CN101631668B - 制作复合材料的加强材的方法 - Google Patents
制作复合材料的加强材的方法 Download PDFInfo
- Publication number
- CN101631668B CN101631668B CN200880008263XA CN200880008263A CN101631668B CN 101631668 B CN101631668 B CN 101631668B CN 200880008263X A CN200880008263X A CN 200880008263XA CN 200880008263 A CN200880008263 A CN 200880008263A CN 101631668 B CN101631668 B CN 101631668B
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- CN
- China
- Prior art keywords
- armature
- coxostermum
- blank
- side direction
- core
- 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 - Fee Related
Links
- 238000000034 method Methods 0.000 title claims abstract description 27
- 239000002131 composite material Substances 0.000 title description 3
- 239000003351 stiffener Substances 0.000 title description 2
- 239000011094 fiberboard Substances 0.000 claims description 12
- 238000004519 manufacturing process Methods 0.000 claims description 4
- 238000005728 strengthening Methods 0.000 claims description 2
- 239000000835 fiber Substances 0.000 abstract description 10
- 238000009958 sewing Methods 0.000 abstract description 5
- 238000005520 cutting process Methods 0.000 abstract description 2
- 238000005452 bending Methods 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 239000011347 resin Substances 0.000 description 4
- 229920005989 resin Polymers 0.000 description 4
- 229920000049 Carbon (fiber) Polymers 0.000 description 2
- 238000006424 Flood reaction Methods 0.000 description 2
- 239000004760 aramid Substances 0.000 description 2
- 229920003235 aromatic polyamide Polymers 0.000 description 2
- 238000009954 braiding Methods 0.000 description 2
- 239000004917 carbon fiber Substances 0.000 description 2
- 238000007598 dipping method Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000003365 glass fiber Substances 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 238000006116 polymerization reaction Methods 0.000 description 2
- 230000002787 reinforcement Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 1
- 230000008595 infiltration Effects 0.000 description 1
- 238000001764 infiltration Methods 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000009732 tufting Methods 0.000 description 1
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
- B29C70/28—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
- B29C70/54—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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
- B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
-
- 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
- B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
- B29C53/02—Bending or folding
- B29C53/04—Bending or folding of plates or sheets
-
- 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
-
- 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
-
- 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.]
- Y10T428/24033—Structurally defined web or sheet [e.g., overall dimension, etc.] including stitching and discrete fastener[s], coating or bond
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Civil Engineering (AREA)
- Architecture (AREA)
- Textile Engineering (AREA)
- Structural Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Footwear And Its Accessory, Manufacturing Method And Apparatuses (AREA)
- Manufacture Of Motors, Generators (AREA)
- Reinforced Plastic Materials (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
- Shaping Of Tube Ends By Bending Or Straightening (AREA)
Abstract
Description
Claims (8)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0701947A FR2913747B1 (fr) | 2007-03-16 | 2007-03-16 | Procede de realisation de raidisseurs en materiau composite |
FR0701947 | 2007-03-16 | ||
PCT/FR2008/000300 WO2008132319A1 (fr) | 2007-03-16 | 2008-03-07 | Procede de realisation de raidisseurs en materiau composite |
Publications (2)
Publication Number | Publication Date |
---|---|
CN101631668A CN101631668A (zh) | 2010-01-20 |
CN101631668B true CN101631668B (zh) | 2013-02-27 |
Family
ID=38669098
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN200880008263XA Expired - Fee Related CN101631668B (zh) | 2007-03-16 | 2008-03-07 | 制作复合材料的加强材的方法 |
Country Status (13)
Country | Link |
---|---|
US (1) | US8205567B2 (zh) |
EP (1) | EP2121295B1 (zh) |
JP (1) | JP5102316B2 (zh) |
CN (1) | CN101631668B (zh) |
AT (1) | ATE477920T1 (zh) |
BR (1) | BRPI0808955A2 (zh) |
CA (1) | CA2680923C (zh) |
DE (1) | DE602008002228D1 (zh) |
ES (1) | ES2350386T3 (zh) |
FR (1) | FR2913747B1 (zh) |
IL (1) | IL200803A0 (zh) |
RU (1) | RU2421336C1 (zh) |
WO (1) | WO2008132319A1 (zh) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8720825B2 (en) * | 2005-03-31 | 2014-05-13 | The Boeing Company | Composite stiffeners for aerospace vehicles |
ES2371951B1 (es) * | 2009-03-25 | 2012-11-21 | Airbus Operations, S.L. | Disposición de junta de elementos estructurales de un material compuesto. |
FR2971194A1 (fr) * | 2011-02-04 | 2012-08-10 | Latecoere | Procede de realisation d'une preforme elementaire formee d'un empilage de couches de renfort a structure fibreuse |
FR2971193B1 (fr) * | 2011-02-04 | 2013-04-26 | Latecoere | Procede de realisation d'une preforme a structure fibreuse presentant la forme d'un profile comportant une ame, et preforme realisee |
FR2972387B1 (fr) * | 2011-03-09 | 2013-04-26 | Latecoere | Procede de realisation d'une preforme comportant au moins deux troncons presentant des epaisseurs differentes. |
GB201115080D0 (en) | 2011-09-01 | 2011-10-19 | Airbus Operations Ltd | An aircraft structure |
CN103407171B (zh) * | 2013-07-30 | 2015-07-15 | 北京航空航天大学 | 一种缝纫增强的纤维增强树脂基复合材料十字型接头的整体成型方法 |
EP3040191B1 (en) * | 2014-12-30 | 2019-08-07 | Airbus Operations, S.L. | Method for manufacturing fillers of composite material |
CN108778698B (zh) * | 2016-03-24 | 2021-03-05 | 本田技研工业株式会社 | 织物处理方法和部件 |
US10220935B2 (en) * | 2016-09-13 | 2019-03-05 | The Boeing Company | Open-channel stiffener |
CN108953978A (zh) * | 2018-06-19 | 2018-12-07 | 哈尔滨工程大学 | 一种h型腹杆和方形弦杆装配的复合材料桁架及其制备方法 |
JP2020142478A (ja) * | 2019-03-08 | 2020-09-10 | トヨタ自動車株式会社 | 成形方法 |
DE102019203906A1 (de) * | 2019-03-21 | 2020-09-24 | Brose Fahrzeugteile Se & Co. Kommanditgesellschaft, Bamberg | Trägerbauteil mit Befestigungsbereich aus einem Faserverbundwerkstoff und mindestens einem ein Befestigungselement arretierenden Stützelement |
CN112173062A (zh) * | 2020-09-25 | 2021-01-05 | 中国直升机设计研究所 | 一种复合材料一体化框梁及制造方法 |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4410577A (en) * | 1981-01-12 | 1983-10-18 | Mcdonnell Douglas Corporation | Woven layered cloth reinforcement for structural components |
US4622254A (en) * | 1981-08-31 | 1986-11-11 | Toray Industries, Inc. | Fiber material for reinforcing plastics |
US4966802A (en) * | 1985-05-10 | 1990-10-30 | The Boeing Company | Composites made of fiber reinforced resin elements joined by adhesive |
US5518564A (en) * | 1992-02-17 | 1996-05-21 | Aerospatiale Societe Nationale Industrielle | Method to embody a complex structural piece by wire or strip contact placing |
EP1023986A1 (en) * | 1999-01-28 | 2000-08-02 | McDonnell Douglas Corporation | Reinforcing member of composite workpieces and associated methods |
CN1479669A (zh) * | 2000-12-12 | 2004-03-03 | 加强材料 |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3996084A (en) * | 1974-06-17 | 1976-12-07 | Mcdonnell Douglas Corporation | Lock core panel |
US4331495A (en) * | 1978-01-19 | 1982-05-25 | Rockwell International Corporation | Method of fabricating a reinforced composite structure |
FR2497839A1 (fr) * | 1981-01-12 | 1982-07-16 | Brochier Fils J | Tissu tridimensionnel pour le renforcement de materiaux stratifies et elements en forme obtenus a partir d'un tel tissu |
JPS5887042A (ja) * | 1981-11-19 | 1983-05-24 | 東レ株式会社 | 繊維強化樹脂用補強材 |
JPS58117160A (ja) * | 1981-12-28 | 1983-07-12 | 東レ株式会社 | 桁材 |
JPH03119138A (ja) * | 1989-09-29 | 1991-05-21 | Shikishima Kanbasu Kk | 繊維補強複合材 |
FR2687173B1 (fr) * | 1992-02-11 | 1995-09-08 | Aerospatiale | Procede pour la realisation d'une armature de fibres pour piece de matiere composite, et piece composite comportant une telle armature. |
US6896841B2 (en) * | 2003-03-20 | 2005-05-24 | The Boeing Company | Molding process and apparatus for producing unified composite structures |
-
2007
- 2007-03-16 FR FR0701947A patent/FR2913747B1/fr not_active Expired - Fee Related
-
2008
- 2008-03-07 US US12/531,565 patent/US8205567B2/en active Active
- 2008-03-07 CN CN200880008263XA patent/CN101631668B/zh not_active Expired - Fee Related
- 2008-03-07 BR BRPI0808955-8A patent/BRPI0808955A2/pt not_active IP Right Cessation
- 2008-03-07 ES ES08775635T patent/ES2350386T3/es active Active
- 2008-03-07 CA CA2680923A patent/CA2680923C/fr active Active
- 2008-03-07 RU RU2009138245/05A patent/RU2421336C1/ru not_active IP Right Cessation
- 2008-03-07 WO PCT/FR2008/000300 patent/WO2008132319A1/fr active Application Filing
- 2008-03-07 EP EP08775635A patent/EP2121295B1/fr active Active
- 2008-03-07 AT AT08775635T patent/ATE477920T1/de not_active IP Right Cessation
- 2008-03-07 DE DE602008002228T patent/DE602008002228D1/de active Active
- 2008-03-07 JP JP2009553178A patent/JP5102316B2/ja not_active Expired - Fee Related
-
2009
- 2009-09-08 IL IL200803A patent/IL200803A0/en unknown
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4410577A (en) * | 1981-01-12 | 1983-10-18 | Mcdonnell Douglas Corporation | Woven layered cloth reinforcement for structural components |
US4622254A (en) * | 1981-08-31 | 1986-11-11 | Toray Industries, Inc. | Fiber material for reinforcing plastics |
US4966802A (en) * | 1985-05-10 | 1990-10-30 | The Boeing Company | Composites made of fiber reinforced resin elements joined by adhesive |
US5518564A (en) * | 1992-02-17 | 1996-05-21 | Aerospatiale Societe Nationale Industrielle | Method to embody a complex structural piece by wire or strip contact placing |
EP1023986A1 (en) * | 1999-01-28 | 2000-08-02 | McDonnell Douglas Corporation | Reinforcing member of composite workpieces and associated methods |
CN1479669A (zh) * | 2000-12-12 | 2004-03-03 | 加强材料 |
Also Published As
Publication number | Publication date |
---|---|
FR2913747B1 (fr) | 2009-04-24 |
CA2680923A1 (fr) | 2008-11-06 |
BRPI0808955A2 (pt) | 2014-08-26 |
ATE477920T1 (de) | 2010-09-15 |
CA2680923C (fr) | 2011-08-02 |
IL200803A0 (en) | 2010-05-17 |
RU2421336C1 (ru) | 2011-06-20 |
DE602008002228D1 (de) | 2010-09-30 |
WO2008132319A1 (fr) | 2008-11-06 |
RU2009138245A (ru) | 2011-04-27 |
CN101631668A (zh) | 2010-01-20 |
US20100096067A1 (en) | 2010-04-22 |
JP5102316B2 (ja) | 2012-12-19 |
US8205567B2 (en) | 2012-06-26 |
EP2121295B1 (fr) | 2010-08-18 |
FR2913747A1 (fr) | 2008-09-19 |
JP2010521336A (ja) | 2010-06-24 |
EP2121295A1 (fr) | 2009-11-25 |
ES2350386T3 (es) | 2011-01-21 |
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C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
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ASS | Succession or assignment of patent right |
Owner name: MESSIER-BUGATTI CORPORATION Free format text: FORMER OWNER: MESSIER-DAUTE CO., LTD. Effective date: 20120130 |
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C41 | Transfer of patent application or patent right or utility model | ||
C53 | Correction of patent of invention or patent application | ||
CB02 | Change of applicant information |
Address after: French Velizy - veraku Bligh Applicant after: MESSIER-BUGATTI-DOWTY Address before: French Velizy - veraku Bligh Applicant before: MESSIER-BUGATTI |
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Free format text: CORRECT: APPLICANT; FROM: MESSIER-BUGATTI CORPORATION TO: MESSIER-BUGATTI-DAUTE CORPORATION |
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TA01 | Transfer of patent application right |
Effective date of registration: 20120130 Address after: French Velizy - veraku Bligh Applicant after: MESSIER-BUGATTI Address before: French Velizy - veraku Bligh Applicant before: MESSIER-DOWTY S.A. |
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