绝缘材料
絕緣材料
절연재료
Insulating Materials
2015年
10期
21-25
,共5页
骆崛逵%严辉%张雪平%李桢林%范和平
駱崛逵%嚴輝%張雪平%李楨林%範和平
락굴규%엄휘%장설평%리정림%범화평
环氧树脂%灌封胶%硅微粉%气相SiO2%改性
環氧樹脂%灌封膠%硅微粉%氣相SiO2%改性
배양수지%관봉효%규미분%기상SiO2%개성
epoxy resin%pouring sealant%silicon powder%aerosil%modification
采用γ-氨丙基三乙氧基硅烷(KH-550)对硅微粉、气相SiO2进行表面改性后,分别使用单一的硅微粉、气相SiO2及复配的硅微粉/气相SiO2作为填料,对环氧树脂电子灌封胶进行改性,制得二元或三元体系的复合材料,并对其力学性能进行比较分析。结果表明:与采用单一填料改性的二元体系相比,采用硅微粉和气相SiO2组合填料改性的三元体系环氧复合材料的力学性能较好;当m(环氧树脂)∶m(硅微粉)∶m(气相SiO2)=100∶120∶3时,复合材料的弯曲强度达到最大值161.44 MPa。
採用γ-氨丙基三乙氧基硅烷(KH-550)對硅微粉、氣相SiO2進行錶麵改性後,分彆使用單一的硅微粉、氣相SiO2及複配的硅微粉/氣相SiO2作為填料,對環氧樹脂電子灌封膠進行改性,製得二元或三元體繫的複閤材料,併對其力學性能進行比較分析。結果錶明:與採用單一填料改性的二元體繫相比,採用硅微粉和氣相SiO2組閤填料改性的三元體繫環氧複閤材料的力學性能較好;噹m(環氧樹脂)∶m(硅微粉)∶m(氣相SiO2)=100∶120∶3時,複閤材料的彎麯彊度達到最大值161.44 MPa。
채용γ-안병기삼을양기규완(KH-550)대규미분、기상SiO2진행표면개성후,분별사용단일적규미분、기상SiO2급복배적규미분/기상SiO2작위전료,대배양수지전자관봉효진행개성,제득이원혹삼원체계적복합재료,병대기역학성능진행비교분석。결과표명:여채용단일전료개성적이원체계상비,채용규미분화기상SiO2조합전료개성적삼원체계배양복합재료적역학성능교호;당m(배양수지)∶m(규미분)∶m(기상SiO2)=100∶120∶3시,복합재료적만곡강도체도최대치161.44 MPa。
The silicon powder and aerosil were modified by γ-Aminopropyltriethoxysilane (KH-550). The silicon powder, aerosil, and silicon powder/aerosil were used as filler to modify epoxy resin pouring seal-ant respectively, and two binary systems and a ternary system composite was prepared, and their mechani-cal properties were analyzed. The results show that the mechanical properties of the ternary system ep-oxy composite filled by silicon powder/aerosil are better. When the mass ratio among eopxy resin, silicon powder, and aerosil is 100∶120∶3, the bending strength attains maximum, which is 161.44 MPa.