-11-13 2021-09-21 Epic Aircraft, LLC Method for forming a composite structure

Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6384932A (ja) * 1986-09-22 1988-04-15 旭化成株式会社 積層パネル
JPH0647850A (ja) * 1992-07-29 1994-02-22 Kawasaki Heavy Ind Ltd ハニカムサンドイッチ構造
JPH08300526A (ja) * 1995-05-01 1996-11-19 Toray Ind Inc 輸送機器用部材
JPH08300538A (ja) * 1995-05-02 1996-11-19 Nordam Group Inc 多層の非対称接合サンドイッチ・パネル
JPH0910871A (ja) * 1995-06-28 1997-01-14 Sankyo Manitetsuku:Kk 中空構造材及びハニカム構造材
JPH10128860A (ja) * 1996-10-30 1998-05-19 Honda Motor Co Ltd 繊維強化プラスチック成形品の製造方法
JPH10273042A (ja) * 1997-03-31 1998-10-13 Kawasaki Heavy Ind Ltd 高速車両の先頭部の耐鳥衝突構造
JP2000043796A (ja) * 1998-07-30 2000-02-15 Japan Aircraft Development Corp 複合材の翼形構造およびその成形方法
WO2002074469A2 (en) * 2000-12-08 2002-09-26 Toyota Motor Sales Usa Inc. A molded composite structure and method of forming same
JP2004017370A (ja) * 2002-06-13 2004-01-22 Kawasaki Heavy Ind Ltd 航空機用複合材パネルの製造方法及びその装置
JP2006502046A (ja) * 2002-10-11 2006-01-19 ザ・ボーイング・カンパニー 複合航空機パネルの避雷および接地手段
JP2010507530A (ja) * 2006-10-26 2010-03-11 ザ・ボーイング・カンパニー 翼パネル構造

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3379945D1 (en) * 1983-09-29 1989-07-06 Boeing Co High strength to weight horizontal and vertical aircraft stabilizer
US4539253A (en) * 1984-03-30 1985-09-03 American Cyanamid Co. High impact strength fiber resin matrix composites
US5102604A (en) * 1990-05-17 1992-04-07 The B.F. Goodrich Company Method for curing fiber reinforced thermosetts or thermoplastics
ES2124550T3 (es) * 1995-01-27 1999-02-01 Sikorsky Aircraft Corp Procedimiento para construir articulos de material compuesto con nucleo en forma de panal.
US5604010A (en) * 1996-01-11 1997-02-18 Hartz; Dale E. Composite honeycomb sandwich structure
EP0853039B1 (de) * 1997-01-10 2003-04-23 Airbus Deutschland GmbH Vorrichtung zum Transport und Befestigen von Frachtcontainern oder Sitzpaletten in einem Flugzeug
US6107976A (en) * 1999-03-25 2000-08-22 Bradley B. Teel Hybrid core sandwich radome
US6703104B1 (en) * 2002-01-04 2004-03-09 Murray L. Neal Panel configuration composite armor
US6799619B2 (en) * 2002-02-06 2004-10-05 The Boeing Company Composite material collation machine and associated method for high rate collation of composite materials
EP1529865B1 (en) * 2002-08-12 2009-01-28 Shikibo Ltd. Preform precursor for fiber-reinforced composite material, preform for fiber-reinforced composite material, and method of manufacturing the precursor and the preform
US6871684B2 (en) * 2002-08-13 2005-03-29 The Boeing Company System for identifying defects in a composite structure
ATE353042T1 (de) * 2003-10-14 2007-02-15 Saab Ab Verfahren zur herstellung einer verbundstruktur
US8052831B2 (en) * 2005-02-02 2011-11-08 The Boeing Company Low temperature, vacuum cure fabrication process for large, honeycomb core stiffened composite structures
US7740932B2 (en) * 2005-03-31 2010-06-22 The Boeing Company Hybrid fiberglass composite structures and methods of forming the same
US7748119B2 (en) * 2005-06-03 2010-07-06 The Boeing Company Method for manufacturing composite components

Patent Citations (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6384932A (ja) * 1986-09-22 1988-04-15 旭化成株式会社 積層パネル
JPH0647850A (ja) * 1992-07-29 1994-02-22 Kawasaki Heavy Ind Ltd ハニカムサンドイッチ構造
JPH08300526A (ja) * 1995-05-01 1996-11-19 Toray Ind Inc 輸送機器用部材
JPH08300538A (ja) * 1995-05-02 1996-11-19 Nordam Group Inc 多層の非対称接合サンドイッチ・パネル
JPH0910871A (ja) * 1995-06-28 1997-01-14 Sankyo Manitetsuku:Kk 中空構造材及びハニカム構造材
JPH10128860A (ja) * 1996-10-30 1998-05-19 Honda Motor Co Ltd 繊維強化プラスチック成形品の製造方法
JPH10273042A (ja) * 1997-03-31 1998-10-13 Kawasaki Heavy Ind Ltd 高速車両の先頭部の耐鳥衝突構造
JP2000043796A (ja) * 1998-07-30 2000-02-15 Japan Aircraft Development Corp 複合材の翼形構造およびその成形方法
WO2002074469A2 (en) * 2000-12-08 2002-09-26 Toyota Motor Sales Usa Inc. A molded composite structure and method of forming same
JP2004017370A (ja) * 2002-06-13 2004-01-22 Kawasaki Heavy Ind Ltd 航空機用複合材パネルの製造方法及びその装置
JP2006502046A (ja) * 2002-10-11 2006-01-19 ザ・ボーイング・カンパニー 複合航空機パネルの避雷および接地手段
JP2010507530A (ja) * 2006-10-26 2010-03-11 ザ・ボーイング・カンパニー 翼パネル構造

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105073370A (zh) * 2013-01-18 2015-11-18 三菱重工业株式会社 复合材料的制造方法
US10086563B2 (en) 2013-01-18 2018-10-02 Mitsubishi Heavy Industries, Ltd. Method of producing composite material
CN105073370B (zh) * 2013-01-18 2018-10-12 三菱重工业株式会社 复合材料的制造方法
JP7606382B2 (ja) 2021-03-26 2024-12-25 株式会社Subaru 複合材構造およびその製造方法

Also Published As

Publication number Publication date
CN101652240B (zh) 2013-07-17
WO2009023312A2 (en) 2009-02-19
CN101652240A (zh) 2010-02-17
US20080277531A1 (en) 2008-11-13
EP2170592A2 (en) 2010-04-07
WO2009023312A3 (en) 2009-04-30
WO2009023312A9 (en) 2009-06-11

Similar Documents

Publication Publication Date Title
JP2010527303A (ja) ハイブリッド複合パネルシステム及び方法
US8490920B2 (en) Composite bulkhead and skin construction
Ghori et al. The role of advanced polymer materials in aerospace
US20100038030A1 (en) Advanced composite aerostructure article having a braided co-cured fly away hollow mandrel and method for fabrication
US20150217850A1 (en) Laminated i-blade stringer
US10919256B2 (en) Composite structure having a variable gage and methods for forming a composite structure having a variable gage
KR20130143690A (ko) 복합재 햇 보강재, 복합재 햇-보강 압력 웨브, 및 그 제조 방법
JP2015519222A (ja) 傾斜ウェブ付きハット型スティフナーおよびその形成方法
EP2076431B1 (en) Wing panel structure
Rajak et al. Advanced polymers in aircraft structures
US20110311782A1 (en) Planar component of an aircraft and method for producing the same
CN111907688B (zh) 复合桁条组件和形成复合桁条组件的方法
US11325689B2 (en) Composite stringer and methods for forming a composite stringer
US8765042B2 (en) Fuselage section of an aircraft and method for the production of the fuselage section
Soutis Recent advances in building with composites
US20200353715A1 (en) Composite Structure Having a Variable Gage and Methods for Forming a Composite Structure Having a Variable Gage
US11745445B2 (en) Method of designing anisotropic composite laminate structure
US20200353699A1 (en) Composite Structure Having a Variable Gage and Methods for Forming a Composite Structure Having a Variable Gage
EP3736204B1 (en) Composite stringer and methods for forming a composite stringer
US11685503B2 (en) Stringer assemblies and methods of forming thereof
Bello Review of Composite Structures in Aeronautic Applications Part
Krämer et al. Experimental and numerical analysis of hollow and foam-filled A-stringer/A-former under axial compression load and bending moment

Legal Events

Date Code Title Description
A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20110425

A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20110425

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20130118

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20130212

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20130510

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20140304

A02 Decision of refusal

Free format text: JAPANESE INTERMEDIATE CODE: A02

Effective date: 20140819