NO322021B1 - Komposittmaterialstruktur - Google Patents
Komposittmaterialstruktur Download PDFInfo
- Publication number
- NO322021B1 NO322021B1 NO20041174A NO20041174A NO322021B1 NO 322021 B1 NO322021 B1 NO 322021B1 NO 20041174 A NO20041174 A NO 20041174A NO 20041174 A NO20041174 A NO 20041174A NO 322021 B1 NO322021 B1 NO 322021B1
- Authority
- NO
- Norway
- Prior art keywords
- rib
- curvature
- parts
- laminated
- wing
- Prior art date
Links
- 239000002131 composite material Substances 0.000 title claims description 18
- 230000032798 delamination Effects 0.000 description 9
- 239000000463 material Substances 0.000 description 9
- 239000000446 fuel Substances 0.000 description 8
- 239000000835 fiber Substances 0.000 description 5
- 238000004519 manufacturing process Methods 0.000 description 5
- 238000013461 design Methods 0.000 description 4
- 238000005452 bending Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 239000002657 fibrous material Substances 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000003351 stiffener Substances 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 244000268528 Platanus occidentalis Species 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000002648 laminated material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
- Moulding By Coating Moulds (AREA)
- Glass Compositions (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GBGB0122050.8A GB0122050D0 (en) | 2001-09-13 | 2001-09-13 | Composite material structure |
| PCT/GB2002/004046 WO2003022677A1 (en) | 2001-09-13 | 2002-09-06 | Composite material structure |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| NO20041174L NO20041174L (no) | 2004-03-19 |
| NO322021B1 true NO322021B1 (no) | 2006-08-07 |
Family
ID=9921965
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NO20041174A NO322021B1 (no) | 2001-09-13 | 2004-03-19 | Komposittmaterialstruktur |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US7380753B2 (es) |
| EP (1) | EP1425215B1 (es) |
| AT (1) | ATE325034T1 (es) |
| CA (1) | CA2459167C (es) |
| DE (1) | DE60211185T2 (es) |
| ES (1) | ES2258645T3 (es) |
| GB (1) | GB0122050D0 (es) |
| NO (1) | NO322021B1 (es) |
| WO (1) | WO2003022677A1 (es) |
Families Citing this family (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB0219451D0 (en) * | 2002-08-21 | 2002-09-25 | Bae Systems Plc | A bracket |
| EP1495859B1 (de) * | 2003-07-08 | 2008-09-03 | Airbus Deutschland GmbH | Leichtbaustruktur |
| EP1666354B1 (de) * | 2004-12-01 | 2010-09-29 | Airbus Operations GmbH | Strukturbauteil, Verfahren zum Herstellen eines Strukturbauteils und Verwendung eines Strukturbauteils für eine Flugzeugschale |
| GB0525691D0 (en) * | 2005-12-16 | 2006-01-25 | Airbus Uk Ltd | A fastener assembly |
| US7721995B2 (en) * | 2006-12-13 | 2010-05-25 | The Boeing Company | Rib support for wing panels |
| GB0813584D0 (en) * | 2008-07-25 | 2008-09-03 | Airbus Uk Ltd | Method of stiffening a rib |
| ES2372828B1 (es) * | 2008-12-17 | 2012-12-13 | Airbus Operations, S.L. | Costilla-herraje. |
| GB0906952D0 (en) | 2009-04-23 | 2009-06-03 | Airbus Uk Ltd | Aircraft assembly and spar |
| ES2739468T3 (es) * | 2009-05-28 | 2020-01-31 | Soc Lorraine De Construction Aeronautique Slca | Panel estructural de borde de salida de material compuesto para un elemento de una aeronave |
| US8408493B2 (en) * | 2010-05-19 | 2013-04-02 | The Boeing Company | Composite stringer end trim |
| GB201110973D0 (en) * | 2011-06-28 | 2011-08-10 | Airbus Operations Ltd | Bracket |
| US8758879B2 (en) * | 2012-06-24 | 2014-06-24 | The Boeing Company | Composite hat stiffener, composite hat-stiffened pressure webs, and methods of making the same |
| US9327470B1 (en) * | 2012-12-05 | 2016-05-03 | The Boeing Company | Variable-radius laminated radius filler and system and method for manufacturing same |
| EP3100852B1 (en) * | 2015-06-03 | 2017-11-15 | Tusas-Türk Havacilik Ve Uzay Sanayii A.S. | A curved laminated structure |
| CN105151271B (zh) * | 2015-09-21 | 2017-12-22 | 中国运载火箭技术研究院 | 一种外形贯穿飞行器机身的复合材料梁结构 |
| US10046525B2 (en) | 2016-09-30 | 2018-08-14 | The Boeing Company | Advanced variable radius laminated composite radius filler |
| CN109625245A (zh) * | 2018-11-02 | 2019-04-16 | 中国航空工业集团公司西安飞机设计研究所 | 一种通用飞机复合材料方向舵及制作方法 |
| CN109334944B (zh) * | 2018-11-12 | 2021-02-26 | 中国直升机设计研究所 | 一种飞机支撑骨架 |
| US11180238B2 (en) * | 2018-11-19 | 2021-11-23 | The Boeing Company | Shear ties for aircraft wing |
| CN114261506B (zh) * | 2021-12-31 | 2024-06-07 | 中国航空工业集团公司西安飞机设计研究所 | 一种具有整体油箱的复合材料机翼 |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4219980A (en) * | 1977-08-26 | 1980-09-02 | Rockwell International Corporation | Reinforced composite structure and method of fabrication thereof |
| US4657615A (en) | 1984-08-20 | 1987-04-14 | The Boeing Company | Composite leading edge/spar member for an aircraft control surface |
| US5358583A (en) | 1988-10-19 | 1994-10-25 | E. I. Du Pont De Nemours And Company | Apparatus and method for shaping fiber reinforced resin matrix materials and product thereof |
| US5514448A (en) | 1992-07-22 | 1996-05-07 | Mitsui Toatsu Chemicals, Inc. | Laminated molding |
| GB9828368D0 (en) | 1998-12-22 | 1999-02-17 | British Aerospace | Forming reinforcing components |
| EP1031406A1 (en) | 1999-02-22 | 2000-08-30 | British Aerospace | Forming reinforcing components |
| US6513757B1 (en) * | 1999-07-19 | 2003-02-04 | Fuji Jukogyo Kabushiki Kaisha | Wing of composite material and method of fabricating the same |
| JP4425424B2 (ja) | 2000-05-01 | 2010-03-03 | 本田技研工業株式会社 | 繊維強化複合材からなるジョグル付き半硬化物品の製造方法、及びそれを用いた予備成形構造体の製造方法 |
-
2001
- 2001-09-13 GB GBGB0122050.8A patent/GB0122050D0/en not_active Ceased
-
2002
- 2002-09-06 ES ES02755321T patent/ES2258645T3/es not_active Expired - Lifetime
- 2002-09-06 EP EP02755321A patent/EP1425215B1/en not_active Expired - Lifetime
- 2002-09-06 DE DE60211185T patent/DE60211185T2/de not_active Expired - Lifetime
- 2002-09-06 AT AT02755321T patent/ATE325034T1/de not_active IP Right Cessation
- 2002-09-06 CA CA002459167A patent/CA2459167C/en not_active Expired - Fee Related
- 2002-09-06 WO PCT/GB2002/004046 patent/WO2003022677A1/en not_active Application Discontinuation
- 2002-09-06 US US10/487,457 patent/US7380753B2/en not_active Expired - Lifetime
-
2004
- 2004-03-19 NO NO20041174A patent/NO322021B1/no not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| CA2459167A1 (en) | 2003-03-20 |
| ATE325034T1 (de) | 2006-06-15 |
| GB0122050D0 (en) | 2001-10-31 |
| NO20041174L (no) | 2004-03-19 |
| US20040244334A1 (en) | 2004-12-09 |
| CA2459167C (en) | 2008-11-18 |
| DE60211185T2 (de) | 2006-09-07 |
| ES2258645T3 (es) | 2006-09-01 |
| WO2003022677A1 (en) | 2003-03-20 |
| EP1425215B1 (en) | 2006-05-03 |
| US7380753B2 (en) | 2008-06-03 |
| EP1425215A1 (en) | 2004-06-09 |
| DE60211185D1 (de) | 2006-06-08 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MM1K | Lapsed by not paying the annual fees |