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CN1443818A - High-strength epoxy impregnating varnish used at extremely low temperature and preparation method and use method thereof - Google Patents

High-strength epoxy impregnating varnish used at extremely low temperature and preparation method and use method thereof Download PDF

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Publication number
CN1443818A
CN1443818A CN 03112866 CN03112866A CN1443818A CN 1443818 A CN1443818 A CN 1443818A CN 03112866 CN03112866 CN 03112866 CN 03112866 A CN03112866 A CN 03112866A CN 1443818 A CN1443818 A CN 1443818A
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Prior art keywords
epoxy
low temperature
parts
utmost point
impregnating varnish
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CN 03112866
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Chinese (zh)
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CN100335574C (en
Inventor
陈强
高秉钧
陈敬林
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Institute of Plasma Physics of CAS
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Institute of Plasma Physics of CAS
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Priority to CNB031128661A priority Critical patent/CN100335574C/en
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Abstract

本发明公开了一种极低温下使用的高强度环氧浸渍漆及其制备方法和使用方法,其特征在于以环氧树脂和增韧环氧树脂混合物为主剂,具有增韧的酸酐为固化剂,纳米二氧化硅填料为增强剂制备而成。首先将环氧树脂和增韧环氧树脂混合,加热至150~250℃,抽真空,脱水1~4小时,再缓慢加入经偶联剂处理的纳米填料,充分搅拌后缓慢降温至室温,使纳米填料悬浮在树脂中,最后再加入酸酐固化剂。本发明既增加环氧绝缘漆在极低温下的强度和抗脆裂性能,又不影响其浸渍性能。The invention discloses a high-strength epoxy dipping paint used at extremely low temperature and its preparation method and application method. Agent, nano-silica filler is prepared as a reinforcing agent. First, mix epoxy resin and toughened epoxy resin, heat to 150-250°C, vacuumize, dehydrate for 1-4 hours, then slowly add nano filler treated with coupling agent, stir well and then cool down to room temperature slowly, so that The nano filler is suspended in the resin, and finally the anhydride curing agent is added. The invention not only increases the strength and anti-brittle performance of the epoxy insulating varnish at extremely low temperature, but also does not affect its impregnation performance.

Description

High-strength epoxy impregnating varnish that utmost point low temperature uses down and preparation method thereof and using method
Technical field
The present invention relates to the high-strength epoxy impregnating varnish that a kind of utmost point low temperature that adds Nano filling uses down, can guarantee to flood fixedly superconducting coil in the steady running of utmost point low temperature lower magnet.Be applicable in the similar utmost point cryogenic magnet device such as large-scale superconducting magnet of magnetic confinement fusion physics facility and stressed big high-intensity magnetic field magnet.
Background technology
The superconducting intense magnetic field magnet, the large-scale superconducting magnet of magnetic confinement superconduction fusion facility is in order to guarantee the operation stability of superconducting magnet, prevent the superconducting magnet quench, the stressed sex change of magnet does not reach the design magneticstrength, and magnet is wanted impregnated insulating paint (1) fixed magnets, guarantees magnet steady running.(2) provide the magnet electric insulation.Not only intensity is low for existing common epoxy insulation varnish, and (as-263 ℃ of liquid heliums) can embrittlement under utmost point low temperature.Add filler and can suitably improve its low temperature intensity and resistance to brittle fracture energy, but the adding of common fillers improves the viscosity of insullac again, influences the saturating machine of insullac.
Summary of the invention
The objective of the invention is to use and make toughener by the Nano filling after the coupling agent treatment and cooperate Resins, epoxy and epoxy resin toughened mixture to make host, the high-strength epoxy impregnating varnish that preparation poling low temperature uses down, make it both increase intensity and the resistance to brittle fracture energy of epoxy insulation varnish under utmost point low temperature, do not influence its saturating machine again.
The present invention is the high-strength epoxy impregnating varnish that uses under a kind of utmost point low temperature, it is characterized in that with Resins, epoxy and epoxy resin toughened mixture be host, to have toughness reinforcing acid anhydrides be solidifying agent, the nano silicon filler is that toughener is prepared from.
Adopt the coupling agent treatment Nano filling, prevent that it is agglomerating because of surface action power, described coupling agent can be r-aminopropyl triethoxysilane, r-glycidyl ether oxygen propyl trimethoxy silicane, r-(metacryloxy) propyl trimethoxy silicane.
Its formulation by weight is:
80~120 parts of Resins, epoxy
5~40 parts of toughness reinforcing epoxies
50~130 parts on acid anhydrides
5~15 parts of nano silicon fillers
Its formulation by weight can also for:
80~120 parts of Resins, epoxy
5~40 parts of toughness reinforcing epoxies
50~130 parts on acid anhydrides
5~15 parts of nano silicon fillers
1~5 part of coupling agent
The preparation method of the high-strength epoxy impregnating varnish that a kind of utmost point low temperature uses down, it is characterized in that at first with Resins, epoxy and epoxy resin toughened mixing, be heated to 150~250 ℃, vacuumize, dewatered 1~4 hour, and slowly added Nano filling again, slowly be cooled to room temperature after fully stirring through coupling agent treatment, Nano filling is suspended in the resin, adds anhydride curing agent at last again.
The preparation method of the high-strength epoxy impregnating varnish that a kind of utmost point low temperature uses down is characterized in that described coupling agent treatment is meant coupling agent and Nano filling mixed to mix thoroughly.
The using method of the high-strength epoxy impregnating varnish that a kind of utmost point low temperature uses down is characterized in that condition of cure: 80~130 ℃ solidified 1~2 hour down, and 140~150 ℃ solidified 1~2 hour, and 160~190 ℃ solidified 5~15 hours.
Effect of the present invention:
The high-strength epoxy impregnating varnish that the utmost point low temperature of the present invention's preparation uses down, after measured:
(1), according to GB GB 1149-81Recording to draw and cut under the intensity room temperature greater than 13.1MPa, is greater than 15.2Mpa in the time of-196 ℃.
(2), room-temperature impact strength is greater than 16.2kg.cm/cm 2
(3), cold cycling impacts, promptly-196 ℃ five minutes, room temperature five minutes, ℃ five minutes again-196, room temperature five minutes .... greater than the not embrittlement of 20 circulation samples.
(4), cold and hot (room temperature-liquid nitrogen) shrinkage coefficient is less than 0.65%.(5) puncture of insulation, under the room temperature greater than 23.4KV/mm.(5), air content is less than 1.7%.
(6) viscosity 40 ℃ less than 63 seconds, viscosity less than time of 75 seconds greater than 10 hours.
Table 1 is listed insullac of the present invention (LH-5) and domestic Shanghai synthetic resin plant 1149,6895, external Britain rutherford experiment chamber 01,02,10,20,30, and the performance of several insullac such as CTD-101K is relatively.LH-4 is the room temperature strength height not only, and intensity is also higher during-196 ℃ of utmost point low temperature.
Table 2 is listed insullac of the present invention (LH-5) and domestic Shanghai synthetic resin plant 1149,6895, and the electric property of several insullac such as external Britain rutherford experiment chamber CTD-101K relatively.
Table 3 is listed the air content after insullac of the present invention (LH-5) saturating machine and the curing thereof.
Table 4 is listed insullac of the present invention (LH-5) and domestic Shanghai synthetic resin plant 1149,6895, external Britain rutherford experiment chamber CTD-101K, and 71A, the cold and hot shrinkage coefficient of several insullac such as 79 is relatively.
Table 1:
The performance sample Tensile strength (MPa) chamber 77K Shearing resistance (MPa) chamber 77K Shock strength (kg.cm/cm 2) Room temperature liquid nitrogen cycle index
?LH-5 >35???>40. >13.1??????????>15.2 >16.2 >20
?1149 ?31????33.5 ?6.0????????????7.4 ?10.7 <5
?6895 ?34????36 ?8.0????????????8.3 ?13.4 <5
?RAL1-PH ?8.4±0.8???????8.9±0.6
?01 ?8.7±0.8???????12±0.2
?02 ?7.8±1.5???????11±1.6
?10 ?8.6±0.4???????12.8±0.
?20 ?9.3±0.4???????9.8±1.8
?30 ?6.2±0.7???????11.1±0.2
?CTD-101K ?10.2???????????18.0 <20
Table 2:
The performance sample ρ s(Ω) ρ v(Ω.m) E B(KV/mm) tgδ
?LH-5 >3.5×10 16 >2.1×10 17 >28.4 <0.0017
?1149 ?1.2×10 14 6.5×10 16 30.5 ?0.0016
?6895 ?3.9×10 14 4.5×10 16 37.2 ?0.012
?CTD-101K >26
Table 3:
Air content (%) Viscosity (being coated with 4) 40 ℃ (S) Viscosity less than time of 75S (hour)
????<1.7 ????<63 ????>10
Table 4:
Insullac ??LH-5 ?1149 ?6895 ?CTD-101K ?71A ?79
The cold and hot contraction of room temperature liquid nitrogen system <0.0083 ?0.011 ?0.013 ?0.013 ?0.010 ?0.011
Embodiment
Embodiment 1:
At first Resins, epoxy 80 grams and toughness reinforcing epoxy 5 grams are mixed and heated to 150 ~ 250 ℃, the degassing, dewater and slowly add nano silicon 5 grams after 1~4 hour again, slowly be cooled to room temperature after fully stirring, nano silicon is suspended in the Resins, epoxy, adds solidifying agent acid anhydrides 50 grams at last again and solidify condition of cure: 80~130 ℃ solidified 1~2 hour down, 140~150 ℃ solidified 1~2 hour, and 160~190 ℃ solidified 5~15 hours.
Embodiment 2:
At first Resins, epoxy 120 grams and toughness reinforcing epoxy 40 grams are mixed and heated to 150~250 ℃, the degassing, dewater and slowly add nano silicon 15 grams after 1~4 hour again, r-aminopropyl triethoxysilane 5 grams, slowly be cooled to room temperature after fully stirring, nano silicon is suspended in the Resins, epoxy, adds solidifying agent acid anhydrides 130 grams at last again and solidify.Condition of cure: 80~130 ℃ solidified 1~2 hour down, and 140~150 ℃ solidified 1~2 hour, and 160~190 ℃ solidified 5~15 hours.
Embodiment 3:
At first Resins, epoxy 100 grams and toughness reinforcing epoxy 30 grams are mixed and heated to 150~250 ℃, the degassing, dewater and slowly add nano silicon 10 grams after 1~4 hour again, r-aminopropyl triethoxysilane 1 gram, slowly be cooled to room temperature after fully stirring, nano silicon is suspended in the Resins, epoxy, adds solidifying agent acid anhydrides 100 grams at last again and solidify.Condition of cure: 80~130 ℃ solidified 1~2 hour down, and 140~150 ℃ solidified 1~2 hour, and 160~190 ℃ solidified 5~15 hours.
Embodiment 4:
At first Resins, epoxy 90 grams and toughness reinforcing epoxy 20 grams are mixed and heated to 150~250 ℃, the degassing, dewater and slowly add nano silicon 8 grams after 1~4 hour again, r-aminopropyl triethoxysilane 2 grams, slowly be cooled to room temperature after fully stirring, nano silicon is suspended in the Resins, epoxy, adds solidifying agent acid anhydrides 95 grams at last again and solidify.Condition of cure: 80~130 ℃ solidified 1~2 hour down, and 140~150 ℃ solidified 1~2 hour, and 160~190 ℃ solidified 5~15 hours.
Embodiment 5:
At first Resins, epoxy 110 grams and toughness reinforcing epoxy 35 grams are mixed and heated to 150~250 ℃, the degassing, dewater and slowly add nano silicon 7 grams after 1~4 hour again, r-aminopropyl triethoxysilane 4 grams, slowly be cooled to room temperature after fully stirring, nano silicon is suspended in the Resins, epoxy, adds solidifying agent acid anhydrides 105 grams at last again and solidify.Condition of cure: 80~130 ℃ solidified 1~2 hour down, and 140~150 ℃ solidified 1~2 hour, and 160~190 ℃ solidified 5~15 hours.
Embodiment 6:
At first Resins, epoxy 120 grams and toughness reinforcing epoxy 40 grams are mixed and heated to 150~250 ℃, the degassing, dewater and slowly add nano silicon 15 grams after 1~4 hour again, r-glycidyl ether oxygen propyl trimethoxy silicane 5 grams, slowly be cooled to room temperature after fully stirring, nano silicon is suspended in the Resins, epoxy, adds solidifying agent acid anhydrides 130 grams at last again and solidify.Condition of cure: 80~130 ℃ solidified 1~2 hour down, and 140~150 ℃ solidified 1~2 hour, and 160~190 ℃ solidified 5~15 hours.
Embodiment 7:
At first Resins, epoxy 100 grams and toughness reinforcing epoxy 30 grams are mixed and heated to 150~250 ℃, the degassing, dewater and slowly add nano silicon 10 grams after 1~4 hour again, r-(metacryloxy) propyl trimethoxy silicane 1 gram, slowly be cooled to room temperature after fully stirring, nano silicon is suspended in the Resins, epoxy, adds solidifying agent acid anhydrides 100 grams at last again and solidify.Condition of cure: 80~130 ℃ solidified 1~2 hour down, and 140~150 ℃ solidified 1~2 hour, and 160~190 ℃ solidified 5~15 hours.

Claims (7)

1, the high-strength epoxy impregnating varnish that uses under a kind of utmost point low temperature is characterized in that with Resins, epoxy and epoxy resin toughened mixture be host, and having toughness reinforcing acid anhydrides is solidifying agent, and the nano silicon filler is that toughener is prepared from.
2,, the high-strength epoxy impregnating varnish that utmost point low temperature according to claim 1 uses down, it is characterized in that adopting earlier the coupling agent treatment Nano filling, prevent that it is agglomerating because of surface action power, described coupling agent can be r-aminopropyl triethoxysilane, r-glycidyl ether oxygen propyl trimethoxy silicane, r-(metacryloxy) propyl trimethoxy silicane.
3, the high-strength epoxy impregnating varnish that uses under the utmost point low temperature according to claim 1 is characterized in that its formulation by weight is:
80~120 parts of Resins, epoxy
5~40 parts of toughness reinforcing epoxies
50~130 parts on acid anhydrides
5~15 parts of nano silicon fillers.
4, the high-strength epoxy impregnating varnish that uses under the utmost point low temperature according to claim 1 is characterized in that its formulation by weight is:
80~120 parts of Resins, epoxy
5~40 parts of toughness reinforcing epoxies
50~130 parts on acid anhydrides
5~15 parts of nano silicon fillers
1~5 part of coupling agent.
5, the preparation method of the high-strength epoxy impregnating varnish that uses under the utmost point low temperature according to claim 1, it is characterized in that at first with Resins, epoxy and epoxy resin toughened mixing, be heated to 150~250 ℃, vacuumize, dewatered 1~4 hour, and slowly added Nano filling again, slowly be cooled to room temperature after fully stirring through coupling agent treatment, Nano filling is suspended in the resin, adds anhydride curing agent at last again.
6, the preparation method of the high-strength epoxy impregnating varnish that uses down of utmost point low temperature according to claim 1 is characterized in that described coupling agent treatment is meant coupling agent and Nano filling mixed to mix thoroughly.
7, the using method of the high-strength epoxy impregnating varnish that uses down of utmost point low temperature according to claim 1, it is characterized in that condition of cure: 80~130 ℃ solidified 1~2 hour down, and 140~150 ℃ solidified 1~2 hour, and 160~190 ℃ solidified 5~15 hours.
CNB031128661A 2003-02-21 2003-02-21 High-strength epoxy impregnating varnish used at extremely low temperature and preparation method and use method thereof Expired - Fee Related CN100335574C (en)

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Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1320020C (en) * 2004-07-02 2007-06-06 大连理工大学 Epoxy resin complex with long chemical storage stability and temperature thixotropy
CN100462384C (en) * 2006-06-22 2009-02-18 上海交通大学 A kind of preparation method of epoxy vacuum pressure impregnation resin
CN101789654A (en) * 2010-02-26 2010-07-28 株洲敏锐轨道电气有限责任公司 Insulating method and device of oil pump motor stator of electric locomotive transformer powered up by frequency converter
CN102684407A (en) * 2012-05-23 2012-09-19 永济新时速电机电器有限责任公司 Method for protecting and fixing assembled permanent magnet in large-power permanent magnet motor
CN102690496A (en) * 2012-06-08 2012-09-26 苏州巨峰电气绝缘系统股份有限公司 Nano modified epoxy vacuum pressure impregnation resin and preparation method thereof
CN103555136A (en) * 2013-10-25 2014-02-05 安徽文峰电子科技集团有限公司 Epoxy impregnating varnish and preparation method thereof
CN103571301A (en) * 2013-09-29 2014-02-12 武汉材料保护研究所 High bonding-strength insulating paint for insulating protection layer of titanium alloy surface
CN108976991A (en) * 2018-07-10 2018-12-11 丹阳市沃德立电工材料有限公司 A kind of high resistant anticorona varnish and preparation method thereof applied to HV Electric Machine Coil
CN110776806A (en) * 2019-10-21 2020-02-11 王利玲 Hyperbranched polymer-SiO 2Modified epoxy resin insulating material and preparation method thereof

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH05287219A (en) * 1992-04-03 1993-11-02 Nippon Kayaku Co Ltd Epoxy resin powder coating material
CN1197098A (en) * 1997-04-24 1998-10-28 中国科学院低温技术实验中心 Low temperature adhesives and curing agents for low temperature adhesives
JP3389533B2 (en) * 1999-06-30 2003-03-24 株式会社日立製作所 Epoxy resin composition and molded coil

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1320020C (en) * 2004-07-02 2007-06-06 大连理工大学 Epoxy resin complex with long chemical storage stability and temperature thixotropy
CN100462384C (en) * 2006-06-22 2009-02-18 上海交通大学 A kind of preparation method of epoxy vacuum pressure impregnation resin
CN101789654A (en) * 2010-02-26 2010-07-28 株洲敏锐轨道电气有限责任公司 Insulating method and device of oil pump motor stator of electric locomotive transformer powered up by frequency converter
CN101789654B (en) * 2010-02-26 2012-12-26 株洲敏锐轨道电气有限责任公司 Insulating method and device of oil pump motor stator of electric locomotive transformer powered up by frequency converter
CN102684407A (en) * 2012-05-23 2012-09-19 永济新时速电机电器有限责任公司 Method for protecting and fixing assembled permanent magnet in large-power permanent magnet motor
CN102690496A (en) * 2012-06-08 2012-09-26 苏州巨峰电气绝缘系统股份有限公司 Nano modified epoxy vacuum pressure impregnation resin and preparation method thereof
CN103571301A (en) * 2013-09-29 2014-02-12 武汉材料保护研究所 High bonding-strength insulating paint for insulating protection layer of titanium alloy surface
CN103571301B (en) * 2013-09-29 2016-05-18 武汉材料保护研究所 A kind of high bond strength coatings for titanium alloy surface insulating protective layer
CN103555136A (en) * 2013-10-25 2014-02-05 安徽文峰电子科技集团有限公司 Epoxy impregnating varnish and preparation method thereof
CN108976991A (en) * 2018-07-10 2018-12-11 丹阳市沃德立电工材料有限公司 A kind of high resistant anticorona varnish and preparation method thereof applied to HV Electric Machine Coil
CN110776806A (en) * 2019-10-21 2020-02-11 王利玲 Hyperbranched polymer-SiO 2Modified epoxy resin insulating material and preparation method thereof

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