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WO2019112460A1 - Composition for impregnating reinforcing material and method for producing same - Google Patents

Composition for impregnating reinforcing material and method for producing same Download PDF

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Publication number
WO2019112460A1
WO2019112460A1 PCT/RU2017/000910 RU2017000910W WO2019112460A1 WO 2019112460 A1 WO2019112460 A1 WO 2019112460A1 RU 2017000910 W RU2017000910 W RU 2017000910W WO 2019112460 A1 WO2019112460 A1 WO 2019112460A1
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WO
WIPO (PCT)
Prior art keywords
melt
composition
composite materials
reinforcing material
catalyst
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Ceased
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PCT/RU2017/000910
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French (fr)
Russian (ru)
Inventor
Илья Александрович ВИХРОВ
Василий Федорович АРИСТОВ
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"syntez-Project" LLC
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"syntez-Project" LLC
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Priority to PCT/RU2017/000910 priority Critical patent/WO2019112460A1/en
Priority to EA202091132A priority patent/EA202091132A1/en
Publication of WO2019112460A1 publication Critical patent/WO2019112460A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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    • 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
    • C08G18/00Polymeric products of isocyanates or isothiocyanates
    • C08G18/02Polymeric products of isocyanates or isothiocyanates of isocyanates or isothiocyanates only
    • 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
    • C08GMACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G18/00Polymeric products of isocyanates or isothiocyanates
    • C08G18/06Polymeric products of isocyanates or isothiocyanates with compounds having active hydrogen
    • C08G18/08Processes
    • C08G18/16Catalysts
    • C08G18/22Catalysts containing metal compounds
    • 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
    • C08K3/00Use of inorganic substances as compounding ingredients
    • C08K3/18Oxygen-containing compounds, e.g. metal carbonyls
    • C08K3/20Oxides; Hydroxides
    • C08K3/22Oxides; Hydroxides of metals
    • CCHEMISTRY; METALLURGY
    • C08ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08LCOMPOSITIONS OF MACROMOLECULAR COMPOUNDS
    • C08L79/00Compositions of macromolecular compounds obtained by reactions forming in the main chain of the macromolecule a linkage containing nitrogen with or without oxygen or carbon only, not provided for in groups C08L61/00 - C08L77/00

Definitions

  • the group of inventions relates to a binder for polymer composite materials, in particular for materials for space purposes, and to methods for their preparation.
  • thermosetting binders In the manufacture of polymer composite materials for space applications, three types of thermosetting binders are mainly used: epoxy, bismaleimide, and polycyanurate.
  • Polycyanurate binders differ from epoxy and bismaleimide binders, first of all, by increased crack resistance during thermal cycling, reduced moisture absorption, high resistance to cosmic radiation, and better dielectric characteristics; therefore, they are most suitable for manufacturing dimensionally stable structures for space purposes.
  • compositions based on aromatic or perfluoroaliphatic dicyanates and metal chelates make it possible to obtain polymers with different physicomechanical properties and at different curing temperatures, depending on the amount and type of metal chelate used.
  • the disadvantage of these compositions is that organic solvents, such as methylene chloride or chloroform, are used to obtain them, which leads to residual solvents in the binder and, as a consequence, the formation of pores in the molding process, which reduces the physicomechanical characteristics of composite materials.
  • compositions based on aromatic dicyanates and liquid solutions of metal acetylacetonates in high-boiling alkyl phenols (patent US 4847233A). These compositions also allow to obtain polymers with different physicomechanical properties and at different curing temperatures, depending on the amount and type of metal chelate used, moreover, the absence of a low-boiling solvent solves the problem of increased pore formation during the molding of products.
  • the disadvantage of these compositions is that a large amount of alkylphenol is used to obtain them (10 or more times the amount of metal acetylacetonate), which is partially chemically bound to the polymer, forming thermally unstable hydrophilic imidocarbonate structures that promote increased moisture absorption and gas evolution at elevated temperatures .
  • compositions based on aromatic dicyanates with nanoscale (average particle size from 1 to 100 nm) filler - zinc oxide in the amount of 0.001-1 weight fractions without the use of solvents and diluents (patent JP 2006-328177). These compositions have a low dependence of catalyst activity on temperature and slightly increase the viscosity of the binder after the introduction of the catalyst.
  • a common task addressed by the group of inventions, and a common technical result achieved using a group of inventions, is the development of a polycyanurate binder with a minimum curing temperature not higher than 125 ° C, which eliminates the use of solvents and / or diluents and reduces the gas evolution of composite materials in products space destination.
  • the task and the required technical result is achieved due to the new method of obtaining the composition of melt binders based on metal chelates and oligocyanurate resins with active cyanate groups for impregnation of reinforcing material in polymer composite materials for space purposes, in which the resin is heated to melt state, the catalyst is introduced into the resulting melt in the form of a dry powder of metal chelates with a particle size of 40-125 microns in an amount of 50- 600 ppm in the ratio of the mass of metal ions to the mass of the composition and mix the melt to a visually homogeneous state.
  • the task and the required technical result is also achieved due to the new composition for impregnating reinforcing material in polymer composite materials for space, obtained by the proposed method, in the form of a solution or melt 50-600 ppm of complex compounds or their mixtures of aluminum ions, transition metals and rare earth elements, with various organic ligands in resins with active cyanate groups, without using any solvents or diluents.
  • the composition is a solution or melt of complex compounds or their mixtures of aluminum ions, transition metals and rare earth elements, with various organic ligands in resins with active cyanate groups, without using any solvents or diluents.
  • the proposed composition (binder) includes monomers with active cyanate groups or oligomers with active cyanate groups or their mixtures, contains 50-600 million parts (in terms of the mass of metal ions to the composition) of the dissolved catalyst and does not contain solvents or active diluents.
  • coordination-saturated complex compounds or their mixtures can be used, in which metal ions are used as complexing agents, and acetylacetonate ions and / or neutral molecules capable of binding to complexing agent, for example, 1, 10 are used as ligand.
  • metal ions are used as complexing agents
  • acetylacetonate ions and / or neutral molecules capable of binding to complexing agent for example, 1, 10 are used as ligand.
  • 1, 10 are used as ligand.
  • -fenantrolin, 2,2 '-bipiridin or triphenylphosphine oxide triphenylphosphine oxide.
  • the binder may also contain various additional components: various polymers, resins, fillers, dyes, pigments, thickeners, lubricants or flame retardants acting as modifiers a binder, and not being solvents or diluents of the metal complex catalyst.
  • the method of obtaining the composition (binder) consists in the fact that at first the catalyst is crushed to a particle size of preferably 40-125 ⁇ m and only after that is introduced into the resin.
  • This method allows to obtain a homogeneous solution (melt) of the catalyst in the resin (as opposed to the patent US 4847233A) without using any solvents or diluents.
  • the particle size may be somewhat outside the specified range, however, the use of particles smaller than 40 microns leads to a significant electrification of particles and makes sowing difficult, and the use of particles larger than 125 microns increases the mixing time or does not allow to achieve homogeneity of the melt.
  • a resin (3 samples of 20 g each) based on bisphenol A dicyanate oligomerized at 170–200 ° C (viscosity of 1.5 Pa * s at 80 ° C) is taken and heated to melt state at 80 ° C.
  • the catalyst is introduced into the melt.
  • the first case in the form of a dry powder of copper acetylacetonate with a particle size of not more than 100 microns in an amount of 300 ppm - 0.0247 g.
  • the second case in the form of a solution 200 ppm - 0.0655 g of acetylacetonate copper in 0,400 g of nonylphenol.
  • Part of the prepared compositions 10 g each, is poured into molds and cured at 125 ° C for 10 hours, the glass transition temperature of the obtained samples is measured. The remaining parts of the prepared compositions are maintained at 80 ° C, periodically measuring the viscosity. The results of viscosity measurements are shown in the table.
  • the oligocyanurate resin (30 g) based on bisphenol M dicyanate is heated to 50 ° C (melt viscosity at a given temperature of 0.5 Pa * s).
  • a catalyst 300 ppm Zn
  • the resulting composition is poured into a mold and cured at 125 ° C for 10 hours.
  • the obtained plastic sample after cooling has a glass transition temperature in the region of 103-108 ° C (according to DSC data).
  • the gelation time of this composition is more than 20 hours at 50 ° C.
  • the oligocyanurate resin (30 g) based on bisphenol A dicyanate is heated to 80 ° C (the melt viscosity at this temperature is 1, 5 Pa * s).
  • a catalyst is injected into the melt (50 ppm Fe) - 0.0094 g of iron acetylacetonate powder (Fe (ac) h) with a particle size of not more than 40 ⁇ m and the melt is well mixed at 80 ° C to a homogeneous state (a transparent mass of dark red is formed colors).
  • the resulting composition is poured into a mold and cured at 125 ° C for 10 hours.
  • the obtained plastic sample after cooling has a glass transition temperature of 133-138 ° C (according to DSC).
  • the gelation time of this composition is about 3 hours at 80 ° C.
  • the oligocyanurate resin (30 g) based on bisphenol A dicyanate is heated to 80 ° C (the melt viscosity at this temperature is 1, 5 Pa * s).
  • a catalyst 300 ppm Zr) —0.0636 g of zirconium acetylacetonate powder (Zr (acac) 4) with a particle size of not more than 125 ⁇ m is introduced into the melt and the melt is well mixed at 80 ° C to a homogeneous state (a transparent yellow mass is formed) .
  • the resulting composition is poured into a mold and cured at 125 ° C for 10 hours.
  • the obtained plastic sample after cooling has a glass transition temperature of 125-130 ° C (according to DSC).
  • the gelation time of this composition is about 8 hours at 80 ° C.
  • the oligocyanurate resin (30 g) based on bisphenol E dicyanate is heated to 40 ° C (melt viscosity at a given temperature of 0.3 Pa * s). Then, a catalyst (600 ppm Tm) —0.0690 g of thulium acetylacetonate phenanthrolinate powder (Tm (acac) 3phen) with a particle size of not more than 100 ⁇ m is introduced into the melt and the melt is well mixed at 40 ° C until homogeneous yellow color). The resulting composition is poured into a mold and cured at 125 ° C for 10 hours. The obtained plastic sample after cooling has a glass transition temperature in the region of 150-155 ° C (according to DSC data). The gelation time of this composition is more than 20 hours at 40 ° C.

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  • Chemical & Material Sciences (AREA)
  • Health & Medical Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Medicinal Chemistry (AREA)
  • Polymers & Plastics (AREA)
  • Organic Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
  • Macromolecular Compounds Obtained By Forming Nitrogen-Containing Linkages In General (AREA)
  • Polyurethanes Or Polyureas (AREA)

Abstract

The group of inventions relates to binders for polymeric composite materials, more particularly for materials for outer space applications, and to methods for producing same. Proposed is a method for producing a composition of melt binders based on metal chelates and oligocyanurate resins with reactive cyanate groups for impregnating reinforcing material in polymer composite materials for outer space applications, wherein a resin is heated to a molten state, a catalyst, consisting of metal chelates in the form of dry powder with a particle size of 40-125 µm, is introduced into the melt produced, the amount of catalyst added being 50-600 ppm based on the ratio of metal ion mass to the total weight of the composition, and the melt is then mixed to a visually uniform state. The composition for impregnating reinforcing material in polymer composite materials for outer space applications produced by the proposed method is in the form of a solution or melt comprising 50-600 ppm of complex compounds or mixtures thereof comprising ions of aluminium, transition metals and rare-earth elements with various organic ligands in resins having reactive cyanate groups, and is solvent- or diluent-free.

Description

КОМПОЗИЦИЯ ДЛЯ ПРОПИТКИ АРМИРУЮЩЕГО МАТЕРИАЛА И  COMPOSITION FOR IMPREGNATION OF REINFORCING MATERIAL AND

СПОСОБ ЕЕ ПОЛУЧЕНИЯ  METHOD OF OBTAINING IT

ОБЛАСТЬ ТЕХНИКИ TECHNICAL FIELD

Группа изобретений относится к связующим для полимерных композиционных материалов, в частности для материалов космического назначения, и к способам их получения.  The group of inventions relates to a binder for polymer composite materials, in particular for materials for space purposes, and to methods for their preparation.

УРОВЕНЬ ТЕХНИКИ  BACKGROUND

При изготовлении полимерных композиционных материалов космического назначения в основном используют три типа термореактивных связующих: эпоксидные, бисмалеимидные и полициануратные. Полициануратные связующие отличаются от эпоксидных и бисмалеимидных связующих, прежде всего, повышенной трещиностойкостью при термоциклировании, пониженным влагопоглощением, высокой устойчивостью к космическому излучению и лучшими диэлектрическими характеристиками, поэтому наиболее подходят для изготовления размеростабильных конструкций космического назначения.  In the manufacture of polymer composite materials for space applications, three types of thermosetting binders are mainly used: epoxy, bismaleimide, and polycyanurate. Polycyanurate binders differ from epoxy and bismaleimide binders, first of all, by increased crack resistance during thermal cycling, reduced moisture absorption, high resistance to cosmic radiation, and better dielectric characteristics; therefore, they are most suitable for manufacturing dimensionally stable structures for space purposes.

Известны композиции на основе ароматических или перфторалифатических дицианатов и хелатов металлов (патент US 3694410). Эти композиции позволяют получать полимеры с различными физико-механическими свойствами и при различной температуре отверждения, в зависимости от количества и типа используемого хелата металла. Недостатком данных композиций является то, что для их получения используют органические растворители, такие как хлористый метилен или хлороформ, что приводит к появлению остаточных растворителей в связующем и как следствие, образованию пор в процессе формования изделий, что снижает физико-механические характеристики композитных материалов.  Known compositions based on aromatic or perfluoroaliphatic dicyanates and metal chelates (patent US 3694410). These compositions make it possible to obtain polymers with different physicomechanical properties and at different curing temperatures, depending on the amount and type of metal chelate used. The disadvantage of these compositions is that organic solvents, such as methylene chloride or chloroform, are used to obtain them, which leads to residual solvents in the binder and, as a consequence, the formation of pores in the molding process, which reduces the physicomechanical characteristics of composite materials.

Известны композиции на основе ароматических дицианатов и жидких растворов ацетилацетонатов металлов в высококипящих алкилфенолах (патент US 4847233А). Данные композиции также позволяют получать полимеры с различными физико-механическими свойствами и при различной температуре отверждения, в зависимости от количества и типа используемого хелата металла, кроме того, отсутствие легкокипящего растворителя решает проблему повышенного порообразование при формовании изделий. Недостатком данных композиций является то, что для их получения используется большое количество алкилфенола (в 10 и более раз превышающее количество ацетилацетоната металла), который частично химически связывается с полимером, образуя термически неустойчивые гидрофильные структуры типа имидокарбонатов, которые способствуют повышенным влагопоглощению и газовыделению при повышенной температуре. Химически не связанный алкилфенол в условиях глубокого вакуума при нахождении изделия в открытом космическом пространстве может диффундировать наружу, оставляя за собой микропоры, что приведёт к изменению геометрии прецизионной размеростабильной конструкции. Кроме того, диффундирующие наружу частички алкилфенола могут осесть за счет электростатического взаимодействия на чувствительные приборы космического аппарата, например, оптику, что может привести к потере рабочих характеристик устройств. Known compositions based on aromatic dicyanates and liquid solutions of metal acetylacetonates in high-boiling alkyl phenols (patent US 4847233A). These compositions also allow to obtain polymers with different physicomechanical properties and at different curing temperatures, depending on the amount and type of metal chelate used, moreover, the absence of a low-boiling solvent solves the problem of increased pore formation during the molding of products. The disadvantage of these compositions is that a large amount of alkylphenol is used to obtain them (10 or more times the amount of metal acetylacetonate), which is partially chemically bound to the polymer, forming thermally unstable hydrophilic imidocarbonate structures that promote increased moisture absorption and gas evolution at elevated temperatures . Chemically unbound alkylphenol under conditions of high vacuum when the product is in open space can diffuse outward, leaving behind micropores, which will lead to a change in the geometry of the precision dimensionally stable design. In addition, the alkylphenol particles diffusing to the outside can settle due to electrostatic interaction on sensitive instruments of the spacecraft, for example, optics, which can lead to loss of device performance.

Наиболее близкой из известных являются композиции на основе ароматических дицианатов с наноразмерным (средний размер частиц от 1 до 100 нм) наполнителем - оксидом цинка в количестве 0.001-1 весовых долей без использования растворителей и разбавителей (патент JP 2006-328177). Эти композиции имеют низкую зависимость активности катализатора от температуры и слабо повышают вязкость связующего после введения катализатора.  The closest known are compositions based on aromatic dicyanates with nanoscale (average particle size from 1 to 100 nm) filler - zinc oxide in the amount of 0.001-1 weight fractions without the use of solvents and diluents (patent JP 2006-328177). These compositions have a low dependence of catalyst activity on temperature and slightly increase the viscosity of the binder after the introduction of the catalyst.

Недостатком данных композиций является то, что для их полимеризации требуются температуры отверждения, заметно выше 120-125 °С, что ограничивает их применение и усложняет процесс изготовления полимерных композиционных материалов. Кроме того, оксид цинка нерастворим в расплавах ароматических дицианатов, это усложняет процесс диспергирования и контроль равномерного распределения катализатора.  The disadvantage of these compositions is that curing temperatures are required for their polymerization, well above 120-125 ° C, which limits their use and complicates the process of manufacturing polymer composite materials. In addition, zinc oxide is insoluble in melts of aromatic dicyanates, this complicates the process of dispersion and control of the uniform distribution of the catalyst.

СУЩНОСТЬ ИЗОБРЕТЕНИЯ  SUMMARY OF INVENTION

Общей задачей, на решение которой направлена группа изобретений, и общим техническим результатом, достигаемом при использовании группы изобретений, является разработка полициануратного связующего с минимальной температурой отверждения не выше 125 °С, позволяющего исключить использование растворителей и/или разбавителей и понизить газовыделение композиционных материалов в изделиях космического назначения.  A common task addressed by the group of inventions, and a common technical result achieved using a group of inventions, is the development of a polycyanurate binder with a minimum curing temperature not higher than 125 ° C, which eliminates the use of solvents and / or diluents and reduces the gas evolution of composite materials in products space destination.

Поставленная задача и требуемый технический результат достигаются за счет нового способа получения композиции расплавных связующих на основе хелатов металлов и олигоциануратных смол с активными цианатными группами для пропитки армирующего материала в полимерных композиционных материалах космического назначения, в котором нагревают смолу до расплавного состояния, вводят в полученный расплав катализатор в виде сухого порошка хелатов металлов с размером частиц 40-125 мкм в количестве 50-600 миллионных долей в отношении массы ионов металла к массе композиции и перемешивают расплав до визуально однородного состояния. The task and the required technical result is achieved due to the new method of obtaining the composition of melt binders based on metal chelates and oligocyanurate resins with active cyanate groups for impregnation of reinforcing material in polymer composite materials for space purposes, in which the resin is heated to melt state, the catalyst is introduced into the resulting melt in the form of a dry powder of metal chelates with a particle size of 40-125 microns in an amount of 50- 600 ppm in the ratio of the mass of metal ions to the mass of the composition and mix the melt to a visually homogeneous state.

Поставленная задача и требуемый технический результат достигаются также за счет новой композиции для пропитки армирующего материала в полимерных композиционных материалах космического назначения, полученной предложенным способом, в виде раствора или расплава 50-600 миллионных долей комплексных соединений или их смесей из ионов алюминия, переходных металлов и редкоземельных элементов, с различными органическими лигандами в смолах с активными цианатными группами, без использованиях каких-либо растворителей или разбавителей.  The task and the required technical result is also achieved due to the new composition for impregnating reinforcing material in polymer composite materials for space, obtained by the proposed method, in the form of a solution or melt 50-600 ppm of complex compounds or their mixtures of aluminum ions, transition metals and rare earth elements, with various organic ligands in resins with active cyanate groups, without using any solvents or diluents.

РАСКРЫТИЕ ИЗОБРЕТЕНИЯ  DISCLOSURE OF INVENTION

Согласно изобретению композиция представляет собой раствор или расплав комплексных соединений или их смесей из ионов алюминия, переходных металлов и редкоземельных элементов, с различными органическими лигандами в смолах с активными цианатными группами, без использованиях каких-либо растворителей или разбавителей. Предлагаемая композиция (связующее) включает мономеры с активными цианатными группами или олигомеры с активными цианатными группами или их смеси, содержит 50-600 милионных долей (в отношении массы ионов металла к массе композиции) растворённого катализатора и не содержит растворителей или активных разбавителей. В качестве катализаторов могут выступать, например, координационно-насыщенные комплексные соединения или их смеси, в которых комплексообразователем являются ионы металлов, а в качестве лиганда используются предпочтительно ацетилацетонат-ионы и/или нейтральные молекулы, способные к связыванию с комплексообразователем, например, 1 ,10-фенантролин, 2,2'-бипиридин или трифенилфосфиноксид. According to the invention, the composition is a solution or melt of complex compounds or their mixtures of aluminum ions, transition metals and rare earth elements, with various organic ligands in resins with active cyanate groups, without using any solvents or diluents. The proposed composition (binder) includes monomers with active cyanate groups or oligomers with active cyanate groups or their mixtures, contains 50-600 million parts (in terms of the mass of metal ions to the composition) of the dissolved catalyst and does not contain solvents or active diluents. As catalysts, for example, coordination-saturated complex compounds or their mixtures can be used, in which metal ions are used as complexing agents, and acetylacetonate ions and / or neutral molecules capable of binding to complexing agent, for example, 1, 10 are used as ligand. -fenantrolin, 2,2 '-bipiridin or triphenylphosphine oxide.

Связующее может также содержать различные дополнительные компоненты: различные полимеры, смолы, наполнители, красители, пигменты, загустители, смазки или антипирены, выступающие в качестве модификаторов связующего, а не являющиеся растворителями или разбавителями металлокомплексного катализатора. The binder may also contain various additional components: various polymers, resins, fillers, dyes, pigments, thickeners, lubricants or flame retardants acting as modifiers a binder, and not being solvents or diluents of the metal complex catalyst.

Согласно изобретению способ получения композиции (связующего) заключается в том, что вначале катализатор измельчают до размера частиц предпочтительно 40-125 мкм и только после этого вводят в смолу. Такой способ позволяет получить гомогенный раствор (расплав) катализатора в смоле (в отличие от патента US 4847233А) без использования каких-либо растворителей или разбавителей. Для достижения результата размер частиц может несколько выходить за рамки указанного диапазона, однако использование частиц размером менее 40 мкм приводит к существенной электризации частиц и затрудняет рассев, а использование частиц размером более 125 мкм увеличивает время перемешивания или вовсе не позволяет добиться гомогенности расплава.  According to the invention, the method of obtaining the composition (binder) consists in the fact that at first the catalyst is crushed to a particle size of preferably 40-125 μm and only after that is introduced into the resin. This method allows to obtain a homogeneous solution (melt) of the catalyst in the resin (as opposed to the patent US 4847233A) without using any solvents or diluents. To achieve the result, the particle size may be somewhat outside the specified range, however, the use of particles smaller than 40 microns leads to a significant electrification of particles and makes sowing difficult, and the use of particles larger than 125 microns increases the mixing time or does not allow to achieve homogeneity of the melt.

Настоящее изобретение иллюстрируется следующими примерами.  The present invention is illustrated by the following examples.

Примеры сравнения.  Examples of comparison.

Берут смолу (3 образца по 20 г) на основе бисфенол А дицианата, олигомеризованную при 170-200 °С (вязкостью 1 ,5 Па*с при 80 °С) и нагревают до расплавного состояния при 80 °С. Далее в расплав вводят катализатор. В первом случае (обр.1) в виде сухого порошка ацетилацетоната меди с размером частиц не более 100 мкм в количестве 300 ppm - 0,0247 г. Во втором случае (обр.2) в виде раствора 200 ppm - 0,0165 г ацетилацетоната меди в 0,400 г нонилфенола. В третье случае (обр.З) в виде раствора 150 ppm - 0,0124 г ацетилацетоната меди в 0,400 г нонилфенола. После введения катализатора хорошо перемешивают расплавы до однородного состояния (гомогенность композиции устанавливают визуально по образованию прозрачного расплава, окрашенного в цвет соответствующего катализатора). A resin (3 samples of 20 g each) based on bisphenol A dicyanate oligomerized at 170–200 ° C (viscosity of 1.5 Pa * s at 80 ° C) is taken and heated to melt state at 80 ° C. Next, the catalyst is introduced into the melt. In the first case (obr.1) in the form of a dry powder of copper acetylacetonate with a particle size of not more than 100 microns in an amount of 300 ppm - 0.0247 g. In the second case (obr.2) in the form of a solution 200 ppm - 0.0655 g of acetylacetonate copper in 0,400 g of nonylphenol. In the third case (obr.z) in the form of a solution of 150 ppm - 0.0124 g of copper acetylacetonate in 0.400 g of nonylphenol. After the introduction of the catalyst, the melts are well stirred until homogeneous (the homogeneity of the composition is established visually by the formation of a transparent melt colored in the color of the corresponding catalyst).

Часть приготовленных композиций - по 10 г от каждой, заливают в формы и отверждают при 125 °С в течение 10 ч, измеряют температуру стеклования полученных образцов. Оставшиеся части приготовленных композиций выдерживают при 80 °С, периодически измеряя вязкость. Результаты измерений вязкости приведены в таблице.

Figure imgf000006_0001
Part of the prepared compositions, 10 g each, is poured into molds and cured at 125 ° C for 10 hours, the glass transition temperature of the obtained samples is measured. The remaining parts of the prepared compositions are maintained at 80 ° C, periodically measuring the viscosity. The results of viscosity measurements are shown in the table.
Figure imgf000006_0001

Чем больше катализатора - тем меньше время сохранения связующим вязкотекучего состояния и тем больше температура стеклования после отверждения. На основании полученных данных видно, что время жизни зависит как от количества введенного катализатора, так и от наличия нонилфенола (обр. 2 приведён в качестве примера для подтверждения этого заключения). Образцами сравнения следует считать обр. 1 и обр. 3, как образцы с примерно одинаковым временем сохранения вязкотекучего состояния. Температура стеклования данных образцов получилась одинаковой по данным ДСК - 135-140 °С. Это говорит о том, что композиции, полученные в отсутствие разбавителя, не уступают по температуре стеклования композициям, полученным с использованием разбавителя, при условии одинакового времени жизни. Преимуществом настоящего изобретения (на примере обр.1) является отсутствие в композиции растворителей и разбавителей, что уменьшает пористость и влагопоглощение изделий из композитных материалов.  The larger the catalyst, the shorter the time it takes to bind a viscous state and the higher the glass transition temperature after curing. Based on the data obtained, it can be seen that the lifetime depends on both the amount of the introduced catalyst and the presence of nonylphenol (sample 2 is given as an example to confirm this conclusion). Examples of comparison should be considered arr. 1 and arr. 3, as samples with approximately the same time to maintain a viscous state. The glass transition temperature of these samples turned out to be the same according to DSC data - 135-140 ° C. This suggests that the compositions obtained in the absence of a diluent are not inferior in the glass transition temperature to compositions obtained using a diluent, provided that they have the same lifetime. The advantage of the present invention (for example, Obr.1) is the absence in the composition of solvents and diluents, which reduces the porosity and moisture absorption of products made of composite materials.

Пример 1  Example 1

Олигоциануратную смолу (30 г) на основе бисфенол М дицианата нагревают до 50 °С (вязкость расплава при данной температуре 0,5 Па*с). Далее в расплав вводят катализатор (300 ppm Zn) - 0,0636 г порошка фенантролината ацетилацетоната цинка (Zn(acac)2phen) с размером частиц не более 100 мкм и хорошо перемешивают расплав при 50 °С до гомогенного состояния (образуется прозрачная масса светло-оранжевого цвета). Полученную композицию заливают в форму и отверждают при 125 °С в течение 10 ч. Полученный образец пластика после охлаждения имеет температуру стеклования в области 103-108 °С (по данным ДСК). Время гелеобразования указанной композиции составляет более 20 ч при 50 °С. The oligocyanurate resin (30 g) based on bisphenol M dicyanate is heated to 50 ° C (melt viscosity at a given temperature of 0.5 Pa * s). Next, a catalyst (300 ppm Zn) —0.0636 g of powder of phenanthrolinate zinc acetylacetonate (Zn (acac) 2phen) with a particle size of not more than 100 μm is introduced into the melt and the melt is well mixed at 50 ° С to a homogeneous state (a transparent mass of light orange). The resulting composition is poured into a mold and cured at 125 ° C for 10 hours. The obtained plastic sample after cooling has a glass transition temperature in the region of 103-108 ° C (according to DSC data). The gelation time of this composition is more than 20 hours at 50 ° C.

Пример 2  Example 2

Олигоциануратную смолу (30 г) на основе бисфенол А дицианата нагревают до 80 °С (вязкость расплава при данной температуре 1 ,5 Па*с). Далее в расплав вводят катализатор (50 ppm Fe) - 0,0094 г порошка ацетилацетоната железа (Ре(асас)з) с размером частиц не более 40 мкм и хорошо перемешивают расплав при 80 °С до гомогенного состояния (образуется прозрачная масса тёмно-красного цвета). Полученную композицию заливают в форму и отверждают при 125 °С в течение 10 ч. Полученный образец пластика после охлаждения имеет температуру стеклования 133-138 °С (по данным ДСК). Время гелеобразования указанной композиции составляет около 3 ч при 80 °С.  The oligocyanurate resin (30 g) based on bisphenol A dicyanate is heated to 80 ° C (the melt viscosity at this temperature is 1, 5 Pa * s). Next, a catalyst is injected into the melt (50 ppm Fe) - 0.0094 g of iron acetylacetonate powder (Fe (ac) h) with a particle size of not more than 40 μm and the melt is well mixed at 80 ° C to a homogeneous state (a transparent mass of dark red is formed colors). The resulting composition is poured into a mold and cured at 125 ° C for 10 hours. The obtained plastic sample after cooling has a glass transition temperature of 133-138 ° C (according to DSC). The gelation time of this composition is about 3 hours at 80 ° C.

Пример 3  Example 3

Олигоциануратную смолу (30 г) на основе бисфенол А дицианата нагревают до 80 °С (вязкость расплава при данной температуре 1 ,5 Па*с). Далее в расплав вводят катализатор (300 ppm Zr) - 0,0636 г порошка ацетилацетоната циркония (Zr(acac)4) с размером частиц не более 125 мкм и хорошо перемешивают расплав при 80 °С до гомогенного состояния (образуется прозрачная масса жёлтого цвета). Полученную композицию заливают в форму и отверждают при 125 °С в течение 10 ч. Полученный образец пластика после охлаждения имеет температуру стеклования 125-130 °С (по данным ДСК). Время гелеобразования указанной композиции составляет около 8 ч при 80 °С.  The oligocyanurate resin (30 g) based on bisphenol A dicyanate is heated to 80 ° C (the melt viscosity at this temperature is 1, 5 Pa * s). Next, a catalyst (300 ppm Zr) —0.0636 g of zirconium acetylacetonate powder (Zr (acac) 4) with a particle size of not more than 125 μm is introduced into the melt and the melt is well mixed at 80 ° C to a homogeneous state (a transparent yellow mass is formed) . The resulting composition is poured into a mold and cured at 125 ° C for 10 hours. The obtained plastic sample after cooling has a glass transition temperature of 125-130 ° C (according to DSC). The gelation time of this composition is about 8 hours at 80 ° C.

Пример 4  Example 4

Олигоциануратную смолу (30 г) на основе бисфенол Е дицианата нагревают до 40 °С (вязкость расплава при данной температуре 0,3 Па*с). Далее в расплав вводят катализатор (600 ppm Tm) - 0,0690 г порошка фенантролината ацетилацетоната тулия (Tm(acac)3phen) с размером частиц не более 100 мкм и хорошо перемешивают расплав при 40 °С до гомогенного состояния (образуется прозрачная масса светло-жёлтого цвета). Полученную композицию заливают в форму и отверждают при 125 °С в течение 10 ч. Полученный образец пластика после охлаждения имеет температуру стеклования в области 150-155 °С (по данным ДСК). Время гелеобразования указанной композиции составляет более 20 ч при 40 °С. The oligocyanurate resin (30 g) based on bisphenol E dicyanate is heated to 40 ° C (melt viscosity at a given temperature of 0.3 Pa * s). Then, a catalyst (600 ppm Tm) —0.0690 g of thulium acetylacetonate phenanthrolinate powder (Tm (acac) 3phen) with a particle size of not more than 100 μm is introduced into the melt and the melt is well mixed at 40 ° C until homogeneous yellow color). The resulting composition is poured into a mold and cured at 125 ° C for 10 hours. The obtained plastic sample after cooling has a glass transition temperature in the region of 150-155 ° C (according to DSC data). The gelation time of this composition is more than 20 hours at 40 ° C.

Claims

ФОРМУЛА ИЗОБРЕТЕНИЯ CLAIM 1. Способ получения композиции расплавных связующих на основе хелатов металлов и олигоциануратных смол с активными цианатными группами для пропитки армирующего материала в полимерных композиционных материалах космического назначения, в котором:  1. The method of obtaining the composition of melt binders based on metal chelates and oligocyanurate resins with active cyanate groups for impregnation of a reinforcing material in polymer composite materials for space purposes, in which: нагревают смолу до расплавного состояния;  heat the resin to melt; вводят в полученный расплав катализатор в виде сухого порошка хелатов металлов с размером частиц 40-125 мкм в количестве 50-600 миллионных долей в отношении массы ионов металла к массе композиции; и  catalyst is introduced into the melt obtained in the form of a dry powder of metal chelates with a particle size of 40-125 μm in an amount of 50-600 ppm in relation to the weight of metal ions to the weight of the composition; and перемешивают расплав до визуально однородного состояния.  mix the melt to a visually homogeneous state. 2. Композиция для пропитки армирующего материала в полимерных композиционных материалах космического назначения, полученная способом по п. 1 , в виде раствора или расплава 50-600 миллионных долей комплексных соединений или их смесей из ионов алюминия, переходных металлов и редкоземельных элементов, с органическими лигандами в смолах с активными цианатными группами, без использованиях каких-либо растворителей или разбавителей.  2. Composition for impregnation of reinforcing material in polymer composite materials for space purposes, obtained by the method according to claim 1, in the form of a solution or melt 50-600 ppm of complex compounds or their mixtures of aluminum ions, transition metals and rare earth elements, with organic ligands resins with active cyanate groups, without using any solvents or thinners.
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