CN205086375U - Three -dimensional prefabricated body - Google Patents
Three -dimensional prefabricated body Download PDFInfo
- Publication number
- CN205086375U CN205086375U CN201520517325.7U CN201520517325U CN205086375U CN 205086375 U CN205086375 U CN 205086375U CN 201520517325 U CN201520517325 U CN 201520517325U CN 205086375 U CN205086375 U CN 205086375U
- Authority
- CN
- China
- Prior art keywords
- layer
- dimensional preform
- continuous fiber
- precast body
- preform according
- 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
Landscapes
- Woven Fabrics (AREA)
- Nonwoven Fabrics (AREA)
Abstract
The utility model discloses a three -dimensional prefabricated body should personally experience sth. Part of the body by quick -witted fabric layer in the prefabrication, the continuous fibers layer, and net plies stromatolite forms the elementary layer, sews up the shaping after a plurality of elementary layers combination acupuncture and is three -dimensional overall structure. The utility model discloses in the well prefabricated body unit aspect with the layer between continuous fibers, improved prefabricated annulus to with the layer between mechanical properties, on satisfying quick low -cost basis, improved prefabricated body mechanical properties. This prefabricated body mechanical properties is good, is difficult for the layering, and the shaping is fast, and the wholeness can be stable, is applicable to ceramic base or resin matrix composite's reinforced materials.
Description
Technical field
The utility model relates to a kind of three-dimensional preform, especially to the lifting of existing ceramic base or polymer matrix composites acupuncture three-dimensional preform performance.
Background technology
Fibre-reinforced composite is because of combination properties such as the mechanics high damage tolerance of its excellence, shock-resistant, anti-layering, antifatigues, and structural behaviour designability is strong, be widely used in tubular, tabular and polymorphic structure function integration parts, wherein according to selecting the difference of Fiber Materials, sealing-top structure parts can be applicable to aerospace field functional material, structural material etc.Bind the skeleton of precast body as such ceramic base or polymer matrix composites, the performance of the good bad influence combination process of its performance and final composite.
Chinese patent (200610013430.2) discloses a kind of capping three-dimensional fabric and method for weaving thereof, preset length in reserve warp thread method, linear latitude line stretching method and length in reserve weft yarn method three kinds of weaving process combine by this method for weaving, prepare the shaping part that binds and then adopt woven or weaving method to proceed the overall end-blocking fabric weaved in body portion.This is weaved, weaving method introduces continuous fiber, and mechanical property is good, but owing to weaving, knitting process is various, artificial participation is many, preparation cost is high, and uniformity and uniformity are difficult to control, and cannot meet the requirement of the high-performance of the precast body that binds, low cost, rapid batch production.
Chinese patent (CN102731130B) discloses designs core according to the physical dimension of antenna house, core is stung into by needle point method with quartz fabric and quartzy felt the imitated structure fabric of corresponding physical dimension, this fabric low cost, rapid shaping, but the quartz fabric described in the method need carry out cutting distinguish according to antenna house profile, cause fiber in face discontinuous, reduce rings of material mechanical property, secondly the quartz fabric interlayer described in the method is acupuncture short fiber, interlayer mechanical property is low, affects the overall performance of fabric.
Utility model content
The utility model is for above-mentioned technical problem, propose a kind of three-dimensional preform, continuous fiber layer is possessed in this precast body unit aspect, elementary layer interlayer possesses sews up continuous fiber and acupuncture short fiber, continuous fiber content is high and be evenly distributed, and hoop, is femalely distributed with continuous fiber to, interlayer, and good, the overall mechanical property of interfacial bonding strength is high, and shaping speed is fast, copying accuracy high.
For achieving the above object, the technical solution of the utility model is as follows:
A kind of three-dimensional preform, this precast body is by machine-woven fabric layer, and continuous fiber layer, net plies lamination forming unit layer, after multiple elementary layer combination acupuncture, sew is three-dimension integrally structure.
Further, in described elementary layer, machine-woven fabric layer, continuous fiber layer and net plies allocation ratio are setting value.
Further, the woven fabric of described machine-woven fabric layer is according to laying after product design profiling cutting, and its surface density is 100 ~ 640g/m
2.
Further, the net tyre surface density of described net plies is 40 ~ 160g/m
2.
Further, the continuous fiber canoe of described continuous fiber layer is spirality or grid-shaped.
Further, the needling density of described precast body is 15 ~ 35 pins/cm
2.
Further, described sewing needle is apart from being 2 ~ 20mm, and line-spacing is 2 ~ 20mm.
Further, the bulk density of described precast body is 0.30 ~ 0.88g/cm
3.
This three-dimensional preform that the utility model relates to, paste continuous fiber layer forming surface interior continuous fiber and net plies lamination forming unit layer uniformly that core laying, spirality or grid-shaped are wound around after woven fabric profiling distinguish cutting in machine-woven fabric layer, elementary layer carries out sew precast body after combination acupuncture.All possess equally distributed continuous fiber with interlayer in this precast body unit aspect, mechanical property is high, and overall performance is stablized.Be wound around by continuous fiber and compensate for woven fabric because cutting across the deficiency of the easy deformation of profiling laying, and form the complete closely knit continuous fiber layer with continuous fiber NE by design canoe in precast body inside, meet the requirement that in precast body unit aspect, all directions fiber volume fraction is high and uniformity is high.More three-dimensional woven, the braiding precast body of binding is compared, and forming process is simple, and shaping speed improves more than 50%, and preparation efficiency is high, cost is low.The precast body inside that is introduced in of isotropism net tire forms effective passage, is conducive to the uniformly penetrating of matrix in recombination process, can be introduced and connect short fiber, form network channel, be convenient to the infiltration of later stage basic material in interlayer direction by acupuncture at interlayer; Suturing skill is adopted to introduce continuous staples at precast body elementary layer interlayer, the continuous fiber of interlayer can significantly improve interlayer mechanical property and the shock resistance lesion capability of material, improve globality and uniformity that precast body strengthens structure, meet the demand for development of Aero-Space functional material, structural material high-performance, low cost.
A kind of three-dimensional preform that the utility model proposes is compared with the disclosed a kind of capping three-dimensional fabric of Chinese patent (200610013430.2), and forming process is simple, and shaping speed improves more than 50%, and preparation efficiency is high, cost is low; The continuous fiber layer in precast body unit aspect and interlayer continuous print staples is added compared with the disclosed imitated structure fabric of a kind of precast body that the utility model proposes and Chinese patent (CN102731130B), improve precast body hoop and interlayer mechanical property, on the basis meeting fast and low-cost, improve precast body mechanical property.
Accompanying drawing explanation
Below in conjunction with accompanying drawing, the utility model is described in further detail:
Fig. 1 is that taper of the present utility model is bound three-dimensional preform schematic diagram;
Fig. 2 is A-A sectional view in Fig. 1;
Fig. 3 is enlarged icon intention in I portion in Fig. 2;
Fig. 4 is that two-stage of the present utility model bores the three-dimensional preform schematic diagram that binds;
Fig. 5 is B-B sectional view in Fig. 4;
Fig. 6 is the spherical three-dimensional preform schematic diagram that binds of the present utility model;
Fig. 7 is C-C sectional view in Fig. 6.
Wherein, respectively meet in figure and be described as follows:
Taper is bound three-dimensional preform---and 1; Taper core---2; Elementary layer---3; Machine-woven fabric layer---4; Continuous fiber layer---5; Net plies---6; Staples---7; Two-stage bores the three-dimensional preform that binds---and 8; Two-stage bores precast body bonding pad of binding---and 9; Two-stage cone core---10; The spherical three-dimensional preform that binds---11; The spherical precast body that binds binds district---and 12; Spherical core---13.
Detailed description of the invention
The exemplary embodiments embodying the utility model feature & benefits will describe in detail in the following description.Be understood that the utility model can have various changes in different embodiments, it neither departs from scope of the present utility model, and explanation wherein and accompanying drawing are the use when explain in itself, and is not used to limit the utility model.
Embodiment 1
Adopt 85tex quartz fibre to prepare taper to bind three-dimensional preform 1, as shown in Figure 1, Figure 2, Figure 3 shows, design cell layer 3 is one deck quartz fibre machine-woven fabric layer 4 one deck continuous fiber layer 5 one deck net plies 6 to contour structures.By (120 ± 8) g/m
2quartz fiber cloth, according to the laminating of profiling cutting shown in Fig. 2,3 taper core 2 laying forming machine nonwoven fabric layer 4, is wound around (50 ± 5) g/m
2quartz fibre formed continuous fiber layer 5, then paving cover one deck (55 ± 5) g/m
2quartz fibre net the form of the foetus becomes net plies 6, and rear normal direction profiling acupuncture molded preforms, needling density is 22 pins/cm
2, repeat above-mentioned steps to final product thickness 25mm, now the interlayer density of precast body elementary layer is 15.6 layers/cm, then carries out overall non-through to precast body and sews up introducing staples 7, sew up degree of depth 20mm, needle gage 15mm, line-spacing 15mm.Precast body bulk density is 0.35g/cm
3.
Embodiment 2
Adopt high silica cloth and 190tex quartz fibre to prepare the two-stage shown in Fig. 4, Fig. 5 and bore the three-dimensional preform 8 that binds, design cell layer 3 is: machine-woven fabric layer 4 one deck continuous fiber layer 5 one deck net plies 6 of two layers of thickness 0.25mm height silica cloth.The ply stacking-sequence of reference Fig. 3 is by (230 ± 10) g/m
2high silica cloth profiling cutting laminating two-stage cone core 10 laying forming machine nonwoven fabric layer 4, is wound around (65 ± 10) g/m
2quartz fibre Gitterfasern layer formed continuous fiber layer 5, paving cover one deck (60 ± 10) g/m
2quartz fibre net the form of the foetus becomes net plies 6, and rear profiling acupuncture molded preforms, needling density is 22 pins/cm
2, repeat above-mentioned steps to final product thickness 30mm, after carry out through and through suture introduce staples 7 in two-stage cone precast body bonding pad 9 of binding, sewing needle is apart from being 8mm, and line-spacing is 5mm, and precast body bulk density is 0.71g/cm
3.
Embodiment 3
Adopt 12K carbon fiber to prepare the spherical three-dimensional preform 11 that binds shown in Fig. 6, Fig. 7, design cell layer 3 is: machine-woven fabric layer 4 one deck continuous fiber layer 5 one deck carbon fibre web plies 6 of one deck satin weave carbon cloth.The ply stacking-sequence of reference Fig. 3 is by (560 ± 20) g/m
2carbon cloth profiling cutting is fitted spherical core 13 laying forming machine nonwoven fabric layer 4, is wound around (95 ± 10) g/m
2carbon fiber mesh fibrage formed continuous fiber layer 5, repave and cover one deck (140 ± 15) g/m
2carbon fibre web the form of the foetus becomes net plies 6, and rear profiling acupuncture molded preforms, needling density is 22 pins/cm
2, repeat above-mentioned steps to final product thickness 15mm, then the spherical precast body that binds district 12 of binding is carried out to through and through suture and introduces staples 7, sewing needle is apart from 10mm, line-spacing 10mm.Now precast body bulk density is 0.83g/cm
3.
The technical solution of the utility model is disclosed as above by embodiment.The change that those skilled in the art do when should recognize the scope and spirit of the present utility model disclosed in the claim do not departed from appended by the utility model and retouching, within the protection domain all belonging to claim of the present utility model.
Claims (8)
1. a three-dimensional preform, is characterized in that, this precast body is by machine-woven fabric layer, and continuous fiber layer, net plies lamination forming unit layer, after multiple elementary layer combination acupuncture, sew is three-dimension integrally structure.
2. three-dimensional preform according to claim 1, is characterized in that, in described elementary layer, machine-woven fabric layer, continuous fiber layer and net plies allocation ratio are setting value.
3. three-dimensional preform according to claim 1 and 2, is characterized in that, the woven fabric of described machine-woven fabric layer is according to laying after product design profiling cutting, and its surface density is 100 ~ 640g/m
2.
4. three-dimensional preform according to claim 1 and 2, is characterized in that, the net tyre surface density of described net plies is 40 ~ 160g/m
2.
5. three-dimensional preform according to claim 1 and 2, is characterized in that, the continuous fiber canoe of described continuous fiber layer is spirality or grid-shaped.
6. three-dimensional preform according to claim 1, is characterized in that, the needling density of described precast body is 15 ~ 35 pins/cm
2.
7. three-dimensional preform according to claim 1, is characterized in that, described sewing needle is apart from being 2 ~ 20mm, and line-spacing is 2 ~ 20mm.
8. three-dimensional preform according to claim 1, is characterized in that, the bulk density of described precast body is 0.30 ~ 0.88g/cm
3.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520517325.7U CN205086375U (en) | 2015-07-16 | 2015-07-16 | Three -dimensional prefabricated body |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520517325.7U CN205086375U (en) | 2015-07-16 | 2015-07-16 | Three -dimensional prefabricated body |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205086375U true CN205086375U (en) | 2016-03-16 |
Family
ID=55477092
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520517325.7U Active CN205086375U (en) | 2015-07-16 | 2015-07-16 | Three -dimensional prefabricated body |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205086375U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105926259A (en) * | 2016-06-13 | 2016-09-07 | 江苏伯龙宇航新材料科技有限公司 | Capping fabric seaming and weaving method and capping fabric structure |
| CN106346635A (en) * | 2016-08-24 | 2017-01-25 | 苏州勤耘纤维集合体科技有限公司 | Preparation method of high-density rotating-type needling preform body |
| CN106435956A (en) * | 2016-10-12 | 2017-02-22 | 中材科技股份有限公司 | Conical hollow sandwich revolved-body fabric and application thereof |
| CN107336377A (en) * | 2017-06-09 | 2017-11-10 | 长沙晶优新材料科技有限公司 | A kind of sewing method of more curved surface fiber cloth prefabricated components |
| CN110549644A (en) * | 2019-09-06 | 2019-12-10 | 长沙晶优新材料科技有限公司 | Antenna cover plate and profiling prefabricated member thereof |
| CN110549645A (en) * | 2019-09-06 | 2019-12-10 | 长沙晶优新材料科技有限公司 | antenna cover plate profiling prefabricated part needling method and antenna cover plate forming method |
-
2015
- 2015-07-16 CN CN201520517325.7U patent/CN205086375U/en active Active
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105926259A (en) * | 2016-06-13 | 2016-09-07 | 江苏伯龙宇航新材料科技有限公司 | Capping fabric seaming and weaving method and capping fabric structure |
| CN106346635A (en) * | 2016-08-24 | 2017-01-25 | 苏州勤耘纤维集合体科技有限公司 | Preparation method of high-density rotating-type needling preform body |
| CN106346635B (en) * | 2016-08-24 | 2019-01-22 | 苏州勤耘纤维集合体科技有限公司 | A kind of preparation method of high density rotary type needle thorn preform |
| CN106435956A (en) * | 2016-10-12 | 2017-02-22 | 中材科技股份有限公司 | Conical hollow sandwich revolved-body fabric and application thereof |
| CN106435956B (en) * | 2016-10-12 | 2018-04-20 | 中材科技股份有限公司 | A kind of tapered hollow sandwich revolving body fabric and its application |
| CN107336377A (en) * | 2017-06-09 | 2017-11-10 | 长沙晶优新材料科技有限公司 | A kind of sewing method of more curved surface fiber cloth prefabricated components |
| CN110549644A (en) * | 2019-09-06 | 2019-12-10 | 长沙晶优新材料科技有限公司 | Antenna cover plate and profiling prefabricated member thereof |
| CN110549645A (en) * | 2019-09-06 | 2019-12-10 | 长沙晶优新材料科技有限公司 | antenna cover plate profiling prefabricated part needling method and antenna cover plate forming method |
| CN110549645B (en) * | 2019-09-06 | 2021-08-06 | 长沙晶优新材料科技有限公司 | Antenna cover plate profiling prefabricated part needling method and antenna cover plate forming method |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205086375U (en) | Three -dimensional prefabricated body | |
| CN106393727A (en) | Three-dimensional preform | |
| Hu | 3-D fibrous assemblies: Properties, applications and modelling of three-dimensional textile structures | |
| CN101342807A (en) | Foam sandwich extensional organization composite material and method of producing the same | |
| CN105014984A (en) | Three-dimensional warp-knitted spacer fabric impact-resistant composite material and manufacturing method and application thereof | |
| CN205009684U (en) | Compound loop bonding goods of glass fiber | |
| CN102166840B (en) | Z direction continuous carbon fiber prefabricated body | |
| US7168272B2 (en) | Crimp-free infusible reinforcement fabric | |
| CN102615870B (en) | Light sandwich-structure composite material and preparation method thereof | |
| CN102400398B (en) | Method for preparing single polymer composite material by using two-component composite fiber | |
| RU2012113099A (en) | Woven blanks, composite materials and methods for their manufacture | |
| CN101736476A (en) | Foam filled stereoscopic reinforced material | |
| CN105835481A (en) | Interlaminar reinforced fiber composite material and manufacturing method thereof | |
| CN104480619A (en) | Jute biaxial weft knitted fabric reinforced polypropylene composite material and manufacturing method thereof | |
| KR102492502B1 (en) | A method for producing a dry preform produced by knitting, a method for producing a product made of a composite material from the preform | |
| CN102452175A (en) | Method for reinforcing openings of laminated composite material load-carrying structure | |
| CN103317733B (en) | Carriage covering composite material with silkworm cocoon-imitating winded and braided structure and preparation method thereof | |
| CN108177396B (en) | Knitted three-dimensional honeycomb structure | |
| CN108237739A (en) | A kind of preparation method of the pre- toughened fiber preform of self-fixing | |
| US20090162604A1 (en) | Knitted Infusion Fabric | |
| CN105711214A (en) | Interlamination reinforced fiber composite material with flow guiding layer and preparation method thereof | |
| CN106544776A (en) | A kind of three dimensional fabric | |
| CN202192817U (en) | Dedicated reinforcing compound felt for pultrusion sectional material | |
| CN203938821U (en) | A kind of three-dimension integrally sandwich tape top fabric | |
| CN201648829U (en) | Foam-filled stereoscopic reinforcing material |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 214205 Jiangsu city of Yixing province huankeyuan apricot Road No. 8 Patentee after: Jiangsu bird High Tech Co., Ltd. Address before: 214205 Jiangsu city of Yixing province huankeyuan apricot Road No. 8 Patentee before: Jiangsu Tianniao High Technology Co., Ltd. |
|
| CP01 | Change in the name or title of a patent holder |
Address after: 214205 Jiangsu city of Yixing province huankeyuan apricot Road No. 8 Patentee after: Jiangsu Tianniao High Technology Co., Ltd. Address before: 214205 Jiangsu city of Yixing province huankeyuan apricot Road No. 8 Patentee before: Jiangsu bird High Tech Co., Ltd. |
|
| CP01 | Change in the name or title of a patent holder |