CN108659462A - A kind of self-repair type can remold the multiple deformation thermoset shape memory resin material of shape - Google Patents

A kind of self-repair type can remold the multiple deformation thermoset shape memory resin material of shape Download PDF

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CN108659462A
CN108659462A CN201810368792.6A CN201810368792A CN108659462A CN 108659462 A CN108659462 A CN 108659462A CN 201810368792 A CN201810368792 A CN 201810368792A CN 108659462 A CN108659462 A CN 108659462A
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shape
self
remold
shape memory
deformation
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CN108659462B (en
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袁莉
丁振杰
顾嫒娟
梁国正
管清宝
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Suzhou University
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    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08LCOMPOSITIONS OF MACROMOLECULAR COMPOUNDS
    • C08L63/00Compositions of epoxy resins; Compositions of derivatives of epoxy resins
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G59/00Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
    • C08G59/18Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
    • C08G59/40Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the curing agents used
    • C08G59/42Polycarboxylic acids; Anhydrides, halides or low molecular weight esters thereof
    • C08G59/4207Polycarboxylic acids; Anhydrides, halides or low molecular weight esters thereof aliphatic
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    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G59/00Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
    • C08G59/18Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
    • C08G59/40Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the curing agents used
    • C08G59/42Polycarboxylic acids; Anhydrides, halides or low molecular weight esters thereof
    • C08G59/4215Polycarboxylic acids; Anhydrides, halides or low molecular weight esters thereof cycloaliphatic
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    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G59/00Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
    • C08G59/18Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
    • C08G59/40Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the curing agents used
    • C08G59/50Amines
    • C08G59/56Amines together with other curing agents
    • C08G59/58Amines together with other curing agents with polycarboxylic acids or with anhydrides, halides, or low-molecular-weight esters thereof
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    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G59/00Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
    • C08G59/18Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
    • C08G59/68Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the catalysts used
    • C08G59/70Chelates
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    • C08G73/00Macromolecular compounds obtained by reactions forming a linkage containing nitrogen with or without oxygen or carbon in the main chain of the macromolecule, not provided for in groups C08G12/00 - C08G71/00
    • C08G73/06Polycondensates having nitrogen-containing heterocyclic rings in the main chain of the macromolecule
    • C08G73/10Polyimides; Polyester-imides; Polyamide-imides; Polyamide acids or similar polyimide precursors
    • C08G73/12Unsaturated polyimide precursors
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    • C08LCOMPOSITIONS OF MACROMOLECULAR COMPOUNDS
    • C08L63/00Compositions of epoxy resins; Compositions of derivatives of epoxy resins
    • C08L63/04Epoxynovolacs
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    • C08L2201/00Properties
    • C08L2201/12Shape memory

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Abstract

The invention discloses a kind of self-repair types can remold the multiple deformation thermoset shape memory resin material of shape, mainly using bismaleimide, aromatic diamine, epoxy resin, dibasic acid anhydride and transesterification accelerating agent as raw material, bimaleimide resin progress chain elongation is reacted by aromatic diamine after forming linear oligomer, epoxy resin, accelerating agent and dibasic acid anhydride are added, a kind of the multiple deformation thermoset shape memory material of shape is remolded with self-repair function through what certain heat curing process was handled.Material prepared by the present invention can not only be remolded as new shape, and deformation recovery, which recycles, still good shape memory effect for 5 times or more, and prepared material, with good self-reparing capability, fracture toughness remediation efficiency reaches 62% or more.Therefore, prepared material has a wide range of applications potentiality in high performance structures function integration material.

Description

A kind of self-repair type can remold the multiple deformation thermoset shape memory resin material of shape
The present invention, which is a kind of entitled self-repair type, can remold the multiple deformation thermoset shape memory resin material of shape And preparation method thereof, the applying date be on December 12nd, 2016, application No. is the divisional application of 201611141129X patents of invention, Belong to product section.
Technical field
The invention belongs to the technical field of shape memory function high-performance resin matrix, be related to it is a kind of have review one's lessons by oneself reactivation Power can remodelled shape multiple deformation thermoset shape memory resin system.
Background technology
Shape-memory polymer(SMPs)It is a kind of unique stimulation-responsive polymer, shape can be with sequencing formula Temporary shapes are fixed into, and under specific environmental stimuli, are returned to original original shape.SMPs can be autonomous as one kind The intellectual material of deformation has the advantages such as lightweight, at low cost, easy processing, change in shape are easy to control, transition temperature is easily adjusted.Make For thermosetting property SMPs, there is superior mechanical property, higher thermal transition temperature and preferably resistance to than thermoplasticity SMPs Hot property and thermal stability, being played in space self-deploys the aerospace fields such as structural member, variable geometry aircraft can not The effect of replacement.Therefore, the high-performance thermosetting SMPs of novel structure-function integration is developed to widening SMPs potential applications With great research significance.
But common thermosetting property SMPs can only remember a temporary shapes at present, then be returned to permanent shape, i.e., dual shape Shape memory effect(It is included in original-shape).This dual-shaped memory variation is using network cross-linked point as stationary phase, between crosslinking points For strand as reversible deformation phase, deformation is the change of the chain conformation based on reversible deformation phase.Thermosetting property SMPs change in shape letters The deficiencies of list, non-programmable deformation, significantly limits its application in emerging technology areas, and the thermosetting of thermal response deformation Property SMPs in repeating heat treatment process, memory cycle bad stability, deformation cycle-index is limited.And contain multiple temperature Although degree transformation or the SMPs of wide scope temperature transition can remember various shapes, only dual-shaped memory effect Superposition, can not realize the reconstruct or remodeling of material shape, cannot be satisfied the reply deformation of two dimension or three dimensions complicated shape. Moreover when being on active service in complex environment, SMPs materials inevitably result from micro-crack equivalent damage, lead to the mechanical property of material It can considerable decrease and shortening materials'use service life and safety.Therefore, prepare have service life can grow and it is safe can The multiple deformation thermoset shape memory resin system of remodelled shape has positive effect.
Invention content
The purpose of the present invention is be directed to current thermoset shape memory resin cannot again it is moulding, cannot effectively realize it is multiple It miscellaneous shape distortion and and the problems such as will appear micro-cracks damage in use, proposes a kind of with Crack Self function Can remodelled shape multiple deformation thermoset shape memory resin system and preparation method thereof.
In order to achieve the above objectives, the technical solution adopted by the present invention is, a kind of self-repair type can remold the multiple deformation heat of shape The preparation method of solidity shape memory resin material, includes the following steps:Bismaleimide and amine compounds are reacted, obtained Oligomer;Then oligomer is added in epoxy resin, adds accelerating agent;Then acid anhydrides is added, obtains prepolymerization system;Pre-polymerization System obtains self-repair type by heat cure can remold the multiple deformation thermoset shape memory resin material of shape.
In above-mentioned technical proposal, the bismaleimide, amine compounds, epoxy resin, accelerating agent, acid anhydrides mass ratio For(5~25)∶(4~18)∶(75~120)∶(12~18)∶(4~8).
In above-mentioned technical proposal, the bismaleimide includes dimaleoyl imino diphenyl-methane, bismaleimide Two methyl phenyl ethers anisole of amido;The amine compounds are diamine compound;The epoxy resin includes bisphenol A type epoxy resin, Bisphenol F Type epoxy resin, hydrogenated epoxy resin, novolac epoxy resin, organosilicon epoxy resin, fire retarding epoxide resin;The accelerating agent is Metal salt;The acid anhydrides is dibasic acid anhydride.
Preferably, the diamine is aromatic diamine or aliphatic diamine, such as diaminodiphenylmethane, two It is aminodiphenyl sulfone, diaminodiphenyl ether, double(4- amino -3- methylcyclohexyls)Methane, benzidine;The dibasic acid anhydride is Aromatic dicarboxylic anhydride or binary aliphatic acid anhydrides, such as dibasic acid anhydride include phthalic anhydride, hexahydrophthalic acid Acid anhydride, glutaric anhydride, adipic anhydride, dodecenylsuccinic acid acid anhydride, methylcyclohexene tetracid dianhydride, methylnadic anhydride;It is described Metal salt includes the metal salt of zinc, tin, magnesium, calcium, such as zinc acetylacetonate, zinc acetate, calcium acetate, magnesium acetate, tin dilaurate two Butyl tin.
In above-mentioned technical proposal, the preferably described bismaleimide and amine compounds react in a solvent;The span comes The condition that acid imide and amine compounds react in a solvent is 55~110 DEG C and reacts 8~15 hours;After removing solvent, obtain low Polymers.Solvent is specially that can disperse solvent, such as ketones solvent of bismaleimide and amine compounds etc., after reaction, is done It is oligomer that dry or revolving, which removes solvent and obtains solid,;Solvent, bismaleimide and amine compounds can not also be used Frit reaction, reaction controllability is poor under the conditions of this, is unfavorable for industrialized production, the preferred bismaleimide of the present invention and amination Object is closed to react in the presence of a solvent.
In above-mentioned technical proposal, oligomer is added in epoxy resin, accelerating agent is added after 90~110 DEG C of mixing;Institute The temperature for stating heat cure is 100~180 DEG C, and the time is 8~15 hours, it is preferred to use staged curing technique.
Preferably, after acid anhydrides being added, prepolymerization system is obtained, addO-on therapy is added, then carries out heat cure;The addition Component includes cyanate ester resin, phenolic resin, organic siliconresin, furane resins;The additive amount of the addO-on therapy is performed polymer It is the 5~10% of quality;By the addition of addO-on therapy, the comprehensive performance of material can be improved.
The present invention further discloses can remold the multiple deformation thermoset shape memory resin of shape according to above-mentioned self-repair type Self-repair type prepared by the preparation method of material can remold the multiple deformation thermoset shape memory resin material of shape.With following skill Art effect:
(1)Material shape can be remolded automatically as new shape, for example plane vertical bar pattern product after molding are at high temperature(180~200 ℃)It is fixed-type inverted U-shaped to stand, in control temperature(20 DEG C about more than glass transition temperature)Under, it is inverted U-shaped to revert to straight After can be bent upwards automatically as stand it is just U-shaped.
(2)Material deformation recovery cycles, can show very stable shape Memory performance, deformation fixed rate is close to 100%.
(3)Material has the function of the micro-crack that heals automatically, and Crack healing efficiency is up to 62% or more.
(4)Material has excellent heat resistance, glass transition temperature(DMA methods)At 110 DEG C~140 DEG C.
The invention also discloses the systems that a kind of self-repair type can remold the multiple deformation thermoset shape memory resin system of shape Preparation Method includes the following steps:Bismaleimide and amine compounds are reacted, oligomer is obtained;Then oligomer is added In epoxy resin, accelerating agent is added;Then acid anhydrides is added, the multiple deformation thermosetting property shape note of shape can be remolded by obtaining self-repair type Recall resin system;The bismaleimide, amine compounds, epoxy resin, accelerating agent, acid anhydrides mass ratio be(5~25)∶(4 ~18)∶(75~120)∶(12~18)∶(4~8).
Preferably, after acid anhydrides being added, prepolymerization system is obtained, addO-on therapy is added, then carries out heat cure;The addition Component includes cyanate ester resin, phenolic resin, organic siliconresin, furane resins;The additive amount of the addO-on therapy is performed polymer It is the 5~10% of quality;By the addition of addO-on therapy, the comprehensive performance of material can be improved.
It is that epoxy-functional is generated with acid anhydrides respectively there are two kinds of crosslinking points stationary phases in Inventive polymers cross-linked network Transesterification key and epoxy-functional and amine curing after crosslinking points.In the present invention, when reaching material glass transition temperature On when, the motility enhancing of chain, the reversible deformation between crosslinking points is mutually the basis of shape memory.When temperature is increased to ester bond Exchange reaction temperature(180~200 DEG C), dynamic ester bond fast exchange reaches balance, and the topological structure of cross-linked network changes, Internal stress relaxes, and temporary shapes for good and all can be fixed up, realize that the reconstruct or remodeling of material shape equally work as material When micro-crack occurs in inside, the fast exchange based on the strand containing ester bond can repair fine fisssure, bond crack surface.
Compared with prior art, the invention has the advantages that:
1. self-repair type disclosed by the invention can remold the multiple deformation thermoset shape memory resin material use dynamic ester of shape and hand over The characteristic for changing key, may be implemented the reconstruct etc. to cross-linked network molecular structure, and strand is under catalyst existence condition and appropriate Under temperature control, exchange reaction can occur and reach dynamic equilibrium, important technical advantage is:Material shape can be remolded automatically New shape, according to embodiments of the present invention, plane vertical bar pattern product after molding are fixed-type for the U that stands in transesterification temperature Shape, in control temperature(It is more than glass transition temperature)Under, then by it is inverted U-shaped be fixed into it is just U-shaped, at this time will be just U-shaped in material glass When being handled on glass transition temperature, will first revert back to can be bent upwards automatically after straight it is just U-shaped as standing;Material deformation returns Multiple cycle-index is more, after 5 loop tests, can show very stable shape-memory properties, compared with initial deformation, shape Become fixed rate and is more than 82% close to 100% and response rate;Material has the function of the micro-crack that heals automatically, and Crack healing efficiency is up to 62% More than.
2. self-repair type disclosed by the invention can remold the multiple deformation thermoset shape memory resin material of shape compared to biography The shape memory thermosets of system, not only in a short time(In 20 seconds)Can fast implement three-dimensional structure part it is automatic at Type, deformation-reply 5 times or more remains to keep good shape-memory properties, and has good crack forming mechanism ability, improves The stability in use of material, in addition, the excellent heat resistance of the more traditional thermoset shape memory material of material prepared by the present invention, Glass transition temperature(DMA methods)At 110 DEG C~140 DEG C.
3. self-repair type disclosed by the invention can remold the preparation side of the multiple deformation thermoset shape memory resin material of shape Method technique is controllable, and raw material composition is reasonable, especially under Additive, can obtain more excellent comprehensive performance;It prepares Process does not have particular/special requirement, is conducive to industrial applications.
Description of the drawings
Fig. 1 is ester exchange reaction and crack forming mechanism mechanism figure;
Fig. 2 is the memory cycle curve graph of 1 material of embodiment;
Fig. 3 is 1 material of embodiment in 180 DEG C of shape deformation recovery remodeling-time diagrams;
Fig. 4 is the memory cycle curve graph of 2 material of embodiment;
Fig. 5 is 2 material of embodiment in 160 DEG C of shape deformation recovery remodeling-time diagrams;
Fig. 6 is 5 cyclic curve figures of shape memory of 3 material of embodiment;
Fig. 7 is 3 material of embodiment in 180 DEG C of shape deformation recovery remodeling-time diagrams.
Specific implementation mode
Embodiment 1
In equipped with cooling and reflux device, by 5g dimaleoyl iminos diphenyl-methane (BMI) and 4g4,4'- diamino hexichol After sulfone is dissolved in acetone, under stirring condition, control temperature 60 C reacts 12h, by solution after rotary evaporation removes acetone solvent, 70 DEG C of vacuum drying 12h obtain bismaleimide/aromatic dicarboxylic amine oligomer powder.Oligomer is added to 75g epoxies Resin(E-54)In, after 100 DEG C are melt into clear solution, 4g accelerating agent zinc acetylacetonates, stir about 3 minutes is added, then add Enter 12g glutaric anhydrides, after being quickly uniformly mixed, be poured into flat plate mold, curing process is pressed after 110 DEG C of vacuum defoamations 110 DEG C/1h+140 DEG C/8h+160 DEG C/2h processing takes out curing materials after natural cooling.
Fig. 1 is ester exchange reaction and crack forming mechanism mechanism figure, and in material of the invention, strand is in catalyst existence condition Under the control of lower and proper temperature, exchange reaction, which can occur, reaches dynamic equilibrium, when micro-crack occurs in material internal, based on ester-containing The fast exchange of key strand can repair fine fisssure, bond crack surface.
Fig. 2 is the memory cycle curve of above-mentioned material(Dynamic thermomechanical is analyzed(DMA)Test).The material of preparation Glass transition temperature is 110 DEG C, and sample is first heated on 130 DEG C;Then sample stretches under external force, continues 2min, then rate be cooled to room temperature, the length of sample is denoted as at this timeε load;External force then is removed, at this time the length note of sample Forε unload ;Then sample is reheated to 130 DEG C or more and triggers recovery of shape, and the length reduction of sample at this time is denoted asε rec .Shape Shape fixed rate(R f )And shape recovery rate(R r )It is calculated using following formula:
In the present embodiment, first deformation fixed rate be 95%, first deformation-recovery rate 76%, undergo 5 times cycle, maximum deformation quantity from 10.48% changes to 10.36%, and largest deformation is maintain initial deformation 98.8%;5 cycles of experience, the deformation quantity of recovery of shape 2.82% is changed to from 2.42%, deformation quantity maintains 83.5%, embodies good shape deformation and recovery cycles stability.Material The heat decomposition temperature of 5wt% weightlessness(Thermal weight loss(TGA)Method)It is 386 DEG C, initial collapse toughness(K ICorginal )For:1.45MPa.m1 /2, fracture specimens are through 200 DEG C of processing 1h, fracture toughness after crack surface healing(K IChealed )For:1.1MPa.m1/2, crack healing effect Rate(K IChealed / K ICorginal )It is 76%.
Fig. 3 is material plane vertical bar pattern product after molding in transesterification temperature(180℃)Fixed-type is the U that stands Shape, 150 DEG C again by it is inverted U-shaped be fixed into it is just U-shaped, in 180 DEG C of shape deformation recovery remodeling-time diagrams.It can be seen from the figure that When the just U-shaped sample that will stand is handled at 180 DEG C, material can be bent downwardly after first reverting back to straight as standing inverted U, material automatically Material can Quick-return remodelled shape in 13 seconds.
Embodiment 2
In equipped with cooling and reflux device, by 13g dimaleoyl iminos diphenyl-methane (BMI) and 9g4,4'- diamino two After benzene sulfone is dissolved in acetone, under stirring condition, control temperature 70 C reacts 12h, and solution is removed acetone solvent through rotary evaporation Afterwards, 70 DEG C of vacuum drying 12h obtain bismaleimide/aromatic dicarboxylic amine oligomer powder.Oligomer is added to 100g Epoxy resin(E-51)In, after 100 DEG C are melt into clear solution, 6.7g accelerating agent zinc acetylacetonates are added, stir about 3 divides Clock adds 15g glutaric anhydrides, after being quickly uniformly mixed, is poured into flat plate mold, is pressed after 110 DEG C of vacuum defoamations Curing process 110 DEG C/1h+140 DEG C/8h+160 DEG C/2h processing takes out curing materials after natural cooling.
Fig. 4 is the memory cycle curve of 2 material of embodiment(DMA is tested).The glass transition temperature of the material of preparation Degree is 128 DEG C, and sample is first heated on 150 DEG C;Then sample stretches under external force, continues 2min, then rate It is cooled to room temperature, the length of sample is denoted as at this timeε load;External force then is removed, the length of sample is at this timeε unload ;Then sample It is reheated to 150 DEG C or more and triggers recovery of shape, the length of sample is reduced at this timeε rec .In the present embodiment, first shape is fixed Rate is 96%, shape recovery rate 79%, undergoes 5 cycles, and maximum deformation quantity changes to 10.67% from 10.84%, and largest deformation is dimension It holds the 98.4% of initial deformation;5 cycles of experience, the deformation quantity of recovery of shape change to 2.75% from 2.36%, and deformation quantity maintains 83.5%, embody good shape deformation and recovery cycles stability.The heat decomposition temperature of material 5wt% weightlessness(TGA methods)For 371 DEG C, initial collapse toughness(K ICorginal )For:1.59MPa.m1/2, fracture specimens are through 200 DEG C of processing 1h, after crack surface healing Fracture toughness(K IChealed )For:1.1MPa.m1/2Crack healing efficiency(K IChealed / K ICorginal )It is 69%.
Fig. 5 is above-mentioned material plane vertical bar pattern product after molding in transesterification temperature(180℃)Fixed-type is to stand It is inverted U-shaped, at 150 DEG C, then by it is inverted U-shaped be fixed into it is just U-shaped after in 160 DEG C of shape deformation recovery remodeling-time diagrams.It can from figure To find out, when just U-shaped sample is handled at 160 DEG C, can be bent upwards automatically as just U-shaped, material of standing after first reverting back to straight In 19 seconds can Quick-return it is again moulding.
Embodiment 3
In equipped with cooling and reflux device, by two methyl phenyl ethers anisole of 25g dimaleoyl iminos and 18g4,4'- diaminodiphenyl ether After being dissolved in acetone, under stirring condition, control temperature 70 C reacts 12h, by solution after rotary evaporation removes acetone solvent, 70 DEG C vacuum drying 12h obtain bismaleimide/aromatic dicarboxylic amine oligomer powder.Oligomer is added to 120g phenol aldehyde types Epoxy resin(F-51)In, after 100 DEG C are melt into clear solution, addition 8g accelerating agent zinc acetylacetonates, stir about 5 minutes, 18g hexahydrophthalic anhydrides are added, after being quickly uniformly mixed, are poured into flat plate mold, in 110 DEG C of vacuum defoamations Afterwards by curing process 110 DEG C/1h+140 DEG C/8h+160 DEG C/2h processing, curing materials are taken out after natural cooling.
Fig. 6 is the memory cycle curve of above-mentioned material(DMA is tested).The glass transition temperature of the material of preparation is 130 DEG C, sample is first heated on 150 DEG C;Then sample stretches under external force, continues 2min, and then rate cools down To room temperature, the length of sample is denoted as at this timeε load;External force then is removed, the length of sample is at this timeε unload ;Then sample is again It is heated to 150 DEG C or more and triggers recovery of shape, the length of sample is reduced at this timeε rec .In the present embodiment, first shape fixed rate is 92%, shape recovery rate 76% undergoes 5 cycles, and largest deformation is maintain initial deformation 98.3%;5 cycles of experience, Maximum deformation quantity changes to 7.53% from 7.66%, and the deformation quantity of recovery of shape changes to 2.03% from 1.72%, and deformation quantity maintains 82%, Embody good shape deformation and recovery cycles stability.The heat decomposition temperature of material 5wt% weightlessness(TGA methods)It is 283 DEG C, Initial collapse toughness(K ICorginal )For:1.76MPa.m1/2, through 200 DEG C of processing 1h, crack surface is broken tough fracture specimens after healing Property(K IChealed )For:1.35MPa.m1/2Crack healing efficiency(K IChealed / K ICorginal )It is 77%.
Fig. 7 is 3 material of embodiment plane vertical bar pattern product after molding in transesterification temperature(180℃)Fixed-type is station It is vertical inverted U-shaped, 150 DEG C again by it is inverted U-shaped be fixed into it is just U-shaped, can be with from figure in 180 DEG C of shape deformation recovery remodeling-time diagrams Find out, when the just U-shaped sample that will stand is handled at 180 DEG C, material can be bent downwardly after first reverting back to straight as the U that stands automatically Type, material in 21 seconds can Quick-return it is again moulding.
Embodiment 4
Two methyl phenyl ethers anisole of 20g dimaleoyl iminos and 15g is bis-(4- amino -3- methylcyclohexyls)Methane under agitation, Frit reaction 4h obtains bismaleimide/binary amine oligomer powder.Oligomer is added to 100g hydrogenated bisphenol A epoxies In resin, after 110 DEG C are melt into clear solution, 7g accelerating agent zinc acetylacetonates are added, stir about 10 minutes adds 13g Hexahydrophthalic anhydride after being quickly uniformly mixed, is poured into flat plate mold, by solidification work after 90 DEG C of vacuum defoamations Skill 100 DEG C/1h+130 DEG C/10h+150 DEG C/4h processing, takes out curing materials after natural cooling, Crack healing efficiency 62%, Glass transition temperature is 116 DEG C, and after five cycles (DMA methods, test method is with embodiment 1), largest deformation is to maintain just The 98.9% of beginning deformation;5 cycles of experience, deformation quantity maintain 85%.
Embodiment 5
In equipped with cooling and reflux device, by two methyl phenyl ethers anisole of 25g dimaleoyl iminos and 14g4,4'- diaminodiphenyl ether After being dissolved in acetone, under stirring condition, solution is obtained bismaleimide/virtue by back flow reaction 8h after drying and removing solvent Fragrant race's binary amine oligomer powder.Oligomer is added in 90g phosphorous epoxy resins, after 90 DEG C are melt into clear solution, 5g accelerating agent zinc acetylacetonates are added, 12g methylcyclohexene tetracid dianhydrides are added under stirring, after being quickly uniformly mixed, Be poured into flat plate mold, after 90 DEG C of vacuum defoamations by 110 DEG C/2h+140 DEG C/5h+160 DEG C/3h of curing process at It manages, curing materials, Crack healing efficiency 69% is taken out after natural cooling, glass transition temperature is 135 DEG C, after five cycles (DMA methods, test method is with embodiment 1), largest deformation are maintain initial deformation 98.5%;5 cycles of experience, deformation quantity Maintain 84%.
Embodiment 6
In equipped with cooling and reflux device, two methyl phenyl ethers anisole of 20g dimaleoyl iminos and 6g benzidines are dissolved in acetone In after, under stirring condition, it is oligomeric to be obtained after drying and removing solvent bismaleimide/diamine by 55 DEG C of reaction 15h for solution Object powder.Oligomer is added in 110g organosilicon epoxy resins, after 90 DEG C are melt into clear solution, 6g accelerating agents are added Zinc acetylacetonate, stir about 20 minutes, adds 17g methylnadic anhydrides, after being quickly uniformly mixed, is poured into tablet In mold, by curing process 110 DEG C/2h+150 DEG C/6h+180 DEG C/1h processing, natural cooling after 90 DEG C of vacuum defoamations After take out curing materials, Crack healing efficiency 64%, glass transition temperature is 129 DEG C, (DMA methods, test side after five cycles Method is with embodiment 1), largest deformation is maintain initial deformation 99%;5 cycles of experience, deformation quantity maintain 85%.
Embodiment 7
In equipped with cooling and reflux device, by two methyl phenyl ethers anisole of 25g dimaleoyl iminos and 18g4,4'- diaminodiphenyl ether After being dissolved in cyclohexanone, under stirring condition, 110 DEG C of reaction 10h of control temperature, by solution after rotary evaporation removes solvent, 70 DEG C vacuum drying 12h obtain bismaleimide/aromatic dicarboxylic amine oligomer powder.Oligomer is added to 120g phenol aldehyde types Epoxy resin(F-51)In, after 100 DEG C are melt into clear solution, addition 8g accelerating agent zinc acetylacetonates, stir about 5 minutes, 18g hexahydrophthalic anhydrides are added, after being quickly uniformly mixed, add 18.9g cyanate ester resins(Bisphenol-A type cyanogen Acid ester resin), stirring is poured into after cyanate dissolving in flat plate mold, by curing process 110 after 110 DEG C of vacuum defoamations DEG C/1h+140 DEG C/8h+160 DEG C/2h processing, curing materials are taken out after natural cooling.Measure Crack healing efficiency 81%, glass Glass transition temperature is 139 DEG C, the heat decomposition temperature of material 5wt% weightlessness(TGA methods)It is 298 DEG C, after five cycles (DMA methods, Test method is with embodiment 3), largest deformation is maintain initial deformation 98%;5 cycles of experience, deformation quantity maintain 82.4%, embody good shape deformation and recovery cycles stability.
Embodiment 8
In equipped with cooling and reflux device, by 5g dimaleoyl iminos diphenyl-methane (BMI) and 4g4,4'- diamino hexichol After sulfone is dissolved in acetone, under stirring condition, control temperature 60 C reacts 12h, by solution after rotary evaporation removes acetone solvent, 70 DEG C of vacuum drying 12h obtain bismaleimide/aromatic dicarboxylic amine oligomer powder.Oligomer is added to 75g epoxies Resin(E-54)In, after 100 DEG C are melt into clear solution, 4g accelerating agent zinc acetylacetonates, stir about 3 minutes is added, then add Enter 12g glutaric anhydrides, after being quickly uniformly mixed, then adds 5g organic siliconresins(Model 9502), quickly it is poured into after stirring It is natural by curing process 110 DEG C/1h+140 DEG C/8h+160 DEG C/2h processing after 110 DEG C of vacuum defoamations in flat plate mold Curing materials are taken out after cooling.Crack healing efficiency 71% is measured, glass transition temperature is 126 DEG C, the heat of material 5wt% weightlessness Decomposition temperature(TGA methods)It it is 393 DEG C, five times cycle can restore original-shape 98%.(DMA methods, test method are same after five cycles Embodiment 1), largest deformation is maintain initial deformation 98.1%;5 cycles of experience, deformation quantity maintain 82%, embody good Good shape deformation and recovery cycles stability.

Claims (8)

1. a kind of self-repair type can remold the multiple deformation thermoset shape memory resin material of shape, which is characterized in that described to review one's lessons by oneself The preparation method that replica can remold the multiple deformation thermoset shape memory resin material of shape includes the following steps:By bismaleimide Amine and amine compounds reaction, obtain oligomer;Then oligomer is added in epoxy resin, adds accelerating agent;Then it is added Acid anhydrides obtains prepolymerization system;Prepolymerization system obtains self-repair type by heat cure can remold the multiple deformation thermosetting property shape note of shape Recall resin material.
2. self-repair type can remold the multiple deformation thermoset shape memory resin material of shape, feature according to claim 1 Be, the bismaleimide, amine compounds, epoxy resin, accelerating agent, acid anhydrides mass ratio be(5~25)∶(4~18)∶ (75~120)∶(12~18)∶(4~8).
3. self-repair type can remold the multiple deformation thermoset shape memory resin material of shape, feature according to claim 1 It is, the bismaleimide includes dimaleoyl imino diphenyl-methane, two methyl phenyl ethers anisole of dimaleoyl imino;The amine Compound is diamine compound;The epoxy resin includes bisphenol A type epoxy resin, bisphenol f type epoxy resin, hydrogenated epoxy Resin, novolac epoxy resin, organosilicon epoxy resin, fire retarding epoxide resin;The accelerating agent is metal salt;The acid anhydrides is two First acid anhydrides.
4. self-repair type can remold the multiple deformation thermoset shape memory resin material of shape, feature according to claim 3 It is, the diamine is aromatic diamine or aliphatic diamine;The dibasic acid anhydride be aromatic dicarboxylic anhydride or Person's binary aliphatic acid anhydrides;The metal salt includes the metal salt of zinc, tin, magnesium, calcium.
5. self-repair type can remold the multiple deformation thermoset shape memory resin material of shape, feature according to claim 4 It is, the diamine includes diaminodiphenylmethane, diaminodiphenylsulfone, diaminodiphenyl ether, double(4- amino -3- methyl Cyclohexyl)Methane, benzidine;The dibasic acid anhydride includes phthalic anhydride, hexahydrophthalic anhydride, glutaric acid Acid anhydride, adipic anhydride, dodecenylsuccinic acid acid anhydride, methylcyclohexene tetracid dianhydride, methylnadic anhydride;The metal salt includes Zinc acetylacetonate, zinc acetate, calcium acetate, magnesium acetate, dibutyl tin laurate.
6. self-repair type can remold the multiple deformation thermoset shape memory resin material of shape, feature according to claim 1 It is, the bismaleimide and amine compounds react in a solvent;The bismaleimide and amine compounds are in solvent The condition of middle reaction is 55~110 DEG C and reacts 8~15 hours;After removing solvent, oligomer is obtained.
7. self-repair type can remold the multiple deformation thermoset shape memory resin material of shape, feature according to claim 1 It is, oligomer is added in epoxy resin, accelerating agent is added after 90~110 DEG C of mixing;The temperature of the heat cure is 100 ~180 DEG C, the time is 8~15 hours.
8. self-repair type can remold the multiple deformation thermoset shape memory resin material of shape, feature according to claim 1 It is, after acid anhydrides is added, obtains prepolymerization system, add addO-on therapy, then carry out heat cure;The addO-on therapy includes cyanogen Acid ester resin, phenolic resin, organic siliconresin, furane resins;The additive amount of the addO-on therapy be prepolymerization system quality 5~ 10%。
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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110078896A (en) * 2019-05-14 2019-08-02 中国科学院大学 A kind of Intrinsical selfreparing epoxy elastomer material and preparation method thereof
CN111423580A (en) * 2020-05-23 2020-07-17 苏州大学 Shape memory resin based on biomass benzoxazine and preparation method and application thereof
CN112961463A (en) * 2021-02-07 2021-06-15 四川大学 Super-tough self-repairing epoxy resin glass polymer material and preparation method thereof

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110054795B (en) * 2018-01-19 2020-07-03 清华大学 Thermosetting polymer material processing, healing and welding method
CN110054863B (en) * 2018-01-19 2020-07-03 清华大学 Method for changing shape of thermosetting polymer material
WO2019165583A1 (en) * 2018-02-27 2019-09-06 苏州大学张家港工业技术研究院 Reversible self-repairing epoxy resin and preparation and recovery remoulding method therefor
CN108484910B (en) * 2018-04-13 2020-05-22 苏州大学 Bismaleimide-based thermosetting shape memory resin and preparation method thereof
CN109705313B (en) * 2019-01-22 2021-03-19 苏州大学 Thermo-adaptive shape memory polymer and application method thereof
CN110105544B (en) * 2019-06-04 2021-09-07 安徽工业大学 Preparation method of self-repairing material based on double repairing mechanisms
CN110330650B (en) * 2019-07-30 2021-07-09 苏州大学 Bismaleimide resin prepolymer and application thereof
CN110330649B (en) * 2019-07-30 2021-04-27 苏州大学 Remodelable bismaleimide resin and application thereof
CN110330648B (en) * 2019-07-30 2021-06-18 苏州大学 Prepolymer for remoldable bismaleimide resin and application thereof
CN110330647B (en) * 2019-07-30 2021-06-18 苏州大学 Remodelable shape memory bismaleimide resin and application thereof
WO2021119874A1 (en) * 2019-12-15 2021-06-24 苏州大学 Epoxy resin system having phase separation structure, preparation method therefor and application thereof
CN111004473B (en) * 2019-12-15 2021-05-25 苏州大学 Epoxy resin system with split-phase structure and preparation method and application thereof
CN113321785B (en) * 2021-05-27 2023-10-17 五邑大学 Shape memory material and preparation method and application thereof

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010144971A1 (en) * 2009-06-19 2010-12-23 Commonwealth Scientific And Industrial Research Organisation Self healing polymer materials
CN104194269A (en) * 2014-08-31 2014-12-10 海安南京大学高新技术研究院 Reversible repair functional matrix resin for pultrusion and preparation method of matrix resin
CN105038220A (en) * 2015-06-23 2015-11-11 南通和泰通讯器材有限公司 High-toughness aramid composite material optical fiber reinforced core and preparation method thereof

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100063241A1 (en) * 2008-09-09 2010-03-11 Spirit Aerosystems, Inc. High performance polyaspartimide resin
CN102786777B (en) * 2012-08-06 2014-12-03 江苏大学 Intrinsic conduction shape memory polymer and preparation method thereof
CN103740054A (en) * 2013-12-17 2014-04-23 中航复合材料有限责任公司 Preparation method of thermosetting shape memory resin with two glass transition temperatures
CN104130426B (en) * 2014-07-01 2017-07-28 哈尔滨工业大学 Thermoset shape memory resin of various shapes and preparation method thereof can be remembered
CN104497270B (en) * 2014-12-18 2016-08-31 中科院广州化学有限公司 Side base substituted biphenyl type shape memory epoxy resin by using liquid crystal and preparation method thereof and application
CN105968808B (en) * 2016-07-05 2018-08-24 苏州大学 A kind of self-repair resin based composites and preparation method thereof

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010144971A1 (en) * 2009-06-19 2010-12-23 Commonwealth Scientific And Industrial Research Organisation Self healing polymer materials
CN104194269A (en) * 2014-08-31 2014-12-10 海安南京大学高新技术研究院 Reversible repair functional matrix resin for pultrusion and preparation method of matrix resin
CN105038220A (en) * 2015-06-23 2015-11-11 南通和泰通讯器材有限公司 High-toughness aramid composite material optical fiber reinforced core and preparation method thereof

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
WU W, ET AL: "Preparation and Characterization of Bismaleimide-Diamine Prepolymers and Their Thermal-Curing Behavior", 《JOURNAL OF APPLIED POLYMER SCIENCE》 *
YUAN Y C, ET AL: "Self-Healing Epoxy Composite with Heat-Resistant Healant", 《APPLIED MATERIALS & INTERFACES》 *

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110078896A (en) * 2019-05-14 2019-08-02 中国科学院大学 A kind of Intrinsical selfreparing epoxy elastomer material and preparation method thereof
CN110078896B (en) * 2019-05-14 2021-06-04 中国科学院大学 Intrinsic self-repairing epoxy elastomer material and preparation method thereof
CN111423580A (en) * 2020-05-23 2020-07-17 苏州大学 Shape memory resin based on biomass benzoxazine and preparation method and application thereof
CN112961463A (en) * 2021-02-07 2021-06-15 四川大学 Super-tough self-repairing epoxy resin glass polymer material and preparation method thereof
CN112961463B (en) * 2021-02-07 2022-04-08 四川大学 Super-tough self-repairing epoxy resin glass polymer material and preparation method thereof

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