CN208075680U - Bulletproof composite part manufacture system based on heat radiation mode - Google Patents

Abstract

The utility model is related to the bulletproof composite part manufacture systems based on heat radiation mode comprising：Heat source, it is arranged to provides thermal energy in a manner of heat radiation to one or more groups of components for being used to form bulletproof composite part being stacked, wherein each group of component includes at least two components, and at least two component is stacked and wherein at least two component is made of different materials respectively；Pressure apparatus, it is arranged for applying pressure towards the component that is stacked and keeps preset duration, so that at least two component in each group of component is laminated shaping after heating up and its appearance profile is made to be bonded to each other receiving the thermal energy.Using this bulletproof composite part manufacture system can high-volume, high efficiency and produce satisfactory, function admirable bulletproof composite part product at low cost.

Description

Bulletproof composite part manufacture system based on heat radiation mode

Technical field

The utility model is related to shellproof technical field more particularly to a kind of bulletproof composite part manufactures based on heat radiation mode System.

Background technology

Disaster, riot, local conflicts or war etc. is occurring in special circumstances, such as flak jackets, bulletproof halmet, bulletproof shield The various safety devices such as board can provide fairly effective protective capability for the personal safety of people.Therefore, with people Continuous improvement for life, security protection consciousness, for being in great demand for these products, and also very to its quality requirement It is high.Currently, although the prior art has been directed to such safety device using material, structure design, manufacturing process, production Equipment etc. has carried out many beneficial researchs and exploration, but currently remains some drawbacks and problem.

For example, existing bulletproof composite panel products are typically the metal or fibre that hard ceramic material, good toughness is respectively adopted Reinforced resin composite material is tieed up as panel, backboard, then they are suppressed using binder and is struck up partnership finished product is made, so And the process for using current device or equipment to carry out pressing operation is relatively time consuming, such as dozens of minutes or several hours are needed, Even more times.For another example, since some bullet proof composite plating compression process in the prior art are bad, it is easy to cause panel Not close, unreliable with backboard combination, this will influence whether the quality and performance of bullet proof composite plating, it is in particular possible to can be made User brings potential serious fatal harm.So it is necessary to for including these above-mentioned situations existing issue or Drawback is fully studied, to be improved.

Utility model content

In view of this, the utility model provides the bulletproof composite part manufacture system based on heat radiation mode, to effectively Ground solves the problems, such as one or more of the above problem and other aspects in the presence of the prior art.

First, a kind of bulletproof composite part manufacture system based on heat radiation mode is provided according to the utility model, it is described Bulletproof composite part manufacture system includes：

Heat source is arranged in a manner of heat radiation to one or more groups of groups for being used to form bulletproof composite part being stacked Part provides thermal energy, wherein each group of component includes at least two components, at least two component is stacked and wherein at least two A component is made of different materials respectively；And

Pressure apparatus is arranged for applying pressure towards the component being stacked and keeps preset duration, with So that at least two component in each group of component is laminated shaping after heating up and makes it receiving the thermal energy Appearance profile is bonded to each other.

In the bulletproof composite part manufacture system according to the present utility model based on heat radiation mode, optionally, it is described extremely It is additionally provided with binder between few two components, for making at least two component heat up it receiving the thermal energy After be laminated bonding and curing molding is integrated.

It is optionally, described multiple in the bulletproof composite part manufacture system according to the present utility model based on heat radiation mode Closing shellproof part manufacture system further includes：

Temperature control equipment is arranged for carrying out monitoring temperature so that at least one at least two component The hull-skin temperature of a component is in preset temperature；And/or

Pressure control device is arranged for carrying out pressure monitor so that at least two component bears to preset Pressure.

In the bulletproof composite part manufacture system according to the present utility model based on heat radiation mode, optionally, the pressure Power apparatus includes：

Cavity, at least part is open to receive the thermal energy outward, and is configured for accommodating the institute being stacked State component；

The first component and second component are separately positioned on above and below the cavity or in the cavity Opposite both sides；And

Fastener and elasticity part, the fastener are connected with the first component and the second component, and described Elasticity part is arranged on the fastener, the first component and the second component are moved toward one another for making and Apply pressure against the component being stacked and to it, so that at least two component is laminated shaping and makes its shape Profile is bonded to each other.

In the bulletproof composite part manufacture system according to the present utility model based on heat radiation mode, optionally, the pressure Power apparatus includes：

Cavity, at least part is open to receive the thermal energy outward, and is configured for accommodating the institute being stacked State component；

The first component and second component are separately positioned on above and below the cavity or in the cavity Opposite both sides；And

Fastener and elasticity part, the fastener are connected with the first component and the second component, and described Elasticity part is arranged on the fastener, the first component and the second component are moved toward one another for making and Apply pressure against the component being stacked and to it, so that at least two components layers pressure viscosity merging curing molding is One.

It is optionally, described tight in the bulletproof composite part manufacture system according to the present utility model based on heat radiation mode Firmware includes at least two nuts and at least two screw rods, and the elasticity part is to be arranged between the screw rod and the nut Spring.

In the bulletproof composite part manufacture system according to the present utility model based on heat radiation mode, optionally, the heat Source is heater box, is arranged for the pressure apparatus being disposed therein to provide thermal energy.

In the bulletproof composite part manufacture system according to the present utility model based on heat radiation mode, optionally, it is described extremely Few two components are plate-like and with the joint surface to match, and the joint surface is planar or at least part is in song Face shape.

In the bulletproof composite part manufacture system according to the present utility model based on heat radiation mode, optionally, it is described extremely Few two components include the first component being made of the first material and the second component that is made of the second material, first material For ultra-high molecular weight polyethylene（PE）Fiber, aramid fiber or combination thereof, second material are boron carbide, carbonization Silicon, aluminium oxide, metal or combination thereof.

It is optionally, described multiple in the bulletproof composite part manufacture system according to the present utility model based on heat radiation mode Shellproof part is closed for constructing at least part of ballistic-resistant article, the ballistic-resistant article include armour, flak jackets, missile-resistant shield, Bulletproof halmet, bulletproof armour.

Compared with prior art, the utility model is by innovatively providing the bulletproof composite part based on heat radiation mode Manufacture system to can not only so that the manufacturing process of bulletproof composite part is very convenient, quick and efficient, but also especially can It enough combines quite close between the components such as panel, backboard of guarantee bulletproof composite part, is reliable, so as to be obviously improved product Quality.High-volume, high efficiency may be implemented using the utility model and produce at low cost satisfactory, function admirable Bulletproof composite part product.

Description of the drawings

The technical solution of the utility model is described in further detail below with reference to drawings and examples, still It should be known that these attached drawings only design for task of explanation, therefore not as the restriction of the scope of the utility model.In addition, Unless otherwise indicated, these attached drawings are meant only to conceptually illustrate structure construction described herein, without to carry out to scale It draws.

Fig. 1 be a bulletproof composite part manufacture system embodiment according to the present utility model based on heat radiation mode just Depending on structural schematic diagram.

Specific implementation mode

Firstly, it is necessary to explanation, below by by way of example come illustrate the utility model based on heat radiation side Composition, structure construction, features and advantages of the bulletproof composite part manufacture system of formula etc., however all descriptions are intended merely to carry out Illustrate, any limitation is formed to the utility model without them should be interpreted as.

In addition, for the arbitrary single technical characteristic for being described by or implying in the embodiment mentioned by this paper, or Shown or implicit arbitrary single technical characteristic in the drawings, the utility model are still allowed in these technical characteristics（Or Its equivalent）Between continue arbitrary combination or delete, may not this practicality that directly refer to herein to obtain Novel more other embodiments.In addition, for the sake of simplifying drawing, same or like parts and feature are same attached It may be only at one or several places are indicated in figure.

Referring to FIG. 1, only symbolically show in the figure one it is according to the present utility model be based on heat radiation side The basic composition situation of the bulletproof composite part manufacture system of formula, below just this is described in detail.

As shown in Figure 1, in this embodiment provided, which includes pressure apparatus and heat Source.Specifically, heat source be within the system be used for thermal energy is provided, i.e., by the heat source can in a manner of heat radiation to one group or Multigroup component for being used to form bulletproof composite part being stacked provides thermal energy.In Fig. 1 examples, heat source is to use heater box 6, Wherein air can be heated by modes such as electrical heating, by the way that pressure apparatus to be arranged in the heater box 6, hot-air will Such as each component 7 for transferring thermal energy to the pressure apparatus in a manner of heat radiation shown in arrow in Fig. 1 and being placed therein.? When practical application, can optionally it be realized to heater box using the device in the prior art such as such as PID controller or device Interior hot air temperature automatically controls, and the temperature of the hot-air is maintained under a preset temperature, so as to provide one A controllable thermal energy.

In the bulletproof composite part manufacture system, pressure apparatus is for applying pressure towards the component 7 being stacked and protecting Hold a preset duration（Concrete numerical value can be chosen in the range of such as -2 hours 2 minutes, and certain concrete numerical value may be used also To be other numerical value, this can be selected according to practical situations）, so that each component in each component 7 receives Thermal energy and they are laminated shaping after heating up so that the appearance profile of these components is bonded to each other.

For example, in the example given, pressure apparatus is provided with the first component 1, second component 2, fastener, elastic force Component 4 and cavity 10, the wherein first component 1 and second component 2 are separately positioned on above and below cavity 10, so as to To be carried out together to the component 7 that three groups be contained in cavity 10 are used to form bulletproof composite part with fastener and elasticity part 4 Clamping and compression process, these components 7 are to be stacked together, and wherein each group of component 7 has the first structure being stacked Part 8 and second component 9.For the purpose of understanding, by this three groups of component 7 and its respective first in the drawing of Fig. 1 Component 8, second component 9 have carried out decomposing display, however they are actually to be stacked together.

It is understood that be in practical applications first component 8 can be stacked in the top of second component 9, or First component 8 can also be stacked in the lower section of second component 9.In addition, in alternative circumstances, the utility model also allows completely The above-mentioned first component 1 is separately positioned on to the opposite both sides of cavity 10 with second component 2（That is the left and right sides）, simultaneously will The above-mentioned component that these are stacked 7 is also correspondingly adjusted to be arranged longitudinally in cavity 10, and the chamber is set to will pass through The first component 1 and second component 2 of 10 both sides of body come to these components 7 carry out clamping and compression process.

For first component 8 and second component 9, different materials composition is respectively adopted in they.It says as an example Bright, such as ultra-high molecular weight polyethylene may be used in first component 8（PE）Fiber, aramid fiber（Kevlar）Fiber or their group It closes to be made, such as boron carbide, silicon carbide, aluminium oxide, metal may be used in second component 9（Including various alloy materials, anti-bullet Steel etc.）Or combination thereof is made, you can be used separately as first component 8 and second component 9 to be processed molding multiple The backboard and panel for closing shellproof part, to the toughness and hardness being accordingly provides for when confrontation bullet impact bulletproof composite part.

For above-mentioned ultra-high molecular weight polyethylene（PE）Fiber is also generally referred to as high-strength high-modulus polyethylene （HSHMPE）Fiber or elongation chain（ECPE）Polyethylene fibre, it refers to the polyethylene process of 1,000,000 or more relative molecular mass It is formed by ultra high molecular weight polyethylene fiber after spinning-super drawing processing, uses the material that first component 8 can be made to have There is enough toughness to fully absorb kinergety of the bullet when impacting bulletproof composite part.In addition, just for example, by using boron carbide, Can be by hot pressed sintering, pressureless sintering or reaction for second component 9 made by silicon carbide and/or aluminium oxide The processing modes such as sintering are formed, these are all permitted by the utility model.

As illustrating, first component 8 and second component 9 can be structured to plate, and they have phase The joint surface matched, such joint surface can be whole outer surfaces of component or a part of outer surface, and can be plane Shape or at least part have curve form.It certainly, can be by above-mentioned first component 8 under different application scenarios It is configured with any other suitable shape with second component 9.

For the fastener in pressure apparatus, it is configured to and 2 phase of the above-mentioned first component 1 and second component Even.As shown in Figure 1, the fastener is typically to use two groups of screw rods 3 and nut 5, by the way that two bolts 3 are separately positioned on first At the respective both ends of component 1 and second component 2, then by two elasticity parts be respectively installed in corresponding screw rod 3 and nut 5 it Between, to form mechanicals efforts between the first component 1 and second component 2, to not only so that above-mentioned three groups are stacked Component 7 can by the bulletproof composite part manufacture system the first component 1 and both second components 2 reliably clamp, Er Qie It is stacked the first component 8 of pressure-bearing in these components 7 and after second component 9 deforms upon shaping, still can make first Component 1 and second component 2 are moved toward one another, to which they can abut against these groups from opposite upper and lower both direction Part 7 is simultaneously continuously applied mechanicals efforts to it and reaches a preset duration, to promote these components can by as desired into Row is laminated shaping and so that their appearance profile is bonded to each other, and thus effectively ensures compacting Shape correction effect.

For the elasticity part in pressure apparatus, as shown in fig. 1, one or more bullets usually can be directly used Spring 5.Furthermore, it is possible to which nut 3 and one or more bullets is similarly arranged in the one end for being optionally located at second component 2 in screw rod 3 Spring 5, thus, it is possible to obviously increase the active force acted on each component in these components 7.Certainly, according to the utility model Purport under, above-mentioned elasticity part is also allowed to using other any components, device or dress for being capable of providing elastic mechanical power It sets.

In the bulletproof composite part manufacture system embodiment, the cavity 10 of pressure apparatus be configured at least part to Outer opening, so that for receiving the thermal energy supplied from heat source 6, such heat, which is provided to be stacked, is contained in the cavity 10 Interior above-mentioned three groups of components 7 so that respective first component 8 and second component 9 temperature after receiving the thermal energy increase, with Just them is promoted to realize that appearance profile is bonded to each other processing in being laminated reforming process.

It should be pointed out that when using the bulletproof composite part manufacture system of the utility model, according to practical application request Situation can coat bonding in advance between the first component 8 in the component 7 for being used to form bulletproof composite part and second component 9 Agent, or can not also coated with adhesive.

For first, if necessary to the coated with adhesive between first component 8 and second component 9, then In above-mentioned lamination reforming process, by the bulletproof composite part manufacture system directly by both first component 8 and second component 9 Simultaneously curing molding is integrated laminate adhesive, to which bulletproof composite part be made.

In addition, if not between first component 8 and second component 9 if coated with adhesive, then can be by above The lamination reforming process discussed first makes first component 8 in these components 7 and second component 9 complete Shape correction, i.e., Their appearance profile has been able to be bonded to each other well, may then wait for the cooling of these components without deforming upon again And then take out them from pressure apparatus, it is then that adhesive coated is between first component 8 and second component 9 and right It pressurizes and a preset duration is kept thus to be made multiple to which these components layer pressure viscosity merging curing molding to be integrated Close shellproof part.It is understood that above-mentioned pressurized operation can also use the bulletproof composite part manufacture system of the utility model It carries out, but is not necessarily to open heat source at this time, the bulletproof composite part manufacture system is either positioned over room temperature environment or one pre- If the pressurized operation is carried out at a temperature of.

Under some optional situations, can temperature control part be set in the bulletproof composite part manufacture system of the utility model Part, so that temperature control unit in this way carries out temperature monitoring, so that above-mentioned first component 8 and/or second The hull-skin temperature of component 9 is in preset temperature, and lamination shaping or even adhering and solidifying are carried out to them to better ensure that with this Effect.Only for example, which may be used adjusts such as infrared measurement of temperature and temperature feedback controller part Control heat source is realized, and is also allowed to according to practical application feelings for the specific monitoring position of each member temperature in component 7 Condition is selected and is adjusted.In addition, above-mentioned preset temperature can also flexibly be set, such as can be Celsius in 20-300 It is selected in the range of degree.

Under some optional situations, can pressure control portion be set in the bulletproof composite part manufacture system of the utility model Part, to carry out pressure monitoring by means of it, so that each component in the component 7 being stacked bears preset pressure, this The preset pressure of sample can flexibly be set according to practical situations, such as can be in the pressure of 0.01-20Mpa It is selected in range.

In conclusion the foregoing advantage for being substantially better than the prior art can be realized using the utility model, So as to high-volume, high efficiency and produce at low cost function admirable high quality bulletproof composite part, it is such compound Shellproof part can also be with the complicated plate of more curved surfaces or other possible shapes, therefore very either plane tabular Suitable for being used for it to be configured to numerous ballistic-resistant articles such as armour, flak jackets, missile-resistant shield, bulletproof halmet, bulletproof armour It is some or all in each self-structure.

The bulletproof composite part according to the present utility model based on heat radiation mode is only elaborated by way of example above Manufacture system, this few example is only for illustrating that the principles of the present invention and embodiments thereof are used, rather than to the utility model Limitation, in the case where not departing from the spirit and scope of the utility model, those skilled in the art can also make various modifications And improvement.For example, although being provided with three groups of components 7 for being used to form bulletproof composite part, and each group of group in providing example Two components 8 and 9 are all equally arranged in part 7, however for respective structure in the specific setting quantity of said modules, each group component Specific setting quantity of part etc., in the case where not departing from the utility model purport be all can according to practical situations come into Row flexible design and selected.For another example, the specific setting quantity of the fastener in pressure apparatus and elasticity part, position etc. Also it is allowed to be selected and adjusted according to concrete application situation.Therefore, all equivalent technical solutions should all belong to The scope of the utility model is simultaneously limited by every claim of the utility model.

Claims (10)

1. a kind of bulletproof composite part manufacture system based on heat radiation mode, which is characterized in that bulletproof composite part manufacture system System includes：

Heat source is arranged to and is carried to one or more groups of components for being used to form bulletproof composite part being stacked in a manner of heat radiation For thermal energy, wherein each group of component includes at least two components, at least two component is stacked and wherein at least two structure Part is made of different materials respectively；And

Pressure apparatus is arranged for applying pressure towards the component being stacked and keeps preset duration, so that At least two component in each group of component is laminated shaping after heating up and makes its shape receiving the thermal energy Profile is bonded to each other.

2. the bulletproof composite part manufacture system based on heat radiation mode according to claim 1, wherein at least two structure It is additionally provided with binder between part, is laminated after heating up for making at least two component receiving the thermal energy It bonds and curing molding is integrated.

3. the bulletproof composite part manufacture system based on heat radiation mode according to claim 1, wherein the bulletproof composite part Manufacture system further includes：

Temperature control equipment is arranged for carrying out monitoring temperature so that at least one structure at least two component The hull-skin temperature of part is in preset temperature；And/or

Pressure control device is arranged for carrying out pressure monitor so that at least two component bears default pressure Power.

4. the bulletproof composite part manufacture system based on heat radiation mode according to claim 1, wherein the pressure apparatus packet It includes：

Cavity, at least part is open to receive the thermal energy outward, and is configured for accommodating described group be stacked Part；

The first component and second component, be separately positioned on above and below the cavity or the cavity phase Opposed both sides；And

Fastener and elasticity part, the fastener are connected with the first component and the second component, and the elastic force Component is arranged on the fastener, for so that the first component and the second component are moved toward one another and against The component that is stacked simultaneously applies pressure to it, so that at least two component is laminated shaping and makes its appearance profile It is bonded to each other.

5. the bulletproof composite part manufacture system based on heat radiation mode according to claim 2, wherein the pressure apparatus packet It includes：

Cavity, at least part is open to receive the thermal energy outward, and is configured for accommodating described group be stacked Part；

The first component and second component, be separately positioned on above and below the cavity or the cavity phase Opposed both sides；And

Fastener and elasticity part, the fastener are connected with the first component and the second component, and the elastic force Component is arranged on the fastener, for so that the first component and the second component are moved toward one another and against The component that is stacked simultaneously applies pressure to it, so that it is one that at least two components layers pressure viscosity, which merges curing molding, Body.

6. the bulletproof composite part manufacture system based on heat radiation mode according to claim 4 or 5, wherein the fastener Including at least two nuts and at least two screw rods, the elasticity part is the bullet being arranged between the screw rod and the nut Spring.

7. according to the bulletproof composite part manufacture system based on heat radiation mode described in any one of claim 1-5, wherein described Heat source is heater box, is arranged for the pressure apparatus being disposed therein to provide thermal energy.

8. according to the bulletproof composite part manufacture system based on heat radiation mode described in any one of claim 1-5, wherein described At least two components are plate-like and with the joint surface to match, and the joint surface is planar or at least part is in Curve form.

9. according to the bulletproof composite part manufacture system based on heat radiation mode described in any one of claim 1-5, wherein described At least two components include the first component being made of the first material and the second component that is made of the second material, first material Material is ultra-high molecular weight polyethylene（PE）Fiber, aramid fiber or combination thereof, second material are boron carbide, carbonization Silicon, aluminium oxide, metal or combination thereof.

10. according to the bulletproof composite part manufacture system based on heat radiation mode described in any one of claim 1-5, wherein institute At least part of bulletproof composite part for constructing ballistic-resistant article is stated, the ballistic-resistant article includes armour, flak jackets, bulletproof shield Board, bulletproof halmet, bulletproof armour.