CN107976115A - A kind of boron carbide-titanium alloy composite armour - Google Patents

A kind of boron carbide-titanium alloy composite armour Download PDF

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Publication number
CN107976115A
CN107976115A CN201711025804.7A CN201711025804A CN107976115A CN 107976115 A CN107976115 A CN 107976115A CN 201711025804 A CN201711025804 A CN 201711025804A CN 107976115 A CN107976115 A CN 107976115A
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CN
China
Prior art keywords
boron carbide
titanium alloy
carbide ceramics
graphene
armour
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Pending
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CN201711025804.7A
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Chinese (zh)
Inventor
夏伦刚
崔毅
赵立
傅肃嘉
方宁象
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Zhejiang Li Tai Composite Ltd Co
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Zhejiang Li Tai Composite Ltd Co
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Priority to CN201711025804.7A priority Critical patent/CN107976115A/en
Publication of CN107976115A publication Critical patent/CN107976115A/en
Pending legal-status Critical Current

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41HARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H5/00Armour; Armour plates
    • F41H5/02Plate construction
    • F41H5/04Plate construction composed of more than one layer
    • F41H5/0414Layered armour containing ceramic material

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Ceramic Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

The present invention provides a kind of boron carbide titanium alloy composite armour, the plate armour includes boron carbide ceramics plate and titanium alloy, the titanium alloy wraps up ceramic wafer, the boron carbide ceramics plate is spliced by boron carbide ceramics piece, the boron carbide ceramics piece is formed by boron carbide ceramics material hot pressing, the boron carbide ceramics material includes boron carbide ceramics matrix and graphene, and the graphene dispersion is in boron carbide ceramics matrix.Graphene uniform is dispersed in boron carbide powder, more than 500MPa has been brought up to from about 350MPa using hot pressed sintering, bending strength afterwards, boron carbide ceramics is poured into a mould with titanium alloy, forms the overall structure that titanium alloy four sides coats boron carbide.

Description

A kind of boron carbide-titanium alloy composite armour
Technical field
The invention belongs to bulletproof ceramic field, and in particular to a kind of boron carbide-titanium alloy composite armour.
Background technology
With the fast development of science and technology, the threat faced on battlefield is increasing so that ballistic armor materials increasingly towards High rigidity, high intensity, high tenacity, the direction of low-density are developed.Conventional metals bullet resistant material is big due to density so that vehicle, ship Oceangoing ship and aircraft have to sacrifice its payload, while the blocked up armoring operating flexibility for reducing equipment again, therefore, lightweight Bullet resistant material has become current research hotspot and development trend.Ceramic material has big intensity height, hardness, high temperature resistant, resists Oxidation, the excellent performance such as density is low, and energy-absorbing effect, wear effects, kinetic effect etc. are beneficial to play ceramic material Anti- resilience energy power, these characteristics are not available for metal material, high molecular material and its composite material.Wherein B4C ceramics tools There is light specific gravity(2.52g/cm3), hardness it is high(~36GPa), elasticity modulus it is big(~45GPa), and good chemical stability Deng excellent properties, it is the bullet-proof ceramic of modern efficient and light weight bulletproof armour first choice, prevents in the soldier of the advanced countries such as American and Britain The fields such as shield, military secret protection, Vehicle protector are widely used.Titanium alloy has excellent hardness and toughness, its density Less than armour steel, although density is only the 60% of armour steel, its intensity can match in excellence or beauty with homogeneous steel, and toughness is also better than most of Aluminum alloy armor, the superior 30%-40% of homogeneous steel armor of integrated protection performance ratio equivalent weight.
B4The fusing point of C is up to 2350 DEG C, pure B4C-material because of its high covalently linkage content and low self-diffusion coefficient, agglutinating property compared with Difference, usually can promote its sintering by adding sintering aid.In addition, B4The low tenacity of C ceramics seriously affects its bulletproof performance. Therefore the mode of component and structure composite can be taken to improve B4The toughness of C ceramics.B at present4The preparation of C ceramics is mainly heat Press three kinds of sintering, pressureless sintering, reaction-sintered techniques.Wherein hot pressed sintering is the main side for preparing high-performance boron carbide ceramics Method, generally with thin boron carbide powder 2100 DEG C i.e. can obtain it is relatively denser in 98% boron carbide product.At present, prepare big Sized ceramics plate armour still suffers from bigger difficulty.
The content of the invention
To solve problem above, the present invention provides a kind of boron carbide-titanium alloy composite armour, which makes pottery including boron carbide Porcelain plate and titanium alloy, the titanium alloy wrap up ceramic wafer, and the boron carbide ceramics plate is spliced by boron carbide ceramics piece, described Boron carbide ceramics piece is formed by boron carbide ceramics material hot pressing, and the boron carbide ceramics material includes boron carbide ceramics matrix and stone Black alkene, the graphene dispersion is in boron carbide ceramics matrix.
Preferably, the boron carbide ceramics piece is in regular hexagon, the hexagon boron carbide ceramics piece surface is arc-shaped, And boron carbide ceramics piece back is convex is equipped with ring-shaped pottery.
Preferably, the ring-shaped pottery is integrally formed with boron carbide ceramics matrix.
Preferably, the mass fraction of the graphene accounts for the 1%~5% of boron carbide ceramics matrix.
Preferably, the titanium alloy is Ti-Al-V-Fe alloys.
Compared with prior art, the invention has the advantages that:
Boron carbide provided by the invention-titanium alloy composite armour, graphene are two-dimensional materials, by surface modification and can be modified, Significantly reduce the mutual attractive force between graphene synusia and avoid reuniting, there is good dispersiveness in some liquid mediums And stability, so as to prepare the graphene solution of stable dispersion, it is mixed with ceramic matrix slurry, implantation effect can be obtained The good graphene of fruit-ceramics mixed material, graphene are by pinning ceramic interface, induction crack deflection, bifurcated and split The mechanism such as line bridging, graphene fracture and extraction energy-absorbing play the role of strengthening toughening.Our company uses the graphene of independent development Toughness reinforcing hot pressing boron carbide technology, graphene uniform is dispersed in boron carbide powder, afterwards using hot pressed sintering, obtains performance Excellent boron carbide ceramics material, its bending strength has brought up to more than 500MPa from about 350MPa after adding graphene, comprehensive Ballistic performance is closed to greatly enhance.Boron carbide ceramics is poured into a mould with titanium alloy, forms the overall knot of titanium alloy four sides cladding boron carbide Structure.The advantages of technology:First, technical maturity, process is simple, can pour into a mould complicated shape and net nearly formed product;
Boron carbide ceramics is poured into a mould with titanium alloy, forms the overall structure that titanium alloy four sides coats boron carbide.The advantages of technology: First, technical maturity, process is simple, can pour into a mould complicated shape and net nearly formed product;Can keep to greatest extent ceramics and The respective characteristic of titanium alloy, the advantages of giving full play to boron carbide ceramics lightweight high hard and titanium alloy high-strength and high ductility;Titanium alloy is to pottery The three-dimensional constraining structure of porcelain plate can effectively slow down adverse effect of the boron carbide ceramics brittleness to material;The design of hexagonal ceramic piece Be conducive to rationally arranging and combine closely for potsherd, and mutually constraint, be conducive to prepare large-sized bulletproof armour.Ceramics The potsherd of the circular protrusions at the back side makes constraint of the titanium alloy to ceramics more firm, improves its anti-multiple elastic energy;High rigidity Boron carbide ceramics and the titanium alloy of high intensity are combined into one structure, and new way has been opened up to prepare high-performance bulletproof composite plate armour Footpath.
The hexagonal ceramic piece that regular hexagon ceramic mold obtains is designed with beneficial to the reasonable arrangement of potsherd and close With reference to, and mutually constraint, facilitate the splicing of ceramic wafer to be conducive to prepare large-sized bulletproof armour.
Brief description of the drawings
Fig. 1 is the structure diagram of comminutor provided by the invention;
Fig. 2 is the top view of potsherd provided by the invention;
Fig. 3 is the side view of potsherd provided by the invention;
Fig. 4 is the top view of boron carbide titanium alloy composite armour provided by the invention;
Fig. 5 is the sectional view of boron carbide titanium alloy composite armour provided by the invention.
Embodiment
The present invention is further described with reference to Figure of description.
The preparation of 1 boron carbide ceramics piece of embodiment
Step 1)Material powder:The boron carbide powder that average grain diameter is 3-5 um is selected to add the graphite of 3%-4% as raw material For powder as sintering aid, the average grain diameter of graphite powder is 1-2 um;
Step 2)Prepare graphene solution:The graphene aqueous solution or alcoholic solution of 1-2 wt% is prepared, adds N- methyl pyrroles Pyrrolidone is dispersant, and ultrasonic disperse 10-20 h, obtain the solution that graphene uniform disperses;The wherein piece footpath > of graphene 10 layers of 1um, number of plies <, the additive amount of graphene account for the 1-5 wt% of boron carbide powder;
Step 3)By step 1)In obtained powder and step 2)In obtained graphene solution add ball milling 8- in ball mill 10h, drum's speed of rotation 30-50rpm, ratio of grinding media to material 2:1;
Step 4)It is granulated:As shown in Figure 1, using comminutor, comminutor is the homemade comminutor of present inventor, is specifically made The structure of grain machine is as shown in Figure 1, including size barrel 1, wriggling pump motor, peristaltic pump 2, sprays disk 3, spray coil motor, comminutor bucket 4, Vltrasonic device 6, discharge port 7, the size barrel 1 are connected with peristaltic pump 2, the peristaltic pump 2 with spray disk 3 connect, it is described spray disk 3 with Comminutor bucket 4 connects, and the comminutor bucket 4 is connected with Vltrasonic device 6, and the spray disk is equipped with air port, wherein the air port can be with For the through hole that surrounding opens up along spray disk center axis.The air port is connected with air blower, be passed through in the Vltrasonic device from Sub- water 5.The specific works step of the comminutor is:It it is 350 revs/min by spray 3 speed setting of disk, the frequency of Vltrasonic device is set It is set to 40-60 KHz;Wriggling pump motor is driven, by above-mentioned steps 3)Slurry in the good size barrel of middle ball milling passes through peristaltic pump 2 It is transported in the spray disk 3 on comminutor top, spray coil motor drive system driving spray disk 3 rotates, and rotating spray disk 3 is made by centrifuging Disperseed with by slurry, scattered slurry is blown in water of the bottom with Vltrasonic device 6 by air blower by air port, and particle does not dissolve in Water and be precipitated to bottom, in this way, obtain the moderate powder of even particle size distribution, good fluidity, moisture, the powder that will be obtained Material drying, drying temperature are 100-110 DEG C, and pelletizing is obtained after drying;
Step 5)Pelletizing is fitted into the graphite jig of preformed shape and carries out hot pressing, 2000-2200 DEG C of temperature, pressure 20- 50MPa, sintering time 30-60min.
As shown in Fig. 2, using graphite jig, regular hexagon potsherd 8 is obtained, as shown in figure 3, potsherd surface is arc-shaped 9, the distance between highest face and potsherd bottom of the arc are 10mm or so, in this way, ballistic performance strengthens;In addition, institute State potsherd back to upwardly extend equipped with ring-shaped pottery 10, ring-shaped pottery raises up, the raised and regular hexagon potsherd 8 It is integrally formed;Its height is for 2mm or so, as shown in Fig. 2, the edge of the ring-shaped pottery piece is close to the side of regular hexagon potsherd Edge, in this way, potsherd is more firm in the process of later stage splicing cast.
2 boron carbides of embodiment-titanium alloy composite armour
Step 1)According to the preparation method of embodiment 1, and 1 step 5 of embodiment)In graphite jig regular hexagon, such as Fig. 2 institutes Show, obtain the potsherd of regular hexagon, potsherd 8 is stitched together to form ceramic wafer 11.
Step 2)First according to the mould of the prefabricated definite shape of size of boron carbide ceramics plate 11, by ceramic wafer to be cast 11 place in a mold, and when preheating 1 is small in 400 DEG C of baking ovens, taking-up is placed in pouring basin.Then smelting furnace is warming up to one Constant temperature degree, pours after titanium alloy is completely melt and casts from around ceramic block, realizes metal to ceramic material after molten titanium alloy graining The encapsulation of material, forms the overall structure of titanium alloy parcel boron carbide ceramics.The dosage of titanium alloy pours into a mould Size calculation according to product, It is as shown in Figure 3 to pour dimensioning.The titanium alloy that the present invention uses is the Ti-Al-V-Fe alloys for having good mechanical and ballistic performance.
As shown in figure 4, one block of boron carbide-titanium alloy composite armour is obtained, the length of 340mm, width 330mm, such as Shown in Fig. 5, distance of 12 upper surface of wrapping layer titanium alloy apart from 11 surface of boron carbide ceramics plate is 3mm, wrapping layer titanium alloy 12 Distance of the lower surface apart from 11 back of boron carbide ceramics plate is 10mm;12 left surface of wrapping layer titanium alloy and right flank distance carbonization The distance on 11 surface of boron ceramic wafer is 5mm.
Comparative example 1
Identical with the experimental procedure of embodiment 1, unique difference does not add graphene solution.
Embodiment 1 and the above-mentioned boron carbide ceramics plate being prepared are subjected to ballistic performance test, the results showed that, add stone Its bending strength has brought up to more than 500MPa from about 350MPa after black alkene, and comprehensive ballistic performance greatly enhances;
Add graphene and toughness reinforcing is carried out to boron carbide ceramics, be dispersed in graphene uniform using techniques such as ultrasound, stirring, ball millings In ceramic matrix, the graphene film of high degree of dispersion is effectively improved the brittleness of ceramic material.
Boron carbide ceramics is poured into a mould with titanium alloy, forms the overall structure that titanium alloy four sides coats boron carbide.The technology Advantage:First, technical maturity, process is simple, can pour into a mould complicated shape and net nearly formed product;
The respective characteristic of ceramics and titanium alloy can be kept to greatest extent, given full play to the high hard and titanium of boron carbide ceramics lightweight and closed The advantages of golden high-strength and high ductility;Titanium alloy can effectively slow down the three-dimensional constraining structure of ceramic wafer boron carbide ceramics brittleness to material Adverse effect;Regular hexagon potsherd is designed with rationally arranging and combining closely beneficial to potsherd, and mutually constraint, has Beneficial to preparing large-sized bulletproof armour.The annular protrusion at the ceramic back side makes constraint of the titanium alloy to ceramics more firm, improves it Anti- multiple elastic energy;The boron carbide ceramics of high rigidity and the titanium alloy of high intensity are combined into one structure, are answered to prepare high-performance Close bulletproof armour and open up new approach.
The foregoing is only a preferred embodiment of the present invention, protection scope of the present invention is not limited thereto, appoint What those skilled in the art is in the technical scope of present disclosure, technique according to the invention scheme and its invention structure Think of is subject to equivalent substitution or change, should all be included within the scope of the present invention.

Claims (5)

  1. A kind of 1. boron carbide-titanium alloy composite armour, it is characterised in that:The plate armour includes boron carbide ceramics plate and titanium alloy, institute State titanium alloy parcel ceramic wafer, the boron carbide ceramics plate is spliced by boron carbide ceramics piece, the boron carbide ceramics piece by Boron carbide ceramics material hot pressing forms, and the boron carbide ceramics material includes boron carbide ceramics matrix and graphene, the graphite Alkene is dispersed in boron carbide ceramics matrix.
  2. 2. boron carbide according to claim 1-titanium alloy composite armour, it is characterised in that:The boron carbide ceramics piece is in Hexagon, the hexagon boron carbide ceramics piece surface is arc-shaped, and boron carbide ceramics piece back is convex is equipped with ring-shaped pottery.
  3. 3. boron carbide according to claim 1-titanium alloy composite armour, it is characterised in that:The ring-shaped pottery and carbonization Boron ceramic matrix is integrally formed.
  4. 4. boron carbide according to claim 1-titanium alloy composite armour, it is characterised in that:The quality of the graphene point Number accounts for the 1%~5% of boron carbide ceramics matrix.
  5. 5. boron carbide according to claim 1-titanium alloy composite armour, it is characterised in that:The titanium alloy is Ti-Al- V-Fe alloys.
CN201711025804.7A 2017-10-27 2017-10-27 A kind of boron carbide-titanium alloy composite armour Pending CN107976115A (en)

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Cited By (4)

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Publication number Priority date Publication date Assignee Title
CN110981526A (en) * 2019-10-31 2020-04-10 武汉理工大学 Preparation method of boron carbide ceramic-metal composite material with bionic structure
CN112361885A (en) * 2020-11-06 2021-02-12 赛福纳米科技(徐州)有限公司 Titanium alloy-ceramic-PE composite bulletproof deck and preparation method thereof
CN113071158A (en) * 2021-04-12 2021-07-06 中国航空制造技术研究院 Composite armor protection structure and preparation method thereof
WO2023113743A3 (en) * 2021-12-15 2023-08-10 Ondokuz Mayis Universitesi Functionally graded multiphase new generation hybrid ballistic armour

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110981526A (en) * 2019-10-31 2020-04-10 武汉理工大学 Preparation method of boron carbide ceramic-metal composite material with bionic structure
CN112361885A (en) * 2020-11-06 2021-02-12 赛福纳米科技(徐州)有限公司 Titanium alloy-ceramic-PE composite bulletproof deck and preparation method thereof
CN113071158A (en) * 2021-04-12 2021-07-06 中国航空制造技术研究院 Composite armor protection structure and preparation method thereof
WO2023113743A3 (en) * 2021-12-15 2023-08-10 Ondokuz Mayis Universitesi Functionally graded multiphase new generation hybrid ballistic armour

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Application publication date: 20180501