JP3640751B2 - Composite material mold and composite material molding method - Google Patents

Composite material mold and composite material molding method Download PDF

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Publication number
JP3640751B2
JP3640751B2 JP34871796A JP34871796A JP3640751B2 JP 3640751 B2 JP3640751 B2 JP 3640751B2 JP 34871796 A JP34871796 A JP 34871796A JP 34871796 A JP34871796 A JP 34871796A JP 3640751 B2 JP3640751 B2 JP 3640751B2
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Prior art keywords
mold
surface plate
composite material
shim
mold surface
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JPH10180892A (en
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口 雅 幸 関
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Subaru Corp
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Fuji Jukogyo KK
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Description

【0001】
【発明の属する技術分野】
本発明は、航空機の外板やフェアリング等の構造部材となる熱硬化性繊維強化樹脂複合材の成形型および複合材の成形方法に係り、特に、曲面や複曲面等の複雑形状の成形品を精度よく成形することができる複合材成形型および複合材の成形方法に関する。
【0002】
【従来の技術】
複合材部品の成形型として、特願昭63−102933号に示されているように、成形型を金属材料で構成し、成形後の寸法・角度変化を予め織り込んで成形型各部の寸法を設定するものや、実開平1−156024号公報に示されているように、成形型表面板と補強枠体を成形すべき複合材と同等の熱膨脹率を有する複合材で構成し、補強枠体と成形型表面板との間に隙間を持たせ、補強枠体と成形型表面板をアングル材を介し部分的に接合するものは知られている。
【0003】
【発明が解決しようとする課題】
複合材部品の成形型を金属材料で構成したものは、成形品が曲面や複曲面等の複雑形状の場合に、成形品自体の変形(寸法・角度変化)予測が困難であるため、成形型に成形品の変形を予め織り込むことができないという問題がある。
【0004】
また、複合材部品の成形型を複合材で構成したものは、成形型と成形品との間の熱膨脹差に起因する変形は防止することができるが、複合材の成形品が材質(繊維・樹脂)、積層繊維配向、板厚、形状あるいは成形プロセス等によっても変形するため、このような要因による成形品の変形は防止することができないという問題がある。
【0005】
そして、このような変形が成形型に発生した場合、航空機の構造組立において重要となる外表面の部品のモールドが合致しない等の重大な問題が生じ、この場合には、成形型の改修・再作が必要となり、過大なコストおよび時間がかかるという問題がある。
【0006】
本発明は、かかる現況に鑑みなされたもので、成形品が曲面や複曲面等の複雑形状の場合であっても、成形後の成形品を所望の形状・寸法に精度よく成形することができる複合材の成形型および複合材の成形方法を提供することを目的とする。
【0007】
本発明の他の目的は、モールドラインの変更が容易で、かつ正確に行なうことができることにある。
【0008】
本発明の他の目的は、成形型表面板の端部から中央部までのモールドラインの調整が可能で、かつ調整後の形状保持を安定させることができることにある。
【0009】
本発明の他の目的は、スタッドボルトの引張・圧縮による成形型表面板の局部的な変形を防止することができることにある。
【0010】
本発明の他の目的は、成形品の硬化中にシムがずれてモールドラインが変化するのを防止することができることにある。
【0011】
本発明のさらに他の目的は、成形品の品質を大幅に向上させることができることにある。
【0012】
【課題を解決するための手段】
本発明の複合材の成形型は、繊維強化樹脂複合材製の成形品と同等の熱膨脹率を有する複合材で形成された成形型表面板と、この成形型表面板を内側から支持する補強枠体と、前記成形型表面板に設けられて補強枠体側に突出する複数のスタッドボルトと、各スタッドボルトを補強枠体に固定する固定金具と、前記成形品と同等の熱膨脹率を有する複合材で形成され成形型表面板と補強枠体との間に介装されて成形型表面板のモールドラインを変化させるシムとを有し、シムの板厚調整で成形型表面板のモールドラインを自在に変化させることが可能となり、成形品が曲面や複曲面等の複雑形状の場合であっても、成形後の成形品を所望の形状・寸法に精度よく成形することが可能となるとともに、モールドラインの変更が容易で、しかも正確に行なうことが可能となる。
【0013】
また、本発明の複合材の成形型では、各スタッドボルトを成形型表面板に一体化されているので、成形型表面板の端部から中央部までのモールドラインの調整が可能となり、また、各スタッドボルトは、固定金具を介し補強枠体に固定されているので、成形型表面板の形状保持を安定させることが可能となり、成形型表面板上で真空引きを行なっても、成形型表面板が反るおそれがない。
【0014】
さらに、本発明の複合材の成形型では、成形型表面板と補強枠体との間にシムが介装されているので、スタッドボルトの引張・圧縮による成形型表面板の局部的な変形を防止することが可能となり、またシムは、成形品と同等の熱膨脹率を有する複合材で形成されているので、熱膨脹により成形型表面板のモールドラインが変化してしまうおそれがなく、また、シムに、スタッドボルト用の挿通孔を設けてあるので、成形品の硬化中にシムがずれてモールドラインが変化するといった不具合がない。
【0015】
本発明の複合材の成形方法は、成形しようとする繊維強化樹脂複合材成形品の複合材と同等の熱膨脹率を有する複合材で成形型表面板を形成し、複数のスタッドボルトを成形型表面板に内側に突出するように設け、成形型表面板を内側から補強枠体で支持し、各スタッドボルトを補強枠体に固定し、成形型表面板と同等の熱膨脹率を有する複合材で形成したシムを成形型表面板と補強枠体との間に介装し、介装するシムにより成形型表面板のモールドラインを変化させ、改修モールド成形型を完成し、この改修モールド成形型により成形品を所望の形状・寸法に精度よく成形することを可能にする。
【0016】
本発明の複合材の成形方法によれば、成形品が材質(繊維・樹脂)、積層繊維配向、板厚、形状あるいは成形プロセス等の要因で変形することがあっても、この変形量をシムで補正し、成形品を所望の形状・寸法に精度よく成形することを可能にする。
【0017】
本発明の複合材の成形方法では、シムを成形型表面板の上に複合材を積層して硬化させて成形した成形品を上記成形型表面板から外した時の上記成形品のモールドラインと正規モールドラインとの差に基づいて製作するようにすることで、成形品の精度がより高くなり、成形品の品質を大幅に向上させることが可能となる。
【0018】
【発明の実施の態様】
以下、本発明の実施の態様を図面を参照して説明する。
【0019】
図1は、本発明の実施の一形態に係る複合材の成形型を示すもので、この成形型1は、成形型表面板2と、この成形型表面板2を内側から支持する補強枠体3と、成形型表面板2の内面から突出する複数のスタッドボルト4と、これら各スタッドボルト4を補強枠体3に固定する固定金具5と、成形型表面板2と補強枠体3との間に介装されるシム6とを備えている。
【0020】
前記成形型表面板2は、図2に示すように、成形品10と同等の熱膨脹率を有するCFRP、GFRP等の治具材を積層して形成されている。前記スタッドボルト4は、成形型表面板2の大きさ、形状等によっても異なるが、通常は200mmピッチ程度の間隔で頭部が成形型表面板2の層間に埋設されて補強枠体3側に突出している。そして、このスタッドボルト4の頭部には、成形型表面板2の層間剥離を防止するため、プライマ等の表面処理が施され、頭部と成形型表面板2とが充分接着するよう考慮されている。
【0021】
また、前記補強枠体3は、ハニカムコアの両面にCFRPを積層して硬化させたハニカムサンドウィッチパネルで組立てられ、成形型表面板2との接触面は成形型表面板2の形状に合わせて加工され、さらに周壁には軽減孔7を穿設して構成され、これにより熱伝達性の向上と軽量化とを施したエッグクレート構造となっている。上記ハニカムサンドウィッチパネルは熱膨張が極めて小さい上に軽量なので、補強枠体3の材料として非常に好ましいものである。
【0022】
また、前記固定金具5は、図2に示すように、各スタッドボルト4の位置に合わせ補強枠体3の壁面にボルト・ナット8を介し取付けられており、スタッドボルト4は、固定金具5を介しその両側から固定ナット9を締付けることにより、固定金具5に固定されるようになっている。
【0023】
また、前記シム6は、成形品10と同等の熱膨脹率を有するCFRP、GFRP、SiCFRP等の治具材を積層するとともに、この素材を70mm×70mm程度に切断して形成されており、その板面には、図2に示すように、スタッドボルト4用の挿通孔11が設けられている。そして、このシム6を成形型表面板2と補強枠体3との間に介装することにより、成形型表面板2のモールドラインを変化させることができるようになっている。
【0024】
次に、本実施の形態の作用について説明する。
【0025】
成形型1の製作に際しては、まず成形型1を製作するための型であるツーリングツールに離型処理を施した後、成形品10と同等の熱膨脹率を有する例えばCFRPのプリプレグを積層して成形型表面板2を製作する。この際、成形型表面板2の大きさ、形状等によっても異なるが、200mm程度のピッチで成形型表面板2の層間にスタッドボルト4の頭部を埋設しておく。また、スタッドボルト4は、成形型表面板2の層間剥離を防止するため、その頭部にプライマ等の表面処理を施したものを用い、スタッドボルト4とCFRPとの接着性をよくする。
【0026】
このように、成形型表面板2にスタッドボルト4を埋設した状態で、バギング・加熱・加圧し、成形型表面板2を硬化させる。そして、硬化後、成形型表面板2の外形仕上げ等を行なう。これと同時あるいは相前後して、シム6として適当な複合材の素材も硬化させておく。
【0027】
成形型表面板2の硬化後、補強枠体3を製作する。補強枠体3は、ハニカムサンドウィッチパネルを組立て、成形型表面板2との接触面は、成形型表面板2の形状に合わせて加工し、周壁には軽減孔7を穿設する。そしてこれにより、熱伝達性の向上および軽量化を施したエッグクレート構造とする。
【0028】
次いで、成形型表面板2に埋設したスタッドボルト4の位置に合わせ、補強枠体3の壁面に固定金具5をボルト・ナット8により固定し、その後スタッドボルト4を、固定金具5の両側から締付けることにより固定金具5に固定する。
【0029】
このようにして、成形型表面板2と補強枠体3とを一体に連結した後、成形型1のポストキュア(二次硬化)を行なって、シム6なしの正規モールドラインの成形型1を完成させる。
【0030】
成形品10の製作に際しては、図3に示すように、正規モールドラインの成形型1を用い、その成形型表面板2の表面に離型処理を行なって複合材を積層し、硬化させ成形品10を成形する。
【0031】
成形後脱型し、図4に示すように、成形品10の変形量12、すなわち正規モールドライン13と成形後の成形品モールドライン14との差を測定する。変形は通常、図4に示すようにRが小さくなるように収縮する。
【0032】
次いで、前後変形量12を用い、図5に示すように、この変形量12と同等板厚のシム6を製作する。このシム6は、予め硬化させておき、変形量12に合わせ研削して製作する。そして、このシム6を図6に示すように成形型1に適用し、改修モールドライン15に変更した改修モールド成形型1′とする。
【0033】
次いで、この改修モールド成形型1′を用い、複合材を積層して硬化させ成形品10′を成形する。そして、成形後の成形品10′につき、図7に示すようにそのモールドライン14′を測定する。
【0034】
通常は、このモールドライン14′が正規モールドライン13と一致することになるが、両モールドライン13,14′が一致しない場合には、両モールドライン13,14′の変形量を測定し、この変形量に基づきシム6を再製作する。そして、このシム6を改修モールド成形型1′にセットして成形品10′を再成形する。これでも、正規モールドライン13にならない場合には、この作業を正規モールドライン13になるまで繰返す。
【0035】
しかして、成形型1の成形型表面板2は、成形品10と同等の熱膨脹率を有する複合材で形成されているので、金属材料を用いた成形型と異なり、熱膨脹差による成形品の変形がない。また、金属材料に比べ軽量化を図ることができ、補強枠体3もハニカム構造体で軽量化が図られているので、成形型1のハンドリング性を大幅に向上させることができる。また、成形型表面板2は低熱膨脹であるため、成形品10の硬化中に成形型1に寸法誤差を生じることがなく、寸法精度の向上を図ることができるとともに、品質の安定化を図ることができる。
【0036】
また、シム6の板厚調整により変形量12を吸収するようにしているので、成形型表面板2のモールドラインを自由に変化させることができ、L型や曲面・複曲面等の複雑形状の成形品であっても、充分に対応することができるとともに、モールドラインの変更が容易で、かつ正確に行なうことができる。
【0037】
また、成形型表面板2に複数のスタッドボルト4の頭部を埋設して一体化しているので、成形型表面板2の端部から中央部までのモールドラインの調整を行なうことができる。また、成形型表面板2と補強枠体3との間にシム6が介装されているので、スタッドボルト4の引張・圧縮による成形型表面板2の局部的な変形を、シム6により防止することができる。
【0038】
また、このシム6は、成形品と同等の熱膨脹率を有する複合材で形成されているので、熱膨脹により成形型1の成形型表面板2のモールドラインが変化してしまうといった不具合がない。またシム6はスタッドボルト4用の挿通孔11を有しているので、成形品10,10′の硬化中に、シム6が位置ずれしてモールドラインが変化してしまうといった不具合もない。
【0039】
また、成形型表面板2は、スタッドボルト4および固定金具5を介し補強枠体3に一体に連結されているので、成形型表面板2の形状保持を安定させ、成形型表面板2上で真空引きを行なっても、成形型表面板2が反るおそれがない。
【0040】
【発明の効果】
以上説明したように、本発明の複合材の成形型は、成形型表面板と、補強枠体と、スタッドボルトと、固定金具と、シムとから構成したので、シムの板厚調整のみにより成形型表面板のモールドラインを自在に変化させることができ、成形品が曲面や複曲面等の複雑形状の場合であっても、成形後の成形品を所望の形状・寸法に精度よく成形することができ、モールドラインの変更が容易で、しかも正確に行なうことができる。
【0041】
また、本発明の複合材の成形型は、各スタッドボルトを成形型表面板に一体化することで、成形型表面板の端部から中央部までのモールドラインの調整が可能となり、各スタッドボルトを補強枠体に固定することで、成形型表面板の形状保持が安定し、成形型表面板上で真空引きを行なっても、成形型表面板が反るおそれがなく、成形型表面板と補強枠体との間にシムを介装することで、スタッドボルトの引張・圧縮による成形型表面板の局部的な変形をシムで防止することができる。また、このシムは、成形品と同等の熱膨脹率を有する複合材で形成することで、熱膨脹により成形型表面板のモールドラインが変化してしまうといった不具合がなく、また、シムにスタッドボルト用の挿通孔を設けることで、成形品の硬化中にシムの位置がずれてモールドラインが変化してしまうといった不具合がない。
【0042】
本発明の複合材の成形方法は、成形しようとする繊維強化樹脂複合材成形品の複合材と同等の熱膨脹率を有する複合材で成形型表面板を形成し、複数のスタッドボルトを成形型表面板に内側に突出するように設け、成形型表面板を内側から補強枠体で支持し、各スタッドボルトを補強枠体に固定し、成形型表面板と同等の熱膨脹率を有する複合材で形成したシムを成形型表面板と補強枠体との間に介装し、介装するシムにより成形型表面板のモールドラインを変化させることで、改修モールド成形型を完成し、この改修モールド成形型を用いて正規成形品を成形するので、成形品が、材質(繊維・樹脂)、積層繊維配向、板厚、形状あるいは成形プロセス等の要因で変形することがあっても、この変形量をシムで補正し、成形品を所望の形状・寸法に精度よく成形することができる。
【0043】
本発明の複合材の成形方法では、シムを成形型表面板の上に複合材を積層して硬化させて成形した成形品を上記成形型表面板から外した時の上記成形品のモールドラインと正規モールドラインとの差に基づいて製作することで、成形品の精度がより高くなり、成形品の品質を大幅に向上させることができる。
【図面の簡単な説明】
【図1】本発明の実施の一形態に係る複合材の成形型を示す斜視図。
【図2】図1のII部拡大図。
【図3】正規モールド成形型を用いた成形品の成形方法を示す図。
【図4】正規モールド成形型を用いて成形された成形品の正規モールドラインからの変形量を示す図。
【図5】図4の変形量に基づき製作されるシムを示す図。
【図6】製作されたシムを装着して構成される改修モールド成形型を用いた成形品の成形方法を示す図。
【図7】改修モールド成形型を用いて成形された成形品の正規モールドラインからの変形量を示す図。
【符号の説明】
1 成形型
1′ 改修モールド成形型
2 成形型表面板
3 補強枠体
4 スタッドボルト
5 固定金具
6 シム
7 軽減孔
8 ボルト・ナット
9 固定ナット
10,10′ 成形品
11 挿通孔
12 変形量
13 正規モールドライン
14 成形品モールドライン
14′ モールドライン
15 改修モールドライン
[0001]
BACKGROUND OF THE INVENTION
The present invention relates to a mold for a thermosetting fiber reinforced resin composite material used as a structural member such as an outer panel or fairing of an aircraft, and a molding method for the composite material, and in particular, a molded product having a complicated shape such as a curved surface or a double curved surface. The present invention relates to a composite material mold and a composite material molding method.
[0002]
[Prior art]
As shown in Japanese Patent Application No. 63-102933, as a mold for composite material parts, the mold is made of a metal material and the dimensions and angle changes after molding are pre-weaved to set the dimensions of each part of the mold. As shown in Japanese Utility Model Laid-Open No. 1-156024, the mold surface plate and the reinforcing frame body are composed of a composite material having a thermal expansion coefficient equivalent to that of the composite material to be molded, and the reinforcing frame body It is known that a gap is provided between the molding die surface plate and the reinforcing frame body and the molding die surface plate are partially joined via an angle member.
[0003]
[Problems to be solved by the invention]
When the mold for composite parts is made of a metal material, it is difficult to predict the deformation (dimension / angle change) of the molded product itself when the molded product has a complicated shape such as a curved surface or double curved surface. However, there is a problem that the deformation of the molded product cannot be woven in advance.
[0004]
In addition, a composite material component mold made of a composite material can prevent deformation due to the difference in thermal expansion between the mold and the molded product, but the composite molded product is made of a material (fiber / Resin), laminated fiber orientation, plate thickness, shape, molding process, and the like, so that there is a problem that deformation of the molded product due to such factors cannot be prevented.
[0005]
If such deformation occurs in the mold, a serious problem such as mismatching of the molds of the outer surface parts, which is important in the structural assembly of the aircraft, occurs. There is a problem that the work is required and it takes excessive cost and time.
[0006]
The present invention has been made in view of the present situation, and even if the molded product has a complicated shape such as a curved surface or a double curved surface, the molded product after molding can be accurately molded into a desired shape and size. It aims at providing the shaping | molding die of a composite material, and the shaping | molding method of a composite material.
[0007]
Another object of the present invention is to easily and accurately change the mold line.
[0008]
Another object of the present invention is to be able to adjust the mold line from the end to the center of the mold surface plate and to stabilize the shape retention after the adjustment.
[0009]
Another object of the present invention is to prevent local deformation of the mold surface plate due to the tension and compression of the stud bolt.
[0010]
Another object of the present invention is to prevent the shim from shifting and the mold line from changing during the curing of the molded product.
[0011]
Still another object of the present invention is to greatly improve the quality of a molded product.
[0012]
[Means for Solving the Problems]
The mold of the composite material of the present invention includes a mold surface plate formed of a composite material having a thermal expansion coefficient equivalent to that of a fiber reinforced resin composite molded product, and a reinforcing frame that supports the mold surface plate from the inside. Body, a plurality of stud bolts provided on the mold surface plate and projecting toward the reinforcing frame body, a fixing bracket for fixing each stud bolt to the reinforcing frame body, and a composite material having a thermal expansion coefficient equivalent to that of the molded product And a shim that is interposed between the mold surface plate and the reinforcing frame to change the mold line of the mold surface plate, and the mold line of the mold surface plate can be freely adjusted by adjusting the thickness of the shim Even when the molded product has a complicated shape such as a curved surface or a double curved surface, the molded product after molding can be accurately molded into a desired shape and size, and the mold Easy to change lines and positive It is possible to perform in.
[0013]
Further, in the molding die of the composite material of the present invention, since each stud bolt is integrated with the molding die surface plate, it is possible to adjust the molding line from the end portion to the central portion of the molding die surface plate, Since each stud bolt is fixed to the reinforcing frame via a fixing bracket, it is possible to stabilize the shape of the mold surface plate, and even if vacuuming is performed on the mold surface plate, There is no risk of warping the face plate.
[0014]
Further, in the composite mold of the present invention, since the shim is interposed between the mold surface plate and the reinforcing frame, local deformation of the mold surface plate due to the tension / compression of the stud bolt is prevented. Since the shim is formed of a composite material having a thermal expansion coefficient equivalent to that of the molded product, there is no risk that the mold line of the mold surface plate will change due to thermal expansion. In addition, since the insertion hole for the stud bolt is provided, there is no inconvenience that the shim is displaced during the curing of the molded product and the mold line is changed.
[0015]
The composite material molding method of the present invention comprises forming a mold surface plate with a composite material having a thermal expansion coefficient equivalent to that of the composite material of the fiber reinforced resin composite material to be molded, and forming a plurality of stud bolts on the mold surface. Formed on the face plate so that it protrudes inward, the mold surface plate is supported by the reinforcement frame from the inside, each stud bolt is fixed to the reinforcement frame, and it is formed of a composite material that has the same thermal expansion coefficient as the mold surface plate The molded shim is interposed between the mold surface plate and the reinforcing frame, and the mold line of the mold surface plate is changed by the shim interposed to complete the refurbishment mold, and the remolded mold is molded. The product can be accurately formed into a desired shape and size.
[0016]
According to the method for molding a composite material of the present invention, even if the molded product is deformed due to factors such as material (fiber / resin), laminated fiber orientation, plate thickness, shape, molding process, etc. And the molded product can be accurately formed into a desired shape and size.
[0017]
In the molding method of the composite material of the present invention, the molded product molded line when the molded product formed by laminating and curing the composite material on the mold surface plate is removed from the mold surface plate, By manufacturing based on the difference from the regular mold line, the accuracy of the molded product becomes higher and the quality of the molded product can be greatly improved.
[0018]
BEST MODE FOR CARRYING OUT THE INVENTION
Embodiments of the present invention will be described below with reference to the drawings.
[0019]
FIG. 1 shows a molding die for a composite material according to an embodiment of the present invention. This molding die 1 includes a molding die surface plate 2 and a reinforcing frame body that supports the molding die surface plate 2 from the inside. 3, a plurality of stud bolts 4 projecting from the inner surface of the mold surface plate 2, a fixing metal 5 that fixes the stud bolts 4 to the reinforcing frame 3, and the mold surface plate 2 and the reinforcing frame 3. And a shim 6 interposed therebetween.
[0020]
As shown in FIG. 2, the mold surface plate 2 is formed by laminating jig materials such as CFRP and GFRP having a thermal expansion coefficient equivalent to that of the molded product 10. The stud bolt 4 varies depending on the size, shape, etc. of the mold surface plate 2, but usually the heads are buried between the layers of the mold surface plate 2 at intervals of about 200 mm and are placed on the reinforcing frame 3 side. It protrudes. Then, the head of the stud bolt 4 is subjected to a surface treatment such as a primer in order to prevent delamination of the mold surface plate 2 so that the head and the mold surface plate 2 are sufficiently bonded. ing.
[0021]
The reinforcing frame 3 is assembled with a honeycomb sandwich panel in which CFRP is laminated and cured on both sides of the honeycomb core, and the contact surface with the mold surface plate 2 is processed according to the shape of the mold surface plate 2. Furthermore, the peripheral wall is formed with a reduction hole 7, thereby providing an egg crate structure with improved heat transfer and reduced weight. The honeycomb sandwich panel is extremely preferable as a material of the reinforcing frame 3 because it has a very small thermal expansion and is lightweight.
[0022]
Further, as shown in FIG. 2, the fixing bracket 5 is attached to the wall surface of the reinforcing frame 3 through bolts and nuts 8 in accordance with the positions of the stud bolts 4. The fixing nut 9 is tightened from both sides of the fixing metal fitting 5 so as to be fixed to the fixing bracket 5.
[0023]
The shim 6 is formed by laminating jig materials such as CFRP, GFRP, and SiCFRP having a thermal expansion coefficient equivalent to that of the molded product 10 and cutting the material into about 70 mm × 70 mm. As shown in FIG. 2, an insertion hole 11 for the stud bolt 4 is provided on the surface. The shim 6 is interposed between the mold surface plate 2 and the reinforcing frame 3, so that the mold line of the mold surface plate 2 can be changed.
[0024]
Next, the operation of the present embodiment will be described.
[0025]
When the mold 1 is manufactured, first, a tooling tool that is a mold for manufacturing the mold 1 is subjected to a mold release process, and then a CFRP prepreg having a thermal expansion coefficient equivalent to that of the molded product 10 is laminated and molded. The mold surface plate 2 is manufactured. At this time, although depending on the size and shape of the mold surface plate 2, the heads of the stud bolts 4 are embedded between the layers of the mold surface plate 2 at a pitch of about 200 mm. Moreover, in order to prevent delamination of the mold surface plate 2, the stud bolt 4 is a head whose surface is treated with a primer or the like to improve the adhesion between the stud bolt 4 and CFRP.
[0026]
Thus, in a state where the stud bolt 4 is embedded in the mold surface plate 2, bagging, heating, and pressurization are performed to cure the mold surface plate 2. And after hardening, the outer shape finish etc. of the shaping | molding die surface board 2 are performed. At the same time or around this time, a composite material suitable for the shim 6 is also cured.
[0027]
After the mold surface plate 2 is cured, the reinforcing frame 3 is manufactured. The reinforcing frame 3 assembles the honeycomb sandwich panel, the contact surface with the mold surface plate 2 is processed according to the shape of the mold surface plate 2, and the reduction holes 7 are formed in the peripheral wall. And thereby, it is set as the egg crate structure which gave the heat-transfer property improvement and weight reduction.
[0028]
Next, in accordance with the position of the stud bolt 4 embedded in the mold surface plate 2, the fixing bracket 5 is fixed to the wall surface of the reinforcing frame 3 with bolts and nuts 8, and then the stud bolt 4 is tightened from both sides of the fixing bracket 5. To fix to the fixing bracket 5.
[0029]
In this way, after the mold surface plate 2 and the reinforcing frame 3 are integrally connected, the mold 1 is post-cured (secondary curing), and the mold 1 of the regular mold line without the shim 6 is obtained. Finalize.
[0030]
When the molded product 10 is manufactured, as shown in FIG. 3, a mold 1 of a regular mold line is used, a mold release process is performed on the surface of the mold surface plate 2, a composite material is laminated, cured, and molded product. 10 is molded.
[0031]
After the molding, the mold is removed, and as shown in FIG. 4, the deformation amount 12 of the molded product 10, that is, the difference between the regular mold line 13 and the molded product mold line 14 after molding is measured. The deformation usually shrinks so that R becomes smaller as shown in FIG.
[0032]
Next, as shown in FIG. 5, a shim 6 having a plate thickness equivalent to the deformation amount 12 is manufactured using the front-rear deformation amount 12. The shim 6 is hardened in advance and is manufactured by grinding according to the deformation amount 12. Then, the shim 6 is applied to the molding die 1 as shown in FIG.
[0033]
Next, using this modified mold mold 1 ', the composite material is laminated and cured to form a molded product 10'. Then, as shown in FIG. 7, the mold line 14 ′ of the molded product 10 ′ after molding is measured.
[0034]
Normally, this mold line 14 'coincides with the regular mold line 13, but when both mold lines 13, 14' do not coincide, the deformation amount of both mold lines 13, 14 'is measured, and this The shim 6 is remanufactured based on the amount of deformation. Then, the shim 6 is set in the modified mold 1 'to remold the molded product 10'. If this still does not become the regular mold line 13, this operation is repeated until the regular mold line 13 is reached.
[0035]
Since the mold surface plate 2 of the mold 1 is formed of a composite material having the same thermal expansion coefficient as that of the molded article 10, unlike the mold using a metal material, the deformation of the molded article due to the difference in thermal expansion. There is no. Further, the weight can be reduced as compared with the metal material, and the reinforcing frame 3 is also made light by the honeycomb structure, so that the handling property of the mold 1 can be greatly improved. Further, since the mold surface plate 2 has a low thermal expansion, there is no dimensional error in the mold 1 during the curing of the molded product 10, and the dimensional accuracy can be improved and the quality can be stabilized. be able to.
[0036]
Further, since the deformation amount 12 is absorbed by adjusting the thickness of the shim 6, the mold line of the mold surface plate 2 can be freely changed, and a complicated shape such as an L shape, a curved surface or a double curved surface can be obtained. Even if it is a molded article, it can respond sufficiently and the mold line can be changed easily and accurately.
[0037]
In addition, since the heads of the plurality of stud bolts 4 are embedded in the mold surface plate 2 and integrated, the mold line from the end to the center of the mold surface plate 2 can be adjusted. Further, since the shim 6 is interposed between the mold surface plate 2 and the reinforcing frame 3, local deformation of the mold surface plate 2 due to the tension / compression of the stud bolt 4 is prevented by the shim 6. can do.
[0038]
Further, since the shim 6 is formed of a composite material having a thermal expansion coefficient equivalent to that of the molded product, there is no problem that the mold line of the mold surface plate 2 of the mold 1 changes due to thermal expansion. Further, since the shim 6 has the insertion hole 11 for the stud bolt 4, there is no problem that the shim 6 is displaced and the mold line is changed while the molded products 10, 10 'are cured.
[0039]
Further, since the mold surface plate 2 is integrally connected to the reinforcing frame 3 via the stud bolt 4 and the fixing bracket 5, the shape retention of the mold surface plate 2 is stabilized, and the mold surface plate 2 is Even if evacuation is performed, there is no possibility that the mold surface plate 2 warps.
[0040]
【The invention's effect】
As described above, the composite material molding die of the present invention is composed of the molding die surface plate, the reinforcing frame body, the stud bolt, the fixing bracket, and the shim, so that the molding is performed only by adjusting the thickness of the shim. The mold line of the mold surface plate can be changed freely, and even if the molded product has a complicated shape such as a curved surface or double curved surface, the molded product after molding is accurately molded into the desired shape and dimensions. The mold line can be changed easily and accurately.
[0041]
Further, the molding die of the composite material of the present invention can adjust the mold line from the end portion to the center portion of the molding die surface plate by integrating each stud bolt with the molding die surface plate. Is fixed to the reinforcing frame so that the shape of the mold surface plate can be maintained stably, and even if evacuation is performed on the mold surface plate, the mold surface plate is not warped. By interposing a shim between the reinforcing frame and the shim, it is possible to prevent local deformation of the mold surface plate due to the tension / compression of the stud bolt. In addition, this shim is made of a composite material having a thermal expansion coefficient equivalent to that of the molded product, so that there is no problem that the mold line of the mold surface plate changes due to thermal expansion, and the shim is used for stud bolts. By providing the insertion hole, there is no problem that the position of the shim is shifted during the curing of the molded product and the mold line is changed.
[0042]
The composite material molding method of the present invention comprises forming a mold surface plate with a composite material having a thermal expansion coefficient equivalent to that of the composite material of the fiber reinforced resin composite material to be molded, and forming a plurality of stud bolts on the mold surface. Formed on the face plate so that it protrudes inward, the mold surface plate is supported by the reinforcement frame from the inside, each stud bolt is fixed to the reinforcement frame, and it is formed of a composite material that has the same thermal expansion coefficient as the mold surface plate The modified shim is completed by interposing the shim between the mold surface plate and the reinforcing frame, and changing the mold line of the mold surface plate by the shim to be interposed. Even if the molded product may be deformed due to factors such as material (fiber / resin), laminated fiber orientation, plate thickness, shape, molding process, etc. To correct the molded product to the desired shape It can be formed with high accuracy in dimensions.
[0043]
In the molding method of the composite material of the present invention, the molded product molded line when the molded product formed by laminating and curing the composite material on the mold surface plate is removed from the mold surface plate, By producing based on the difference from the regular mold line, the accuracy of the molded product is further increased, and the quality of the molded product can be greatly improved.
[Brief description of the drawings]
FIG. 1 is a perspective view showing a composite mold according to an embodiment of the present invention.
FIG. 2 is an enlarged view of a part II in FIG.
FIG. 3 is a view showing a molding method of a molded product using a regular mold.
FIG. 4 is a view showing the amount of deformation from a regular mold line of a molded product molded using a regular mold.
FIG. 5 is a view showing a shim manufactured based on the deformation amount of FIG. 4;
FIG. 6 is a view showing a molding method of a molded product using a modified mold die configured by mounting a manufactured shim.
FIG. 7 is a view showing a deformation amount from a normal mold line of a molded product molded using a modified mold.
[Explanation of symbols]
DESCRIPTION OF SYMBOLS 1 Mold 1 'Remodeling mold 2 Mold surface plate 3 Reinforcement frame 4 Stud bolt 5 Fixing bracket 6 Shim 7 Reduction hole 8 Bolt / nut 9 Fixing nut 10, 10' Molded product 11 Insertion hole 12 Deformation amount 13 Regular Mold line 14 Molded product mold line 14 'Mold line 15 Repair mold line

Claims (4)

繊維強化樹脂複合材製の成形品と同等の熱膨脹率を有する複合材で形成された成形型表面板と、この成形型表面板を内側から支持する補強枠体と、前記成形型表面板に設けられて補強枠体側に突出する複数のスタッドボルトと、各スタッドボルトを補強枠体に固定する固定金具と、前記成形品と同等の熱膨脹率を有する複合材で形成され成形型表面板と補強枠体との間に介装されて成形型表面板のモールドラインを変化させるシムとを具備することを特徴とする複合材の成形型。A mold surface plate formed of a composite material having a coefficient of thermal expansion equivalent to that of a molded product made of a fiber reinforced resin composite material, a reinforcing frame that supports the mold surface plate from the inside, and the mold surface plate A plurality of stud bolts projecting toward the reinforcing frame body, a fixing metal fitting for fixing each stud bolt to the reinforcing frame body, and a molding die surface plate and a reinforcing frame formed of a composite material having a thermal expansion coefficient equivalent to that of the molded product A mold for composite material, comprising a shim interposed between the body and a shim for changing the mold line of the surface plate of the mold. シムは、スタッドボルト用の挿通孔を有していることを特徴とする請求項1記載の複合材の成形型。The mold for molding a composite material according to claim 1, wherein the shim has an insertion hole for a stud bolt. 成形しようとする繊維強化樹脂複合材成形品の複合材と同等の熱膨脹率を有する複合材で成形型表面板を形成し、複数のスタッドボルトを成形型表面板に内側に突出するように設け、成形型表面板を内側から補強枠体で支持し、各スタッドボルトを補強枠体に固定し、成形型表面板と同等の熱膨脹率を有する複合材で形成したシムを成形型表面板と補強枠体との間に介装し、介装するシムにより成形型表面板のモールドラインを変化させることを特徴とする複合材の成形方法。Forming a mold surface plate with a composite material having a thermal expansion coefficient equivalent to that of the composite material of the fiber reinforced resin composite material to be molded, and providing a plurality of stud bolts so as to protrude inward from the mold surface plate; The mold surface plate is supported by a reinforcing frame from the inside, each stud bolt is fixed to the reinforcement frame, and a shim formed of a composite material having the same thermal expansion coefficient as the mold surface plate is formed. A molding method for a composite material, characterized in that the molding line of the molding die surface plate is changed by a shim interposed between the body and the shim. シムは、成形型表面板の上に複合材を積層して硬化させて成形した成形品を上記成形型表面板から外した時の上記成形品のモールドラインと正規モールドラインとの差に基づいて製作されることを特徴とする請求項3に記載の複合材の成形方法。Shim is based on the difference between the mold line of the molded product and the regular mold line when the molded product formed by laminating and curing the composite material on the mold surface plate is removed from the mold surface plate. The method of forming a composite material according to claim 3, wherein the composite material is manufactured.
JP34871796A 1996-12-26 1996-12-26 Composite material mold and composite material molding method Expired - Fee Related JP3640751B2 (en)

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GB0519364D0 (en) * 2005-09-22 2005-11-02 Airbus Uk Ltd Assembly of aircraft components
AT503547B1 (en) * 2006-05-16 2007-11-15 Fischer Adv Components Gmbh Mold for fiber-reinforced, plastic-composite aerospace components, comprises supported, fiber-reinforced composite with low coefficient of thermal expansion
US7787979B2 (en) * 2007-03-14 2010-08-31 The Boeing Company Splicing fuselage sections without shims
US9597843B2 (en) * 2014-05-15 2017-03-21 The Boeing Company Method and apparatus for layup tooling

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