JP2006249165A - Method for producing resin composition for self-adhesive type prepreg - Google Patents
Method for producing resin composition for self-adhesive type prepreg Download PDFInfo
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Abstract
Description
この発明は自己接着型プリプレグ用樹脂組成物の製造方法に関し、さらに詳しくは、樹脂の最低粘度を適正化することによりプリプレグの圧縮強度及び引張強度をバランス良く保持すると共に、ハニカムパネルに適用した場合のハニカムコアへの流動性を良好にして、ハニカムコアとの間の剥離強度を向上させる自己接着型プリプレグ用樹脂組成物の製造方法に関する。 The present invention relates to a method for producing a resin composition for a self-adhesive prepreg, and more specifically, when the compressive strength and tensile strength of a prepreg are maintained in a well-balanced state by optimizing the minimum viscosity of the resin and applied to a honeycomb panel. The present invention relates to a method for producing a resin composition for a self-adhesive prepreg, which improves the fluidity of a honeycomb core to improve the peel strength between the honeycomb core and the honeycomb core.
マトリックス樹脂を溶剤に溶かし、硬化剤や添加剤を混合してクロス、マット、ロービング等に含浸させて得る成形材料としてのプリプレグ(繊維強化複合材料)は、その優れた力学物性等から航空機や自動車をはじめとした産業用途に幅広く使用されている。 A prepreg (fiber reinforced composite material) as a molding material obtained by dissolving a matrix resin in a solvent and mixing a curing agent or additive and impregnating cloth, mat, roving, etc. is an aircraft and automobile due to its excellent mechanical properties. Widely used in industrial applications such as
特に、航空機用の構造材料には、軽量化の観点から、プリプレグを面板としたハニカムパネルが多岐にわたり使用されている。一般に、ハニカムパネルは紙、アルミニウム、アラミド、ガラス、等の素材からなるハニカムコアの両面にプリプレグを接着させることによって製造している。 In particular, honeycomb panels having prepregs as face plates are widely used for aircraft structural materials from the viewpoint of weight reduction. In general, a honeycomb panel is manufactured by adhering a prepreg to both surfaces of a honeycomb core made of a material such as paper, aluminum, aramid, and glass.
従来、ハニカムコアとプリプレグとを接着させるには、ハニカムコアとプリプレグとの間にフィルム状の接着剤を挟み込んで加熱することにより、プリプレグそのものの硬化とプリプレグとハニカムコアとの接着を同時に行なう方法が一般的に採用されてきた。しかしながら、近年は、ハニカムコアの軽量化と成形コストの低減という見地から、プリプレグに使用する樹脂に接着剤と同等の特性を付与することにより、フィルム状の接着剤を使用することなしにハニカムパネルを成形する研究が行なわれている(例えば、特許文献1、2参照)。 Conventionally, in order to bond a honeycomb core and a prepreg, a film-like adhesive is sandwiched between the honeycomb core and the prepreg and heated to simultaneously cure the prepreg itself and bond the prepreg and the honeycomb core. Has generally been adopted. However, in recent years, from the viewpoint of reducing the weight of the honeycomb core and reducing the molding cost, the honeycomb panel can be formed without using a film-like adhesive by giving the resin used for the prepreg the same characteristics as the adhesive. Research has been conducted on molding (see, for example, Patent Documents 1 and 2).
しかしながら、従来のフィルム状の接着剤と同等の特性(特に、剥離強度)を有すると共に、ハニカムパネルの面板としての物性(特に、引張強度、高温時の圧縮強度)を充分に満たし得るような自己接着型プリプレグ用樹脂組成物の開発には未だ至っていないのが現状である。
この発明の目的は、かかる従来の問題点を解消するもので、プリプレグの圧縮強度及び引張強度をバランス良く保持すると共に、ハニカムパネルに適用した場合のハニカムコアとの間の剥離強度を向上させる自己接着型プリプレグ用樹脂組成物の製造方法を提供することにある。 An object of the present invention is to solve such a conventional problem, and to maintain a good balance between the compressive strength and tensile strength of the prepreg and to improve the peel strength with the honeycomb core when applied to a honeycomb panel. It is providing the manufacturing method of the resin composition for adhesion type prepregs.
上記目的を達成するためのこの発明の自己接着型プリプレグ用樹脂組成物の製造方法は、複数種のエポキシ樹脂組成物及び熱可塑性樹脂を混合して重合させる第一ステ−ジング工程と、該第一ステ−ジング工程により得られたエポキシ樹脂組成物に新たな別のエポキシ樹脂組成物及び硬化剤を混合して重合させる第二ステ−ジング工程と、該第二ステ−ジング工程により得られたエポキシ樹脂組成物に新たなエポキシ樹脂、固形ゴム及び硬化剤を混合して最終組成物を得ることを特徴とする。 In order to achieve the above object, a method for producing a self-adhesive prepreg resin composition of the present invention comprises a first staging step in which a plurality of epoxy resin compositions and a thermoplastic resin are mixed and polymerized; A second staging step in which another epoxy resin composition and a curing agent mixed with the epoxy resin composition obtained in one staging step are polymerized, and obtained by the second staging step A new epoxy resin, solid rubber and a curing agent are mixed with the epoxy resin composition to obtain a final composition.
この発明によれば、エポキシ樹脂組成物の重合工程を2段階にすると共に、最初の重合工程において熱可塑性樹脂を混合し、2段階目の重合工程により得られたエポキシ樹脂組成物に新たなエポキシ樹脂組成物と固形ゴムとを加えて最終組成物としたので、最初の重合工程におけるウレタン樹脂の混合により、最終組成物として得られたエポキシ樹脂の最低粘度が適正化されて、プリプレグの圧縮強度及び引張強度をバランス良く保持すると共に、ハニカムパネルに適用した場合のハニカムコアへの流動性を良好にして、ハニカム壁を充分に濡らして良好なフィレットを形成し、これによりプリプレグとハニカムコアとの間の剥離強度を向上させることができる。しかも、エポキシ樹脂の製造方法としては、特段の工程を付加するものではないので、作業性を低下させることがない。 According to this invention, the polymerization process of the epoxy resin composition is made into two stages, and a thermoplastic resin is mixed in the first polymerization process, and a new epoxy is added to the epoxy resin composition obtained by the second polymerization process. Since the final composition was made by adding the resin composition and solid rubber, the minimum viscosity of the epoxy resin obtained as the final composition was optimized by mixing the urethane resin in the first polymerization step, and the compressive strength of the prepreg In addition, the tensile strength is maintained in a well-balanced state, and the fluidity to the honeycomb core when applied to a honeycomb panel is improved, so that the honeycomb wall is sufficiently wetted to form a good fillet, thereby forming the prepreg and the honeycomb core. The peel strength between them can be improved. In addition, since the epoxy resin manufacturing method does not add any special process, workability is not deteriorated.
以下、この発明の構成につき詳細に説明する。 The configuration of the present invention will be described in detail below.
この発明の自己接着型プリプレグ用樹脂組成物の製造方法は、複数種のエポキシ樹脂組成物及び熱可塑性樹脂を混合して重合させる第一ステ−ジング工程と、この第一ステ−ジング工程により得られたエポキシ樹脂組成物に新たな別のエポキシ樹脂組成物及び硬化剤を混合して重合させる第二ステ−ジング工程と、この第二ステ−ジング工程により得られたエポキシ樹脂組成物に新たなエポキシ樹脂、固形ゴム及び硬化剤を混合して最終組成物を得るものである。 The manufacturing method of the resin composition for self-adhesive prepreg of the present invention is obtained by a first staging step of mixing and polymerizing a plurality of types of epoxy resin compositions and a thermoplastic resin, and the first staging step. A second staging step in which another epoxy resin composition and a curing agent are mixed and polymerized with the obtained epoxy resin composition, and a new staging step is added to the epoxy resin composition obtained by the second staging step. An epoxy resin, solid rubber and a curing agent are mixed to obtain a final composition.
このように第一ステ−ジング工程において熱可塑性樹脂を混合したことにより、最終組成物としてのエポキシ樹脂は最低粘度が適正化されて、プリプレグの圧縮強度及び引張強度をバランス良く保持すると共に、ハニカムパネルに適用した場合のハニカムコアへの流動性を良好にして、ハニカム壁を充分に濡らして良好なフィレットを形成し、これによりプリプレグとハニカムコアとの間の剥離強度を向上させることができる。しかも、エポキシ樹脂の製造方法としては、特段の工程を付加するものではないので、作業性を低下させることがない。 As described above, by mixing the thermoplastic resin in the first staging step, the epoxy resin as the final composition is optimized for the minimum viscosity, and the compressive strength and tensile strength of the prepreg are maintained in a well-balanced manner. When applied to a panel, the fluidity to the honeycomb core is improved, and the honeycomb wall is sufficiently wetted to form a good fillet, whereby the peel strength between the prepreg and the honeycomb core can be improved. In addition, since the epoxy resin manufacturing method does not add any special process, workability is not deteriorated.
エポキシ樹脂としては、アミン類、フェノ−ル類、炭素炭素二重結合を有する化合物を前駆体とするエポキシ樹脂が好ましく使用される。アミン類を前駆体とするエポキシ樹脂としては、テトラグリシジルジアミノジフェニルメタン、トリグリシジルーp−アミノフェノール、トリグリシジルアミノクレゾールの各種異性体等が挙げられる。この中でもテトラグリシジルジアミノジフェニルメタンは耐熱性に優れるため、航空機用ハニカムパネルの面板に使用するプリプレグ用樹脂組成物として好ましく使用される。 As the epoxy resin, amine resins, phenols, and epoxy resins having a compound having a carbon-carbon double bond as a precursor are preferably used. Examples of the epoxy resin having an amine as a precursor include various isomers of tetraglycidyldiaminodiphenylmethane, triglycidyl p-aminophenol, and triglycidylaminocresol. Among these, tetraglycidyldiaminodiphenylmethane is preferably used as a resin composition for a prepreg used for a face plate of an aircraft honeycomb panel because it is excellent in heat resistance.
また、フェノ−ル類を前駆体とするエポキシ樹脂組成物としては、ビスフェノ−ルA型エポキシ樹脂、ビスフェノ−ルF型エポキシ樹脂、ビスフェノ−ルS型エポキシ樹脂、フェノールノボラック型エポキシ樹脂、クレゾールノボラック型エポキシ樹脂、レゾルシノール型エポキシ樹脂、等が挙げられる。 Examples of the epoxy resin composition having phenol as a precursor include bisphenol A type epoxy resin, bisphenol F type epoxy resin, bisphenol S type epoxy resin, phenol novolac type epoxy resin, cresol novolac. Type epoxy resin, resorcinol type epoxy resin, and the like.
さらに、炭素炭素二重結合を有する化合物を前駆体とするエポキシ樹脂としては、ビフェニル型エポキシ樹脂、ジシクロペンタジエン型エポキシ樹脂、等が挙げられ、特にナフタレン骨格を有するエポキシ樹脂は、耐吸水性や耐熱性に優れることから、航空機用ハニカムパネルの面板に使用するプリプレグ用樹脂組成物として好ましく使用される。 Further, examples of the epoxy resin having a compound having a carbon-carbon double bond as a precursor include a biphenyl type epoxy resin, a dicyclopentadiene type epoxy resin, and the like. In particular, an epoxy resin having a naphthalene skeleton has water absorption resistance and Since it is excellent in heat resistance, it is preferably used as a resin composition for a prepreg used for a face plate of an aircraft honeycomb panel.
この発明において、プリプレグ用樹脂組成物の基材となるエポキシ樹脂は、上述する各種のエポキシ樹脂の中から選ばれた複数種のエポキシ樹脂を適宜配合して用いるとよい。好ましくは、2官能のエポキシ樹脂と3官能以上の多官能のエポキシ樹脂とを配合するとよい。これにより、樹脂の流動性と硬化後の耐熱性とを兼ね備えたエポキシ樹脂とすることができる。 In this invention, the epoxy resin used as the base material of the resin composition for prepreg may be appropriately mixed with a plurality of types of epoxy resins selected from the various epoxy resins described above. Preferably, a bifunctional epoxy resin and a trifunctional or higher polyfunctional epoxy resin may be blended. Thereby, it can be set as the epoxy resin which has the fluidity | liquidity of resin, and the heat resistance after hardening.
上述する第一ステージング工程において混合する熱可塑性樹脂としては、主鎖に炭素炭素結合、アミド結合、イミド結合、ウレタン結合、エステル結合、エ−テル結合、カ−ボネ−ト結合、カルボニル結合、シロキサン結合、スルフォン結合、などを含有する熱可塑性樹脂が使用される。これらの中でも、特にウレタン樹脂を使用するとよい。 The thermoplastic resin mixed in the first staging step described above includes carbon-carbon bonds, amide bonds, imide bonds, urethane bonds, ester bonds, ether bonds, carbonate bonds, carbonyl bonds, siloxanes in the main chain. Thermoplastic resins containing bonds, sulfone bonds, etc. are used. Among these, it is particularly preferable to use a urethane resin.
さらに、熱可塑性樹脂の配合割合を、第一ステージング工程におけるエポキシ樹脂100重量部に対して18重量部以上、好ましくは20重量部以上にするとよい。熱可塑性樹脂の配合割合が18重量部未満では、エポキシ樹脂の最低粘度が低下して、ハニカムパネルに適用した場合のハニカム壁に良好なフィレットを形成することが難しくなる。 Furthermore, the blending ratio of the thermoplastic resin may be 18 parts by weight or more, preferably 20 parts by weight or more with respect to 100 parts by weight of the epoxy resin in the first staging step. When the blending ratio of the thermoplastic resin is less than 18 parts by weight, the minimum viscosity of the epoxy resin is lowered, and it becomes difficult to form a good fillet on the honeycomb wall when applied to the honeycomb panel.
この発明における第二ステ−ジング工程後に加える固形ゴムとしては、エポキシ樹脂との相溶性の面から、ブタジエンとアクリロニトリルとのランダムコポリマ−であるアクリロニトリル−ブタジエン共重合体が好ましく使用される。さらに、エポキシ樹脂との接着性を高めるために官能基を有する固形ゴムが好ましく使用される。官能基としては、カルボキシル基やアミノ基が挙げられるが、特にカルボキシル基を含有する固形アクリロニトリル−ブタジエンゴムが好ましい。 As the solid rubber added after the second staging step in the present invention, an acrylonitrile-butadiene copolymer which is a random copolymer of butadiene and acrylonitrile is preferably used from the viewpoint of compatibility with the epoxy resin. Furthermore, a solid rubber having a functional group is preferably used in order to enhance the adhesion with the epoxy resin. Examples of the functional group include a carboxyl group and an amino group, and a solid acrylonitrile-butadiene rubber containing a carboxyl group is particularly preferable.
さらに、固形ゴムの配合割合を、最終組成物におけるエポキシ樹脂100重量部に対して5〜7重量部とするとよい。これにより、樹脂の最低粘度を上昇させて成形時の樹脂過剰流出を防ぎながら靱性を確保すると共に、接着性を向上させることができる。さらに、プリプレグの圧縮強度と引張強度とを一層バランス良く向上させることができる。固形ゴムの配合割合が5重量部未満では樹脂の最低粘度が低下し過ぎて成形時の樹脂過剰流出が防げなくなると共に接着性が低下することになり、7重量部超では樹脂の最低粘度が高くなり過ぎて成形時の樹脂流出が得られなくなる。 Furthermore, the blending ratio of the solid rubber is preferably 5 to 7 parts by weight with respect to 100 parts by weight of the epoxy resin in the final composition. As a result, it is possible to increase the minimum viscosity of the resin and prevent tough resin outflow during molding to ensure toughness and improve adhesiveness. Furthermore, the compressive strength and tensile strength of the prepreg can be improved with a better balance. If the blending ratio of the solid rubber is less than 5 parts by weight, the minimum viscosity of the resin will be too low to prevent excessive resin outflow at the time of molding and the adhesiveness will be reduced. If it exceeds 7 parts by weight, the minimum viscosity of the resin will be high. It becomes too much and resin outflow at the time of molding cannot be obtained.
この発明に使用される硬化剤としては、エポキシ基と反応し得る活性基を有する化合物であれば、特に限定されるものではない。好ましくは、アミノ基、酸無水物基、アジド基を有する化合物が適している。さらに具体的には、ジシアンジアミド、ジアミノジフェニルメタン、ジアミノジフェニルスルフォンの各種異性体、アミノ安息香酸エステル類、各種酸無水物、フェノールノボラック樹脂、クレゾールノボラック樹脂、ポリフェノール化合物、等が挙げられる。 The curing agent used in the present invention is not particularly limited as long as it is a compound having an active group capable of reacting with an epoxy group. Preferably, a compound having an amino group, an acid anhydride group, or an azide group is suitable. More specifically, dicyandiamide, diaminodiphenylmethane, various isomers of diaminodiphenylsulfone, aminobenzoic acid esters, various acid anhydrides, phenol novolac resin, cresol novolac resin, polyphenol compound, and the like can be mentioned.
上述するように、この発明の自己接着型プリプレグ用樹脂組成物の製造方法は、エポキシ樹脂組成物の重合工程を2段階にすると共に、最初の重合工程においてウレタン樹脂を混合し、2段階目の重合工程により得られたエポキシ樹脂組成物に新たなエポキシ樹脂組成物と固形ゴムとを加えて最終組成物としたので、最初の重合工程におけるウレタン樹脂の混合により、最終組成物として得られたエポキシ樹脂の最低粘度が適正化されて、プリプレグの圧縮強度及び引張強度をバランス良く保持すると共に、ハニカムパネルに適用した場合のハニカム壁に良好なフィレットを形成し、ハニカムコアとの間の剥離強度を向上させることから、特に航空機用のハニカムパネルの面板用として好ましく利用される。 As described above, the method for producing a resin composition for a self-adhesive prepreg according to the present invention comprises a two-stage polymerization process for an epoxy resin composition and a urethane resin mixed in the first polymerization process. Since a new epoxy resin composition and solid rubber were added to the epoxy resin composition obtained in the polymerization step to obtain a final composition, the epoxy obtained as the final composition by mixing the urethane resin in the first polymerization step The minimum viscosity of the resin is optimized and the compressive strength and tensile strength of the prepreg are maintained in a well-balanced manner, and a good fillet is formed on the honeycomb wall when applied to a honeycomb panel, and the peel strength between the honeycomb core is increased. Since it improves, it is preferably used particularly for a face panel of an aircraft honeycomb panel.
表1のようにエポキシ樹脂を構成する組成、重量及び重合工程を異ならせて、表の中段に示す「最終組成物」からなる本発明によるエポキシ樹脂(実施例1)及び比較によるエポキシ樹脂(比較例1〜3)を作製すると共に、それぞれのエポキシ樹脂を使用して以下に示す方法により4種のプリプレグを作製した。なお、比較例2ではエポキシ樹脂を重合させる工程を1段階とし、比較例3ではエポキシ樹脂を重合させる工程を含んでいない。
〔プリプレグの作製〕
それぞれの樹脂組成物をリバ−スロ−ルコ−タ−を用いて離型紙上に塗布し、樹脂目付65g/m2 の樹脂フィルムを作製した。次いで、この樹脂フィルム2枚を平織状に織られた炭素繊維(東レ(株)社製、T300−3K)の両面から重ね合わせて、加熱加圧して樹脂組成物を炭素繊維に含浸させた。樹脂組成物を含浸させた後、樹脂フィルムを剥離して、剥離面の片面にポリエチレンフィルムを配して巻き取り、プリプレグシ−トを得た。
The epoxy resin according to the present invention (Example 1) and the comparative epoxy resin (comparison) comprising the “final composition” shown in the middle part of the table, with different compositions, weights and polymerization steps constituting the epoxy resin as shown in Table 1. While producing Examples 1-3), 4 types of prepregs were produced by the method shown below using each epoxy resin. In Comparative Example 2, the step of polymerizing the epoxy resin is one stage, and in Comparative Example 3, the step of polymerizing the epoxy resin is not included.
[Preparation of prepreg]
Each resin composition was applied onto a release paper using a reverse roll coater to prepare a resin film having a resin basis weight of 65 g / m 2 . Next, the two resin films were superposed on both sides of a plain weave carbon fiber (T300-3K, manufactured by Toray Industries, Inc.) and heated and pressed to impregnate the carbon fiber with the resin composition. After impregnating the resin composition, the resin film was peeled off, and a polyethylene film was placed on one side of the peeled surface and wound up to obtain a prepreg sheet.
上述する5種の樹脂組成物について以下の方法により最低粘度を測定すると共に、これら5種の樹脂組成物を含浸させたプリプレグについて以下の試験方法により有孔圧縮強度、平面引張強度及び剥離強度を測定し、これらの結果を表1に併記した。 The minimum viscosity of the five types of resin compositions described above is measured by the following method, and the prepreg impregnated with these five types of resin compositions is measured for porous compressive strength, plane tensile strength and peel strength by the following test methods. Measurements were made and the results are shown in Table 1.
〔最低粘度〕
レオメトリックス社製の動的粘弾性装置(ARES−II)を使用して、パラレルプレ−
ト法(直径25.4mm)により、昇温速度2.8℃/分、周波数10rad/秒、歪み1%の条件の下でそれぞれの樹脂の最低粘度(Pa・s)を測定し、その結果を表1に記載した。
[Minimum viscosity]
Using a dynamic viscoelastic device (ARES-II) manufactured by Rheometrics,
The minimum viscosity (Pa · s) of each resin was measured under the conditions of a heating rate of 2.8 ° C./min, a frequency of 10 rad / sec, and a strain of 1% by the G method (diameter 25.4 mm). Are listed in Table 1.
〔有孔圧縮強度〕
それぞれの樹脂からなるプリプレグを16枚積層してバッグに入れ、これをオ−トクレ−ブ内で180℃、2時間(昇温速度2.8℃/分)加熱し、硬化させて成形板を作製した。この間、オ−トクレ−ブ内を圧空で0.32MPaに加圧した。
[Perforated compressive strength]
Sixteen prepregs made of each resin are laminated and placed in a bag, which is heated in an autoclave at 180 ° C. for 2 hours (heating rate: 2.8 ° C./min) and cured to form a molded plate. Produced. During this time, the inside of the autoclave was pressurized to 0.32 MPa with compressed air.
得られた成形板を所定の寸法に加工して各試験片を作製し、ボ−イング社試験法に準拠して、試験条件を(1)23℃における乾燥状態、及び(2)93℃における吸湿状態、とした場合の各試験片の有孔圧縮強度(MPa)を測定した。なお、吸湿状態における各試験片としては、70℃の温水に2週間浸した後、取り出した試験片を用いた。 The obtained molded plate was processed into a predetermined size to produce each test piece, and the test conditions were (1) dry state at 23 ° C. and (2) 93 ° C. The perforated compressive strength (MPa) of each test piece in the moisture absorption state was measured. In addition, as each test piece in a hygroscopic state, the test piece taken out after being immersed in warm water of 70 ° C. for 2 weeks was used.
〔平面引張強度〕
上記〔有孔圧縮強度〕の測定の際に使用した成形板を所定の寸法に加工して各試験片を作製し、MIL−STD−401に準拠して、23℃(乾燥状態)における各試験片の平面引張強度(MPa)を測定した。
[Plane tensile strength]
The molded plate used in the measurement of the above [Perforated compressive strength] is processed into predetermined dimensions to produce each test piece, and each test at 23 ° C. (dry state) according to MIL-STD-401. The plane tensile strength (MPa) of the piece was measured.
〔剥離強度〕
それぞれの樹脂からなるプリプレグを2枚積層し、これをハニカムコア(昭和飛行機工業(株)社製、ノ−メックスSAH−1/8−8.0)の両面に配置した後バッグに入れ、これをオ−トクレ−ブ内で180℃、2時間(昇温速度2.8℃/分)加熱し、硬化させてハニカムパネルを作製した。この間、オ−トクレ−ブ内を圧空で0.32MPaに加圧した。
[Peel strength]
Two prepregs made of each resin are laminated and placed on both sides of a honeycomb core (Nomex SAH-1 / 8-8.0, manufactured by Showa Aircraft Industry Co., Ltd.) and placed in a bag. Was heated in an autoclave at 180 ° C. for 2 hours (heating rate: 2.8 ° C./min) and cured to prepare a honeycomb panel. During this time, the inside of the autoclave was pressurized to 0.32 MPa with compressed air.
得られたハニカムパネルを所定の寸法に加工し、ASTM D1781に準拠して、23℃(乾燥状態)における各試験片の剥離強度(lb−in/3in)を測定した。
The obtained honeycomb panel was processed into a predetermined size, and the peel strength (lb-in / 3 in) of each test piece at 23 ° C. (dry state) was measured in accordance with ASTM D1781.
表1の特性評価結果より、実施例1のエポキシ樹脂組成物は、熱可塑性樹脂を混合後に二段階ステージングを施した結果、比較例1〜3の最低粘度と比較して高粘度を示し、プリプレグの有孔圧縮強度と平面引張強度が同等でありながら、ハニカムパネルに適用した場合の剥離強度が高く、優れた自己接着性を示すことが確認された。これに対して、比較例1〜3に示す熱可塑性樹脂を混合せずにステージング工程を施したエポキシ樹脂組成物、及び熱可塑性樹脂を混合せずにステージング工程もほどこしていないエポキシ樹脂組成物は、ハニカムパネルにおける剥離強度が低く、充分な自己接着性が認められなかった。
From the property evaluation results in Table 1, the epoxy resin composition of Example 1 was subjected to two-stage staging after mixing the thermoplastic resin. As a result, the epoxy resin composition showed higher viscosity than the lowest viscosity of Comparative Examples 1 to 3, and the prepreg While the porous compressive strength and the plane tensile strength of each were equal, the peel strength when applied to a honeycomb panel was high, and excellent self-adhesiveness was exhibited. On the other hand, the epoxy resin composition which performed the staging process without mixing the thermoplastic resin shown in Comparative Examples 1 to 3, and the epoxy resin composition which has not been subjected to the staging process without mixing the thermoplastic resin The peel strength of the honeycomb panel was low, and sufficient self-adhesion was not recognized.
Claims (5)
The method for producing a resin composition for self-adhesive prepreg according to any one of claims 1 to 4, wherein a blending ratio of the solid rubber is 5 to 7 parts by weight with respect to 100 parts by weight of the epoxy resin in the final composition. .
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JP2001040122A (en) * | 1999-05-25 | 2001-02-13 | Toray Ind Inc | Prepreg and fiber reinforced composite material |
JP2001031838A (en) * | 1999-07-22 | 2001-02-06 | Toho Rayon Co Ltd | Epoxy resin composition for self-adhesive facing material and prepreg |
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