CN107471765A - A kind of improved carbon fiber battenboard - Google Patents

A kind of improved carbon fiber battenboard Download PDF

Info

Publication number
CN107471765A
CN107471765A CN201710687814.0A CN201710687814A CN107471765A CN 107471765 A CN107471765 A CN 107471765A CN 201710687814 A CN201710687814 A CN 201710687814A CN 107471765 A CN107471765 A CN 107471765A
Authority
CN
China
Prior art keywords
carbon fiber
layer
equilateral triangle
top panel
lower panel
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
CN201710687814.0A
Other languages
Chinese (zh)
Inventor
张雪姣
景徐荣
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.)
Wuxi Mountain Show Technology Co Ltd
Original Assignee
Wuxi Mountain Show Technology Co Ltd
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 Wuxi Mountain Show Technology Co Ltd filed Critical Wuxi Mountain Show Technology Co Ltd
Priority to CN201710687814.0A priority Critical patent/CN107471765A/en
Publication of CN107471765A publication Critical patent/CN107471765A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B5/00Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/02Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions
    • B32B3/08Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions characterised by added members at particular parts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/10Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/12Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B33/00Layered products characterised by particular properties or particular surface features, e.g. particular surface coatings; Layered products designed for particular purposes not covered by another single class
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04Interconnection of layers
    • B32B7/10Interconnection of layers at least one layer having inter-reactive properties
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2262/00Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
    • B32B2262/10Inorganic fibres
    • B32B2262/106Carbon fibres, e.g. graphite fibres
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/50Properties of the layers or laminate having particular mechanical properties
    • B32B2307/536Hardness

Landscapes

  • Laminated Bodies (AREA)

Abstract

A kind of improved carbon fiber battenboard, sequentially consist of lower panel, laminboard layer and top panel, the inner surface of the top panel and lower panel lays carbon fiber prepreg, the laminboard layer is equilateral triangle grid packed layer, the pre- horizontalization cap in each summit of each equilateral triangle, the flat cap is cylindrical carbon fiber prepreg, equilateral triangle stability is more preferable, intensity and toughness is more preferable, on ensuring, lower panel is completely embedded firmly with laminboard layer, spy is in the pre- horizontalization cap in each summit of equilateral triangle, expand the contact surface of connection, decorative layer is using separated type decorating film and is printed on decorative pattern, it is conveniently replaceable.

Description

A kind of improved carbon fiber battenboard
Technical field
The present invention relates to carbon fiber board field, more particularly to a kind of improved carbon fiber battenboard.
Background technology
Carbon fiber(Carbon fiber, abbreviation CF), it is a kind of high intensity of phosphorus content more than 95%, high modulus fibre New fiber materials.It is to be piled up to form along fiber axial direction by organic fibers such as flake graphites, through carbonization and stone Microcrystalline graphite material obtained from blackization processing.Carbon fiber " soft outside but hard inside ", quality is lighter than metallic aluminium, but intensity is higher than steel Iron, and there is corrosion-resistant, high-modulus characteristic, all it is important materials in defence and military and civilian aspect.It not only has carbon The intrinsic intrinsic property of material, have both the soft machinability of textile fabric again, be reinforcing fiber of new generation.
Just because of a variety of advantages of carbon fiber, carbon fiber mixes with other materials, and application field becomes very extensive, should For fields such as fishing tackle, sports equipment, sports goods, Aero-Space, in military affairs be used for manufacture rocket, guided missile, satellite, radar, The important war products such as bullet-proof car, flak jackets;Carbon fiber composite board and carbon fiber battenboard are also extensively using for environmental protection finishing Field.
Existing carbon fiber battenboard, laminboard layer are usually that foam stuffing or honeycomb filler are made, and sheet material is not subtracted resistance to compression Preferably mitigate board quality while anti-impact force, saving material, reduce and prepare cost, with the quick hair of economic society Exhibition, the application field of carbon fiber sandwich sheet are constantly expanded, and the sheet material of superpower super rigidity is particularly needed in high-technology field, Such as model airplane making, rocket launcher makes, and automotive component etc., existing battenboard does not reach this target call.
The content of the invention
The technical problem to be solved in the present invention is overcome the deficiencies in the prior art, there is provided it is a kind of simple in construction, it is superpower super firm A kind of improved carbon fiber battenboard of degree.
To realize that the present invention provides following technical scheme:A kind of improved carbon fiber battenboard, is sequentially consisted of down Panel, laminboard layer and top panel, the inner surface of the top panel and lower panel lay carbon fiber prepreg, and the laminboard layer is Equilateral triangle grid packed layer, the pre- horizontalization cap in each summit of each equilateral triangle, the flat cap are that cylindrical carbon fiber is pre- Leaching material.
Preferably, the laminboard layer is aluminium alloy or titanium alloy equilateral triangle grid packed layer.
Preferably, there is adhesive layer between the laminboard layer and top panel and lower panel, the adhesive layer is ring Oxygen tree fat.
Preferably, the outer surface of the top panel is additionally provided with waterproof layer, diaphragm and decorative layer.
Preferably, the decorative layer is separated type decorating film, decorative pattern is printed on decorative layer.
Usefulness of the present invention:Latticed using equilateral triangle composition is used as laminboard layer, and stability is more preferable, and intensity is firm Degree is more preferable, special to connect in the pre- horizontalization cap in each summit of equilateral triangle, expansion to ensure that upper and lower panel and laminboard layer are completely embedded firmly The contact surface connect, decorative layer is using separated type decorating film and is printed on decorative pattern, is conveniently replaceable.
Brief description of the drawings
Fig. 1 is schematic structural view of the invention.
Fig. 2 is layer sandwich structure schematic diagram.
In figure:1 be lower panel, 2 be adhesive layer, 3 be laminboard layer, 4 be adhesive layer, 5 be top panel, 6 be waterproof layer, 7 it is diaphragm, 8 be decorative layer, 9 is flat cap.
Embodiment
A kind of improved carbon fiber battenboard, sequentially consists of lower panel 1, laminboard layer 3 and top panel 5, it is described on The inner surface of panel 5 and lower panel 1 lays carbon fiber prepreg, and the laminboard layer 3 is equilateral triangle grid packed layer, each The pre- horizontalization cap 9 in each summit of equilateral triangle, the flat cap 9 are cylindrical carbon fiber prepreg, and the laminboard layer 3 closes for aluminium Gold or titanium alloy equilateral triangle grid packed layer, it is provided between the laminboard layer 3 and top panel between adhesive layer 4 and lower panel Provided with adhesive layer 2, the adhesive layer 4 and adhesive layer 2 are to be additionally provided with for epoxy resin, the outer surface of the top panel Waterproof layer 6, diaphragm 7 and decorative layer 8, the decorative layer 8 are separated type decorating film, are printed on decorative pattern on decorative layer.
The invention is not limited in a kind of improved carbon fiber battenboard involved by above-mentioned embodiment, is familiar with this Person skilled in the art can also make a variety of changes accordingly, but any be equal or similar change should all be covered with of the invention In the range of the claims in the present invention.

Claims (5)

1. a kind of improved carbon fiber battenboard, sequentially consists of lower panel, laminboard layer and top panel, it is characterised in that: The inner surface of the top panel and lower panel lays carbon fiber prepreg, and the laminboard layer is equilateral triangle grid packed layer, The pre- horizontalization cap in each summit of each equilateral triangle, the flat cap is cylindrical carbon fiber prepreg.
A kind of 2. improved carbon fiber battenboard according to claim 1, it is characterised in that:The laminboard layer is aluminium alloy Or titanium alloy equilateral triangle grid packed layer.
A kind of 3. improved carbon fiber battenboard according to claim 1, it is characterised in that:The laminboard layer and top panel There is adhesive layer between lower panel, the adhesive layer is epoxy resin.
A kind of 4. improved carbon fiber battenboard according to claim 1, it is characterised in that:The outer surface of the top panel It is additionally provided with waterproof layer, diaphragm and decorative layer.
A kind of 5. improved carbon fiber battenboard according to claim 4, it is characterised in that:The decorative layer is separable Type decorating film, decorative pattern is printed on decorative layer.
CN201710687814.0A 2017-08-11 2017-08-11 A kind of improved carbon fiber battenboard Pending CN107471765A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710687814.0A CN107471765A (en) 2017-08-11 2017-08-11 A kind of improved carbon fiber battenboard

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710687814.0A CN107471765A (en) 2017-08-11 2017-08-11 A kind of improved carbon fiber battenboard

Publications (1)

Publication Number Publication Date
CN107471765A true CN107471765A (en) 2017-12-15

Family

ID=60599524

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710687814.0A Pending CN107471765A (en) 2017-08-11 2017-08-11 A kind of improved carbon fiber battenboard

Country Status (1)

Country Link
CN (1) CN107471765A (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101122362A (en) * 2007-09-19 2008-02-13 哈尔滨工业大学 Fibre-reinforced composite lattice sandwich plate and its preparing process
CN202357543U (en) * 2011-08-15 2012-08-01 中国航空工业集团公司西安飞机设计研究所 Light board material with multilayer structure
CN104175616A (en) * 2014-09-16 2014-12-03 哈尔滨工业大学 Honeycomb-type composite material laminboard and hot press molding method thereof
CN106592853A (en) * 2016-11-07 2017-04-26 北京建筑大学 Concrete sandwich board and manufacturing method thereof

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101122362A (en) * 2007-09-19 2008-02-13 哈尔滨工业大学 Fibre-reinforced composite lattice sandwich plate and its preparing process
CN202357543U (en) * 2011-08-15 2012-08-01 中国航空工业集团公司西安飞机设计研究所 Light board material with multilayer structure
CN104175616A (en) * 2014-09-16 2014-12-03 哈尔滨工业大学 Honeycomb-type composite material laminboard and hot press molding method thereof
CN106592853A (en) * 2016-11-07 2017-04-26 北京建筑大学 Concrete sandwich board and manufacturing method thereof

Similar Documents

Publication Publication Date Title
Zheng et al. Biomimetic architectured Kevlar/polyimide composites with ultra-light, superior anti-compressive and flame-retardant properties
CN207105780U (en) A kind of improved carbon fiber battenboard
KR20180128850A (en) Aramid composite for protection, and method of manufacturing for the same and laminate for protection manufactured thereof
CN104743099A (en) Three-dimensional braided composite material propeller blade for airplane and manufacturing method of propeller blade
CN107471765A (en) A kind of improved carbon fiber battenboard
CN103009717A (en) Lightweight high-temperature resistant carbon fiber and metal mixed laminate
CN206781132U (en) A kind of highly dense woven fabric fabric leather Rotating fields of multilayer
CN108088312B (en) Combined bulletproof ceramic armor splicing structure and preparation method thereof
CN207166908U (en) A kind of frame side of electronic product casing
CN202119332U (en) Bulletproof stab-resistant protective garment
CN207172903U (en) Grid cloth enhanced polymer honeycomb aluminum composite laminboard
CN109677042B (en) High-strength light multi-layer carbon fiber special-shaped cabin wall plate
CN107454782A (en) A kind of frame side of electronic product casing
CN217077936U (en) High-curved-surface three-dimensional composite structure bulletproof material
CN206832133U (en) A kind of shellproof wallboard of shelter and shellproof shelter
CN108673984B (en) Bulletproof composite material and preparation method and application thereof
CN102632665B (en) A kind of aramid fiber strengthens resin-based thorn-proof composite material
GB2089434A (en) Composite Ducts for Jet Pipes
CN214010116U (en) Flexible breathable bulletproof composite material
CN109320196A (en) Three-dimensional hollow woven part reinforced silica aerogel composite material
CN209869584U (en) Light high-strength unidirectional carbon fiber laminated board
CN208602720U (en) A kind of rocket efficient and light weight moves airvane entirely
CN207035954U (en) A kind of combined human body armour
CN109159518A (en) A kind of aviation aircraft composite plate
CN105669230A (en) High temperature resistant graphite C/C compound material preparation technology

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
RJ01 Rejection of invention patent application after publication

Application publication date: 20171215