CN101758923B - Composite material box-shaped rib and manufacturing method thereof - Google Patents
Composite material box-shaped rib and manufacturing method thereof Download PDFInfo
- Publication number
- CN101758923B CN101758923B CN2008102364740A CN200810236474A CN101758923B CN 101758923 B CN101758923 B CN 101758923B CN 2008102364740 A CN2008102364740 A CN 2008102364740A CN 200810236474 A CN200810236474 A CN 200810236474A CN 101758923 B CN101758923 B CN 101758923B
- Authority
- CN
- China
- Prior art keywords
- box
- layer
- paving
- rib
- composite material
- 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.)
- Active
Links
Images
Classifications
-
- 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
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
Description
Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2008102364740A CN101758923B (en) | 2008-12-25 | 2008-12-25 | Composite material box-shaped rib and manufacturing method thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2008102364740A CN101758923B (en) | 2008-12-25 | 2008-12-25 | Composite material box-shaped rib and manufacturing method thereof |
Publications (2)
Publication Number | Publication Date |
---|---|
CN101758923A CN101758923A (en) | 2010-06-30 |
CN101758923B true CN101758923B (en) | 2012-05-09 |
Family
ID=42490341
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2008102364740A Active CN101758923B (en) | 2008-12-25 | 2008-12-25 | Composite material box-shaped rib and manufacturing method thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN101758923B (en) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2013078646A1 (en) * | 2011-11-30 | 2013-06-06 | Airbus S.A.S. | Airplane component having a box structure |
WO2013078649A1 (en) * | 2011-11-30 | 2013-06-06 | Airbus S.A.S. | Component having a box structure for an airplane airfoil |
GB201307066D0 (en) | 2013-04-18 | 2013-05-29 | Airbus Operations Ltd | Winglet and braided composite spar |
CN103264513B (en) * | 2013-05-30 | 2015-10-21 | 中国商用飞机有限责任公司 | The overall co-curing moulding technique of composite many beams box section |
CN105666893A (en) * | 2014-11-17 | 2016-06-15 | 昌河飞机工业(集团)有限责任公司 | Laying and positioning method for prepreg slices |
CN107541832B (en) * | 2017-08-30 | 2020-03-06 | 杭州碳谱新材料科技有限公司 | Carbon-aluminum composite material heald frame |
CN108032988B (en) * | 2017-10-25 | 2020-06-16 | 北京航空航天大学 | Fiber reinforced composite aircraft cabin connecting structure and preparation method thereof |
CN110481059B (en) * | 2019-09-24 | 2021-06-18 | 航天特种材料及工艺技术研究所 | Composite material foam sandwich structure and forming method thereof |
CN111002762B (en) * | 2019-12-31 | 2024-02-06 | 东莞艾可迅复合材料有限公司 | Hub decoration and manufacturing method thereof |
CN114434824A (en) * | 2021-12-24 | 2022-05-06 | 中航通用飞机有限责任公司珠海复合材料科技分公司 | Forming method of integral special-shaped composite rib |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4084029A (en) * | 1977-07-25 | 1978-04-11 | The Boeing Company | Sine wave beam web and method of manufacture |
CN2526258Y (en) * | 2001-10-24 | 2002-12-18 | 于耀庆 | Structure of aircraft wing of composite material |
CN101249885A (en) * | 2006-12-13 | 2008-08-27 | 波音公司 | Rib support for wing panels |
-
2008
- 2008-12-25 CN CN2008102364740A patent/CN101758923B/en active Active
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4084029A (en) * | 1977-07-25 | 1978-04-11 | The Boeing Company | Sine wave beam web and method of manufacture |
CN2526258Y (en) * | 2001-10-24 | 2002-12-18 | 于耀庆 | Structure of aircraft wing of composite material |
CN101249885A (en) * | 2006-12-13 | 2008-08-27 | 波音公司 | Rib support for wing panels |
Also Published As
Publication number | Publication date |
---|---|
CN101758923A (en) | 2010-06-30 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN101758923B (en) | Composite material box-shaped rib and manufacturing method thereof | |
JP7409885B2 (en) | Molded composite stringer | |
CN103963319B (en) | A kind of matrix material adds prepreg/Resin Film Infusion curing molding method altogether of muscle wallboard | |
US9278748B2 (en) | Processes to fabricate composite tubular-reinforced panels integrating skin and stringers and the panels thereby fabricated | |
CN110181835B (en) | Forming method of variable-section double-taper aramid fiber honeycomb sandwich structure | |
US7416401B2 (en) | Lightweight composite fairing bar and method for manufacturing the same | |
US20130127092A1 (en) | Moulded multilayer plastics component with continuously reinforced fibre plies and process for producing this component | |
CN103538715B (en) | A kind of matrix material �� type ear blade terminal and overall curing molding method altogether thereof | |
CN111470068B (en) | Grille cover body structure for aircraft and manufacturing method thereof | |
US20150151524A1 (en) | Methods for fabricating stabilized honeycomb core composite laminate structures | |
CN104210670A (en) | Hybrid tool for curing pieces of composite material | |
CN106891548A (en) | A kind of T-shaped Material Stiffened Panel forming frock of composite and forming method | |
CN104816661B (en) | Continuous fiber thermoplastic composite plastic seat framework and preparation method thereof | |
CN105946327A (en) | Glass fiber fabric having double-sided twill stereo structure and method for preparing composite material | |
CN208247512U (en) | Composite material drum Material Stiffened Panel solidifying and molding device | |
CN113400677A (en) | Auxiliary die and preparation method of grid structure reinforced foam sandwich composite material | |
CN106739245A (en) | Electronic product casing and its manufacture method | |
CN107559155B (en) | Wind turbine generator system blade, paving bonding method thereof and wind turbine generator system | |
CN114571749A (en) | Three-dimensional reinforced prefabricated part of wind power blade and preparation method thereof | |
CN102470613A (en) | Laminated composite material rod, fabrication method and use in composite material structure | |
CN103522553B (en) | Impact-resistant tension skin structural part process | |
CN110303693A (en) | A kind of compression-moulding methods of small-sized aerofoil Composite Sandwich part | |
CN214726637U (en) | Root splicing type wind power blade | |
CN110641042B (en) | Forming method of X-shaped bracket made of composite material | |
CN117429598B (en) | Special-shaped reinforced rigidity-variable composite material structure and forming method thereof |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
ASS | Succession or assignment of patent right |
Owner name: FESHER AVIATION COMPONENTS (ZHENJIANG) CO., LTD. Free format text: FORMER OWNER: XI AN AIRCRAFT INDUSTRY GROUP CO., LTD. Effective date: 20150130 Owner name: XI AN AIRCRAFT INDUSTRY GROUP CO., LTD. Effective date: 20150130 |
|
C41 | Transfer of patent application or patent right or utility model | ||
COR | Change of bibliographic data |
Free format text: CORRECT: ADDRESS; FROM: 710089 XI AN, SHAANXI PROVINCE TO: 212132 ZHENJIANG, JIANGSU PROVINCE |
|
TR01 | Transfer of patent right |
Effective date of registration: 20150130 Address after: Zhenjiang City, Jiangsu Province, Dagang District 212132 case of the main road No. 88 Patentee after: Fischer aviation components (Zhenjiang) Co., Ltd. Patentee after: Xi'an Aircraft Industry Group Co., Ltd. Address before: 1 No. 710089 Shaanxi province Xi'an city Yanliang District West Avenue Patentee before: Xi'an Aircraft Industry Group Co., Ltd. |