CN103835067A - Quasi-three dimensional prefabricated member - Google Patents

Quasi-three dimensional prefabricated member Download PDF

Info

Publication number
CN103835067A
CN103835067A CN201410092438.7A CN201410092438A CN103835067A CN 103835067 A CN103835067 A CN 103835067A CN 201410092438 A CN201410092438 A CN 201410092438A CN 103835067 A CN103835067 A CN 103835067A
Authority
CN
China
Prior art keywords
quasi
dimensional
density
carbon fiber
dimensional prefab
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
CN201410092438.7A
Other languages
Chinese (zh)
Inventor
蒋洪亮
谢美琴
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.)
YIXING YITAI CARBON FIBER WEAVING Co Ltd
Original Assignee
YIXING YITAI CARBON FIBER WEAVING 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 YIXING YITAI CARBON FIBER WEAVING Co Ltd filed Critical YIXING YITAI CARBON FIBER WEAVING Co Ltd
Priority to CN201410092438.7A priority Critical patent/CN103835067A/en
Publication of CN103835067A publication Critical patent/CN103835067A/en
Pending legal-status Critical Current

Links

Images

Abstract

The invention discloses a quasi-three dimensional prefabricated member. The quasi-three dimensional prefabricated member comprises a non-weft fabric and a net tire alternative laminate, wherein continuous needling permeation is conducted on a plurality of fixed layers of the non-weft fabric and the net tire alternative laminate through a bidirectional feeding needle machine in the vertical direction, the adjacent layers are connected through vertical fibers generated between the layers, the quasi-three dimensional prefabricated member of a carbon fiber whole structure is obtained, and the volume density of the quasi-three dimensional prefabricated member ranges from 0.45 g/cm<3> to 0.70 g/cm<3>. The quasi-three dimensional prefabricated member reduces the number of carbonization technologies and avoids deformation caused by contraction of long and short fibers and coking caused by uneven density in a carbonization process; the internal structure and hole distribution of the quasi-three dimensional prefabricated member are optimized; base carbon is easily adsorbed and borne in a CVD process, and friction and abrasion resistant performance, and heat conducting performance, tensile strength and shearing strength in the vertical direction of a carbon brake disc of an airplane are greatly enhanced. The Z-direction longitudinal reinforced fiber content of the quasi-three dimensional prefabricated member is improved, and consistency of density among the layers is controlled effectively.

Description

A kind of quasi three-dimensional prefab
Technical field
The invention provides a kind of quasi three-dimensional prefab, the integrally-built quasi three-dimensional prefab of especially a kind of carbon fiber, is specially adapted to Direct precipitation carbon subsequently and is machined for the C/C structural material of airplane carbon brake disc.
Background technology
Aircraft carbon brake is the strong friction material of a kind of circular superelevation, English, U.S., method three states have just started the exploitation to aircraft carbon brake material as far back as mid-term nineteen sixties, in reinforcing material performance and production technology, update and improve, to the early 1980s, only have B.F.Goodrich company of the U.S., Goodyer company, Honeywell company, Dunlop company of Britain and French Messier-Bugatti company to provide airplane carbon brake disc for Boeing, Airbus SAS.The prefabricated component technology of airplane carbon brake disc mainly comprises pre-oxidized fibers acupuncture prefabricated component technology, carbon fiber continuous fiber knitting skill, carbon fiber staple fiber and resin or pitch compound thermal molded curing technology.Prepare various high-performance C/C composites, all need first to prepare charcoal fibre three-dimensional prefabricated component, charcoal fibre three-dimensional prefabricated component refers to that X all has the structural strength of expectation to, Y-direction, Z-direction.
Pre-oxidized fibers acupuncture prefabricated component technology is mainstream technology in the world at present, comprises preoxidized polyacrylonitrile long fiber (PANOF) and the short folded three dimensional fabric that forms of pre-oxidized polyacrylonitrile fiber (PANOF) net plies of cutting, through technical process such as acupuncture, carbonizations.But the prefabricated component that pre-oxidized polyacrylonitrile fiber (PANOF) is made must carry out carbonation process and be converted into carbon fiber structural.Pre-oxidized polyacrylonitrile fiber thermal conductivity factor is low, carbonization poor controllability, technology difficulty large, high to equipment and technological requirement, and pre-oxidation prefabricated component is in high temperature cabonization process, the long and short fiber of prefabricated component inside produces different stress and wriggles and cause overall shrinkage distortion, easily layering; Also easily cause coking if control bad technique in carbonisation, be combined into the place of concentrating after C/C composite and easily form inhomogeneous low density area, the friction and wear behavior uniformity of the each aspect of final products is had to certain influence.And in carbonisation, discharge a large amount of volatile poisonous crystalline solid of white hydrogen cyanide amine with sharp aroma, operator and environment are affected.
Carbon fiber continuous fiber knitting skill is to utilize polyacrylonitrile-radical long carbon fiber (PANCF) to weave the flat fabric forming, be stacked to required certain thickness, then carry out resin or bituminizing hot moulding and solidify, through carbonization technique, rely on carbonisation resin carbon or RESEARCH OF PYROCARBON bonding.This technology connects because vertical direction does not have fiber, purely relies on resin carbon or RESEARCH OF PYROCARBON in carbonisation next bonding, the face that the flies carbon brake disc of making, vertical direction mechanics performance can be very not high, thermal conductivity factor also can be under some influence, if technology controlling and process is bad, and the easy layering of product.Plane (X, Y-direction) adopts expensive 1K and 3K carbon fiber to make conventionally, complex procedures, and fabrication cycle is long, fiber utilization rate is low, cost is high.
Carbon fiber staple fiber and resin or pitch compound thermal molded curing technology adopt polyacrylonitrile-radical chopped carbon fiber (PANCF) and resin compounded hot moulding curing technology, carrying out resin or bituminizing hot moulding by polyacrylonitrile-radical chopped carbon fiber solidifies, through carbonization technique, rely on carbonisation resin carbon or RESEARCH OF PYROCARBON bonding.The major defect that this technology exists and the major defect of carbon fiber continuous fiber knitting skill are similar.
Summary of the invention
The object of the invention is to overcome above-mentioned the deficiencies in the prior art, provides a kind of little to X, Y-direction fibre damage, and on plane performance, substantially without impact, and the introducing of Z-direction fiber is easy, and Z-direction reinforced fiber content is high, the quasi three-dimensional prefab of interlayer consistent in density.
The object of the invention is to be achieved through the following technical solutions:
A kind of quasi three-dimensional prefab, it comprises laid fabric and net tire alternative stacked, the some fixing levels of vertical direction continuous needle infiltration through two-way feeding needing machine in laid fabric and net tire alternative stacked, produce vertical direction fiber at interlayer and connect adjacent some layers, make the integrally-built quasi three-dimensional prefab of a kind of carbon fiber, the bulk density of described quasi three-dimensional prefab is 0.45~0.70g/cm 3.
Of the present invention can acupuncture laid fabric, be thickness 0.15~0.3mm, the surface density 20~300g/m being made by the radially superimposed acupuncture of polyacrylonitrile-radical long carbon fiber 2thin layer laid fabric, described laid fabric is conducive to follow-up acupuncture and obtains the permanent Z-direction fiber shifting.
Net tire of the present invention, be by polyacrylonitrile-radical chopped carbon fiber through steam or chemical handling flexibly, mechanical shredding, be carded to thickness 0.15~0.3mm, surface density 20~300g/m 2thin type net felt fabric.The length of described polyacrylonitrile-radical chopped carbon fiber is 60~90mm.
Polyacrylonitrile-radical chopped carbon fiber steam treatment is: polyacrylonitrile-radical chopped carbon fiber adds moisture to make to keep chopped carbon fiber to keep 40~70% humidity, and 25~30 DEG C are incubated 1~5 hour.
The mechanical shredding of polyacrylonitrile-radical chopped carbon fiber of the present invention is to utilize transmission system, along single roller opener roll axial direction, forms " S " type cloth pin mode, has reached little to the fibre damage of shredding, the better object of laxity.
Net tire of the present invention, after steam or chemical flexible modification, shredding are processed, strengthen the flexibility of chopped carbon fiber, and in net process, make it to produce certain holding, net the form of the foetus formula has the porous of random distribution, not only, for follow-up carbon deposition provides sufficient space, be conducive to the more charcoals of deposition, improved C/C complex carbon residue; And deposition C-structure distribution performance is good, be conducive to improve the overall performance of making material.
Between laid fabric, lay net tire, described adjacent laid fabric interlayer preferably, with the staggered laying of 0 degree/90 degree angle, is conducive to save material.
Described needling density 30~50 pins/cm 2.
10~25 layers/cm of interlayer density of described quasi three-dimensional prefab.The thickness of described quasi three-dimensional prefab is 10~400mm.
Vertical direction (Z-direction) fiber content 25%~55% of described quasi three-dimensional prefab.
A preparation method for quasi three-dimensional prefab, is characterized in that: the method comprises the following steps:
(1) the thickness 0.15~0.3mm, the surface density 20~300g/m that, are made by the radially superimposed acupuncture of polyacrylonitrile-radical long carbon fiber 2laid fabric; By polyacrylonitrile-radical chopped carbon fiber through steam or chemical handling flexibly, mechanical shredding, be carded to thickness 0.15~0.3mm, surface density 20~300g/m 2net tire;
(2), laid fabric and net tire alternative stacked, control adjacent laid fabric interlayer with the staggered laying of 0 degree/90 degree angle;
(3) the some fixing levels of vertical direction continuous needle infiltration, through two-way feeding needing machine in laid fabric and net tire alternative stacked, needling density 30~50 pins/cm 2, produce vertical direction fiber at interlayer and connect adjacent some layers, making bulk density is 0.45~0.70g/cm 3, 10~25 layers/cm of interlayer density the integrally-built quasi three-dimensional prefab of carbon fiber.
Described two-way feeding needing machine, comprise frame, be located at the motor of frame top, needle beam, needle plate, stripping web plate, corresponding to the holder web plate of below of stripping web plate, for controlling the Worm gear feed screw Lift Part of holder web plate lifting, by bearing, horizontal rotating shaft is installed at upper rack described, horizontal rotating shaft by belt by Motor Drive, two bidirectional cams are installed in the horizontal rotating shaft left and right sides, corresponding to described bidirectional cam below, the first two-way guide pillar is installed, the first two-way guide pillar contacts with corresponding bidirectional cam, needle beam is fixed under the first two-way guide pillar, be positioned at two bidirectional cam outsides at horizontal rotating shaft and be also provided with two the second two-way guide pillars, the second two-way guide pillar lower end is provided with oil cylinder, described oil cylinder and stripping web plate are fixed, be provided with in the both sides of correspondence holder web plate horizontal plane and feed to curtain, described Worm gear feed screw Lift Part comprises worm gear, screw mandrel, and 4 worm gears are fixed on framework soleplate, and 4 rhizoid bars are moved up and down by worm-gear driven, and 4 rhizoid masthead ends are fixing holder web plate jointly, described Worm gear feed screw Lift Part and feed to curtain by the control of automation variable-speed motor.
In process of production, Motor Drive horizontal rotating shaft drives bidirectional cam, the first two-way guide pillar, the second two-way guide pillar to pump, and carries out acupuncture; By the feeding to curtain feeding frequency and speed and control Worm gear feed screw Lift Part and regulate the holder web plate of two-way feeding needing machine to decline of automation variable-speed motor control both sides, the thicker holder web plate of goods is lower.When one side is fed to curtain feed, synchronously carry out acupuncture, the complete prefabrication that is fixed level of acupuncture, adjusts holder web plate and declines, and feeds the superimposed some fixing levels of acupuncture infiltration that carry out of virgin material to curtain input, until obtain certain thickness quasi three-dimensional prefab with opposite side.In acupuncture course, due to the effect of stripping web plate upper cylinder, effectively control density and the interlayer density of quasi three-dimensional prefab.
Compared to the prior art, beneficial effect of the present invention:
1, adopt polyacrylonitrile-based carbon fibre to replace pre-oxidized polyacrylonitrile fiber, reduce carbonization technique link, avoided in carbonisation because long and short fiber shrinks the distortion causing, the coking that density unevenness causes.Utilize net tire prepared by the PANCF filling aspect as prefabricated component, in follow-up acupuncture forming process, easily produce Z-direction fiber and improve prefabricated component Z direction strength, optimized prefabricated component internal structure and distribution of pores.
2, aircraft carbon brake is the strong friction material of a kind of circular superelevation, in view of its direction of motion, long carbon fiber laid fabric is reasonably laid different angles at X, Y in-plane, offers plane tension, the rupture strength of the prefabricated component optimum of manufacturing aeroplane brake discs.
3, adopt chopped carbon fiber net tire and long fiber laid fabric to lay lamination, the some fixing levels of continuous needle infiltration, and the accurate three dimension stereo fabric joining with the some fixing level adjoining, acupuncture has increased the longitudinally continuous penetrability fiber of a certain amount of Z-direction to vertical direction, make it easily to adsorb bearing substrate carbon in CVD process, thereby greatly improve the anti-wear polishing machine of airplane carbon brake disc, heat conductivility, tensile strength and the shear strength of vertical direction.
4, laid fabric only only has one direction tension force, and overlap without fiber, reduce guiding puncture continuous fibers resistance, and acupuncture is also few to fibre damage, by increasing acupuncture thickness, can be by the staple fiber net tire of lamination and long carbon fiber flat fabric, carry out continuous needle and permeate gradually some fixing levels, improve the longitudinal reinforced fiber content of Z-direction of prefabricated component, effectively controlled interlayer consistent in density.
Brief description of the drawings
Fig. 1 is the three-dimensional structure schematic diagram of quasi three-dimensional prefab of the present invention.
In Fig. 1,31-laid fabric, 32-net tire.
Fig. 2 is the structural representation of two-way feeding needing machine.
Fig. 3 is the side view of two-way feeding needing machine.
Detailed description of the invention
The present invention will be further described in conjunction with the accompanying drawings and embodiments.
As shown in Figures 2 and 3, a kind of two-way feeding needing machine, comprise frame 1, be located at the motor 2 at frame 1 top, needle beam 9, needle plate 10, stripping web plate 12, corresponding to the holder web plate 13 of below of stripping web plate 12, for controlling the Worm gear feed screw Lift Part of holder web plate 13 liftings, horizontal rotating shaft 4 is arranged on frame 1 top by bearing 3, horizontal rotating shaft 4 is driven by motor 2 by belt 11, in horizontal rotating shaft 4 left and right sides, two bidirectional cams 5 are installed, corresponding to described bidirectional cam 5 belows, the first two-way guide pillar 6 is installed, the first two-way guide pillar 6 contacts with corresponding bidirectional cam 5, needle beam 9 is fixed on the first two-way guide pillar 6 times, be positioned at two bidirectional cam 5 outsides at horizontal rotating shaft 4 and be also provided with two the second two-way guide pillars 7, the second two-way guide pillar 7 lower ends are provided with oil cylinder 8, described oil cylinder 8 and stripping web plate 12 are fixing, be provided with in the both sides of correspondence holder web plate 13 horizontal planes and feed to curtain 16, described Worm gear feed screw Lift Part comprises that worm gear 15,14,4 worm gears 15 of screw mandrel are fixed on framework soleplate, and 4 rhizoid bars 14 are driven and moved up and down by worm gear 15, and 4 rhizoid bar 14 tops are fixing holder web plate 13 jointly, described Worm gear feed screw Lift Part and feed to curtain 16 by the control of automation variable-speed motor.
In process of production, motor 2 drives horizontal rotating shaft 4 to drive bidirectional cam 5, the first two-way guide pillar 6, the second two-way guide pillar 7 to pump, and carries out acupuncture; By the feeding to curtain 16 feeding frequencies and speed and control Worm gear feed screw Lift Part and regulate the holder web plate 13 of two-way feeding needing machine to decline of automation variable-speed motor control both sides, the thicker holder web plate of goods is lower.When feeding to curtain 16 feed, one side synchronously carries out acupuncture, the complete prefabrication that is fixed level of acupuncture, adjust holder web plate 13 and decline, feed the virgin material of inputting the superimposed some fixing levels of acupuncture infiltration that carry out to curtain 16 with opposite side, until obtain certain thickness quasi three-dimensional prefab.In acupuncture course, because stripping web plate 12 upper cylinders 8 act on, effectively control density and the interlayer density of quasi three-dimensional prefab.
Embodiment 1
Polyacrylonitrile-radical long carbon fiber is cut into the polyacrylonitrile-radical chopped carbon fiber that length is 60mm, spraying moisture makes chopped carbon fiber keep 40% humidity, maintain the temperature at 25 DEG C 5 hours, make its softening modification, take out after staple fiber along single roller opener roll axial direction, " S " type of formation cloth pin mode, shredding is the wadding fibrous suede of 90% shatter value, then unclogs and readjusts into thickness 0.3mm, surface density 200g/m by carding machine 2thin type net felt fabric (net tire).Radially superimposed polyacrylonitrile-radical long carbon fiber acupuncture is become to thickness 0.3mm, surface density 250g/m 2thin layer laid fabric.As shown in Figure 1, by laid fabric and net tire alternative stacked, adjacent laid fabric interlayer is spent the staggered laying of angle with 0 degree/90, and makes the two-layer laid fabric that is of outermost, according to needling density 40 pins/cm 2in vertical direction (Z direction) the continuous needle infiltration of laid fabric and net tire alternative stacked, make to hold in the palm the web plate 5mm that once declines by automation variable-speed motor control Worm gear feed screw Lift Part, until acupuncture becomes the quasi three-dimensional prefab of thickness 400mm, the 20 layers/cm of quasi three-dimensional prefab interlayer density, the bulk density 0.45g/cm that make 3, vertical direction fiber content 38%.
Embodiment 2
Polyacrylonitrile-radical long carbon fiber is cut into the polyacrylonitrile-radical chopped carbon fiber that length is 70mm, squirt surface with octadecyl dimethyl ethoxy quaternary ammonium nitrate, being placed in closed container deposits 20 hours, make its softening modification, take out dewatered drying at normal temperatures, after staple fiber, along single roller opener roll axial direction, form " S " type cloth pin mode, shredding is the wadding fibrous suede of 90% shatter value, then unclogs and readjusts into thickness 0.15mm, surface density 80g/m by carding machine 2thin type net felt fabric (net tire).Directed polyacrylonitrile-radical long carbon fiber superimposed acupuncture is become to thickness 0.15mm, surface density 100g/m 2thin layer laid fabric.As shown in Figure 1, by laid fabric and net tire alternative stacked, adjacent laid fabric interlayer is spent the staggered laying of angle with 0 degree/90, and makes the two-layer laid fabric that is of outermost, according to needling density 45 pins/cm 2in vertical direction (Z direction) the continuous needle infiltration of laid fabric and net tire alternative stacked, make to hold in the palm the web plate 4mm that once declines by automation variable-speed motor control Worm gear feed screw Lift Part, until acupuncture becomes the quasi three-dimensional prefab of thickness 300mm, the 19 layers/cm of quasi three-dimensional prefab interlayer density, the bulk density 0.70g/cm that make 3, vertical direction fiber content 45%.
Embodiment 3
Polyacrylonitrile-radical long carbon fiber is cut into the polyacrylonitrile-radical chopped carbon fiber that length is 80mm, spraying moisture makes chopped carbon fiber keep 70% humidity, maintain the temperature at 25 DEG C 3 hours, make its softening modification, after taking out after staple fiber along single roller opener roll axial direction, " S " type of formation cloth pin mode, shredding is the wadding fibrous suede of 90% shatter value, then unclogs and readjusts into thickness 0.2mm, surface density 125g/m by carding machine 2thin type net felt fabric (net tire).Directed polyacrylonitrile-radical long carbon fiber superimposed acupuncture is become to thickness 0.25mm, surface density 200g/m 2thin layer laid fabric.As shown in Figure 1, by laid fabric and net tire alternative stacked, adjacent laid fabric interlayer is spent the staggered laying of angle with 0 degree/90, and makes the two-layer laid fabric that is of outermost, according to needling density 50 pins/cm 2in vertical direction (Z direction) the continuous needle infiltration of laid fabric and net tire alternative stacked, make to hold in the palm the web plate 5mm that once declines by automation variable-speed motor control Worm gear feed screw Lift Part, until acupuncture becomes the quasi three-dimensional prefab of thickness 350mm, the 16 layers/cm of quasi three-dimensional prefab interlayer density, the bulk density 0.65g/cm that make 3, vertical direction fiber content 55%.
Embodiment 4
Polyacrylonitrile-radical long carbon fiber is cut into the polyacrylonitrile-radical chopped carbon fiber that length is 85mm, spraying moisture makes chopped carbon fiber keep 60% humidity, maintain the temperature at 25 DEG C 2 hours, make its softening modification, after taking out after staple fiber along single roller opener roll axial direction, " S " type of formation cloth pin mode, shredding is the wadding fibrous suede of 90% shatter value, then unclogs and readjusts into thickness 0.25mm, surface density 150g/m by carding machine 2thin type net felt fabric (net tire).Directed polyacrylonitrile-radical long carbon fiber superimposed acupuncture is become to thickness 0.25mm, surface density 200g/m 2thin layer laid fabric.As shown in Figure 1, laid fabric is laid and net tire alternative stacked in X, Y-direction different angles, adjacent laid fabric is 60 degree in the laying angle of X, Y-direction, and makes the two-layer laid fabric that is of outermost, according to needling density 50 pins/cm 2, acupuncture thickness 350mm is in vertical direction (Z direction) the continuous needle infiltration of laid fabric and net tire alternative stacked, make to hold in the palm the web plate 4mm that once declines by automation variable-speed motor control Worm gear feed screw Lift Part, until acupuncture becomes the quasi three-dimensional prefab of thickness 80mm, the 12 layers/cm of quasi three-dimensional prefab interlayer density, the bulk density 0.60g/cm that make 3, vertical direction fiber content 52%.

Claims (9)

1. a quasi three-dimensional prefab, it is characterized in that: it comprises laid fabric and net tire alternative stacked, the some fixing levels of vertical direction continuous needle infiltration through two-way feeding needing machine in laid fabric and net tire alternative stacked, produce vertical direction fiber at interlayer and connect adjacent some layers, make the integrally-built quasi three-dimensional prefab of a kind of carbon fiber, the bulk density of described quasi three-dimensional prefab is 0.45~0.70g/cm 3.
2. quasi three-dimensional prefab according to claim 1, is characterized in that: described laid fabric is thickness 0.15~0.3mm, the surface density 20~300g/m being made up of the radially superimposed acupuncture of polyacrylonitrile-radical long carbon fiber 2thin layer bondedfibre fabric.
3. quasi three-dimensional prefab according to claim 1, is characterized in that: described net tire be by polyacrylonitrile-radical chopped carbon fiber through steam or chemical handling flexibly, mechanical shredding, be carded to thickness 0.15~0.3mm, surface density 20~300g/m 2thin type net felt fabric; The length of described polyacrylonitrile-radical chopped carbon fiber is 60~90mm.
4. quasi three-dimensional prefab according to claim 1, is characterized in that: described adjacent laid fabric interlayer is with the staggered laying of 0 degree/90 degree angle.
5. quasi three-dimensional prefab according to claim 1, is characterized in that: needling density 30~50 pins/cm 2.
6. quasi three-dimensional prefab according to claim 1, is characterized in that: 10~25 layers/cm of interlayer density of described quasi three-dimensional prefab.
7. quasi three-dimensional prefab according to claim 1, is characterized in that: the thickness of described quasi three-dimensional prefab is 10~400mm.
8. quasi three-dimensional prefab according to claim 1, is characterized in that: the vertical direction fiber content 25%~55% of described quasi three-dimensional prefab.
9. a preparation method for quasi three-dimensional prefab, is characterized in that: the method comprises the following steps:
(1) the thickness 0.15~0.3mm, the surface density 20~300g/m that, are made by the radially superimposed acupuncture of polyacrylonitrile-radical long carbon fiber 2laid fabric; By polyacrylonitrile-radical chopped carbon fiber through steam or chemical handling flexibly, mechanical shredding, be carded to thickness 0.15~0.3mm, surface density 20~300g/m 2net tire;
(2), laid fabric and net tire alternative stacked, control adjacent laid fabric interlayer with the staggered laying of 0 degree/90 degree angle;
(3) the some fixing levels of vertical direction continuous needle infiltration, through two-way feeding needing machine in laid fabric and net tire alternative stacked, needling density 30~50 pins/cm 2, produce vertical direction fiber at interlayer and connect adjacent some layers, making bulk density is 0.45~0.70g/cm 3, 10~25 layers/cm of interlayer density the integrally-built quasi three-dimensional prefab of carbon fiber.
CN201410092438.7A 2014-03-13 2014-03-13 Quasi-three dimensional prefabricated member Pending CN103835067A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410092438.7A CN103835067A (en) 2014-03-13 2014-03-13 Quasi-three dimensional prefabricated member

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410092438.7A CN103835067A (en) 2014-03-13 2014-03-13 Quasi-three dimensional prefabricated member

Publications (1)

Publication Number Publication Date
CN103835067A true CN103835067A (en) 2014-06-04

Family

ID=50798948

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410092438.7A Pending CN103835067A (en) 2014-03-13 2014-03-13 Quasi-three dimensional prefabricated member

Country Status (1)

Country Link
CN (1) CN103835067A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109267243A (en) * 2018-12-11 2019-01-25 上海善巧碳素设备科技有限公司 Brake block needing machine and brake block production method
CN110004596A (en) * 2018-01-04 2019-07-12 宜兴市宜泰碳纤维织造有限公司 A kind of improved needing machine
CN110747578A (en) * 2019-10-25 2020-02-04 江苏天鸟高新技术股份有限公司 High-density carbon fiber needled felt and preparation method thereof
CN110952223A (en) * 2019-12-23 2020-04-03 宜兴市华恒高性能纤维织造有限公司 Novel acupuncture three-dimensional structure
CN110998005A (en) * 2017-06-19 2020-04-10 利达公司 Overlapped multi-layer fibrous batts and method of making same
CN110978660A (en) * 2019-12-16 2020-04-10 航天特种材料及工艺技术研究所 Design method of gradient fiber preform
CN111746061A (en) * 2019-03-29 2020-10-09 中国科学院宁波材料技术与工程研究所 Three-dimensional fabric laminated needling composite material and preparation method thereof
CN114013127A (en) * 2022-01-06 2022-02-08 天津工业大学 Non-woven fabric reinforced composite material and preparation method thereof
WO2024055392A1 (en) * 2022-09-15 2024-03-21 南京航空航天大学 Weaving and needling integrated preform formation method and preform formation device

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5599603A (en) * 1989-07-25 1997-02-04 Dunlop Limited, A British Company Manufacture of carbon fibre preform
CN1408920A (en) * 2002-08-27 2003-04-09 宜兴市天鸟高新技术有限公司 Non-woven needle-punched fabric and quasi three-dimensional prefab
CN101492861A (en) * 2009-03-02 2009-07-29 宜兴市飞舟高新科技材料有限公司 Automatic multifunctional needle machine
CN101575766A (en) * 2009-06-10 2009-11-11 西安超码科技有限公司 Method for manufacturing needle-punched carbon fiber pseudo-three-dimensional preform
CN101899748A (en) * 2010-05-28 2010-12-01 上海麦戈士科贸有限公司 High-temperature resistant carbon fiber heat insulation felt
CN102505340A (en) * 2011-10-14 2012-06-20 大连隆田科技有限公司 Method and device for preparing pre-oxidation fiber thick felt
CN102619024A (en) * 2012-03-14 2012-08-01 江阴中丽碳纤维有限公司 Method for preparing polyacrylonitrile preoxidized fiber flakes
CN103233323A (en) * 2013-05-07 2013-08-07 江苏天鸟高新技术股份有限公司 Annular fiber prefabricated member and production method thereof

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5599603A (en) * 1989-07-25 1997-02-04 Dunlop Limited, A British Company Manufacture of carbon fibre preform
CN1408920A (en) * 2002-08-27 2003-04-09 宜兴市天鸟高新技术有限公司 Non-woven needle-punched fabric and quasi three-dimensional prefab
CN101492861A (en) * 2009-03-02 2009-07-29 宜兴市飞舟高新科技材料有限公司 Automatic multifunctional needle machine
CN101575766A (en) * 2009-06-10 2009-11-11 西安超码科技有限公司 Method for manufacturing needle-punched carbon fiber pseudo-three-dimensional preform
CN101899748A (en) * 2010-05-28 2010-12-01 上海麦戈士科贸有限公司 High-temperature resistant carbon fiber heat insulation felt
CN102505340A (en) * 2011-10-14 2012-06-20 大连隆田科技有限公司 Method and device for preparing pre-oxidation fiber thick felt
CN102619024A (en) * 2012-03-14 2012-08-01 江阴中丽碳纤维有限公司 Method for preparing polyacrylonitrile preoxidized fiber flakes
CN103233323A (en) * 2013-05-07 2013-08-07 江苏天鸟高新技术股份有限公司 Annular fiber prefabricated member and production method thereof

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
黄启忠等著: "《高性能炭/炭复合材料制备、结构与应用》", 31 December 2010, 中南大学出版社 *

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110998005A (en) * 2017-06-19 2020-04-10 利达公司 Overlapped multi-layer fibrous batts and method of making same
CN110004596A (en) * 2018-01-04 2019-07-12 宜兴市宜泰碳纤维织造有限公司 A kind of improved needing machine
CN109267243A (en) * 2018-12-11 2019-01-25 上海善巧碳素设备科技有限公司 Brake block needing machine and brake block production method
CN109267243B (en) * 2018-12-11 2023-08-15 常州善巧复合材料科技有限公司 Brake pad needling machine and brake pad production method
CN111746061A (en) * 2019-03-29 2020-10-09 中国科学院宁波材料技术与工程研究所 Three-dimensional fabric laminated needling composite material and preparation method thereof
CN110747578A (en) * 2019-10-25 2020-02-04 江苏天鸟高新技术股份有限公司 High-density carbon fiber needled felt and preparation method thereof
CN110978660A (en) * 2019-12-16 2020-04-10 航天特种材料及工艺技术研究所 Design method of gradient fiber preform
CN110952223A (en) * 2019-12-23 2020-04-03 宜兴市华恒高性能纤维织造有限公司 Novel acupuncture three-dimensional structure
CN114013127A (en) * 2022-01-06 2022-02-08 天津工业大学 Non-woven fabric reinforced composite material and preparation method thereof
CN114013127B (en) * 2022-01-06 2022-04-29 天津工业大学 Non-woven fabric reinforced composite material and preparation method thereof
WO2024055392A1 (en) * 2022-09-15 2024-03-21 南京航空航天大学 Weaving and needling integrated preform formation method and preform formation device

Similar Documents

Publication Publication Date Title
CN103835067A (en) Quasi-three dimensional prefabricated member
EP2314445B1 (en) A method for manufacturing a composite body and a composite body manufacturing arrangement
CN103909691B (en) Carbon-fiber needled preformed body with gradiently-changed body density
US3994762A (en) Carbon fiber composites
CN103921369B (en) A kind of dry method pre-impregnating process of thermoplastic resin-based pre-preg band
CN102731131B (en) High-performance fiber heat-insulating material prefabricating bodies and preparation method thereof
CN111636144A (en) Preparation process of carbon-carbon composite material flat plate
EP3085823B1 (en) Low z high performance carbon composite materials
CN102166840B (en) Z direction continuous carbon fiber prefabricated body
CN101503844A (en) Pre-oxidized fiber filament / pre-oxidized fiber net tire composite pricking prefabricated body and method for manufacturing the same
CN101503843A (en) Pre-oxidized fiber filament / pre-oxidized fiber net tire composite pricking prefabricated body and method for manufacturing the same
CN203866505U (en) Needling machine
KR20130102090A (en) Structural warp knit sheet and laminate thereof
WO2011012587A1 (en) Process for the production of a core with integrated bridging fibers for panels made of composite materials, panel that is obtained and device
KR101180504B1 (en) Fiber opening apparatus of carbon fiber
CN201873841U (en) Composite-fiber needled prefabricating body
US20100223766A1 (en) Low z preform
CN106965425A (en) A kind of composite adaptively increases and decreases yarn three-dimensional woven method
CN105619842A (en) Two-in-one impregnation method and device for continuous fiber-reinforced thermoplastic prepreg belts
CN112522857A (en) Preparation method of high-thickness hard felt
AU2010280570B2 (en) Method for making a core having built-in cross-linking fibers for composite material panels, resulting panel, and device
CN103879076A (en) Knitted fabric needled felt aggregate and preparation method thereof
CN201873842U (en) PANOF (Polyacrylonitrile Oxidized Fiber) acupuncture preform
CN110386242B (en) Toughening of composites using three-dimensional printed thermoplastic pins
CN111020875A (en) Production process of fiber fabric reinforced geotextile

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication

Application publication date: 20140604

RJ01 Rejection of invention patent application after publication