CN110901210A - Production process of strong-foam composite material - Google Patents

Production process of strong-foam composite material Download PDF

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Publication number
CN110901210A
CN110901210A CN201911193810.2A CN201911193810A CN110901210A CN 110901210 A CN110901210 A CN 110901210A CN 201911193810 A CN201911193810 A CN 201911193810A CN 110901210 A CN110901210 A CN 110901210A
Authority
CN
China
Prior art keywords
foam composite
strong
composite material
panel
foam
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
CN201911193810.2A
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Chinese (zh)
Inventor
陈建平
王志坚
王志强
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.)
NANJING TONGKE TECHNOLOGY DEVELOPMENT Co Ltd
Original Assignee
NANJING TONGKE TECHNOLOGY DEVELOPMENT 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 NANJING TONGKE TECHNOLOGY DEVELOPMENT Co Ltd filed Critical NANJING TONGKE TECHNOLOGY DEVELOPMENT Co Ltd
Priority to CN201911193810.2A priority Critical patent/CN110901210A/en
Publication of CN110901210A publication Critical patent/CN110901210A/en
Pending legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/12Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by using adhesives
    • B32B37/1284Application of adhesive
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/50Properties of the layers or laminate having particular mechanical properties
    • B32B2307/558Impact strength, toughness
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/70Other properties
    • B32B2307/718Weight, e.g. weight per square meter
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/70Other properties
    • B32B2307/72Density
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/70Other properties
    • B32B2307/726Permeability to liquids, absorption
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00Properties of the layers or laminate
    • B32B2307/70Other properties
    • B32B2307/732Dimensional properties

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  • Laminated Bodies (AREA)

Abstract

The invention discloses a production process of a strong-foam composite material, and relates to the technical field of composite materials. The method comprises the following steps: firstly, prefabricating carbon fiber pellets; secondly, preparing a strong-foam composite laminate; thirdly, prefabricating a front panel; fourthly, prefabricating a back panel; fifthly, preparing the strong foam composite material; firstly, one side of the front panel is completely and firmly bonded with the front side of the strong-foam composite laminate by using an adhesive, and then one side of the back panel is completely and firmly bonded with the back side of the strong-foam composite laminate by using the adhesive, so that the strong-foam composite material is obtained. The invention has the advantages that the strong foam composite material has the advantages of light weight: the specific gravity is 0.5-1.0, the structural strength is high, and the energy absorption is as follows: and (4) bulletproof and impact-resistant.

Description

Production process of strong-foam composite material
Technical Field
The invention relates to the technical field of composite materials, in particular to a production process of a strong-foam composite material.
Background
At present, the pressure-resistant light high-strength material is generally prepared by a method of filling light hollow microspheres with resin, and in order to reduce the overall density of the pressure-resistant light high-strength material, the pressure-resistant light high-strength material is generally prepared by filling more light hollow microspheres or filling light hollow microspheres with smaller density. Over the years, the filling amount of the light hollow microspheres approaches the limit through various filling process optimization, and high-strength composite materials with lower density are further developed to sink into the bottleneck.
Disclosure of Invention
Aiming at the defects of the prior art, the invention provides a production process of a strong foam composite material, and the strong foam composite material is a novel composite material with low density, high strength, low water absorption and low volume deformation rate, so as to solve the problems in the background technology.
In order to achieve the purpose, the invention provides the following technical scheme: a production process of a strong foam composite material comprises the following steps:
firstly, prefabricating carbon fiber pellets; firstly, injecting a foam resin into a metal mold with a lifting temperature control system, heating to 110 ℃ until the foam resin of the metal mold begins to expand and form a globular shape, and keeping for 2-3 hours; injecting the carbon fiber into a metal mold, heating to 200 ℃, and transferring to the second step after the foam pellets are completely wrapped with the carbon fiber;
secondly, preparing a strong-foam composite laminate; placing the carbon fiber pellets prepared in the first step into a square die, cutting the carbon fiber pellets as required, cooling the cut carbon fiber pellets, and demolding to obtain a square high-foam composite laminate;
thirdly, prefabricating a front panel; cutting the size of the front panel according to the square high-foam composite laminate prepared in the second step so that the front panel can completely cover the front of the high-foam composite laminate;
fourthly, prefabricating a back panel, and cutting the size of the back panel according to the square strong-foam composite laminate manufactured in the second step so that the back panel can completely cover the back of the strong-foam composite laminate;
fifthly, preparing the strong foam composite material; firstly, one side of the front panel is completely and firmly bonded with the front side of the strong-foam composite laminate by using an adhesive, and then one side of the back panel is completely and firmly bonded with the back side of the strong-foam composite laminate by using the adhesive, so that the strong-foam composite material is obtained.
As a preferable technical solution of the present invention, the front panel in the third step is a ceramic panel or a metal panel.
As a preferable technical solution of the present invention, the front panel in the third step is a metal panel.
As a preferable technical scheme of the invention, the front panel is a steel plate or a titanium plate.
In a preferred embodiment of the present invention, the back panel in the fourth section is a PE aramid fiber back panel.
In a preferred embodiment of the present invention, the front plate in the third step and the back plate in the fourth step are both ceramic plates or metal plates.
In a preferred embodiment of the present invention, the front panel in the third step and the back panel in the fourth step are both PE aramid fiber panels.
Advantageous effects
Compared with the prior art, the strong foam composite material prepared by the invention has the following beneficial effects: the strong foam composite material has the advantages of light weight: the specific gravity is 0.5-1.0, the structural strength is high, and the energy absorption is as follows: and (4) bulletproof and impact-resistant.
Drawings
FIG. 1 is a process flow diagram of the present invention.
FIG. 2 is a schematic structural diagram of the present invention.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1, a process for producing a high-foam composite material includes the following steps:
firstly, prefabricating carbon fiber pellets; firstly, injecting a foam resin into a metal mold with a lifting temperature control system, heating to 110 ℃ until the foam resin of the metal mold begins to expand and form a globular shape, and keeping for 2-3 hours; injecting the carbon fiber into a metal mold, heating to 200 ℃, and transferring to the second step after the foam pellets are completely wrapped with the carbon fiber;
secondly, preparing a strong-foam composite laminate; placing the carbon fiber pellets prepared in the first step into a square die, cutting the carbon fiber pellets as required, cooling the cut carbon fiber pellets, and demolding to obtain a square high-foam composite laminate;
thirdly, prefabricating a front panel; cutting the size of the front panel according to the square high-foam composite laminate prepared in the second step so that the front panel can completely cover the front of the high-foam composite laminate;
fourthly, prefabricating a back panel, and cutting the size of the back panel according to the square strong-foam composite laminate manufactured in the second step so that the back panel can completely cover the back of the strong-foam composite laminate;
fifthly, preparing the strong foam composite material; firstly, one side of the front panel is completely and firmly bonded with the front side of the strong-foam composite laminate by using an adhesive, and then one side of the back panel is completely and firmly bonded with the back side of the strong-foam composite laminate by using the adhesive, so that the strong-foam composite material is obtained.
Fig. 2 shows a strong foam composite material manufactured by the manufacturing process of the invention, which comprises a front layer 1, a strong foam composite material layer 2, a back layer 3 and carbon fiber pellets 4.
Preferably, the front panel in the third step is a ceramic panel or a metal panel.
Preferably, the front panel in the third step is a metal panel.
Preferably, the front panel is a steel plate or a titanium plate.
Preferably, the back panel in the fourth part is a PE aramid fiber back panel.
Preferably, the front plate in the third step and the back plate in the fourth step are both ceramic panels or metal panels.
Preferably, the front panel in the third step and the back panel in the fourth step are both PE aramid fiber panels.
It should be noted that, in this document, terms such as "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (7)

1. A production process of a strong-foam composite material is characterized by comprising the following steps: the method comprises the following steps:
firstly, prefabricating carbon fiber pellets; firstly, injecting a foam resin into a metal mold with a lifting temperature control system, heating to 110 ℃ until the foam resin of the metal mold begins to expand and form a globular shape, and keeping for 2-3 hours; injecting the carbon fiber into a metal mold, heating to 200 ℃, and transferring to the second step after the foam pellets are completely wrapped with the carbon fiber;
secondly, preparing a strong-foam composite laminate; placing the carbon fiber pellets prepared in the first step into a square die, cutting the carbon fiber pellets as required, cooling the cut carbon fiber pellets, and demolding to obtain a square high-foam composite laminate;
thirdly, prefabricating a front panel; cutting the size of the front panel according to the square high-foam composite laminate prepared in the second step so that the front panel can completely cover the front of the high-foam composite laminate;
fourthly, prefabricating a back panel; cutting the size of the back panel according to the square strong-bubble composite laminate prepared in the second step so that the back panel can completely cover the back of the strong-bubble composite laminate;
fifthly, preparing the strong foam composite material; firstly, one side of the front panel is completely and firmly bonded with the front side of the strong-foam composite laminate by using an adhesive, and then one side of the back panel is completely and firmly bonded with the back side of the strong-foam composite laminate by using the adhesive, so that the strong-foam composite material is obtained.
2. The process for producing a high-foam composite material according to claim 1, wherein: the front panel in the third step is a ceramic panel or a metal panel.
3. The process for producing a high-foam composite material according to claim 2, wherein: and the front panel in the third step is a metal panel.
4. A process for the production of a high-foam composite material according to claim 3, characterized in that: and the front panel in the third step is a steel plate or a titanium plate.
5. The process for producing a high-foam composite material according to claim 1, wherein: the back panel in the fourth part is a PE aramid fiber back panel.
6. The process for producing a high-foam composite material according to claim 1, wherein: and the front panel in the third step and the back panel in the fourth part are both ceramic panels or metal panels.
7. The process for producing a high-foam composite material according to claim 1, wherein: and the front panel in the third step and the back panel in the fourth part are both PE aramid fiber panels.
CN201911193810.2A 2019-11-28 2019-11-28 Production process of strong-foam composite material Pending CN110901210A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201911193810.2A CN110901210A (en) 2019-11-28 2019-11-28 Production process of strong-foam composite material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201911193810.2A CN110901210A (en) 2019-11-28 2019-11-28 Production process of strong-foam composite material

Publications (1)

Publication Number Publication Date
CN110901210A true CN110901210A (en) 2020-03-24

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Application Number Title Priority Date Filing Date
CN201911193810.2A Pending CN110901210A (en) 2019-11-28 2019-11-28 Production process of strong-foam composite material

Country Status (1)

Country Link
CN (1) CN110901210A (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1944500A (en) * 2006-09-28 2007-04-11 湘潭大学 Fiber forced foamed polymer material and its preparing method
CN100391710C (en) * 2000-08-08 2008-06-04 莫尔德特有限公司 Composite material with microsphere particles
CN201143757Y (en) * 2007-11-13 2008-11-05 重庆工学院 Apparatus for continuously producing short fibre reinforced polymer foaming compound material
CN104236394A (en) * 2014-09-12 2014-12-24 浙江美盾防护技术有限公司 Armor plate, method for manufacturing armor plate and armored equipment
CN211363768U (en) * 2019-11-28 2020-08-28 南京同科科技发展有限公司 Bulletproof equipment core material

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100391710C (en) * 2000-08-08 2008-06-04 莫尔德特有限公司 Composite material with microsphere particles
CN1944500A (en) * 2006-09-28 2007-04-11 湘潭大学 Fiber forced foamed polymer material and its preparing method
CN201143757Y (en) * 2007-11-13 2008-11-05 重庆工学院 Apparatus for continuously producing short fibre reinforced polymer foaming compound material
CN104236394A (en) * 2014-09-12 2014-12-24 浙江美盾防护技术有限公司 Armor plate, method for manufacturing armor plate and armored equipment
CN211363768U (en) * 2019-11-28 2020-08-28 南京同科科技发展有限公司 Bulletproof equipment core material

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Application publication date: 20200324