CN109467726A - Using glass microballoon reinforcing fiber/polymer matrix composites laminate interlaminar strength Enhancement Method - Google Patents

Using glass microballoon reinforcing fiber/polymer matrix composites laminate interlaminar strength Enhancement Method Download PDF

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Publication number
CN109467726A
CN109467726A CN201811202450.3A CN201811202450A CN109467726A CN 109467726 A CN109467726 A CN 109467726A CN 201811202450 A CN201811202450 A CN 201811202450A CN 109467726 A CN109467726 A CN 109467726A
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China
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glass microballoon
glass
laying
resin
polymer matrix
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Pending
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CN201811202450.3A
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Chinese (zh)
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李俭
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Xiamen University
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Xiamen University
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Priority to CN201811202450.3A priority Critical patent/CN109467726A/en
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    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J5/00Manufacture of articles or shaped materials containing macromolecular substances
    • C08J5/24Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08JWORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
    • C08J2363/00Characterised by the use of epoxy resins; Derivatives of epoxy resins
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08KUse of inorganic or non-macromolecular organic substances as compounding ingredients
    • C08K7/00Use of ingredients characterised by shape
    • C08K7/22Expanded, porous or hollow particles
    • C08K7/24Expanded, porous or hollow particles inorganic
    • C08K7/28Glass

Abstract

Using glass microballoon reinforcing fiber/polymer matrix composites laminate interlaminar strength Enhancement Method, it is related to fiber/resin based composites.Method one: manual pasting forming process is the following steps are included: cut fiber cloth by design requirement, by resin and curing agent blending, stirring, deaeration processing;By one layer of fiber cloth paving of cutting in die surface, make thermoplastic resin-impregnated fibers cloth, removes the field trashes such as the bubble in fiber cloth;Glass microballoon is dispensed or is sprayed the fiber cloth surface after dipping;After the completion of glass microballoon is dispensed or sprayed, then it is coated with next layer of fiber cloth, after impregnating resin, then dispenses or spray glass microballoon, until whole laying layings finish.Method two: prepreg/autoclave forming process is the following steps are included: cut prepreg by design requirement;By design laying laying prepreg, glass microballoon is uniformly sprayed between laying, after the completion of sprinkling/laying, through autoclave molding.

Description

Using glass microballoon reinforcing fiber/polymer matrix composites laminate interlaminar strength Enhancement Method
Technical field
The present invention relates to fiber/resin based composites, more particularly, to multiple using glass microballoon reinforcing fiber/resin base The Enhancement Method of condensation material laminate interlaminar strength.
Background technique
Fiber/resin based composites are that the industrial circles such as aerospace, building, ship, Oil & Gas Storage are widely used Structural material has many advantages, such as high-strength light, corrosion-resistant, antifatigue.But fiber/resin base composite material laminated plate interlaminar strength It is low, cause its bending resistance, anti-lateral shear ability poor, improving fiber/resin base composite material laminated plate interlaminar strength is always work One of the target that journey circle is pursued.Mainly there are resin toughening, reinforcement suture, three-dimensional to knit using more interlaminar improvement method at present The methods of object, these method general technology processes are more complicated, higher cost.
Chinese patent CN1718632A discloses a kind of hollow microbead reinforced epoxy resin composite material and preparation method thereof.It presses Parts by weight meter, the component of the composite material include: 100 parts of epoxy resin, 8~100 parts of curing agent, 10~35 parts of diluent, 6~13 parts and 60~130 parts of reinforcing material of coupling agent, reinforcing material is cenosphere.The preparation step of the composite material includes Solidify after screening and pretreatment, the pregel of composite material and the microwave of composite material to cenosphere.
High-performance glass microballon is a kind of powdered ultralight inorganic non-metallic material of hollow ball, by glass microballoon and epoxy Resin-bonded can form foam type composite material, and so as to improve the mechanical property of resin material, the present invention utilizes this principle, It is proposed reinforcing fiber/polymer matrix composites laminate interlaminar strength method.
Summary of the invention
The purpose of the present invention is to provide use glass microballoon to utilize Resin Flow and glass microballoon table for raw material Face capillary principle, method is simple and easy, and convenient to carry out uses glass microballoon reinforcing fiber/polymer matrix composites laminate layer Between intensity Enhancement Method.
The method of the present invention one: manual pasting forming process the following steps are included:
1) fiber cloth is cut by design requirement, resin and curing agent is blended, stirring, deaeration processing;
In step 1), epoxy resin is can be used in the resin, and Epicote 1006A toughening can be used in the epoxy resin The mass ratio of type epoxy resin, resin and curing agent can be 10 ︰ 6, and the deaeration processing can be used vacuum environment case and carry out deaeration Processing.
2) one layer of fiber cloth paving for cutting step 1) makes thermoplastic resin-impregnated fibers cloth in die surface, removes fiber cloth In the field trashes such as bubble;
3) glass microballoon is dispensed or is sprayed the fiber cloth surface after dipping;
It is described that glass microballoon is dispensed or sprayed the fiber cloth surface after dipping in step 3), it can be by glass microballoon By surface density 20g/cm2The fiber cloth surface after dipping is uniformly dispensed or sprays using spraying or spraying equipment;The glass Hollow glass spheres can be used in microballon, and the glass microballoon (3M brand) that the trade mark is S22 can be used in the hollow glass spheres, described 75 μm of the maximum particle diameter of hollow glass spheres;The laminate reinforcement glass fabric, carbon cloth, matrix resin are Epicote1006A toughened epoxy resin;To guarantee that glass microballoon is uniformly distributed in laminated plate face, the spray of profession can be used It spreads or spraying equipment.
4) after the completion of glass microballoon is dispensed or sprayed, then it is coated with next layer of fiber cloth, after impregnating resin, then dispenses or spray Glass microballoon, until whole laying layings finish.
Entire laying/spreading or spraying process need to be completed in resin mobile window, therefore answer that selecting liquidity is good, window Phase longer resin, while laying/spreading or spraying environment temperature cannot be excessively high, avoid the premature gel of resin.In addition, glass Microballon belongs to molecule, is easy to diffuse in air, and operator should wear the protector such as mask, eyeshade.
The method of the present invention two: prepreg/autoclave forming process the following steps are included:
1) prepreg is cut by design requirement;
2) by design laying laying prepreg, glass microballoon is uniformly sprayed between laying, after the completion of sprinkling/laying, Through autoclave molding.
In step 2), the specific method by design laying laying prepreg can are as follows: glass microballoon is pressed surface density 20g/cm2It is uniformly dispensed or is sprayed in prepreg surface using the spraying or spraying equipment of profession;The glass microballoon can be used The glass microballoon (3M brand) that the trade mark is S22 can be used in hollow glass spheres, the hollow glass spheres, and the hollow glass is small 75 μm of the maximum particle diameter of ball.
The present invention uses glass microballoon for raw material, utilizes Resin Flow and glass microballoon surface capillary principle, side Method is simple and easy, convenient to carry out.The laminate of S22 glass microballoon is added to, in solidification process, due to Resin Flow and glass Bead surface capillarity forms polymeric foam thin layer between laminate laying.Method proposed by the invention is suitable for hand Paste moulding process and autoclave forming process.
Detailed description of the invention
Fig. 1 is short beam three point bending test experimental provision schematic diagram.
Fig. 2 is short beam three point bending test test specimen schematic diagram.
Fig. 3 is long beam three point bending test experimental provision schematic diagram.
Fig. 4 is long beam three point bending test test specimen schematic diagram.
Specific embodiment
Following embodiment will the present invention is further illustrated in conjunction with attached drawing.
The method that the embodiment of the present invention is proposed is suitable for manual pasting forming process and autoclave forming process, described to use glass Specific step is as follows for glass microballon reinforcing fiber/polymer matrix composites laminate interlaminar strength Enhancement Method:
To manual pasting forming process, laminate raw material are glass fabric or carbon cloth and matrix resin, matrix tree Rouge is in the majority with epoxy resin.Glass microballoon uses the trade mark for the glass microballoon (3M brand) of S22, and this glass microballoon is a kind of sky Heart glass pellet, 75 μm of maximum particle diameter;When forming composite, by design requirement cut fiber cloth, by the fiber being pre-designed/ Substrate quality is than weighing resin, curing agent (needing addition toughener, colorant etc. when necessary);By resin, curing agent (+toughening Agent etc.) it blends to scale, it is sufficiently stirred, and carry out deaeration processing using vacuum environment case.One layer of fiber cloth paving is existed Die surface, and resin is made to be sufficiently impregnated fiber cloth, pay attention to removing the bubble etc. in fiber cloth and be mingled with, the works such as felt rolling can be used Has assistant soakage;After fiber cloth thorough impregnation, S22 glass microballoon is pressed into surface density 20g/cm2It uniformly dispenses or sprays in dipping Manual spreading can be used if necessary to which molding laminated plate suqare is smaller in fiber cloth surface afterwards, if area is larger, to guarantee Glass microballoon is uniformly distributed in laminated plate face, and spraying or the spraying equipment of profession can be used;After the completion of glass microballoon sprays, then It is coated with next layer of fiber cloth, impregnating resin, then sprays glass microballoon ..., is repeated the above process, until all fibres cloth is coated with It completes.After the completion of being coated with, the lamination order of glass fabric/resin and glass microballoon is as illustrated in fig. 1 and 2.Entire laying/spraying Process need to be completed in resin mobile window, therefore answer that selecting liquidity is good, the longer resin of window phase, while laying/spraying Environment temperature cannot be excessively high, avoids the premature gel of resin.In addition, glass microballoon belongs to molecule, it is easy to diffuse in air In, operator should wear the protector such as mask, eyeshade.
According to prepreg/autoclave forming process, method implementation process is similar with hand paste process, only without impregnating tree Rouge is uniformly sprayed glass microballoon between laying, by design laying laying prepreg through autoclave molding.It is added to S22 glass The laminate of glass microballon, in solidification process, due to Resin Flow and glass microballoon surface capillary, between laminate laying Form polymeric foam thin layer.
Method validation:
By the method for the invention, processing verifying sample, reinforcement uses fiberglass scrim, and specification is surface density 800g/m2;Matrix uses IPKOT 1006A epoxy resin (10 ︰ 6 of resin and curing agent ratio);Reinforcement mass fraction is 55%;Using hand paste process machining composite material plate.
Interlaminar shear strength is measured by short beam bend test, transverse bending strength is measured by long amount bend test.It is short Bending experiment of beam ASTM D2344 [2] standard is carried out, and (experimental standard has for long beam deflection test basis ASTM D790 [3] development Corresponding Chinese national standard is corresponding to it).By experimental standard machining experiment, experimental facilities uses Instron5569 universal testing machine, Experimental situation is interior, dry state, temperature are 24 DEG C, by experimental standard requirement measurement experiment part size.Shear strength experiment uses Short beam three-point bending test (Fig. 1 and 2), specimen thickness d, the long L=6d of testpieces;Width b=2d, test specimen use two o'clock branch Support applies load, supporting point interval Span=4d in two supporting point midpoints;Bending strength experiment uses long beam three-point bending It tests (Fig. 3 and 4), two supporting point span Span=16d, width is about 12.7mm, a length of fulcrum span+20.
Shear strength and bending strength are calculated by following two formula:
Wherein, σSFor interlaminar shear strength;σFFor transverse bending strength;PmSFor peak load in short beam bend test;PmF For the peak load in the 3 points of curved experiments of long beam;D is specimen thickness;B is specimen width;LsBetween the fixed support of long beam deflection Span.
The sample for being not added with and adding glass microballoon is tested respectively, takes the result average value of 5 effective test specimens such as Shown in table 1.
Table 1
Interlaminar shear strength (MPa) Transverse bending strength (MPa)
Add glass microballoon 7.9 74.5
It is not added with glass microballoon 6.3 59.4
The experimental results showed that the bending strength and interlaminar shear strength of laminate are equal after by present invention addition glass microballoon It is significantly improved, it was demonstrated that intensity enhancing method is effective between laminate layer proposed by the invention.

Claims (10)

1. using glass microballoon reinforcing fiber/polymer matrix composites laminate interlaminar strength Enhancement Method, it is characterised in that Manual pasting forming process the following steps are included:
1) fiber cloth is cut by design requirement, resin and curing agent is blended, stirring, deaeration processing;
2) one layer of fiber cloth paving for cutting step 1) makes thermoplastic resin-impregnated fibers cloth in die surface, removes in fiber cloth The field trashes such as bubble;
3) glass microballoon is dispensed or is sprayed the fiber cloth surface after dipping;
4) after the completion of glass microballoon is dispensed or sprayed, then it is coated with next layer of fiber cloth, after impregnating resin, then dispenses or spray glass Microballon, until whole laying layings finish.
2. using the enhancing of glass microballoon reinforcing fiber/polymer matrix composites laminate interlaminar strength as described in claim 1 Method, it is characterised in that in step 1), the resin uses epoxy resin, and Epicote can be used in the epoxy resin 1006A toughened epoxy resin.
3. using the enhancing of glass microballoon reinforcing fiber/polymer matrix composites laminate interlaminar strength as described in claim 1 Method, it is characterised in that in step 1), the mass ratio of the resin and curing agent is 10 ︰ 6.
4. using the enhancing of glass microballoon reinforcing fiber/polymer matrix composites laminate interlaminar strength as described in claim 1 Method, it is characterised in that in step 1), the deaeration processing carries out deaeration processing using vacuum environment case.
5. using the enhancing of glass microballoon reinforcing fiber/polymer matrix composites laminate interlaminar strength as described in claim 1 Method, it is characterised in that it is described that glass microballoon is dispensed or sprayed the fiber cloth surface after dipping in step 3), it is by glass Glass microballon presses surface density 20g/cm2The fiber cloth surface after dipping is uniformly dispensed or sprays using spraying or spraying equipment.
6. using the enhancing of glass microballoon reinforcing fiber/polymer matrix composites laminate interlaminar strength as described in claim 1 Method, it is characterised in that the glass microballoon uses hollow glass spheres, and it is S22's that the trade mark, which can be used, in the hollow glass spheres Glass microballoon, the maximum particle diameter of the hollow glass spheres can be 75 μm;Laminate reinforcement glass fabric, carbon cloth, Epicote 1006A toughened epoxy resin can be used in matrix resin.
7. using glass microballoon reinforcing fiber/polymer matrix composites laminate interlaminar strength Enhancement Method, it is characterised in that Prepreg/autoclave forming process the following steps are included:
1) prepreg is cut by design requirement;
2) by design laying laying prepreg, glass microballoon is uniformly sprayed between laying, after the completion of sprinkling/laying, through heat Press jug forming.
8. using the enhancing of glass microballoon reinforcing fiber/polymer matrix composites laminate interlaminar strength as claimed in claim 7 Method, it is characterised in that in step 2), described press designs laying laying prepreg method particularly includes: glass microballoon is pressed face Density 20g/cm2It is uniformly dispensed or is sprayed in prepreg surface using the spraying or spraying equipment of profession.
9. using the enhancing of glass microballoon reinforcing fiber/polymer matrix composites laminate interlaminar strength as claimed in claim 7 Method, it is characterised in that in step 2), the glass microballoon uses hollow glass spheres, and the hollow glass spheres can be used The trade mark is the glass microballoon of S22.
10. using the enhancing of glass microballoon reinforcing fiber/polymer matrix composites laminate interlaminar strength as claimed in claim 9 Method, it is characterised in that in step 2), the maximum particle diameter of the hollow glass spheres is 75 μm.
CN201811202450.3A 2018-10-16 2018-10-16 Using glass microballoon reinforcing fiber/polymer matrix composites laminate interlaminar strength Enhancement Method Pending CN109467726A (en)

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110077051A (en) * 2019-04-18 2019-08-02 河南泛锐复合材料研究院有限公司 A kind of preparation method for bulletproof armour plate interlayer composite material
CN110626020A (en) * 2019-08-06 2019-12-31 衢州艾科科技有限公司 Polyurethane reinforced composite material and preparation method thereof
CN112318953A (en) * 2020-11-03 2021-02-05 广东航科新材料有限公司 Large-width high-surface-appearance-quality plate structure and preparation method thereof
CN113059869A (en) * 2021-03-25 2021-07-02 沈阳航空航天大学 Glass fiber laminated plate with pre-buried carbon powder reinforced medium and preparation method thereof
CN113321913A (en) * 2021-06-15 2021-08-31 威驰腾(福建)汽车有限公司 Carbon fiber cotton composite material and preparation method thereof
CN113462125A (en) * 2021-07-14 2021-10-01 巩义市泛锐熠辉复合材料有限公司 Resin foam preform, member made of resin foam preform, and method for producing the same
CN113943471A (en) * 2021-11-04 2022-01-18 成都鲁晨新材料科技有限公司 Low-density prepreg, preparation method and application

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102482438A (en) * 2009-09-04 2012-05-30 赫克塞尔合成有限公司 Improvements in composite materials
CN103249776A (en) * 2010-12-22 2013-08-14 氰特科技股份有限公司 Epoxy resin system containing insoluble and partially soluble or swellable toughening particles for use in prepreg and structural component applications
CN103764393A (en) * 2011-08-29 2014-04-30 氰特科技股份有限公司 Interlaminar toughening of thermoplastics
CN104023979A (en) * 2011-12-23 2014-09-03 东丽株式会社 Prepreg, Fiber Reinforced Composite Material, And Manufacturing Method For Fiber Reinforced Composite Material
CN104356605A (en) * 2014-12-11 2015-02-18 哈尔滨广龙通用航空科技有限公司 Light prepreg for unmanned aerial vehicle shell and preparation method of prepreg
CN105813833A (en) * 2013-12-13 2016-07-27 塞特工业公司 Composite materials with electrically conductive and delamination resistant properties
CN106147227A (en) * 2015-04-09 2016-11-23 深圳光启创新技术有限公司 A kind of high-frequency copper-clad plate, prepreg and preparation method thereof
CN107107537A (en) * 2014-09-22 2017-08-29 塞特工业公司 Composite with high Z-direction electrical conductivity
CN107266694A (en) * 2010-05-27 2017-10-20 赫克塞尔合成有限公司 Structural thermoplastic's material in composite material interlayer

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102482438A (en) * 2009-09-04 2012-05-30 赫克塞尔合成有限公司 Improvements in composite materials
CN107266694A (en) * 2010-05-27 2017-10-20 赫克塞尔合成有限公司 Structural thermoplastic's material in composite material interlayer
CN103249776A (en) * 2010-12-22 2013-08-14 氰特科技股份有限公司 Epoxy resin system containing insoluble and partially soluble or swellable toughening particles for use in prepreg and structural component applications
CN103764393A (en) * 2011-08-29 2014-04-30 氰特科技股份有限公司 Interlaminar toughening of thermoplastics
CN104023979A (en) * 2011-12-23 2014-09-03 东丽株式会社 Prepreg, Fiber Reinforced Composite Material, And Manufacturing Method For Fiber Reinforced Composite Material
CN105813833A (en) * 2013-12-13 2016-07-27 塞特工业公司 Composite materials with electrically conductive and delamination resistant properties
CN107107537A (en) * 2014-09-22 2017-08-29 塞特工业公司 Composite with high Z-direction electrical conductivity
CN104356605A (en) * 2014-12-11 2015-02-18 哈尔滨广龙通用航空科技有限公司 Light prepreg for unmanned aerial vehicle shell and preparation method of prepreg
CN106147227A (en) * 2015-04-09 2016-11-23 深圳光启创新技术有限公司 A kind of high-frequency copper-clad plate, prepreg and preparation method thereof

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110077051A (en) * 2019-04-18 2019-08-02 河南泛锐复合材料研究院有限公司 A kind of preparation method for bulletproof armour plate interlayer composite material
CN110626020A (en) * 2019-08-06 2019-12-31 衢州艾科科技有限公司 Polyurethane reinforced composite material and preparation method thereof
CN110626020B (en) * 2019-08-06 2021-12-14 衢州艾科科技有限公司 Polyurethane reinforced composite material and preparation method thereof
CN112318953A (en) * 2020-11-03 2021-02-05 广东航科新材料有限公司 Large-width high-surface-appearance-quality plate structure and preparation method thereof
CN113059869A (en) * 2021-03-25 2021-07-02 沈阳航空航天大学 Glass fiber laminated plate with pre-buried carbon powder reinforced medium and preparation method thereof
CN113059869B (en) * 2021-03-25 2022-11-04 沈阳航空航天大学 Glass fiber laminated plate with pre-buried carbon powder reinforced medium and preparation method thereof
CN113321913A (en) * 2021-06-15 2021-08-31 威驰腾(福建)汽车有限公司 Carbon fiber cotton composite material and preparation method thereof
CN113321913B (en) * 2021-06-15 2022-11-08 威驰腾(福建)汽车有限公司 Carbon fiber cotton composite material and preparation method thereof
CN113462125A (en) * 2021-07-14 2021-10-01 巩义市泛锐熠辉复合材料有限公司 Resin foam preform, member made of resin foam preform, and method for producing the same
CN113943471A (en) * 2021-11-04 2022-01-18 成都鲁晨新材料科技有限公司 Low-density prepreg, preparation method and application

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