JPH1199529A - Integral molding method for composite material - Google Patents

Integral molding method for composite material

Info

Publication number
JPH1199529A
JPH1199529A JP26635297A JP26635297A JPH1199529A JP H1199529 A JPH1199529 A JP H1199529A JP 26635297 A JP26635297 A JP 26635297A JP 26635297 A JP26635297 A JP 26635297A JP H1199529 A JPH1199529 A JP H1199529A
Authority
JP
Japan
Prior art keywords
base material
girder
composite
jig
molding
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.)
Withdrawn
Application number
JP26635297A
Other languages
Japanese (ja)
Inventor
Kazuhiro Hirako
一弘 平子
Masaaki Nishiguchi
正明 西口
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries 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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP26635297A priority Critical patent/JPH1199529A/en
Publication of JPH1199529A publication Critical patent/JPH1199529A/en
Withdrawn legal-status Critical Current

Links

Abstract

PROBLEM TO BE SOLVED: To provide a composite integral molding method, with which a composite material is integrally molded its production cost can be reduced and, in addition, the same production quality as that of the conventional integral molding can be realized without requiring the use of an upper side jig and a molding jig, in which a rubber sheet is used, in the conventional integral molding method. SOLUTION: By laminating a filmy composite material for forming a part member 5 onto the surface of a beam forming mold 10, the part member 5, which is bonded to a composite material base material 06 laminated onto the surface of a lower side jig 04 so as to reinforce the base material 10, is formed. Next, in order to arrange the part member 5 to the predetermined position, to which the base material 06 is bonded, the position of the beam forming mold 10, to which the part member 5 is laminated, is adjusted and arranged. Thus, the part member 5, which is arranged at the predetermined position of the base material 06, is bonded to the base material 06.

Description

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

【0001】[0001]

【発明の属する技術分野】本発明は、航空機の機体製造
等において、下側治具表面上に複合材部材を積層した基
材上に、複合材部材を積層し、単体に成形され、強度を
補強する、部分部材を積み上げて一体成形して機体等の
製造を行う際に、単体に成形された部分部材の成形型を
そのまま使用して、基材と一体成形し、構造体を形成す
るようにした複合材一体成形方法に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a method of manufacturing an airframe, for example, by laminating a composite member on a base material on which a composite member is laminated on the surface of a lower jig, and molding the composite member into a single body. Reinforcement, when stacking and integrally forming partial members and manufacturing an airframe, etc., use the molding die of the partial member formed as a single body as it is, and integrally mold with the base material to form a structure The present invention relates to a method for integrally molding a composite material.

【0002】[0002]

【従来の技術】軽量、高強度を必要とする航空機の主
翼、胴体、尾翼等からなる機体の構造体等には、下側治
具表面に複合材部材を積層して形成された基材上に、補
強材となる部分部材を接合して一体成形したものが近年
多く採用されている。この一体成形は、ゴムシート等か
らなる、バキュームバックで、基材および基材上に接合
する状態に配設された部分部材を被覆した後、バキュー
ムプラグを用いてバキュームバック内を真空引きし、基
体と部分部材とが一体成形する形状になるように、成形
治具で成形した後、オートクレーブ(autoclav
e)内に入れ、加熱・加圧して基材と部分部材とを一体
化するようにしている。
2. Description of the Related Art An airframe structure including a main wing, a fuselage, a tail fin, etc. of an aircraft requiring light weight and high strength is provided with a base member formed by laminating a composite member on the surface of a lower jig. In recent years, a member formed by integrally joining partial members serving as a reinforcing material has been adopted in recent years. This integral molding is made of a rubber sheet, etc., after covering the base material and the partial members arranged in a state of being joined on the base material with a vacuum back, and then evacuating the inside of the vacuum back using a vacuum plug, After molding with a molding jig so that the base and the partial member are integrally molded, an autoclave (autoclave) is formed.
e), and the substrate and the partial member are integrated by heating and pressing.

【0003】図2は、このような基材と部分部材とを一
体化するため、本出願人が特開平8−207065号
「バキュームバック構造及びこれを用いた複合材の一体
成形方法」として提案した複合材一体成形方法に使用す
る成形治具を示す図である。
FIG. 2 shows that the present applicant proposes a method of integrally forming a vacuum back structure and a composite material using the same in Japanese Patent Application Laid-Open No. Hei 8-2070065 in order to integrate such a base material and a partial member. FIG. 6 is a view showing a molding jig used in the composite material integral molding method described above.

【0004】図に示すように、この複合材一体成形方法
に採用される成形治具08は、上側治具01、下側治具
04及びゴムシート02からなり、下側治具04表面上
で積層成形され、外板となる基材としての複合材外板0
6と、複合材外板06に直交して設けられ、桁材となり
複合材外板06の補強を行う、部分部材としての複合材
桁部材05とをゴムシート02で完全に包み込み、ゴム
シート02内に開口させて設けたバキュームプラグ03
を用いてゴムシート02内の真空引きを行い、上側治具
01および下側治具04に形成された一体成形を行う形
状に、複合材外板06および複合材桁部材05をなつか
せる。
[0004] As shown in the figure, a molding jig 08 employed in this composite material integral molding method comprises an upper jig 01, a lower jig 04 and a rubber sheet 02, and is formed on the surface of the lower jig 04. Composite outer plate 0 as a base material to be laminated and formed as an outer plate
6 and a composite girder member 05 as a partial member, which is provided orthogonal to the composite outer plate 06 and serves as a girder material and reinforces the composite outer plate 06, is completely wrapped in the rubber sheet 02, and Vacuum plug 03 opened inside
Then, the composite material outer plate 06 and the composite material girder member 05 are brought into a shape formed in the upper jig 01 and the lower jig 04 to be integrally formed by evacuating the rubber sheet 02.

【0005】次に、成形治具08で一体成形する形状の
公差内に一体化された複合材桁部材05および複合材外
板06を、図示省略したオートクレーブ内に搬入して行
う硬化工程において、流体圧07をゴムシート02外側
から負荷する事で複合材外板06および複合材桁部材0
5を全体を数気圧以下で均一に加圧するとともに、20
0℃以下で加熱することで複合材外板06と複合材桁部
材05とを一体化するようにしている。また、硬化後の
複合材桁部材05の高さは、複合材桁部材05の上端部
を固着し、上端部形状を形成する上側治具01の高さ精
度を保持することで精度を保証するようにしている。
[0005] Next, in a curing step in which the composite girder member 05 and the composite outer plate 06 integrated within the tolerance of the shape to be integrally molded by the molding jig 08 are carried into an autoclave (not shown), By applying a fluid pressure 07 from the outside of the rubber sheet 02, the composite outer plate 06 and the composite girder member 0
5 is uniformly pressurized at a pressure of several atmospheres or less.
By heating at 0 ° C. or lower, the composite outer plate 06 and the composite girder member 05 are integrated. The height of the composite girder member 05 after curing is assured by fixing the upper end of the composite girder member 05 and maintaining the height accuracy of the upper jig 01 forming the upper end shape. Like that.

【0006】しかしながら、このような成形治具08を
構成する上側治具01、ゴムシート02の使用は、成形
治具08高騰の要因となっており、複数の複合材部材を
一体に成形する成形治具の低コスト化実現の為には、こ
のような成形治具08を使用して一体成形することな
く、しかも、このような成形治具08を使用して一体成
形したものと同等の製品品質が得られる複合材一体成形
方法の開発が、従来から課題となっていた。
However, the use of the upper jig 01 and the rubber sheet 02 constituting such a molding jig 08 causes a rise in the molding jig 08, and a molding for integrally molding a plurality of composite members. In order to reduce the cost of the jig, a product equivalent to that integrally formed using such a forming jig 08 without using such a forming jig 08 and integrally forming the same. The development of a method for integrally forming a composite material that can provide high quality has conventionally been an issue.

【0007】[0007]

【発明が解決しようとする課題】本発明は、従来の複合
材一体成形方法において、製造コストの高騰の原因とな
っていた、上側治具およびゴムシートを使用する成形治
具を使用する必要がなく、複合材の一体成形を行うこと
ができ、製造コストを低減でき、しかも、従来の成形治
具を使用して一体成形した製品と同等な一体成形の製品
品質にできる、複合材一体成形方法を提供することを課
題とする。
SUMMARY OF THE INVENTION According to the present invention, it is necessary to use an upper jig and a molding jig using a rubber sheet, which have caused a rise in manufacturing cost in the conventional method of integrally molding a composite material. In addition, the composite material can be integrally molded, the production cost can be reduced, and the product quality of the integral molding can be equal to the product integrally molded using the conventional molding jig. The task is to provide

【0008】[0008]

【課題を解決するための手段】このため、本発明の複合
材一体成形方法は、次の手段を採用した。
Therefore, the method of integrally molding a composite material according to the present invention employs the following means.

【0009】(1)部分部材を形成するエポキシ樹脂を
含有する炭素繊維等からなる複合材繊維を織り、膜状に
された複合材を、部分部材を表面に形成するようにした
桁成形型の表面に積層して、単体の一定厚みの強度を有
する成形材に形成し、下側治具表面に積層された複合材
製の基材上に接合され、基材を補強するようにした部分
部材を形成する工程。なお、下側治具表面に積層される
複合材製の基材は、部分部材と同種の複合材で形成され
るとともに、積層される膜状の複合材の間にハニカムコ
アを挟み込み、強度、剛性に富む構造のものにすること
もできる。
(1) A girder forming die in which a composite material formed by weaving a composite material made of carbon fiber or the like containing an epoxy resin and forming a partial member to form a film is formed on the surface of the partial member. A partial member that is laminated on the surface, formed into a single-piece molded material having a certain thickness of strength, and joined on a composite base material laminated on the lower jig surface to reinforce the base material Forming a. The composite base material laminated on the lower jig surface is formed of the same kind of composite material as the partial member, and the honeycomb core is sandwiched between the laminated film-like composite materials, and the strength, A structure having a high rigidity can also be used.

【0010】(2)基材に接合する所定位置に部分部材
を配置するために、積層された単体の成形材にされた部
分部材が接合される基材の所定位置に配置されるよう
に、部分部材を積層した桁成形型を移動させて、位置を
調整して配置する工程。なお、桁成形型の位置調整は、
基材の上方に架設されたロケータ、およびロケータから
垂下され、部分部材を基材に接合する所定位置に配置で
きるように、桁成形型を配置できるようにしたスライデ
ィングロケータ等からなり、桁成形型を基材上で3次元
的に位置調整できるものにすることが好ましい。
(2) In order to dispose the partial member at a predetermined position to be joined to the base material, the partial member formed into a laminated single-piece molding material is arranged at a predetermined position on the base material to be joined. A step of moving the girder mold on which the partial members are laminated, adjusting the position, and disposing the same. In addition, the position adjustment of the girder mold
A locator erected above the base material, and a sliding locator that is suspended from the locator and allows a girder forming die to be placed at a predetermined position where the partial member is joined to the base material, and the girder forming die It is preferable that the position can be adjusted three-dimensionally on the base material.

【0011】(3)基材の所定位置に配置された部分部
材を、桁成形型とともにオートクレーブ等内に搬入し、
加熱、加圧することにより基材に接合する工程。なお、
一体成形する形状に桁成形型を配置する工程で配置され
た部分部材を基材に接合するために、基材および桁成形
型に積層された部分部材を一様に加圧するため、これら
を被覆する被覆材には、本発明の方法では1気圧以下の
加圧で良いため、ナイロンフィルムで充分であり、これ
を使用するようにすることが好ましい。
(3) The partial member arranged at a predetermined position on the base material is carried into an autoclave or the like together with the girder mold,
A step of joining to a substrate by heating and pressing. In addition,
In order to uniformly press the base member and the partial members laminated on the girder mold in order to join the partial members arranged in the step of arranging the girder mold to the shape to be integrally molded to the base material, they are coated. In the method of the present invention, a pressure of 1 atm or less is sufficient for the coating material, and a nylon film is sufficient. It is preferable to use the nylon film.

【0012】(a)本発明の複合材一体成形方法によれ
ば、積層して部分部材を形成する桁成形型をそのまま使
用して、部分部材と基材とを一体成形するようにしたた
め、従来、成形治具コストの高騰の原因となっていた上
側治具適用が不要となり、さらに部分部材と基材との一
体成形時に、空気漏れ防止を確保しながら行う真空引き
を行い、外部から加圧するようにしていた、従来のゴム
シート適用が、加圧力を小さくできるため必ずしも必要
とせず、ナイロンフィルムでもできるようになる。これ
により、ゴムシートに代え、ナイロンフィルムで被覆し
て真空引きを行い、低圧での外部から加圧を行うように
できるので、従来の欠点となっていた成形治具コストを
この点からも大幅に低減することができる。
(A) According to the method of integrally molding a composite material of the present invention, the partial member and the base material are integrally molded by directly using the girder mold that is laminated to form the partial member. The need to apply the upper jig, which has caused the rise in the cost of the molding jig, is eliminated, and furthermore, during integral molding of the partial member and the base material, vacuum is applied while preventing air leakage, and pressure is applied from the outside. The application of the conventional rubber sheet, which has been made as described above, is not always necessary because the pressing force can be reduced, and the application can be made with a nylon film. As a result, instead of the rubber sheet, it is possible to apply vacuum from the outside by coating with a nylon film and applying low pressure from the outside. Can be reduced.

【0013】また、部分部材を一体成形する基材の所定
位置に配置する桁成形型は、部分部材を積層状態で部分
部材を保持して配置されるため、従来の上側治具を必要
とすることなく、部分部材の基材の所定位置への配置が
正確になる。
Further, the girder mold in which the partial members are disposed at predetermined positions on the base material on which the partial members are integrally formed requires a conventional upper jig because the partial members are disposed while holding the partial members in a laminated state. Without this, the arrangement of the partial members at the predetermined position of the base material becomes accurate.

【0014】さらに、桁成形型は、基材上に架設された
ロケータから垂下されたスライディングロケータを介し
て、位置決めするようにすれば、一体成形された部分部
材の高さも公差内の所定高さにできる。これにより、従
来上側治具を使って一体成形した部材と同等の、硬化後
の部分部材の高さ精度も確保する事が出来る。
Further, if the girder mold is positioned via a sliding locator suspended from a locator erected on the base material, the height of the integrally formed partial member is also within a predetermined height within a tolerance. Can be. As a result, it is possible to ensure the same height accuracy of the cured partial member as that of a member integrally formed using the conventional upper jig.

【0015】また、本発明の複合部材一体成形方法は、
上述(1)、(2)、(3)の手段の採用に加え、次の
手段を採用した。
Further, the method for integrally molding a composite member according to the present invention comprises:
In addition to the above-described means (1), (2), and (3), the following means were employed.

【0016】(4)部分部材を基材の所定位置に配置す
る桁成形型を配置する工程が、基材に接合する所定位置
に、部分部材を配置する成形公差の範囲に穿設された、
スライディングロケータに設けた長穴を移動できるボル
トの長穴の所定位置を固定することにより桁成形型を移
動させて行うようにした。なお、スライディングロケー
タに設けられ桁成形型を移動させる長穴は、水平方向、
又は鉛直方向にボルトを移動させて、長穴の所定位置を
ボルトで固定して、桁成形型の位置調整を精密に行うこ
とができるようにすることが好ましい。また、鉛直方向
の位置調整を行う長穴は、基材上方に架設されたロケー
タから垂下され、桁成形型と一体に固定されるスライデ
ィングロケータに設けるようにすることが好ましい。
(4) The step of arranging a girder forming die for arranging the partial member at a predetermined position of the base material is performed at a predetermined position where the partial member is to be joined to the base material within a range of molding tolerance for arranging the partial member.
The girder forming die is moved by fixing a predetermined position of a long hole of a bolt which can move a long hole provided in a sliding locator. The slot provided in the sliding locator to move the girder mold is horizontal,
Alternatively, it is preferable that the bolt is moved in the vertical direction and a predetermined position of the long hole is fixed with the bolt so that the position of the beam forming die can be precisely adjusted. Further, it is preferable that the elongated hole for adjusting the position in the vertical direction is provided on a sliding locator that is suspended from a locator provided above the base material and fixed integrally with the girder mold.

【0017】本発明の複合材一体成形方法によれば、ボ
ルトが長穴内を移動して長穴の所定位置の固定により、
部分部材を一体成形する基材上の成形公差の範囲に設置
することができる。また、鉛直方向に設けた長穴、より
好ましくはロケータから垂下されたスライディングロケ
ータに鉛直方向に設けた長穴内でボルトを移動させて桁
成形型を上下に、自在にスライディング出来るようにし
たために、桁成形型の上面に外部からの圧力がかかる硬
化工程時においては、流体圧が桁成形型を介して桁成形
型の下面側に伝搬される。しかも、鉛直方向の長穴を成
形公差の範囲に設けるようにしているため、桁成形型の
上下スライド量は、硬化後の桁高さ精度公差内となり、
桁高さ精度は精密に確保ができる。
According to the method of integrally molding a composite material of the present invention, the bolt moves in the elongated hole and the predetermined position of the elongated hole is fixed.
The partial member can be installed within a molding tolerance range on a substrate on which the partial member is integrally molded. Also, to move the bolts in the elongated holes provided in the vertical direction, more preferably in the elongated holes provided in the vertical direction on the sliding locator suspended from the locator, so that the girder mold can be freely slid up and down. During the hardening step in which an external pressure is applied to the upper surface of the girder, fluid pressure is transmitted to the lower surface of the girder via the girder. In addition, since the vertical slot is provided in the range of the molding tolerance, the vertical sliding amount of the girder mold is within the tolerance of the girder height after curing,
Girder height accuracy can be secured precisely.

【0018】[0018]

【発明の実施の形態】以下、本発明の複合材一体成形方
法の実施の一形態を図面にもとづき説明する。図1は、
本発明の複合材一体成形方法の実施の一形態を示すた
め、本実施の形態に使用する成形治具の全体構造を示す
図である。なお、図において、図1に示したものと同一
部材には同一符号を付して説明は、極力省略する。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS One embodiment of the method for integrally forming a composite material according to the present invention will be described below with reference to the drawings. FIG.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a view showing an entire structure of a molding jig used in the present embodiment to show one embodiment of a method of integrally forming a composite material of the present invention. In the drawings, the same members as those shown in FIG. 1 are denoted by the same reference numerals, and description thereof will be omitted as much as possible.

【0019】図において、部分部材としての複合材桁部
材9は、桁成形型10に積層した状態で形成されてい
る。複合材桁部材9は、基材としての複合材外板6の両
端に立設された支柱10の間に架設されたロケータ12
から、下方に垂設された図示省略した縦ロケータに後述
する図示省略されたボルトで結合され、上下動できるス
ライディングロケータ13により、桁成形型10を介し
て位置決めを行い、複合材外板6上の所定の位置にセッ
トされる。
In the figure, a composite girder member 9 as a partial member is formed in a state of being laminated on a girder mold 10. The composite girder member 9 includes a locator 12 erected between columns 10 erected on both ends of a composite outer panel 6 as a base material.
Is positioned by a sliding locator 13 which can be moved up and down by a sliding locator 13 which is connected to a vertical locator (not shown) vertically suspended downward and which can be moved up and down, and is positioned on the composite material outer plate 6. Is set to a predetermined position.

【0020】ロケータ12から垂設された縦ロケータと
スライディングロケータ13の取付部は、硬化後の複合
材桁部材5の高さを精度公差内にする長穴14が設けら
れており、この長穴14内を移動できるボルトを長穴1
4の所定の位置で固定することにより、スライディング
ロケータ13を上下動させて、桁成形型10が上下に自
在にスライド出来、複合材桁部材5を複合材外板6上の
一体成形を行う所定の位置(高さ)に配置できる。
The mounting portion of the vertical locator and the sliding locator 13 vertically provided from the locator 12 is provided with an elongated hole 14 for keeping the height of the cured composite girder member 5 within the tolerance of accuracy. Bolt that can move inside 14
4, the sliding locator 13 is moved up and down so that the girder forming die 10 can slide up and down freely, and the composite girder member 5 is integrally formed on the composite outer plate 6. Position (height).

【0021】また、長穴14を移動してスライディング
ロケータ13を固定するボルトの螺合するロケータ12
から垂設した縦ロケータとロケータ12との間にも水平
方向の長穴を設け、この長穴内を移動できるボルトの固
定により、スライディングロケータ13の横方向の移動
もできるようになり、桁成形型10が水平にも自在にス
ライドでき、複合材桁部材5を複合材外板6上の一体成
形を行う所定の位置に3次元的に位置調整して配置でき
るようにすることもできる。
Further, the locator 12 into which the bolt for fixing the sliding locator 13 by moving the elongated hole 14 is screwed.
A long hole in the horizontal direction is also provided between the vertical locator and the locator 12 which are vertically suspended from the vertical direction. By fixing a bolt which can move in the long hole, the sliding locator 13 can be moved in the horizontal direction, and the girder forming die is formed. 10 can be freely slid horizontally, and the composite girder member 5 can be three-dimensionally adjusted and arranged at a predetermined position on the composite outer plate 6 where integral molding is performed.

【0022】また、スライディングロケータ13と桁成
形型10を固定する固定ボルト15締め結合部は、2重
のOリング16を用いて空気漏れ防止構造としており、
複合材外板6と桁成形型10のみをナイロンフィルム1
7で包み込んだ状態で、真空引きを行う。
Further, the fastening portion for fastening the fixing bolt 15 for fixing the sliding locator 13 and the girder forming mold 10 has an air leakage prevention structure using a double O-ring 16,
Only the composite outer panel 6 and the girder mold 10 are made of nylon film 1
Vacuuming is performed in the state of being wrapped in 7.

【0023】本実施の形態の成形治具20を用いて、複
合材一体成形を行う場合は、複合材桁部材9を構成する
膜状のエポキシ樹脂を含浸させた炭素繊維の織布を積層
して、複合材桁部材9を形成する桁成形型10をそのま
ま使用して一体成形する為、従来の上側治具01適用が
不要となる。また、桁成形型10は、特にスライディン
グロケータ13を介して上下に自在にスライド出来るよ
うにしたため、桁成形型10の上面にかかる硬化工程の
流体圧07が桁成形型10を介して下面側に伝搬され
る。桁成形型10の上下スライド量は、長穴14の長さ
が精度公差内にしてある為、複合材桁部材9の硬化後の
桁高さ精度の確保が可能である。
When the composite material is integrally molded using the molding jig 20 of the present embodiment, a carbon fiber woven fabric impregnated with a film-like epoxy resin constituting the composite girder member 9 is laminated. Thus, since the girder forming die 10 for forming the composite girder member 9 is used as it is and integrally formed, the conventional application of the upper jig 01 becomes unnecessary. In addition, since the girder mold 10 can be freely slid up and down particularly through the sliding locator 13, the fluid pressure 07 of the curing process applied to the upper surface of the girder mold 10 is applied to the lower surface side via the girder mold 10. Propagated. The vertical sliding amount of the girder forming die 10 is within the tolerance of the accuracy of the length of the elongated hole 14, so that the girder height accuracy of the composite girder member 9 after curing can be ensured.

【0024】さらに、空気漏れ防止を確保しながら、ナ
イロンフィルム17で真空引きが出来る為、従来のゴム
シート適用が不要となる。このように、本実施の形態の
成形治具は、従来の成形治具の上側治具01、ゴムシー
ト02の適用が不要となり、成形治具を低廉価で実現す
る事が出来る。又、従来と同等の硬化後の桁高さ精度も
確保する事が出来る。
Further, since the vacuum can be evacuated with the nylon film 17 while ensuring the prevention of air leakage, it is not necessary to apply the conventional rubber sheet. As described above, the forming jig of the present embodiment does not require the application of the upper jig 01 and the rubber sheet 02 of the conventional forming jig, and can realize the forming jig at low cost. In addition, the same accuracy of the girder height after curing as in the conventional case can be secured.

【0025】[0025]

【発明の効果】以上、説明したように、本発明の複合材
一体成形方法は、部分部材を形成する膜状にされた複合
材を、桁成形型の表面に積層して、下側治具表面に積層
された複合材製の基材上に接合され、基材を補強するよ
うにした部分部材を形成する工程、基材に接合する所定
位置に、部分部材を配置するために、部分部材が、所定
位置に配置されるように、部分部材を積層した桁成形型
の位置を調整して配置する工程および基材の所定位置に
配置された部分部材を加熱、外部からの加圧により基材
に接合する工程からなるものとした。
As described above, according to the method for integrally molding a composite material of the present invention, a composite material formed into a film forming a partial member is laminated on the surface of a girder mold, and a lower jig is formed. A step of forming a partial member joined to a composite base material laminated on the surface to reinforce the base material, and to arrange the partial member at a predetermined position to be joined to the base material, Is arranged and adjusted by adjusting the position of the girder forming die on which the partial members are stacked so that the partial members are arranged at the predetermined positions, and the partial members arranged at the predetermined positions of the base material are heated and externally pressurized. It consisted of the step of joining to the material.

【0026】これにより、部分部材を積層して形成する
桁成形型をそのまま使用して、部分部材と基材とを一体
成形するようにしたため、従来、成形治具コストの高騰
の原因となっていた、上側治具が不要となり、さらに、
部分部材と基材との一体成形等に、空気漏れ防止を確保
しながら行う真空引きを行うゴムシート適用が必ずしも
必要ではなくなり、従来の欠点となっていた、成形治具
コストを大幅に低減することができる。また、部分部材
を一体成形する基材の所定位置に配置する桁成形型は、
部分部材を積層状態で保持して配置するため、従来の上
側治具を必要とすることなく、部分部材の基材の所定位
置への配置が正確になる。
As a result, since the girder mold formed by laminating the partial members is used as it is to integrally mold the partial members and the base material, conventionally, the cost of the molding jig has risen. In addition, the upper jig becomes unnecessary,
It is not always necessary to apply a rubber sheet for performing vacuum evacuation while ensuring the prevention of air leakage in the integral molding of the partial member and the base material, and the cost of the molding jig, which has been a drawback in the past, is greatly reduced. be able to. In addition, the girder mold for arranging the partial members at predetermined positions on the base material for integrally molding,
Since the partial members are held and arranged in a stacked state, the arrangement of the partial members at the predetermined position of the base material becomes accurate without the need for a conventional upper jig.

【0027】また、本発明の複合材一体成形方法は桁成
形型を配置する工程が、基材に接合する所定位置に部分
部材を配置する成形公差の範囲に穿設された、長穴を移
動する桁成形型に固定されたボルトの移動により行うよ
うにした。
In the method for integrally molding a composite material according to the present invention, the step of arranging the girder mold includes moving an elongated hole formed within a molding tolerance within which a partial member is arranged at a predetermined position to be joined to the base material. This is performed by moving a bolt fixed to a girder forming die.

【0028】これにより、ボルトの長穴内を移動させ長
穴の所定位置を固定することにより、部分部材を一体成
形する基材上の成形公差の範囲に設置することができ
る。また、鉛直方向に設けた長穴、より好ましくはロケ
ータから垂下されたスライディングロケータに鉛直方向
に設けた長穴内で、ボルトを移動させて桁成形型を上下
自在にスライド出来るため、桁成形型の上面にかかる硬
化工程時においては、流体圧が桁成形型を介して桁成形
型の下面側に伝搬され、しかも、鉛直方向の長穴を成形
公差の範囲に設けるようにしているため、桁成形型の上
下スライド量は、硬化後の部分部材である、複合材桁部
材の桁高さは、精度公差内となり、桁高さ精度の確保が
できる。
Thus, by moving the bolt in the elongated hole and fixing the predetermined position of the elongated hole, the partial member can be set within a molding tolerance range on the base material on which the integral member is integrally molded. In addition, in the elongated hole provided in the vertical direction, more preferably in the elongated hole provided in the sliding locator suspended from the locator in the vertical direction, the bolt can be moved and the girder mold can be slid up and down freely. During the curing process on the upper surface, the fluid pressure is transmitted to the lower surface of the girder via the girder, and the slot in the vertical direction is provided within the range of the molding tolerance. The amount of vertical sliding of the mold is such that the girder height of the composite girder member, which is a partial member after curing, is within the tolerance of accuracy, and the girder height accuracy can be secured.

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

【図1】本発明の複合材一体成形方法の実施の一形態を
示すため、本実施の形態に使用する成形治具の全体構造
を示す図で、図1(a)は全体断面図、図1(b)は図
1(a)に示すA部詳細断面図である。
FIG. 1 is a view showing an entire structure of a forming jig used in the present embodiment to show one embodiment of a method of integrally forming a composite material according to the present invention, and FIG. FIG. 1B is a detailed sectional view of a portion A shown in FIG.

【図2】従来の複合材一体成形方法に使用している成形
治具の全体断面図である。
FIG. 2 is an overall sectional view of a molding jig used in a conventional method of integrally molding a composite material.

【符号の説明】[Explanation of symbols]

01 上側治具 02 ゴムシート 03 バキュームプラグ 4,04 下側治具 05 部分部材としての複合材桁部材 6,06 基材としての複合材外板 07 流体圧 08 成形治具 9 部分部材としての複合材桁部材 10 桁成形型 11 支柱 12 ロケータ 13 スライディングロケータ 14 長穴 15 固定ボルト 16 Oリング 17 ナイロンフィルム 20 成形治具 01 Upper jig 02 Rubber sheet 03 Vacuum plug 4,04 Lower jig 05 Composite girder member as partial member 6,06 Composite outer plate as base material 07 Fluid pressure 08 Molding jig 9 Composite as partial member Material girder member 10 girder forming die 11 support 12 locator 13 sliding locator 14 long hole 15 fixing bolt 16 O-ring 17 nylon film 20 forming jig

───────────────────────────────────────────────────── フロントページの続き (51)Int.Cl.6 識別記号 FI B29L 9:00 31:30 ──────────────────────────────────────────────────の Continued on the front page (51) Int.Cl. 6 Identification code FI B29L 9:00 31:30

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 下側治具表面に積層された複合材製の基
材上に、単体で成形された複合材製の部分部材を接合し
て、一体に成形する複合材一体成形方法において、前記
部分部材を桁成形型に積層して形成する工程と、前記基
材に接合する所定位置に前記部分部材を配置するため
に、前記桁成形型を配置する工程と、前記基材の所定位
置に配置された前記部分部材を前記基材に接合する工程
とからなることを特徴とする複合材一体成形方法。
1. A composite material integral molding method in which a composite material partial member molded as a single body is joined to a composite material base material laminated on a lower jig surface and integrally molded. A step of laminating and forming the partial member on a girder forming die, a step of disposing the girder forming die to arrange the partial member at a predetermined position to be joined to the base material, and a predetermined position of the base material Joining the partial member arranged on the base material to the base material.
【請求項2】 前記桁成形型を配置する工程が、前記基
材に接合する所定位置に前記部分部材を配置する成形公
差の範囲に穿設された長穴内を移動できるボルトの固定
により、前記桁成形型を移動させ配置するようにしたこ
とを特徴とする請求項1の複合材一体成形方法。
2. The method according to claim 1, wherein the step of disposing the girder forming die is performed by fixing a bolt that can move in an elongated hole formed in a range of molding tolerance in which the partial member is disposed at a predetermined position to be joined to the base material. 2. The method according to claim 1, wherein the beam forming die is moved and arranged.
JP26635297A 1997-09-30 1997-09-30 Integral molding method for composite material Withdrawn JPH1199529A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP26635297A JPH1199529A (en) 1997-09-30 1997-09-30 Integral molding method for composite material

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP26635297A JPH1199529A (en) 1997-09-30 1997-09-30 Integral molding method for composite material

Publications (1)

Publication Number Publication Date
JPH1199529A true JPH1199529A (en) 1999-04-13

Family

ID=17429757

Family Applications (1)

Application Number Title Priority Date Filing Date
JP26635297A Withdrawn JPH1199529A (en) 1997-09-30 1997-09-30 Integral molding method for composite material

Country Status (1)

Country Link
JP (1) JPH1199529A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2004106548A (en) * 2002-09-13 2004-04-08 Northrop Grumman Corp Manufacture method for vacuum-assisted transfer molding of cosetting resin
JP2009298400A (en) * 2008-06-13 2009-12-24 Boeing Co:The Method and device to form and mount longeron

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2004106548A (en) * 2002-09-13 2004-04-08 Northrop Grumman Corp Manufacture method for vacuum-assisted transfer molding of cosetting resin
JP2009298400A (en) * 2008-06-13 2009-12-24 Boeing Co:The Method and device to form and mount longeron

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