JP3127947B2 - Composite molding - Google Patents

Composite molding

Info

Publication number
JP3127947B2
JP3127947B2 JP06213000A JP21300094A JP3127947B2 JP 3127947 B2 JP3127947 B2 JP 3127947B2 JP 06213000 A JP06213000 A JP 06213000A JP 21300094 A JP21300094 A JP 21300094A JP 3127947 B2 JP3127947 B2 JP 3127947B2
Authority
JP
Japan
Prior art keywords
acm
composite molded
ceramic
resin
strength
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
JP06213000A
Other languages
Japanese (ja)
Other versions
JPH0872200A (en
Inventor
芳士郎 舘
俊明 八木
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Sumitomo Bakelite Co Ltd
Original Assignee
Sumitomo Bakelite Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Sumitomo Bakelite Co Ltd filed Critical Sumitomo Bakelite Co Ltd
Priority to JP06213000A priority Critical patent/JP3127947B2/en
Publication of JPH0872200A publication Critical patent/JPH0872200A/en
Application granted granted Critical
Publication of JP3127947B2 publication Critical patent/JP3127947B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【産業上の利用分野】本発明はセラミックと高強度繊維
強化プラスチック(以下、ACMという)から成る複合
成形物においてセラミック(板又は成形物)の側から高
速な飛来物を受けた場合、セラミックの割れを適度に押
え、更に割れた破片が出来るだけ外部へ飛び散らない様
にすると共に、セラミックと反対側のACMのふくらみ
を小さくし、且つACMがセラミックと出来るだけ剥離
しないように、更にACMにて上記複合成形物を包み込
むことにより高速な飛来物に対し優れた耐衝撃性を持つ
軽量な複合成形物に関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a composite molded article made of ceramic and high-strength fiber reinforced plastic (hereinafter, referred to as ACM) when a high-speed flying object is received from the ceramic (plate or molded article) side. Hold the cracks appropriately, keep the broken pieces from scattering to the outside as much as possible, reduce the bulge of the ACM on the opposite side of the ceramic, and further remove the ACM from the ceramic as much as possible with the ACM. The present invention relates to a lightweight composite molded article having excellent impact resistance to high-speed flying objects by enclosing the composite molded article.

【0002】[0002]

【従来の技術】高所から落下又は高速に飛来する物体に
対する耐衝撃体は金属の単体又はその合金あるはセラミ
ックとその裏面にACMを接着等の化学的方法又はボル
ト/ナット等による機械的方法にて固定することにより
軽量で耐衝撃性に優れた複合成形物が得られること(金
属板との組合せについては、特開平3−58835〜5
8837号公報にて開示)は今日では公知の事実であ
る。しかしながら、衝撃力が非常に強い場合、又は数回
以上繰返し同部所に衝撃力が加わる場合、特にセラミッ
ク/ACM複合成形物においては、初回の衝撃力で衝撃
部位周辺のセラミックが破壊され、ACMとも剥離が起
こるので同じ部所に繰り返し衝撃力が加わるとセラミッ
クによる衝撃吸収力が急速に低下し、裏面のACMに直
接衝撃力が加わる場合も生じ、耐衝撃体としては著しく
その機能が低下する現象が起こり、この点を改善する必
要が生じて来た。
2. Description of the Related Art A shock-resistant body against an object falling from a high place or flying at a high speed is a chemical method such as adhesion of ACM to the back surface of a single metal or its alloy or ceramic, or a mechanical method such as a bolt / nut. (A combination with a metal plate is disclosed in JP-A-3-58835-5).
No. 8837) is a known fact today. However, when the impact force is very strong, or when the impact force is repeatedly applied to the same portion several times or more, especially in a ceramic / ACM composite molded article, the ceramic around the impact site is broken by the first impact force, and the ACM When the impact force is repeatedly applied to the same part, the impact absorption force by the ceramic is rapidly reduced, and the impact force may be directly applied to the ACM on the back surface. A phenomenon has arisen, and it is necessary to improve this point.

【0003】[0003]

【発明が解決しようとする課題】本発明はセラミック
(板及び成形物)の裏面にACMを固定することにより
軽量で耐衝撃性の良い複合成形物が得られるとの知見の
もとに更に強力で繰返し衝撃力が加わった場合の耐衝撃
性を大きくする為に種々検討した結果、セラミック/A
CM複合成形物を更にACM(本体と同一材又は異種
材)で全体又は部分的に包み込むことにより、強力で繰
返し衝撃力を受けた際、セラミックの破壊を抑え、その
破片の飛び出しを少くし、セラミック/ACM間の剥離
を減少させ、ACM後部のふくらみを極めて少なくした
耐衝撃性の優れた複合成形物を完成させるに至ったもの
である。
SUMMARY OF THE INVENTION The present invention is based on the finding that by fixing ACM on the back surface of ceramic (plate and molded product), a composite molded product having light weight and good impact resistance can be obtained. As a result of various investigations to increase the impact resistance when a repeated impact force is applied, ceramic / A
By further wrapping the CM composite molded product entirely or partially with ACM (same material or different material as the main body), when repeatedly subjected to strong and repeated impact force, it suppresses the breakage of ceramics and reduces the projection of fragments. This has led to the completion of a composite molded article having excellent impact resistance, in which the separation between the ceramic and the ACM is reduced and the bulge at the rear of the ACM is extremely reduced.

【0004】[0004]

【課題を解決するための手段】本発明は、セラミックと
高強度繊維強化プラスチックからなる複合成形物におい
て、セラミックと高強度繊維強化プラスチックとを積層
してなる複合成形体を高強度繊維強化プラスチックにて
包み込むことを特徴とする複合成形物に関するものであ
る。
SUMMARY OF THE INVENTION The present invention relates to a composite molded article comprising ceramic and high-strength fiber-reinforced plastic, wherein a composite molded article obtained by laminating ceramic and high-strength fiber-reinforced plastic is converted into a high-strength fiber-reinforced plastic. The present invention relates to a composite molded article characterized in that it is wrapped.

【0005】ここに用いられるセラミックは主としてフ
ァインセラミックと呼ばれているもので、アルミナ(純
度90〜99.9)系、窒化ケイ素系、炭化ケイ素系、
ジルコニア系等特に問わない。又セラミック単独及び2
種類以上のセラミックを組み合わせても良い。セラミッ
クの物性としては、ビッカース硬度1000kg/mm2
上、曲げ強度30kgf/mm2 以上、弾性率2.8×104
kg/mm2 以上が好ましい。
The ceramics used here are mainly called fine ceramics and include alumina (purity 90 to 99.9), silicon nitride, silicon carbide, and the like.
It does not matter in particular such as zirconia. Ceramic only and 2
More than two types of ceramics may be combined. The physical properties of the ceramic include a Vickers hardness of 1000 kg / mm 2 or more, a bending strength of 30 kgf / mm 2 or more, and an elastic modulus of 2.8 × 10 4.
kg / mm 2 or more is preferred.

【0006】一方ACMとして用いれる高強度繊維とし
ては引張強度を密度で割った比引張強度が10×106c
m 以上であり、弾性率を密度で割った比弾性率が2.5
×108cm 以上のものである。具体的には、高強度ガラ
ス繊維、カーボン繊維、アラミド繊維、芳香族ポリエス
テル繊維、高強度ポリエチレン繊維、高強度ナイロン繊
維等である。一般のガラス繊維、ナイロン繊維及びポリ
エステル繊維などは該当しない。比引張強度あるいは比
弾性率が前記値以下の繊維を用いた場合、その複合成形
物の耐衝撃性は必ずしも十分ではない。
On the other hand, as high strength fibers used as ACM, specific tensile strength obtained by dividing tensile strength by density is 10 × 10 6 c
m or more, and the specific elastic modulus obtained by dividing the elastic modulus by the density is 2.5
× 10 8 cm or more. Specifically, high-strength glass fiber, carbon fiber, aramid fiber, aromatic polyester fiber, high-strength polyethylene fiber, high-strength nylon fiber, and the like. General glass fiber, nylon fiber, polyester fiber, etc. are not applicable. When fibers having a specific tensile strength or a specific elastic modulus of not more than the above values are used, the impact resistance of the composite molded product is not always sufficient.

【0007】一方、これら高強度繊維に含浸又はコーテ
ィングする樹脂としては、熱硬化性樹脂では、フェノー
ル樹脂、エポキシ樹脂、ポリウレタン樹脂、不飽和ポリ
エステル樹脂、ビニルエステル樹脂及びポリイミド樹脂
等であり、熱可塑性樹脂としては、ポリエチレン、ポリ
プロピレンなどのポリオレフィン、ポリアミド、ポリエ
ステル、ポリビニルアセテート、ポリエーテルサルファ
イド、ポリフェニルサルファイド、ポリエーテル、エー
テルケトン等、更には熱可塑性ポリウレタン、スチレ
ン、ブタジエンゴム、ニトリルゴム、アクリルニトリル
スチレン(AS)樹脂、ネオプレン等の合成ゴム又はエ
ラストマーなどである。
On the other hand, the resin for impregnating or coating these high-strength fibers is a thermosetting resin such as a phenol resin, an epoxy resin, a polyurethane resin, an unsaturated polyester resin, a vinyl ester resin and a polyimide resin. Examples of resins include polyolefins such as polyethylene and polypropylene, polyamides, polyesters, polyvinyl acetates, polyether sulfides, polyphenyl sulfides, polyethers, ether ketones, and the like. (AS) Resin, synthetic rubber such as neoprene, or elastomer.

【0008】ACMを得るには、熱硬化性樹脂の場合、
高強度繊維に熱硬化性樹脂を含浸又は塗布してプリプレ
グを作製し、このプリプレグを複数枚重ね、加熱加圧す
る圧縮成形法、あるいはプリプレグを作らないハンドレ
イアップ法などがある。樹脂含有率は5〜80%(重量
%、以下同じ)の範囲であるが、通常は5〜50%、好
ましくは8〜30%である。一方、熱可塑性樹脂の場
合、高強度繊維と熱可塑性樹脂フィルム或いは織布など
のシート状物とを交互に複数枚重ね合わせ加熱、加圧す
る圧縮成形法や、樹脂を予め溶融しておきその樹脂を高
強度繊維に付着させる方法もある。熱可塑性樹脂の含有
率も上記熱硬化性樹脂と同じである。
In order to obtain ACM, in the case of a thermosetting resin,
A prepreg is prepared by impregnating or coating a high-strength fiber with a thermosetting resin, a plurality of prepregs are stacked, and a compression molding method in which heat and pressure are applied, or a hand lay-up method in which a prepreg is not formed is used. The resin content is in the range of 5 to 80% (weight%, the same applies hereinafter), but is usually 5 to 50%, preferably 8 to 30%. On the other hand, in the case of thermoplastic resin, a compression molding method in which a plurality of high-strength fibers and a sheet-like material such as a thermoplastic resin film or a woven fabric are alternately laminated and heated and pressed, or the resin is melted in advance and the resin is melted. There is also a method of adhering to a high-strength fiber. The content of the thermoplastic resin is the same as that of the thermosetting resin.

【0009】[0009]

【作用】上述の方法で得られたACMをセラミックの裏
面に固定する方法としては、ボルトやリベット等の機械
的方法、あるいはACMに用いられる樹脂そのもの、あ
るいは合成ゴム系やエポキシ樹脂等の接着剤で接着する
化学的方法等があるが、樹脂及び接着剤等でACM/セ
ラミック間を密着させる方が望ましい。
The ACM obtained by the above method is fixed to the back surface of the ceramic by a mechanical method such as a bolt or a rivet, a resin itself used for the ACM, or an adhesive such as a synthetic rubber or epoxy resin. Although there is a chemical method for bonding, the ACM / ceramic is preferably brought into close contact with a resin and an adhesive.

【0010】本発明において、この様にして作製された
複合成形物の耐衝撃性を更に向上させる為、この複合成
形品をACMで包み込む。具体的には、複合成形物に使
用された高強度繊維と樹脂又は複合成形物と密着性の良
い他の高強度繊維と樹脂とで得られたプリプレグで複合
成形物を包み込んで加熱加圧して硬化させる方法、ハン
ドレイアップ法で複合成形物を包み込みながら成形する
方法、熱可塑性樹脂シートと高強度繊維を交互に包み込
んで加熱溶融し加圧する方法、あるいは熱可塑性樹脂が
付着した高強度繊維で複合成形体を包み込んで加熱加圧
する方法等がある。樹脂含有率は複合成形物本体より多
少高い方が好ましい。即ち10〜80%の範囲、通常1
5〜70%、好ましくは20〜60%である。包み込む
時の積層数は1〜30層、通常は1〜20層、好ましく
は2〜15層である。
In the present invention, in order to further improve the impact resistance of the composite molded product thus produced, the composite molded product is wrapped in ACM. Specifically, the composite molded product is wrapped with a prepreg obtained from the high-strength fiber and resin used for the composite molded product or another high-strength fiber and resin having good adhesion to the composite molded product, and heated and pressed. A method of curing, a method of molding while wrapping the composite molded product by the hand lay-up method, a method of alternately wrapping a thermoplastic resin sheet and high-strength fibers, heating and melting and pressing, or a high-strength fiber with thermoplastic resin attached There is a method in which the composite molded body is wrapped and heated and pressed. It is preferable that the resin content is slightly higher than that of the composite molded article body. That is, in the range of 10 to 80%, usually 1
It is 5 to 70%, preferably 20 to 60%. The number of layers to be wrapped is 1 to 30 layers, usually 1 to 20 layers, and preferably 2 to 15 layers.

【0011】この様にして得られたACMで包まれたセ
ラミック/ACM複合成形物は、包まれていない複合成
形物単独と比較して、例えば大きな衝撃力や高速な飛来
物が衝突した際、その衝撃力によって複合成形物内のセ
ラミックが破壊された際、セラミックの破壊面積及びク
ラックを小さくすると共にセラミックとACMとの接着
層の剥離を非常に少なくし、更にACM後部のふくらみ
も、ACMで包み込まれている為、相互の引張効果によ
り著しく小さくすることが可能となる。繰り返し同一部
位又はその付近に2回以上の衝撃を受けた場合でも包み
込まれている為破壊が大きく進まず衝撃力によってAC
Mに大きなダメージを与えることはない。
The ceramic / ACM composite molded article wrapped with ACM obtained in this way has a larger impact force and a higher-speed flying object, for example, when compared with the non-wrapped composite molded article alone. When the ceramic in the composite molded article is broken by the impact force, the fracture area and cracks of the ceramic are reduced, the peeling of the adhesive layer between the ceramic and the ACM is extremely reduced, and the bulge at the rear of the ACM is also reduced by the ACM. Because they are wrapped, they can be significantly reduced due to the mutual tensile effect. Even if the impact is repeatedly applied to the same part or its vicinity two or more times, it is wrapped, so the destruction does not proceed greatly and the AC by the impact force
It doesn't do much damage to M.

【0012】[0012]

【実施例】以下、本発明を実施例にて具体的に説明す
る。
The present invention will be specifically described below with reference to examples.

【0013】≪実施例1≫比引張強度が16×106c
m、比弾性率3.2×108cm の高強度ガスラ繊維からな
る平織織布(目付量:230g/m2 )にレゾール型フ
ェノール樹脂を含浸し乾燥して樹脂分約20%のプリプ
レグを得た。このプリプレグを3枚重ね、150℃、1
00kg/cm2 で加熱、加圧してACM板を得た。このA
CM板を純度92%のアルミナセラミック(厚さ3mm)
にフェノール樹脂系ハンドレイアップ用樹脂にて固定し
図1に示す複合成形体Aを得た。この複合成形体Aに上
記プリプレグを約80℃で加熱後、2回巻き付け、オー
トクレーブに入れ、150℃、10kg/cm2 で加熱、加
圧して図2に示す複合成形物Bを得た。
Example 1 Specific tensile strength is 16 × 10 6 c
m, a plain woven fabric (basis weight: 230 g / m 2 ) made of high-strength gasla fiber having a specific elastic modulus of 3.2 × 10 8 cm, impregnated with a resol-type phenol resin and dried to obtain a prepreg having a resin content of about 20%. Obtained. Three prepregs are stacked at 150.degree.
An ACM plate was obtained by heating and pressing at 00 kg / cm 2 . This A
CM board made of 92% pure alumina ceramic (thickness 3mm)
Was fixed with a phenol resin-based hand lay-up resin to obtain a composite molded body A shown in FIG. The composite prepreg A was heated at about 80 ° C., wound twice, placed in an autoclave, and heated and pressurized at 150 ° C. and 10 kg / cm 2 to obtain a composite molded article B shown in FIG.

【0014】≪実施例2≫比引張強度が29×106c
m、比弾性率10×108cmの高強度ポリエチレン繊維か
らなる織布(目付量:350g/m2 )にビスフェノー
ルA型エポキシ樹脂を含表面にコーティングし、乾燥し
て樹脂分約25%のプリプレグを得た。このプリプレグ
を10枚重ね、110℃、50kg/cm2 で加熱してAC
M板を得た。このACM板を窒化ケイ素セラミック(厚
さ4mm)にエポキシ樹脂で接着し複合成形体Cを得た。
この複合成形物Cに上記ポリエチレン織布とビニルエス
テル樹脂を用いてハンドレイアップ成形により2回巻き
付け室温で硬化させ複合成形物Dを得た。
Example 2 Specific tensile strength is 29 × 10 6 c
m, a woven fabric (basis weight: 350 g / m 2 ) made of high-strength polyethylene fiber having a specific elastic modulus of 10 × 10 8 cm, coated with a bisphenol A type epoxy resin on the surface, dried, and dried to a resin content of about 25%. I got a prepreg. 10 prepregs are stacked and heated at 110 ° C. and 50 kg / cm 2 to obtain AC.
An M plate was obtained. This ACM plate was bonded to a silicon nitride ceramic (4 mm thick) with an epoxy resin to obtain a composite molded product C.
The composite molded article C was wound twice by hand lay-up molding using the polyethylene woven fabric and the vinyl ester resin and cured at room temperature to obtain a composite molded article D.

【0015】≪実施例3≫比引張強度が21×106c
m、比弾性率6.4×108cm のアラミド繊維織布(目付
量:450g/m2 )にABS樹脂の18%MEK溶液
を含浸し、乾燥して樹脂分約20%のプリプレグを得
た。このプリプレグを3枚重ね150℃、100kg/cm
2 で加熱加圧してACM板を得た。このACM板を炭化
ケイ素セラミック(厚さ3mm)に合成ゴム系接着剤で接
着し複合成形体Eを得た。この複合成形体Eに上記アラ
ミド織布プリプレグを2回巻き付け真空プレスに入れ、
加熱加圧して複合成形物Fを得た。
Example 3 Specific tensile strength is 21 × 10 6 c
An aramid fiber woven cloth (basis weight: 450 g / m 2 ) having a specific elastic modulus of 6.4 × 10 8 cm is impregnated with an 18% MEK solution of ABS resin and dried to obtain a prepreg having a resin content of about 20%. Was. Three layers of this prepreg are stacked at 150 ° C. and 100 kg / cm
An ACM plate was obtained by heating and pressing at 2 . The ACM plate was bonded to a silicon carbide ceramic (thickness: 3 mm) with a synthetic rubber adhesive to obtain a composite molded body E. The aramid woven prepreg is wound twice around the composite molded body E and put into a vacuum press,
Heat and pressure were applied to obtain a composite molded product F.

【0016】≪実施例4≫比引張強度が20×106c
m、比弾性率4.9×108cm の芳香族ポリエステル繊維
の織布(目付量:260g/m2 )6枚と高延伸させた
ポリエチレンフィルム(厚さ100μm)7枚を交互に
重ね合わせ、130℃、70kg/cm2 で加熱、加圧して
ACM板(両表面はポリエチレンフィルム)を得た。こ
のACM板をジルコニア系セラミック(厚さ2mm)にエ
ポキシ系接着剤にて固定し複合成形体Gを得た。この複
合成形体Gに上記ポリエチレンフィルムとポリエステル
織布とを重ね合わせ3回巻いた後、上記と同じ条件で加
熱、加圧して複合成形物Hを得た。
Example 4 Specific tensile strength is 20 × 10 6 c
m, a woven fabric of aromatic polyester fibers having a specific elastic modulus of 4.9 × 10 8 cm (basis weight: 260 g / m 2 ) and seven highly stretched polyethylene films (thickness: 100 μm) are alternately laminated. Heating and pressing at 130 ° C. and 70 kg / cm 2 yielded an ACM plate (both surfaces were polyethylene films). The ACM plate was fixed to a zirconia-based ceramic (2 mm thick) with an epoxy-based adhesive to obtain a composite molded body G. After laminating the above-mentioned polyethylene film and polyester woven fabric three times on this composite molded product G and heating and pressing it under the same conditions as above, a composite molded product H was obtained.

【0017】≪実施例5≫比引張強度が32×106c
m、比弾性率12×108cm高強度ポリエチレン繊維から
成る一方向不織布(目付量:130g/m2 )にポリウ
レタン変性ビニルエステル樹脂を表面にコーティング
し、乾燥して樹脂分約30%のプリプレグを得た。この
プリプレグを直交方向に交互に10枚重ね、120℃、
60kg/cm2 で加熱、加圧してACM板を得た。このA
CM板を純度99%のアルミナセラミック(厚さ4mm)
にウレタン系接着剤で接着し、複合成形体Iを得た。こ
の複合成形体Iに上記高張力高弾性カーボン織布(目付
量:約200g/m2 )と上記同樹脂とを用いてハンド
レイアップ成形にて4回巻き付け硬化して複合成形物J
を得た。
Example 5 Specific tensile strength is 32 × 10 6 c
m, a unidirectional nonwoven fabric (basis weight: 130 g / m 2 ) made of high-strength polyethylene fiber with a specific elastic modulus of 12 × 10 8 cm, coated with a polyurethane-modified vinyl ester resin on the surface, and dried to prepare a prepreg having a resin content of about 30%. I got 10 prepregs are alternately stacked in the orthogonal direction at 120 ° C.
An ACM plate was obtained by heating and pressing at 60 kg / cm 2 . This A
CM board made of 99% pure alumina ceramic (4mm thick)
Was bonded with a urethane-based adhesive to obtain a composite molded article I. The composite molded article I was wound around the composite molded article I four times by hand lay-up molding using the high-tensile high-elastic carbon woven fabric (weight per unit area: about 200 g / m 2 ) and the same resin, and was cured.
I got

【0018】≪比較例1≫実施例1で得られたプリプレ
グを5枚重ねたもの及び2枚重ねたものをそれぞれ別々
に150℃、100kg/cm2 で加熱、加圧して2種のA
CM板を得た。次いで実施例1と同じ純度92%アルミ
ナセラミック(厚さ3mm)の裏面に5枚重ねのACM
を、表面に前記2枚重ねのACMをそれぞれハンドレイ
アップ用フェノール樹脂にて固定し図3で示す複合成形
物Kを得た。
Comparative Example 1 Five prepregs and two prepregs obtained in Example 1 were separately heated and pressed at 150 ° C. and 100 kg / cm 2 to obtain two kinds of A.
A CM board was obtained. Next, five ACMs were stacked on the back surface of the same 92% pure alumina ceramic (thickness: 3 mm) as in Example 1.
Was fixed on the surface with a phenol resin for hand lay-up, respectively, to obtain a composite molded product K shown in FIG.

【0019】≪比較例2≫実施例2において得られたプ
リプレグを12枚重ねたもの及び2枚重ねたものをそれ
ぞれ別々に実施例2と同じ条件で加熱、加圧して2種の
ACM板を得た。窒化ケイ素セラミック(厚さ4mm)の
裏面に12枚重ねのACMを、表面に2枚重ねのACM
をそれぞれエポキシ樹脂で接着し複合成形物Lを得た。
COMPARATIVE EXAMPLE 2 Twelve prepregs obtained in Example 2 and two prepregs obtained in Example 2 were separately heated and pressed under the same conditions as in Example 2 to form two types of ACM plates. Obtained. 12 layers of ACM on the back and 2 layers of ACM on the back of silicon nitride ceramic (4mm thick)
Were bonded with an epoxy resin to obtain a composite molded product L.

【0020】≪比較例3≫実施例3において得られたプ
リプレグを5枚重ねたもの及び2枚重ねたものをそれぞ
れ別々に実施例3と同条件で加熱、加圧して2種のAC
M板を得た。炭化ケイ素セラミック(厚さ3mm)の裏面
に5枚重ねのACMを、表面に2枚重ねのACMをそれ
ぞれ合成ゴム系接着剤で接着し、複合成形Mを得た。
Comparative Example 3 Five prepregs obtained in Example 3 and two prepregs obtained in Example 3 were separately heated and pressed under the same conditions as in Example 3 to obtain two types of AC.
An M plate was obtained. Five ACMs were adhered to the back surface of the silicon carbide ceramic (thickness: 3 mm), and two ACMs were adhered to the front surface with a synthetic rubber-based adhesive, respectively, to obtain a composite molding M.

【0021】≪比較例4≫実施例4において高延伸させ
たポリエチレンフィルム(厚さ100μm)10枚とポ
リエステル織布9枚とを交互に重ね合わせたもの及びポ
リエチレンフィルム3枚とポリエステル織布3枚とを交
互に重ね合わせたものをそれぞれ別々に実施例4と同じ
条件で加熱、加圧して2種のACM板を得た。ジルコニ
ア系セラミック(厚さ3mm)の裏面にポリエステル織布
9枚のACMを、表面に3枚のACMをそれぞれエポキ
シ系接着剤にて固定し複合成形物Nを得た。
Comparative Example 4 Ten high-stretched polyethylene films (thickness: 100 μm) and nine polyester woven fabrics alternately laminated in Example 4 and three polyethylene films and three polyester woven fabrics Were alternately heated and pressed separately under the same conditions as in Example 4 to obtain two types of ACM plates. Nine polyester woven fabric ACMs were fixed on the back surface of the zirconia ceramic (thickness: 3 mm), and three ACMs were fixed on the front surface with epoxy adhesives, respectively, to obtain a composite molded product N.

【0022】≪比較例5≫実施例5において得られたA
CM板に、カーボン織布4枚と実施例と同じ樹脂とを用
いてハンドレイアップ成形したACMを純度99%のア
ルミセラミック(厚さ4mm)の裏面に、表面にはカーボ
ン織布4枚のみを前記樹脂でハンドレイアップ成形した
ACM板をウレタン系接着剤で接着し複合成形物Pを得
た。上記複合成形物をMIL-STD-662に従って
1.1g弾を用い約850m/sec の速度で耐貫通衝撃
試験を行った。結果を表1に示す。
{Comparative Example 5} A obtained in Example 5
ACM made by hand lay-up molding on a CM board using four carbon woven fabrics and the same resin as in the example, on the back of a 99% pure aluminum ceramic (4 mm thick), and only four carbon woven fabrics on the front An ACM plate formed by hand lay-up molding with the above resin was adhered with a urethane-based adhesive to obtain a composite molded product P. According to MIL-STD-662
A penetration resistance test was performed at a speed of about 850 m / sec using a 1.1 g bullet. Table 1 shows the results.

【0023】[0023]

【表1】 [Table 1]

【0024】[0024]

【発明の効果】以上の結果からも明らかなように、本発
明の複合成形物は耐衝撃性に優れ、衝撃試験後において
セラミックの破壊面積が小さく、かつACM板とセラミ
ックとの剥離も少なく又成形物裏面のふくらみも小さ
い。
As is clear from the above results, the composite molded article of the present invention is excellent in impact resistance, has a small fracture area of the ceramic after the impact test, and has little peeling between the ACM plate and the ceramic. The bulge on the back of the molded product is also small.

【図面の簡単な説明】[Brief description of the drawings]

【図1】 実施例1における複合成形体Aの概略断面図FIG. 1 is a schematic cross-sectional view of a composite molded body A in Example 1.

【図2】 実施例1における複合成形物Bの概略断面図FIG. 2 is a schematic sectional view of a composite molded product B in Example 1.

【図3】 比較例1における複合成形物Kの概略断面図FIG. 3 is a schematic cross-sectional view of a composite molded product K in Comparative Example 1.

【符号の説明】[Explanation of symbols]

1 セラミック板 2,3 ACM 4 セラミック板 5,6 ACM 1 ceramic plate 2,3 ACM 4 ceramic plate 5,6 ACM

Claims (1)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 セラミックと高強度繊維強化プラスチッ
クからなる複合成形物において、セラミックと高強度繊
維強化プラスチックとを積層してなる複合成形体を高強
度繊維強化プラスチックにて包み込むことを特徴とする
複合成形物。
1. A composite formed from ceramic and high-strength fiber-reinforced plastic, wherein a composite formed by laminating ceramic and high-strength fiber-reinforced plastic is wrapped with high-strength fiber-reinforced plastic. Moldings.
JP06213000A 1994-09-06 1994-09-06 Composite molding Expired - Lifetime JP3127947B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP06213000A JP3127947B2 (en) 1994-09-06 1994-09-06 Composite molding

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP06213000A JP3127947B2 (en) 1994-09-06 1994-09-06 Composite molding

Publications (2)

Publication Number Publication Date
JPH0872200A JPH0872200A (en) 1996-03-19
JP3127947B2 true JP3127947B2 (en) 2001-01-29

Family

ID=16631827

Family Applications (1)

Application Number Title Priority Date Filing Date
JP06213000A Expired - Lifetime JP3127947B2 (en) 1994-09-06 1994-09-06 Composite molding

Country Status (1)

Country Link
JP (1) JP3127947B2 (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NZ511530A (en) * 1998-11-09 2003-05-30 Pinnacle Armor Llc Method and apparatus for defeating high-velocity projectiles by use of imbricated pattern of tiles on backing sheet
JP2003269898A (en) * 2002-03-12 2003-09-25 Sumitomo Bakelite Co Ltd Composite laminated body and bulletproof helmet
US7718245B2 (en) * 2005-12-29 2010-05-18 Honeywell International Inc. Restrained breast plates, vehicle armored plates and helmets
JP5117911B2 (en) * 2008-04-03 2013-01-16 新日鉄住金マテリアルズ株式会社 Structure containing ceramics and carbon fiber reinforced plastic
JP5291376B2 (en) * 2008-04-28 2013-09-18 京セラケミカル株式会社 Compound bulletproof board
JP5956294B2 (en) 2012-09-13 2016-07-27 日本碍子株式会社 Laminated body
JP6237130B2 (en) * 2013-11-06 2017-11-29 東ソー株式会社 Composite plate and manufacturing method thereof
CN109373819A (en) * 2018-12-06 2019-02-22 长沙盾甲新材料科技有限公司 High-strength polyurethane/fiber/ceramic structure armour
JP7439451B2 (en) * 2019-10-28 2024-02-28 ウシオ電機株式会社 Carbon fiber reinforced plastic structure, its manufacturing method and measuring device

Also Published As

Publication number Publication date
JPH0872200A (en) 1996-03-19

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