CN113246339B - Carbon fiber reinforced prepreg material and method for forming coated missile wing by using same - Google Patents
Carbon fiber reinforced prepreg material and method for forming coated missile wing by using same Download PDFInfo
- Publication number
- CN113246339B CN113246339B CN202110800222.1A CN202110800222A CN113246339B CN 113246339 B CN113246339 B CN 113246339B CN 202110800222 A CN202110800222 A CN 202110800222A CN 113246339 B CN113246339 B CN 113246339B
- Authority
- CN
- China
- Prior art keywords
- carbon fiber
- fiber reinforced
- reinforced prepreg
- missile wing
- fiber fabric
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B15/00—Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00
- B29B15/08—Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00 of reinforcements or fillers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B15/00—Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00
- B29B15/08—Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00 of reinforcements or fillers
- B29B15/10—Coating or impregnating independently of the moulding or shaping step
- B29B15/12—Coating or impregnating independently of the moulding or shaping step of reinforcements of indefinite length
- B29B15/122—Coating or impregnating independently of the moulding or shaping step of reinforcements of indefinite length with a matrix in liquid form, e.g. as melt, solution or latex
- B29B15/125—Coating or impregnating independently of the moulding or shaping step of reinforcements of indefinite length with a matrix in liquid form, e.g. as melt, solution or latex by dipping
-
- 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
- B29L2031/777—Weapons
- B29L2031/7772—Cartridges
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Robotics (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Reinforced Plastic Materials (AREA)
- Laminated Bodies (AREA)
Abstract
Description
Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202110800222.1A CN113246339B (en) | 2021-07-15 | 2021-07-15 | Carbon fiber reinforced prepreg material and method for forming coated missile wing by using same |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202110800222.1A CN113246339B (en) | 2021-07-15 | 2021-07-15 | Carbon fiber reinforced prepreg material and method for forming coated missile wing by using same |
Publications (2)
Publication Number | Publication Date |
---|---|
CN113246339A CN113246339A (en) | 2021-08-13 |
CN113246339B true CN113246339B (en) | 2021-09-21 |
Family
ID=77180488
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202110800222.1A Active CN113246339B (en) | 2021-07-15 | 2021-07-15 | Carbon fiber reinforced prepreg material and method for forming coated missile wing by using same |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN113246339B (en) |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1298043A (en) * | 1969-12-27 | 1972-11-29 | Bayer Ag | Process for the continuous graphitisation of carbon filaments, carbon fibres, carbon fibre strips and carbon yarn |
CN1837285A (en) * | 2005-09-09 | 2006-09-27 | 大连理工大学 | Method for interface modification of continuous fibre reinforced polyarylether resin-base composite materials containing diazacyclo group |
CN1853303A (en) * | 2003-09-18 | 2006-10-25 | 3M创新有限公司 | Fuel cell gas diffusion layer |
CN102350305A (en) * | 2011-09-09 | 2012-02-15 | 华北电力大学 | Method for modifying activated carbon fiber by dielectric barrier discharge |
CN104419181A (en) * | 2013-09-05 | 2015-03-18 | 青岛欣展塑胶有限公司 | High-rigidity high-stability polycarbonate-modified plastic |
CN104629367A (en) * | 2013-11-13 | 2015-05-20 | 宁波博利隆复合材料科技有限公司 | Carbon-fiber-reinforced polyphenyl thioether composite material and preparation method thereof |
CN108589307A (en) * | 2018-01-27 | 2018-09-28 | 福星东联(北京)科技有限公司 | A kind of carbon fibre composite for buffer arm |
CN110509575A (en) * | 2019-08-28 | 2019-11-29 | 湖北三江航天江北机械工程有限公司 | Carbon fiber composite material casing precision missile wing seat is laid with winding, molding method |
CN112933955A (en) * | 2021-01-25 | 2021-06-11 | 大连理工大学 | Preparation method and application of carbon nanofiber material capable of realizing high sulfur capacity |
CN113022039A (en) * | 2021-03-28 | 2021-06-25 | 绍兴宝旌复合材料有限公司 | High-temperature-resistant composite material missile wing and preparation method thereof |
CN113045900A (en) * | 2021-04-19 | 2021-06-29 | 山东道恩高分子材料股份有限公司 | Continuous carbon fiber reinforced polyphenylene sulfide composite material |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101580594B (en) * | 2009-06-10 | 2011-06-08 | 沈阳航空工业学院 | Method for modifying aramid fiber composite material interface by dielectric barrier discharge plasma technique |
CN109337369A (en) * | 2018-10-22 | 2019-02-15 | 杭州如墨科技有限公司 | A kind of preparation method of carbon fiber enhanced polyphenylene sulfide composite material |
-
2021
- 2021-07-15 CN CN202110800222.1A patent/CN113246339B/en active Active
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1298043A (en) * | 1969-12-27 | 1972-11-29 | Bayer Ag | Process for the continuous graphitisation of carbon filaments, carbon fibres, carbon fibre strips and carbon yarn |
CN1853303A (en) * | 2003-09-18 | 2006-10-25 | 3M创新有限公司 | Fuel cell gas diffusion layer |
CN1837285A (en) * | 2005-09-09 | 2006-09-27 | 大连理工大学 | Method for interface modification of continuous fibre reinforced polyarylether resin-base composite materials containing diazacyclo group |
CN102350305A (en) * | 2011-09-09 | 2012-02-15 | 华北电力大学 | Method for modifying activated carbon fiber by dielectric barrier discharge |
CN104419181A (en) * | 2013-09-05 | 2015-03-18 | 青岛欣展塑胶有限公司 | High-rigidity high-stability polycarbonate-modified plastic |
CN104629367A (en) * | 2013-11-13 | 2015-05-20 | 宁波博利隆复合材料科技有限公司 | Carbon-fiber-reinforced polyphenyl thioether composite material and preparation method thereof |
CN108589307A (en) * | 2018-01-27 | 2018-09-28 | 福星东联(北京)科技有限公司 | A kind of carbon fibre composite for buffer arm |
CN110509575A (en) * | 2019-08-28 | 2019-11-29 | 湖北三江航天江北机械工程有限公司 | Carbon fiber composite material casing precision missile wing seat is laid with winding, molding method |
CN112933955A (en) * | 2021-01-25 | 2021-06-11 | 大连理工大学 | Preparation method and application of carbon nanofiber material capable of realizing high sulfur capacity |
CN113022039A (en) * | 2021-03-28 | 2021-06-25 | 绍兴宝旌复合材料有限公司 | High-temperature-resistant composite material missile wing and preparation method thereof |
CN113045900A (en) * | 2021-04-19 | 2021-06-29 | 山东道恩高分子材料股份有限公司 | Continuous carbon fiber reinforced polyphenylene sulfide composite material |
Non-Patent Citations (1)
Title |
---|
Adhesion Improvement of Thermoplastics-Based Composites by Atmospheric Plasma and UV Treatments;Gennaro Scarselli等;《Applied Composite Materials》;20210105(第28期);71-89 * |
Also Published As
Publication number | Publication date |
---|---|
CN113246339A (en) | 2021-08-13 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP5355454B2 (en) | Hybrid laminate and aircraft fuselage part | |
JP4969363B2 (en) | Prepreg and carbon fiber reinforced composites | |
US20180304580A1 (en) | Fiber-metal laminate and its manufacturing method | |
CN110539531A (en) | Nanoreinforced films and laminates for aerospace structures | |
CN104842619A (en) | Prepreg manufacturing process of high-tenacity multilayer structure | |
CN113246339B (en) | Carbon fiber reinforced prepreg material and method for forming coated missile wing by using same | |
CN112248480A (en) | Mixed material pad | |
CN114179462B (en) | Self-adhesive composite material honeycomb plate and preparation method thereof | |
JP2016528345A (en) | Process for producing thermoplastic fiber composite and fan blade formed thereby | |
WO1996021695A1 (en) | Prepregs and carbon fiber-reinforced composite material | |
EP3040307B1 (en) | Graphene fiber for aerospace composites | |
CN106739364A (en) | A kind of aramid fiber/Al alloy composite and its preparation method and application | |
DE102011105377B4 (en) | Curable prepreg with improved properties for composites | |
CN107880494A (en) | A kind of carbon fibre initial rinse fabric and preparation method thereof and metal fiber composite | |
CN106147228A (en) | A kind of be wall material with polyimides sheet material cellular structural material and preparation method thereof | |
JP2009114557A (en) | Uniformly surface-treated carbon fiber and method for producing the same | |
KR20130078153A (en) | Method for manufacturing polymer electrolyte reinforced membrane andpolymer electrolyte reinforced membrane | |
CN113024855B (en) | High-toughness carbon fiber/epoxy resin composite material based on RFI process and preparation method thereof | |
KR101174958B1 (en) | Method for manufacturing of aramid prepreg and aramid steel composite | |
US9416236B2 (en) | Fiber reinforced plastics material and method for production thereof | |
CN109233193A (en) | A kind of preparation method with carbon fiber-glass fiber reinforcing glass steel part phenoplasts | |
CN113470906A (en) | Production process of electron beam curing mica tape | |
JPS6397635A (en) | Fiber-reinforced epoxy resin prepreg having interleaf | |
JP5455408B2 (en) | Polyacrylonitrile-based carbon fiber and method for producing the same | |
KR20030049703A (en) | Manufacturing process of nickel-plated carbon fibers by electroplating method |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant | ||
PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of invention: Carbon fiber reinforced prepreg material and its coating wing forming method Effective date of registration: 20211215 Granted publication date: 20210921 Pledgee: Tianjin Kerong Financing Guarantee Co.,Ltd. Pledgor: BEIJING AEROSPACE TIANMEI TECHNOLOGY Co.,Ltd.|BEIJING HANGTIAN HEXING TECHNOLOGY Co.,Ltd. Registration number: Y2021120000068 |
|
CP01 | Change in the name or title of a patent holder | ||
CP01 | Change in the name or title of a patent holder |
Address after: Area B, No.1 Factory building, No.26 Siwei Road, development zone, Dongli District, Tianjin Patentee after: BEIJING AEROSPACE TIANMEI TECHNOLOGY Co.,Ltd. Patentee after: Beijing Aerospace Hexing Technology Co.,Ltd. Address before: Area B, No.1 Factory building, No.26 Siwei Road, development zone, Dongli District, Tianjin Patentee before: BEIJING AEROSPACE TIANMEI TECHNOLOGY Co.,Ltd. Patentee before: BEIJING HANGTIAN HEXING TECHNOLOGY Co.,Ltd. |
|
PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20230303 Granted publication date: 20210921 Pledgee: Tianjin Kerong Financing Guarantee Co.,Ltd. Pledgor: BEIJING HANGTIAN HEXING TECHNOLOGY Co.,Ltd.|BEIJING AEROSPACE TIANMEI TECHNOLOGY Co.,Ltd. Registration number: Y2021120000068 |