JP2011011477A - Method for molding prepreg molding for hollow structure and method for molding composite material molding - Google Patents

Method for molding prepreg molding for hollow structure and method for molding composite material molding Download PDF

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JP2011011477A
JP2011011477A JP2009158125A JP2009158125A JP2011011477A JP 2011011477 A JP2011011477 A JP 2011011477A JP 2009158125 A JP2009158125 A JP 2009158125A JP 2009158125 A JP2009158125 A JP 2009158125A JP 2011011477 A JP2011011477 A JP 2011011477A
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prepreg
mold
release film
molded body
hollow structure
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JP5315147B2 (en
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Masaki Namaizawa
正樹 生井沢
Hiroshi Kato
洋 加藤
Akira Hirayama
明 平山
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Honda Motor Co Ltd
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Abstract

PROBLEM TO BE SOLVED: To provide a method for molding a prepreg molding for a hollow structure which facilitates demolding when a silicon-made core mold is used and a method for molding a composite material molding.SOLUTION: The method includes a first process in which an inside release film 52 as a first release film is coated on a silicon-made core mold 51 for a rear edge, and an outside release film 54 as a second release film is coated on the inside release film 52, a second process in which after a prepreg 28P for the rear edge as a prepreg for the hollow structure is laminated on the outside release film 54, the prepreg 28P for the rear edge is adhered to the silicon-made core mold 51 for the rear edge through the inside release film 52 and the outside release film 54 by applying pressure on the prepreg 28P for the rear edge to obtain a prepreg molding 28 for the rear edge, and a third process for demolding the silicon-made core mold 51 for the rear edge with the inside release film 52 from the longitudinal direction.

Description

本発明は、中空構造用プリプレグ成形体の成形方法及び複合材成形品の成形方法に関するものである。   The present invention relates to a method for forming a hollow structure prepreg molded body and a method for molding a composite material molded article.

従来の中空構造用プリプレグ成形体の成形方法及び複合材成形品の成形方法として、ストレートで長尺な金属製中子型にプリプレグを積層し、このプリプレグから金属製中子型を脱型することで中空構造物用プリプレグとしてのプリプレグ積層体を成形する成形方法が知られている(例えば、特許文献1参照。)。   As a conventional method for forming a hollow structure prepreg molded body and a composite material molded product, a prepreg is laminated on a straight and long metal core mold, and the metal core mold is removed from the prepreg. A molding method for molding a prepreg laminate as a prepreg for a hollow structure is known (for example, see Patent Document 1).

特許文献1の図3、図4によれば、ストレートで長尺状の金属製中子型としての芯金10にプリプレグを積層し、その後、プリプレグから芯金10を長尺方向に脱型してプリプレグ積層体12を形成し、このプリプレグ積層体12を、下型22に積層された下側外皮用プリプレグ21の上に複数個並列配置し、その上に上側外皮用プリプレグ25を積層し、これらの下型22、下側外皮用プリプレグ21、複数のプリプレグ積層体12及び上側外皮用プリプレグ25を真空バッグで覆い、この真空バッグ内を真空引きし、加圧・加熱して複合材成形物を得る。   According to FIGS. 3 and 4 of Patent Document 1, a prepreg is laminated on a core metal 10 as a straight and long metal core mold, and then the core metal 10 is removed from the prepreg in the longitudinal direction. A plurality of prepreg laminates 12 are arranged in parallel on the lower skin prepreg 21 laminated on the lower mold 22, and the upper skin prepreg 25 is laminated thereon. The lower mold 22, the lower skin prepreg 21, the plurality of prepreg laminates 12 and the upper skin prepreg 25 are covered with a vacuum bag, and the vacuum bag is evacuated, pressurized and heated to form a composite material. Get.

特許第4187878号公報Japanese Patent No. 4187878

特許文献1のプリプレグ積層体12が、ストレート部を有する長尺状の単純な形状である場合には、ストレートの芯金10で成形後に芯金10の脱型は容易に行えるが、中空構造物用プリプレグが三次元的な複雑形状になると、長尺方向から三次元的形状の芯金を脱型することが困難になる。脱型を容易に行うには、三次元的形状の芯金を分割型にする必要があり、型のコストは増大する。   In the case where the prepreg laminate 12 of Patent Document 1 is a long and simple shape having a straight portion, the core bar 10 can be easily demolded after being molded with the straight core bar 10, but the hollow structure When the prepreg for use has a three-dimensional complicated shape, it becomes difficult to remove the three-dimensional cored bar from the long direction. In order to perform demolding easily, it is necessary to use a three-dimensional cored bar as a split mold, which increases the cost of the mold.

そこで、金属製の芯金の代わりに、柔軟性があり、三次元的形状に追従可能なシリコン製中子型を使用すれば、脱型が容易になるとともに型のコストを低減することが可能であるが、シリコン製中子型は、その密着性とプリプレグの粘着性とによって、離型フィルムからシリコン製中子型を脱型するのは困難になる。   Therefore, if a silicon core mold that is flexible and can follow a three-dimensional shape is used instead of a metal core, it is easy to remove the mold and reduce the cost of the mold. However, it is difficult for the silicon core mold to be removed from the release film due to the adhesion and the adhesiveness of the prepreg.

本発明の目的は、シリコン製中子型を使用する際に脱型を容易にする中空構造用プリプレグ成形体の成形方法及び複合材成形品の成形方法を提供することにある。   An object of the present invention is to provide a method for forming a hollow structure prepreg molded body and a method for molding a composite molded article that facilitates demolding when a silicon core mold is used.

請求項1に係る発明は、長尺状で三次元形状からなる複合材成形品を形成する中空構造用プリプレグ成形体の成形方法において、シリコン製中子型上に第1離型フィルムを被覆し、この第1離型フィルム上に第2離型フィルムを被覆する第1工程と、第2離型フィルム上に中空構造用プリプレグを積層した後に、中空構造用プリプレグに圧力を加えてシリコン製中子型に第1離型フィルム、第2離型フィルムを介して中空構造用プリプレグを密着させて中空構造用プリプレグ成形体を得る第2工程と、シリコン製中子型を第1離型フィルムと共に長尺方向から脱型する第3工程と、を含むことを特徴とする。   According to a first aspect of the present invention, there is provided a method for forming a hollow structure prepreg molded body that forms a long and three-dimensional composite molded article, wherein a first release film is coated on a silicon core mold. The first step of coating the second release film on the first release film, and laminating the hollow structure prepreg on the second release film, and then applying pressure to the hollow structure prepreg A second step of bringing the hollow structure prepreg into close contact with the core mold through the first mold release film and the second mold release film, and a silicon core mold together with the first mold release film; And a third step of removing the mold from the longitudinal direction.

中空構造物用プリプレグ成形体からシリコン製中子型を脱型するときには、中空構造物用プリプレグ成形体の三次元形状の内面に追従するようにシリコン製中子型が変形するとともに、シリコン製中子型に密着して一体になった第1離型フィルムが第2離型フィルムから離れる。   When removing the silicon core mold from the hollow structure prepreg molded body, the silicon core mold is deformed so as to follow the inner surface of the three-dimensional shape of the hollow structure prepreg molded body. The first release film that comes into close contact with the child mold is separated from the second release film.

請求項2に係る発明は、請求項1記載の中空構造用プリプレグ成形体の成形方法により複合材成形品を成形する複合材成形品の成形方法であって、第1工程及び第2工程で得られるシリコン製中子型付き中空構造物用プリプレグ成形体を、下型に載せた下側外皮用プリプレグ上に配置する第4工程と、中空構造物用プリプレグ成形体上に上側外皮用プリプレグを積層する第5工程と、その後、下側外皮用プリプレグ、中空構造物用プリプレグ成形体及び上側外皮用プリプレグを加圧・加熱して硬化させ、複合材成形品を得る最終工程と、からなり、第4工程より後で且つ最終工程より前までに、第3工程を実施することを特徴とする。   The invention according to claim 2 is a method of forming a composite material molded product by molding a composite material molded product by the molding method of the hollow structure prepreg molded product according to claim 1, which is obtained in the first step and the second step. A fourth step of placing the prepreg molded body for a hollow structure with a silicon core mold on the prepreg for the lower skin placed on the lower mold, and laminating the prepreg for the upper skin on the prepreg molded body for the hollow structure And a final step of obtaining a composite molded article by pressurizing and heating the prepreg for the lower skin, the prepreg molded body for the hollow structure and the prepreg for the upper skin, and then curing. The third step is performed after the fourth step and before the final step.

下側外皮用プリプレグ、中空構造物用プリプレグ成形体及び上側外皮用プリプレグを加圧・加熱する際には、シリコン製中子型が脱型された中空構造物用プリプレグ成形体の形状を保持するために中空構造物用プリプレグ成形体内にチューブバッグを挿入して中空構造物用プリプレグ成形体にチューブバッグから内圧を作用させる。   When pressing and heating the lower skin prepreg, the hollow structure prepreg molded body, and the upper shell prepreg molded body, the shape of the hollow structure prepreg molded body from which the silicon core mold is removed is maintained. Therefore, a tube bag is inserted into the hollow structure prepreg molded body, and an internal pressure is applied to the hollow structure prepreg molded body from the tube bag.

中空構造物用プリプレグ成形体が硬化した後にチューブバッグを離型する際には、中空構造物用プリプレグ成形体内に残っていた第2離型フィルムがチューブバッグの離型を容易にする。   When the tube bag is released after the hollow structure prepreg molded body is cured, the second release film remaining in the hollow structure prepreg molded body facilitates the release of the tube bag.

請求項1に係る発明では、シリコン製中子型上に第1離型フィルムを被覆し、この第1離型フィルム上に第2離型フィルムを被覆する第1工程と、第2離型フィルム上に中空構造用プリプレグを積層した後に、中空構造用プリプレグに圧力を加えてシリコン製中子型に第1離型フィルム、第2離型フィルムを介して中空構造用プリプレグを密着させて中空構造用プリプレグを得る第2工程と、シリコン製中子型を第1離型フィルムと共に長尺方向から脱型する第3工程と、を含むので、三次元形状の複合材成形品の製造に際し、第1離型フィルムと一体になったシリコン製中子型を中空構造物用プリプレグ成形体の中空部に第2離型フィルムを介して追従させながら容易に脱型することができる。また、金属製中子型のような高価な分割中子型が不要となり、コストを低減することができる。   In the invention according to claim 1, the first release film is coated on the silicon core mold and the second release film is coated on the first mold release film, and the second mold release film. After the hollow structure prepreg is laminated, pressure is applied to the hollow structure prepreg so that the hollow structure prepreg is brought into close contact with the silicon core mold via the first release film and the second release film. A second step of obtaining a prepreg for use, and a third step of releasing the silicon core mold from the longitudinal direction together with the first release film. The silicon core die integrated with the first release film can be easily removed while following the hollow portion of the prepreg molded body for a hollow structure via the second release film. Further, an expensive split core type such as a metal core type is not required, and the cost can be reduced.

請求項2に係る発明では、第1工程及び第2工程で得られるシリコン製中子型付き中空構造物用プリプレグ成形体を、下型に載せた下側外皮用プリプレグ上に配置する第4工程と、中空構造物用プリプレグ成形体上に上側外皮用プリプレグを積層する第5工程と、その後、下側外皮用プリプレグ、中空構造物用プリプレグ成形体及び上側外皮用プリプレグを加圧・加熱して硬化させ、複合材成形品を得る最終工程と、からなり、第4工程より後で且つ最終工程より前までに、第3工程を実施するので、複合材成形品の成形時には、シリコン製中子型を引き抜いた後に、中空構造物用プリプレグ成形体の内側に残った第2離型フィルムが、加圧・加熱時に中空構造物用プリプレグ成形体内に挿入されるチューブバッグを離型処理するための離型フィルムに利用され、この結果、離型が容易になるとともに、複合材成形品の成形時の大幅な離型コスト削減を図ることができる。   In the invention which concerns on Claim 2, the 4th process which arrange | positions the prepreg molded object for hollow structures with a silicon core type | mold obtained by a 1st process and a 2nd process on the prepreg for lower skins mounted in the lower mold | type. And a fifth step of laminating the upper skin prepreg on the hollow structure prepreg molding, and then pressurizing and heating the lower skin prepreg, the hollow structure prepreg molding, and the upper skin prepreg And a final step for obtaining a composite molded product, and the third step is carried out after the fourth step and before the final step. Therefore, when molding the composite molded product, a silicon core is formed. After the mold is pulled out, the second release film remaining inside the hollow structure prepreg molded body is used to release the tube bag inserted into the hollow structure prepreg molded body during pressurization and heating. Mold release Is utilized to Irumu, As a result, the release is facilitated, it is possible to significantly release cost savings in molding of the composite molded article.

本発明に係る複合材成形品の完成品を示す斜視図である。It is a perspective view which shows the finished product of the composite material molded product which concerns on this invention. 本発明に係る複合材成形品の一成形段階を示す斜視図である。It is a perspective view which shows one shaping | molding step of the composite material molded article which concerns on this invention. 本発明に係る複合材成形品の一成形段階を示す第1要部拡大斜視図である。It is a 1st principal part expansion perspective view which shows one shaping | molding step of the composite material molded product which concerns on this invention. 本発明に係る複合材成形品の一成形段階を示す第2要部拡大斜視図である。It is a 2nd principal part expansion perspective view which shows one shaping | molding step of the composite material molded article which concerns on this invention. 本発明に係る複合材成形品の前縁型を示す要部斜視図である。It is a principal part perspective view which shows the front edge type | mold of the composite material molded product which concerns on this invention. 本発明に係る複合材成形品の後中間型を示す斜視図である。It is a perspective view which shows the back intermediate mold of the composite material molded product which concerns on this invention. 本発明に係る複合材成形品の後中間型を示す要部斜視図である。It is a principal part perspective view which shows the back intermediate type | mold of the composite material molded product which concerns on this invention. 本発明に係る前縁用プリプレグ成形体の成形方法を示す作用図である。It is an effect | action figure which shows the shaping | molding method of the prepreg molded object for front edges which concerns on this invention. 本発明に係る前中間用プリプレグ成形体の成形方法を示す作用図である。It is an effect | action figure which shows the shaping | molding method of the prepreg molded object for front intermediates which concerns on this invention. 本発明に係る後中間用プリプレグ成形体の成形方法を示す作用図である。It is an effect | action figure which shows the shaping | molding method of the prepreg molded object for back intermediates concerning this invention. 本発明に係る後縁用プリプレグ成形体の成形方法を示す第1作用図である。It is the 1st operation view showing the molding method of the prepreg molding for trailing edges concerning the present invention. 本発明に係る後縁用プリプレグ成形体の成形方法を示す第2作用図である。It is a 2nd operation | movement figure which shows the shaping | molding method of the prepreg molded object for trailing edges which concerns on this invention. 本発明に係る複合材成形品の成形方法を示す第1作用図である。It is the 1st operation figure showing the molding method of the composite material molded article concerning the present invention. 本発明に係る複合材成形品の成形方法を示す第2作用図である。It is a 2nd operation | movement figure which shows the shaping | molding method of the composite material molded product which concerns on this invention. 本発明に係る複合材成形品の成形方法を示す第3作用図である。It is a 3rd operation | movement figure which shows the shaping | molding method of the composite material molded product which concerns on this invention. 本発明に係る複合材成形品の成形中の作用を示す作用図である。It is an operation | movement figure which shows the effect | action in the shaping | molding of the composite material molded article which concerns on this invention.

本発明の実施の形態を添付図に基づいて以下に説明する。なお、図面は符号の向きに見るものとする。   Embodiments of the present invention will be described below with reference to the accompanying drawings. The drawings are viewed in the direction of the reference numerals.

本発明の実施例を説明する。
図1に示すように、エルロン(Aileron)10は、航空機の主翼の後縁に可動するように取付けられる繊維強化複合材料製の補助翼であり、上側外板11と、下側外板12と、これらの上側外板11及び下側外板12とに上下に渡すとともに長手方向に延びる複数の中間桁13〜15とからなる一体成形品である。なお、符号10a〜10dは上側外板11、下側外板12及び中間桁13〜15で囲まれた中空部、17はエルロン10の前縁、18はエルロン10の後縁である。
上記のエルロン10の後縁18は、長手方向に単純なストレート形状ではなく、長手方向でわずかに捩れるように形成されている。
上側外板11は、機構部品の組込みのための凹状開口部11aを有する。
Examples of the present invention will be described.
As shown in FIG. 1, an aileron 10 is an auxiliary wing made of a fiber-reinforced composite material that is movably attached to a trailing edge of an aircraft main wing, and includes an upper skin 11, a lower skin 12, These are integrally molded products comprising a plurality of intermediate girders 13 to 15 which are passed up and down to the upper outer plate 11 and the lower outer plate 12 and extend in the longitudinal direction. Reference numerals 10 a to 10 d are hollow portions surrounded by the upper outer plate 11, the lower outer plate 12 and the intermediate girders 13 to 15, 17 is a front edge of the aileron 10, and 18 is a rear edge of the aileron 10.
The rear edge 18 of the aileron 10 is not a simple straight shape in the longitudinal direction, but is formed to be slightly twisted in the longitudinal direction.
The upper outer plate 11 has a concave opening 11a for assembling a mechanical part.

図2〜図4はエルロン10(図1参照)の成形工程の途中の一段階を示すもので、即ち、後述する図13(b)における真空バッグ83及びシール部材84を除いた状態である。
図2は下型21の上にシート状の外皮用プリプレグ(Prepreg)22を載せ、この外皮用プリプレグ22の上に中空構造物用プリプレグ集合体23を載せた状態を示している。
2 to 4 show one stage in the process of forming the aileron 10 (see FIG. 1), that is, a state in which a vacuum bag 83 and a seal member 84 in FIG.
FIG. 2 shows a state in which a sheet-like prepreg 22 for skin is placed on the lower mold 21 and a prepreg assembly 23 for hollow structure is placed on the prepreg 22 for skin.

中空構造物用プリプレグ集合体23は、エルロン10の前縁部を形成するために中子型(詳細は後述する。)に巻かれて成形された前縁用プリプレグ成形体25と、エルロン10の中間部前部を形成するために中子型に巻かれて成形された前中間用プリプレグ成形体26と、エルロン10の中間部後部を形成するために中子型に巻かれて成形された後中間用プリプレグ成形体27と、エルロン10の後縁部を形成するために中子型に巻かれて成形された後縁用プリプレグ成形体28とを前後に隣り合うように並べたものである。   The hollow structure prepreg assembly 23 includes a front edge prepreg molded body 25 that is wound around a core mold (details will be described later) in order to form a front edge portion of the aileron 10, and the aileron 10. After the intermediate prepreg molded body 26 is formed by being wound around a core mold to form the middle front part, and after being wound around the core mold to be formed at the middle rear part of the aileron 10 The intermediate prepreg molded body 27 and the trailing edge prepreg molded body 28 that is wound around a core mold to form the rear edge of the aileron 10 are arranged side by side in the front-rear direction.

上記の外皮用プリプレグ22は、強化繊維の織布にマトリックス樹脂として熱硬化性樹脂又は熱可塑性樹脂を含浸させた完全に硬化する前のものであり、シート状に形成されている。   The above-described prepreg 22 for outer skin is a sheet before it is completely cured by impregnating a woven fabric of reinforcing fibers with a thermosetting resin or a thermoplastic resin as a matrix resin.

上記の強化繊維としては、炭素繊維、アラミド繊維、ガラス繊維、ボロン繊維が好適である。
上記の熱硬化性樹脂としては、エポキシ樹脂、ポリウレタン、不飽和ポリエステル、ビスマレイミド樹脂、フェノール樹脂が好適である。
上記の熱可塑性樹脂としては、ナイロン6、ナイロン66、ポリエチレンテレフタレート、PEEKが好適である。
As the reinforcing fiber, carbon fiber, aramid fiber, glass fiber, and boron fiber are suitable.
As said thermosetting resin, an epoxy resin, a polyurethane, unsaturated polyester, a bismaleimide resin, and a phenol resin are suitable.
As the above-mentioned thermoplastic resin, nylon 6, nylon 66, polyethylene terephthalate, and PEEK are suitable.

また、上記の前縁用プリプレグ成形体25、前中間用プリプレグ成形体26、後中間用プリプレグ成形体27及び後縁用プリプレグ成形体28は、外皮用プリプレグ22と同一材料である後述するプリプレグ(前縁用プリプレグ25P(図7(b)参照)、前中間用プリプレグ26P(図9(a)参照)、後中間用プリプレグ27P(図10(b)参照)、後縁用プリプレグ28P(図12(a)参照))を中子型により成形したものである。   Further, the prepreg molded body 25 for the front edge, the prepreg molded body 26 for the front intermediate, the prepreg molded body 27 for the rear intermediate, and the prepreg molded body 28 for the rear edge are made of the same material as the prepreg 22 for the outer skin, which will be described later. Front edge prepreg 25P (see FIG. 7B), front intermediate prepreg 26P (see FIG. 9A), rear intermediate prepreg 27P (see FIG. 10B), and rear edge prepreg 28P (FIG. 12). (Refer to (a))).

図3に示すように、前縁用プリプレグ成形体25は、金属製中子型としての前縁型31の表面に巻かれて成形されたものである。
前縁型31は、前縁上型32と、この前縁上型32の下方に配置された前縁下型33と、これらの前縁上型32及び前縁下型33の位置決めをする前縁型用キー34とからなり、前縁型用キー34は、前縁上型32及び前縁下型33のそれぞれの合わせ面に形成された長手方向に延びる一対のキー溝に嵌合している。
As shown in FIG. 3, the prepreg molded body 25 for the leading edge is formed by being wound around the surface of the leading edge mold 31 as a metal core mold.
The leading edge mold 31 includes a leading edge upper mold 32, a leading edge lower mold 33 disposed below the leading edge upper mold 32, and a front edge positioning of the leading edge upper mold 32 and the leading edge lower mold 33. The leading edge type key 34 is fitted in a pair of key grooves extending in the longitudinal direction formed on the mating surfaces of the leading edge upper mold 32 and the leading edge lower mold 33. Yes.

前中間用プリプレグ成形体26は、柔軟性のある前中間用シリコン製中子型35と、この前中間用シリコン製中子型35の表面を覆うふっ素樹脂(例えば、テフロン(登録商標))製の内側離型フィルム36と、この内側離型フィルム36の表面を覆うふっ素樹脂製の外側離型フィルム37とが内側に配置され、外側離型フィルム37に巻かれて成形されたものである。
上記の前中間用シリコン製中子型35、内側離型フィルム36は、前中間用プリプレグ挿入物38を構成するものである。
The front intermediate prepreg molded body 26 is made of a flexible front intermediate silicon core mold 35 and a fluorine resin (for example, Teflon (registered trademark)) covering the surface of the front intermediate silicon core mold 35. The inner release film 36 and the outer release film 37 made of a fluororesin covering the surface of the inner release film 36 are arranged inside and wound around the outer release film 37 to be molded.
The front intermediate silicon core mold 35 and the inner release film 36 constitute the front intermediate prepreg insert 38.

後中間用プリプレグ成形体27は、金属製中子型としての後中間型39に巻かれて成形されたものであり、上面に後中間凹部27aが形成されている。
後中間型39は、上から順に配置された中間上型41、中間中型42、中間下型43と、中間上型41及び中間中型42のそれぞれを互いに位置決めするとともに、中間中型42及び中間下型43のそれぞれを互いに位置決めする中間型用キー45とからなる。
The rear intermediate prepreg molded body 27 is formed by being wound around a rear intermediate mold 39 as a metal core mold, and has a rear intermediate concave portion 27a formed on the upper surface.
The rear intermediate mold 39 positions the middle upper mold 41, the middle middle mold 42, the middle lower mold 43, the middle upper mold 41 and the middle middle mold 42, which are arranged in order from the top, and the middle middle mold 42 and the middle lower mold 42. It comprises an intermediate type key 45 for positioning each of 43.

後縁用プリプレグ成形体28は、柔軟性のある後縁用シリコン製中子型51と、この後縁用シリコン製中子型51の表面を覆うふっ素樹脂(例えば、テフロン(登録商標))製の内側離型フィルム52と、この内側離型フィルム52上の一部に配置された後縁用金属製中子型53と、内側離型フィルム52及び後縁用金属製中子型53の表面を覆うふっ素樹脂製の外側離型フィルム54とが内側に配置され、外側離型フィルム54に巻かれて成形されたものであり、上面に後縁凹部28aが形成されている。   The trailing edge prepreg molding 28 is made of a flexible trailing edge silicon core 51 and a fluorine resin (for example, Teflon (registered trademark)) covering the surface of the trailing edge silicon core 51. Inner release film 52, rear edge metal core mold 53 disposed on a part of inner release film 52, and inner release film 52 and rear edge metal core mold 53. An outer release film 54 made of a fluororesin is disposed on the inner side, wound around the outer release film 54 and molded, and a rear edge recess 28a is formed on the upper surface.

上記の後中間凹部27a及び後縁凹部28aは、前述の凹状開口部11a(図1参照)となる部分である。
後縁用シリコン製中子型51、内側離型フィルム52及び後縁用金属製中子型53は、後縁用プリプレグ挿入物56を構成するものである。
The rear intermediate concave portion 27a and the rear edge concave portion 28a are portions that become the aforementioned concave opening portion 11a (see FIG. 1).
The trailing edge silicon core mold 51, the inner release film 52, and the trailing edge metal core mold 53 constitute the trailing edge prepreg insert 56.

図4に示すように、下型21は、前縁型31を含む前縁用プリプレグ成形体25、前中間用プリプレグ挿入物38及び外側離型フィルム37を含む前中間用プリプレグ成形体26、後中間型39を含む後中間用プリプレグ成形体27、後縁用プリプレグ挿入物56及び外側離型フィルム54を含む後縁用プリプレグ成形体28のそれぞれの一端を位置決めする位置決めピン61〜66が設けられている。   As shown in FIG. 4, the lower die 21 includes a front edge prepreg molded body 25 including a front edge mold 31, a front intermediate prepreg molded body 26 including a front intermediate prepreg insert 38 and an outer release film 37, and a rear. Positioning pins 61 to 66 for positioning one end of each of the rear intermediate prepreg molded body 27 including the intermediate mold 39, the rear edge prepreg insert 56, and the rear edge prepreg molded body 28 including the outer release film 54 are provided. ing.

次に、前述の図2〜図4にて概要説明した後中間型39について詳細説明する。
図5に示すように、後中間型39は、その長手方向に延びるように配置された一体成形の長尺な繊維強化複合材料製の中間型用キー45を備える。なお、符号41bは後中間用プリプレグ成形体27(図3参照)の後中間凹部27a(図3参照)を形成するために中間上型41の上面に形成された中間上型凹部である。
Next, the intermediate mold 39 will be described in detail after having been outlined with reference to FIGS.
As shown in FIG. 5, the rear intermediate mold 39 includes an intermediate mold key 45 made of an integrally formed long fiber-reinforced composite material and disposed so as to extend in the longitudinal direction. Reference numeral 41b denotes an intermediate upper mold recess formed on the upper surface of the intermediate upper mold 41 in order to form a rear intermediate recess 27a (see FIG. 3) of the rear intermediate prepreg molded body 27 (see FIG. 3).

図6に示すように、中間上型41の中間中型42への合わせ面である下面41a、中間中型42の中間上型41への合わせ面である上面42a、中間中型42の中間下型43への合わせ面である下面42b、中間下型43の中間中型42への合わせ面である上面43aに、それぞれキー溝41c,42c,42d,43cが後中間型39の長手方向に延びるように形成され、キー溝41cとキー溝42c、キー溝42dとキー溝43cにそれぞれ中間型用キー45が嵌合されている。   As shown in FIG. 6, the lower surface 41 a that is the mating surface of the intermediate upper mold 41 to the intermediate middle mold 42, the upper surface 42 a that is the mating surface of the intermediate middle mold 42 to the intermediate upper mold 41, and the middle lower mold 43 of the intermediate middle mold 42. Key grooves 41 c, 42 c, 42 d, 43 c are formed on the lower surface 42 b that is the mating surface of the intermediate lower mold 43 and the upper surface 43 a that is the mating surface of the intermediate lower mold 43 to the intermediate middle mold 42, respectively, so as to extend in the longitudinal direction of the rear intermediate mold 39. The intermediate-type key 45 is fitted in the key groove 41c and the key groove 42c, and the key groove 42d and the key groove 43c, respectively.

この結果、中間上型41と中間中型42とが中間型用キー45に直交する方向にずれないように位置決めされ、同様に、中間中型42と中間下型43とが中間型用キー45に直交する方向にずれないように位置決めされている。   As a result, the middle upper mold 41 and the middle middle mold 42 are positioned so as not to be displaced in the direction perpendicular to the middle mold key 45. Similarly, the middle middle mold 42 and the middle lower mold 43 are perpendicular to the middle mold key 45. It is positioned so that it does not shift in the direction of

また、嵌合により発生する摩擦力によって、中間上型41と中間中型42とが中間型用キー45に沿う方向にずれにくくなり、同様に、嵌合により発生する摩擦力によって、中間中型42と中間下型43とが中間型用キー45に沿う方向にずれにくくなる。   Moreover, the intermediate upper mold 41 and the intermediate intermediate mold 42 are not easily displaced in the direction along the intermediate mold key 45 by the frictional force generated by the fitting. Similarly, the intermediate upper mold 42 and the intermediate intermediate mold 42 are separated by the frictional force generated by the fitting. The middle lower mold 43 is less likely to be displaced in the direction along the middle mold key 45.

中間型用キー45は、下型に形成された長尺の溝に長繊維であるガラス樹脂を液状の樹脂(エポキシ樹脂等)を塗布しながら複数積層し、上型により加圧するとともに加熱することにより形成されたものであり、長尺であっても平行度、真直度等の精度が高められ、且つ型成形により安価に成形されている。   The intermediate mold key 45 is formed by laminating a plurality of glass resins, which are long fibers, in a long groove formed in the lower mold while applying a liquid resin (epoxy resin, etc.), and pressurizing and heating the upper mold. Even if it is long, the accuracy such as parallelism and straightness is improved, and it is molded at low cost by molding.

次に、図7〜図12において、エルロン10の成形工程の途中の一段階である各成形体25,26,27,28の成形方法について説明する。
図7(a)は前縁型31の横断面を示している。
図7(b)において、前縁型31の表面に離型剤を塗布した後に、前縁型31にシート状の前縁用プリプレグ25Pを両端部が重なるように巻く。
Next, in FIG. 7 to FIG. 12, a method for forming each of the molded bodies 25, 26, 27, 28, which is one stage in the middle of the process of forming the aileron 10, will be described.
FIG. 7A shows a cross section of the leading edge mold 31.
In FIG. 7B, after applying a release agent to the surface of the leading edge mold 31, a sheet-like leading edge prepreg 25 </ b> P is wound around the leading edge mold 31 so that both ends overlap.

前縁用プリプレグ25Pを巻いた前縁型31に図示せぬ真空バッグを被せ、真空バッグ内を真空引きして、真空バッグで前縁用プリプレグ25Pに圧力を加えることにより、前縁用プリプレグ25Pを前縁型31に密着させ、図7(c)に示すように、前縁用プリプレグ成形体25に成形する。   A front edge mold 31 wound with a front edge prepreg 25P is covered with a vacuum bag (not shown), the inside of the vacuum bag is evacuated, and pressure is applied to the front edge prepreg 25P with the vacuum bag, thereby leading the front edge prepreg 25P. Is brought into close contact with the front edge mold 31 and formed into a prepreg molded body 25 for the front edge as shown in FIG.

図8(a)は柔軟性のある前中間用シリコン製中子型35の横断面を示している。
図8(b)において、前中間用シリコン製中子型35に内側離型フィルム36を巻いて、前中間用シリコン製中子型35の表面を内側離型フィルム36で被覆する。
図8(c)は内側離型フィルム36を前中間用シリコン製中子型35の表面に密着させた状態を示している。
FIG. 8A shows a cross section of the flexible front intermediate silicon core die 35.
In FIG. 8B, the inner release film 36 is wound around the front intermediate silicon core mold 35, and the surface of the front intermediate silicon core mold 35 is covered with the inner release film 36.
FIG. 8C shows a state in which the inner release film 36 is in close contact with the surface of the front intermediate silicon core die 35.

図8(d)において、内側離型フィルム36上に外側離型フィルム37を巻いて、内側離型フィルム36を外側離型フィルム37で被覆する。
図8(e)は外側離型フィルム37を内側離型フィルム36に密着させた状態を示している。
In FIG. 8D, an outer release film 37 is wound on the inner release film 36, and the inner release film 36 is covered with the outer release film 37.
FIG. 8E shows a state in which the outer release film 37 is in close contact with the inner release film 36.

図9(a)において、前中間用プリプレグ挿入物38を被覆した外側離型フィルム37の表面にシート状の前中間用プリプレグ26Pを両端部が重なるように巻く。
図9(b)において、前中間用プリプレグ26Pで覆われた外側離型フィルム37及び前中間用プリプレグ挿入物38を平板77上に載せ、真空バッグ78を被せる。なお、符号79は平板77と真空バッグ78との間をシールするシール部材である。
In FIG. 9A, a sheet-like front intermediate prepreg 26P is wound on the surface of the outer release film 37 coated with the front intermediate prepreg insert 38 so that both ends overlap.
In FIG. 9B, the outer release film 37 and the front intermediate prepreg insert 38 covered with the front intermediate prepreg 26P are placed on a flat plate 77 and covered with a vacuum bag 78. Reference numeral 79 denotes a seal member that seals between the flat plate 77 and the vacuum bag 78.

そして、真空バッグ78内を真空引きし、前中間用プリプレグ26Pを外側離型フィルム37に密着させて、図9(c)に示すように、前中間用プリプレグ成形体26に成形する。
これで、図9(d)に示すように、前中間用プリプレグ成形体26を含む前中間用中間成形品80が完成する。
Then, the inside of the vacuum bag 78 is evacuated and the front intermediate prepreg 26P is brought into close contact with the outer release film 37 to form the front intermediate prepreg molded body 26 as shown in FIG.
Thus, as shown in FIG. 9 (d), the intermediate intermediate product 80 for the front intermediate including the front intermediate prepreg molded body 26 is completed.

図10(a)は後中間型39の横断面を示している。
図10(b)において、後中間型39の表面に離型剤を塗布した後に、後中間型39にシート状の後中間用プリプレグ27Pを両端部が重なるように巻く。
FIG. 10A shows a cross section of the rear intermediate mold 39.
In FIG. 10B, after a release agent is applied to the surface of the rear intermediate mold 39, a sheet-shaped rear intermediate prepreg 27P is wound around the rear intermediate mold 39 so that both ends thereof overlap.

そして、後中間用プリプレグ27Pを巻いた後中間型39に図示せぬ真空バッグを被せ、真空バッグ内を真空引きして、真空バッグで後中間用プリプレグ27Pに圧力を加えることにより、後中間用プリプレグ27Pを後中間型39に密着させて、図10(c)に示すように、後中間用プリプレグ成形体27に成形する。   Then, after winding the rear intermediate prepreg 27P, the intermediate mold 39 is covered with a vacuum bag (not shown), the inside of the vacuum bag is evacuated, and pressure is applied to the rear intermediate prepreg 27P with the vacuum bag. The prepreg 27P is brought into close contact with the rear intermediate mold 39 and formed into a rear intermediate prepreg molded body 27 as shown in FIG.

図11(a)において、後縁用シリコン製中子型51に内側離型フィルム52を巻いて、後縁用シリコン製中子型51の表面を内側離型フィルム52で被覆する。
図11(b)は内側離型フィルム52を後縁用シリコン製中子型51の表面に密着させた状態を示している。
図11(c)において、後縁用シリコン製中子型51に形成された段部51aに内側離型フィルム52を介して後縁用金属製中子型53を載せる。
In FIG. 11A, the inner release film 52 is wound around the rear edge silicon core mold 51, and the surface of the rear edge silicon core mold 51 is covered with the inner release film 52.
FIG. 11B shows a state in which the inner release film 52 is in close contact with the surface of the silicon core mold 51 for the trailing edge.
In FIG. 11 (c), the metal core mold 53 for the trailing edge is placed on the step portion 51 a formed in the silicon core mold 51 for the trailing edge via the inner release film 52.

図11(d)において、内側離型フィルム52及び後縁用金属製中子型53を外側離型フィルム54で一括して被覆する。
図11(e)は外側離型フィルム54を内側離型フィルム52及び後縁用金属製中子型53の表面に密着させた状態を示している。
In FIG. 11 (d), the inner release film 52 and the trailing edge metal core mold 53 are collectively covered with the outer release film 54.
FIG. 11E shows a state in which the outer release film 54 is in close contact with the surfaces of the inner release film 52 and the trailing edge metal core die 53.

図12(a)において、後縁用プリプレグ挿入物56を被覆した外側離型フィルム54の表面にシート状の後縁用プリプレグ28Pを両端部が重なるように巻く。
図12(b)において、後縁用プリプレグ28Pで覆われた外側離型フィルム54及び後縁用プリプレグ挿入物56を平板77上に載せ、真空バック78を被せる。
In FIG. 12A, a sheet-like rear edge prepreg 28P is wound around the surface of the outer release film 54 coated with the rear edge prepreg insert 56 so that both ends thereof overlap each other.
In FIG. 12B, the outer release film 54 and the trailing edge prepreg insert 56 covered with the trailing edge prepreg 28P are placed on a flat plate 77 and covered with a vacuum bag 78.

そして、真空バッグ78内を真空引きし、後縁用プリプレグ28Pを外側離型フィルム54に密着させて、図12(c)に示すように、後縁用プリプレグ成形体28に成形する。
これで、図12(d)に示すように、後縁用プリプレグ成形体28を含む後縁用中間成形品81が完成する。
Then, the inside of the vacuum bag 78 is evacuated, the trailing edge prepreg 28P is brought into close contact with the outer release film 54, and is formed into the trailing edge prepreg molded body 28 as shown in FIG.
Thus, as shown in FIG. 12D, the trailing edge intermediate molded product 81 including the trailing edge prepreg molded body 28 is completed.

次に、完成した各成形体25,26,27,28が、後述する図13の如く積層され、更に、図14、図15の各工程を経てエルロンが完成することになる。
図13について説明する。
図13(a)において、下型21の表面に離型剤を塗布した後、外皮用プリプレグ22を下型21に積層する。外皮用プリプレグ22のうち、下型21の凹部21a内に配置された部分は下側プリプレグ22aである。
Next, the completed molded bodies 25, 26, 27, and 28 are laminated as shown in FIG. 13, which will be described later, and the ailerons are completed through the processes shown in FIGS.
FIG. 13 will be described.
In FIG. 13A, after applying a release agent to the surface of the lower mold 21, a prepreg 22 for skin is laminated on the lower mold 21. Of the prepreg 22 for the outer skin, the portion arranged in the recess 21a of the lower mold 21 is the lower prepreg 22a.

図13(b)において、前述した前縁用プリプレグ成形体25、前中間用プリプレグ成形体26、後中間用プリプレグ成形体27及び後縁用プリプレグ成形体28を外皮用プリプレグ22の上に前後方向(図の左右方向)に隣り合うように並べ、これらの下型21、外皮用プリプレグ22、前縁用プリプレグ成形体25、前中間用プリプレグ成形体26、後中間用プリプレグ成形体27及び後縁用プリプレグ成形体28の上を真空バッグ83で覆う。なお、符号84は下型21と真空バッグ83との間をシールするシール部材である。   13B, the front edge prepreg molded body 25, the front intermediate prepreg molded body 26, the rear intermediate prepreg molded body 27, and the rear edge prepreg molded body 28 are placed on the outer prepreg 22 in the front-rear direction. These are placed adjacent to each other (left and right in the figure), and these lower mold 21, outer prepreg 22, front edge prepreg molded body 25, front intermediate prepreg molded body 26, rear intermediate prepreg molded body 27, and rear edge The prepreg molded body 28 is covered with a vacuum bag 83. Reference numeral 84 denotes a seal member that seals between the lower mold 21 and the vacuum bag 83.

図13(c)において、真空バッグ83内を真空引きし、真空バッグ83で中空構造物用プリプレグ集合体23に圧力を加え、外皮用プリプレグ22と、前縁用プリプレグ成形体25、前中間用プリプレグ成形体26、後中間用プリプレグ成形体27、後縁用プリプレグ成形体28とを密着させる。   In FIG. 13 (c), the vacuum bag 83 is evacuated, and the vacuum bag 83 is used to apply pressure to the hollow structure prepreg assembly 23 so that the prepreg 22 for the outer skin, the prepreg molded body 25 for the leading edge, and the front intermediate The prepreg molded body 26, the rear intermediate prepreg molded body 27, and the trailing edge prepreg molded body 28 are brought into close contact with each other.

図13(d)において、外皮用プリプレグ22の残った部分、即ち、下型21の平坦部21b,21c(図13(a)参照)に載っていた部分22b,22cを中空構造物用プリプレグ集合体23上に折り曲げて両端部が重なるように載せる。
外皮用プリプレグ22の部分22b,22cは、上側プリプレグ22dを構成している。
In FIG. 13 (d), the remaining portion of the prepreg 22 for outer skin, that is, the portions 22b and 22c placed on the flat portions 21b and 21c of the lower mold 21 (see FIG. 13 (a)) are assembled into the prepreg set for hollow structures. Bend on the body 23 and place it so that both ends overlap.
The portions 22b and 22c of the prepreg 22 for outer skin constitute an upper prepreg 22d.

図14(a)〜(d)では、図13(d)に示した外皮用プリプレグ22を省いた状態を示している。
図14(a)において、後縁用プリプレグ成形体28内から、まず、内側離型フィルム52で覆われた後縁用シリコン製中子型51を長手方向に抜き、この後で、後縁用金属製中子型53(図12(d)参照)を抜く。また、同様にして、前中間用プリプレグ成形体26内から内側離型フィルム36で覆われた前中間用シリコン製中子型35を抜く。
14A to 14D show a state in which the prepreg 22 for outer skin shown in FIG. 13D is omitted.
In FIG. 14A, from the inside of the prepreg molded body 28 for the trailing edge, first, the trailing edge silicon core mold 51 covered with the inner release film 52 is pulled out in the longitudinal direction. The metal core mold 53 (see FIG. 12D) is pulled out. Similarly, the front intermediate silicon core die 35 covered with the inner release film 36 is removed from the front intermediate prepreg molded body 26.

後縁用シリコン製中子型51は、その性質上、内側離型フィルム52が密着しやすく、また、内側離型フィルム52と外側離型フィルム54とは離れやすいため、後縁用シリコン製中子型51は、内側離型フィルム52と一体になって脱型することになる。   The silicon core mold 51 for the trailing edge is easily contacted with the inner mold release film 52 due to its nature, and the inner mold release film 52 and the outer mold release film 54 are easily separated from each other. The child mold 51 is removed from the inner mold release film 52 together.

また、図14(b)のように、外側離型フィルム54は、後縁用プリプレグ成形体28の内面側に密着し、内面に残ることになる。
なお、後縁用シリコン製中子型51を抜くと、そこに空間が出来ることになり、後縁用金属製中子型53を下方向に脱落させることが可能になり、後縁用金属製中子型53を長手方向に抜くことが可能になる。(後縁用金属製中子型53には、凹状開口部11a(図1参照)に追従するように中子型凹部が形成されており、後縁用シリコン製中子型51を抜かないと、凹状開口部11aと中子型凹部が噛み合った状態のため、後縁用金属製中子型53が抜けない。)
Further, as shown in FIG. 14B, the outer release film 54 is in close contact with the inner surface side of the trailing edge prepreg molded body 28 and remains on the inner surface.
When the silicon core mold 51 for the trailing edge is pulled out, a space is created there, and the metal core mold 53 for the trailing edge can be dropped downward, and the metal mold for the trailing edge can be removed. The core mold 53 can be pulled out in the longitudinal direction. (In the metal core mold 53 for the trailing edge, a core-shaped recess is formed so as to follow the concave opening 11a (see FIG. 1), and the silicon core mold 51 for the trailing edge must be removed. (Because the concave opening 11a and the core-type recess are meshed with each other, the metal core 53 for the trailing edge cannot be removed.)

同様にして、図14(a)において、内側離型フィルム36と前中間用シリコン製中子型35とが一体になって脱型され、前中間用プリプレグ成形体26の内面側には外側離型フィルム37(図9(d)参照)が密着することになる。   Similarly, in FIG. 14A, the inner release film 36 and the front intermediate silicon core die 35 are integrally removed, and the outer intermediate prepreg molded body 26 is separated from the outer surface by the outer release. The mold film 37 (see FIG. 9D) comes into close contact.

図14(c)において、前中間用プリプレグ成形体26の中空部にナイロン製のチューブバッグ85を挿入し、後縁用プリプレグ成形体28の中空部にナイロン製のチューブバッグ86を挿入する。チューブバッグ85,86の両端は、それぞれ開口部85a,86a(手前側の符号85a,86aのみ図示)になっている。
図14(d)はチューブバッグ85が前中間用プリプレグ成形体26内に挿入され、チューブバッグ86が後縁用プリプレグ成形体28内に挿入された状態を示している。
14C, a nylon tube bag 85 is inserted into the hollow portion of the front intermediate prepreg molded body 26, and a nylon tube bag 86 is inserted into the hollow portion of the trailing edge prepreg molded body 28. Both ends of the tube bags 85 and 86 are openings 85a and 86a (only the reference numerals 85a and 86a on the front side are shown), respectively.
FIG. 14D shows a state where the tube bag 85 is inserted into the front intermediate prepreg molded body 26 and the tube bag 86 is inserted into the trailing edge prepreg molded body 28.

図15(a)において、外皮用プリプレグ22及び下型21上に上型に相当する炭素繊維強化プラスチック製のプレッシャプレート91を載せる。
図15(b)において、プレッシャプレート91の上に、真空引きによる減圧時に通気するためのブリーザ92を載せ、下型21、プレッシャプレート91及びブリーザ92の上を真空バッグ93で覆い、真空バッグ93内を真空引きする。なお、チューブバッグ85,86の両端部である開口部85a,86a(図14(d)参照)は、真空バッグ93の外側に露出している。
In FIG. 15A, a pressure plate 91 made of carbon fiber reinforced plastic corresponding to the upper mold is placed on the prepreg 22 for outer skin and the lower mold 21.
In FIG. 15 (b), a breather 92 is provided on the pressure plate 91 for venting when the pressure is reduced by evacuation. The lower die 21, the pressure plate 91 and the breather 92 are covered with a vacuum bag 93. The inside is evacuated. Note that openings 85 a and 86 a (see FIG. 14D) that are both ends of the tube bags 85 and 86 are exposed to the outside of the vacuum bag 93.

図15(c)において、真空バッグ93内を真空引きした状態で、オートクレーブ内に入れ、0.3〜0.6MPaに加圧、120〜180℃に加熱する。加圧、加熱が終了し、温度が常温まで低下すれば、各プリプレグ、プリプレグ成形体が結合、本硬化してエルロン10が得られる。   In FIG.15 (c), in the state which evacuated the vacuum bag 93, it puts in an autoclave, pressurizes to 0.3-0.6 MPa, and heats to 120-180 degreeC. When the pressurization and heating are completed and the temperature is lowered to room temperature, the prepregs and the prepreg molded body are bonded and finally cured to obtain the aileron 10.

上記の後、エルロン10から前縁型31、後中間型39及びチューブバッグ85,86を取り外す。
前縁型31については、図3において、前縁上型32又は前縁下型33のいずれかを長手方向に向けてハンマー等で軽く叩いて前縁上型32と前縁下型33と前縁型用キー34との相対的な位置関係をずらし、この状態で工具(ペンチ等)で前縁型用キー34の端部を挟んで引き抜き、前縁上型32及び前縁下型33の一方を引き抜き、前縁上型32及び前縁下型33の他方を引き抜く。
After the above, the front edge mold 31, the rear intermediate mold 39, and the tube bags 85 and 86 are removed from the aileron 10.
For the leading edge mold 31, in FIG. 3, either the leading edge upper mold 32 or the leading edge lower mold 33 is lightly tapped with a hammer or the like in the longitudinal direction, and the leading edge upper mold 32, the leading edge lower mold 33, or the The relative positional relationship with the edge type key 34 is shifted, and in this state, the front edge type key 34 is pulled out with a tool (such as pliers) to pull out the front edge upper mold 32 and the front edge lower mold 33. One is pulled out, and the other of the leading edge upper mold 32 and the leading edge lower mold 33 is pulled out.

後中間型39についても、図3において、前縁型31と同様に、中間上型41、中間中型42又は中間下型43のいずれかを長手方向に向けてハンマー等で軽く叩いて中間上型41、中間中型42、中間下型43及び中間型用キー45の相対的な位置関係をずらし、この状態で2本の中間型用キー45をそれぞれ工具(ペンチ等)で端部を挟んで引き抜き、まず、中間中型42を引き抜き、次いで、残りの中間上型41及び中間下型43を引き抜く。   As with the front edge mold 31, the rear intermediate mold 39 is also lightly tapped with a hammer or the like in the longitudinal direction in the middle upper mold 41, the middle middle mold 42, or the middle lower mold 43 in the longitudinal direction in FIG. 3. 41, the intermediate middle mold 42, the middle lower mold 43, and the middle mold key 45 are shifted relative to each other, and in this state, the two middle mold keys 45 are each pulled out with a tool (such as pliers) between the ends. First, the middle middle mold 42 is pulled out, and then the remaining middle upper mold 41 and middle lower mold 43 are pulled out.

図15(c)に戻って、チューブバッグ85,86については、前中間用プリプレグ成形体26及び後縁用プリプレグ成形体28の内面にそれぞれ外側離型フィルム37(図9(d)参照),54(図14(b)参照)が残っているため、取り外しやすくなっている。   Returning to FIG. 15C, for the tube bags 85 and 86, on the inner surfaces of the front intermediate prepreg molded body 26 and the rear edge prepreg molded body 28, respectively, an outer release film 37 (see FIG. 9D), Since 54 (see FIG. 14B) remains, it is easy to remove.

前中間用プリプレグ成形体26及び後縁用プリプレグ成形体28の内面側(チューブバッグ85,86と接する面)には、通常、離型フィルムを配置する作業が大変である。
本発明では、二重になった離型フィルムのうちの内側離型フィルムと中子型とを一緒に引き抜くことで、外側離型フィルムが前中間用プリプレグ成形体26、後縁用プリプレグ成形体28の内面側に密着して残るため、通常の離型フィルムの配置作業が要らなくなる。
Usually, it is difficult to dispose a release film on the inner surface side of the front intermediate prepreg molded body 26 and the rear edge prepreg molded body 28 (surface in contact with the tube bags 85 and 86).
In the present invention, the inner mold release film and the core mold of the double mold release film are pulled out together so that the outer mold release film becomes the front intermediate prepreg molded body 26 and the trailing edge prepreg molded body. Since it remains in close contact with the inner surface side of 28, a normal release film placement operation is not required.

以上に述べたオートクレーブ内での加圧・加熱時の作用を説明する。
図16に示すように、前中間用プリプレグ成形体26内のチューブバッグ85及び後縁用プリプレグ成形体28内のチューブバッグ86にそれぞれ圧縮空気を送り、前中間用プリプレグ成形体26及び後縁用プリプレグ成形体28に所定の圧力を作用させる。
The action at the time of pressurization and heating in the autoclave described above will be described.
As shown in FIG. 16, compressed air is sent to the tube bag 85 in the front intermediate prepreg molded body 26 and the tube bag 86 in the rear edge prepreg molded body 28, respectively, so that the front intermediate prepreg molded body 26 and the rear edge A predetermined pressure is applied to the prepreg molded body 28.

この状態で、真空バッグ内を真空引きさせ、外皮用プリプレグ22に外側から所定の圧力を作用させるとともに、外皮用プリプレグ22及び外皮用プリプレグ22内の各プリプレグを所定の温度に加熱する。   In this state, the inside of the vacuum bag is evacuated, a predetermined pressure is applied to the outer skin prepreg 22 from the outside, and the outer prepreg 22 and each prepreg in the outer skin prepreg 22 are heated to a predetermined temperature.

この結果、前中間用プリプレグ成形体26及び後縁用プリプレグ成形体28は所定の形状に維持されながら、前縁用プリプレグ成形体25、前中間用プリプレグ成形体26、後中間用プリプレグ成形体27及び後縁用プリプレグ成形体28と外皮用プリプレグ22とが結合し、加圧・加熱を終了させて常温まで低下した後に、エルロン10(図1参照)が完成する。   As a result, while the front intermediate prepreg molded body 26 and the rear edge prepreg molded body 28 are maintained in a predetermined shape, the front edge prepreg molded body 25, the front intermediate prepreg molded body 26, and the rear intermediate prepreg molded body 27. Then, after the trailing edge prepreg molded body 28 and the outer skin prepreg 22 are combined and the pressurization and heating are finished and the temperature is lowered to room temperature, the aileron 10 (see FIG. 1) is completed.

上記の図1、図11、図12、図14に示したように、長尺状で三次元形状からなる複合材成形品としてのエルロン10を形成する中空構造用プリプレグ成形体としての後縁用プリプレグ成形体28の成形方法において、シリコン製中子型としての後縁用シリコン製中子型51上に第1離型フィルムとしての内側離型フィルム52を被覆し、この内側離型フィルム52上に第2離型フィルムとしての外側離型フィルム54を被覆する第1工程と、外側離型フィルム54上に中空構造用プリプレグとしての後縁用プリプレグ28Pを積層した後に、後縁用プリプレグ28Pに圧力を加えて後縁用シリコン製中子型51に内側離型フィルム52、外側離型フィルム54を介して後縁用プリプレグ28Pを密着させて後縁用プリプレグ成形体28を得る第2工程と、後縁用シリコン製中子型51を内側離型フィルム52と共に長尺方向から脱型する第3工程と、を含むので、三次元形状のエルロン10の製造に際し、内側離型フィルム52と一体になった柔軟性の有る後縁用シリコン製中子型51を後縁用プリプレグ成形体28の中空部に外側離型フィルム54を介して追従させながら容易に脱型することができる。また、金属製中子型のような高価な分割中子型が不要となり、コストを低減することができる。   As shown in FIGS. 1, 11, 12, and 14, the trailing edge as a hollow structure prepreg molded body that forms the aileron 10 as a composite material molded product having a long and three-dimensional shape. In the molding method of the prepreg molded body 28, the inner mold release film 52 as the first mold release film is covered on the silicon mold 51 for the rear edge as the silicon mold, and the inner mold release film 52 is covered. The first step of coating the outer release film 54 as the second release film and the rear edge prepreg 28P as the hollow structure prepreg on the outer release film 54 are laminated on the rear edge prepreg 28P. By applying pressure, the trailing edge prepreg 28P is brought into intimate contact with the trailing edge silicon core mold 51 via the inner release film 52 and the outer release film 54, thereby forming the trailing edge prepreg molded body 28. And a third step of releasing the trailing edge silicon core mold 51 together with the inner release film 52 from the longitudinal direction. Therefore, when the three-dimensional aileron 10 is manufactured, the inner mold release The flexible core mold 51 for the trailing edge integrated with the mold film 52 is easily removed while following the hollow portion of the prepreg molded body 28 for the trailing edge via the outer release film 54. Can do. Further, an expensive split core type such as a metal core type is not required, and the cost can be reduced.

上記の図1、図13〜図15に示したように、後縁用プリプレグ成形体28の成形方法によりエルロン10を成形するエルロン10の成形方法であって、第1工程及び第2工程で得られる後縁用シリコン製中子型51付き後縁用プリプレグ成形体28を、下型21に載せた下側外皮用プリプレグとしての下側プリプレグ22a上に配置する第4工程と、後縁用プリプレグ成形体28上に上側外皮用プリプレグとしての上側プリプレグ22dを積層する第5工程と、その後、下側プリプレグ22a、後縁用プリプレグ成形体28及び上側プリプレグ22dを加圧・加熱して硬化させ、エルロン10を得る最終工程と、からなり、第4工程より後で且つ最終工程より前までに、第3工程を実施するので、エルロン10の成形時には、後縁用シリコン製中子型51を引き抜いた後に、後縁用プリプレグ成形体28の内側に残った外側離型フィルム54が、加圧・加熱時に後縁用プリプレグ成形体28内に挿入されるチューブバッグ86を離型処理するための離型フィルムに利用され、この結果、離型が容易になるとともに、エルロン10の成形時の大幅な離型コスト削減を図ることができる。   As shown in FIG. 1 and FIG. 13 to FIG. 15, the aileron 10 is formed by the forming method of the trailing edge prepreg molded body 28, and is obtained in the first step and the second step. A fourth step of placing the rear edge prepreg molded body 28 with the silicon core mold 51 for the rear edge on the lower prepreg 22a as the prepreg for the lower skin placed on the lower mold 21, and the prepreg for the rear edge The fifth step of laminating the upper prepreg 22d as the upper skin prepreg on the molded body 28, and then the lower prepreg 22a, the trailing edge prepreg molded body 28 and the upper prepreg 22d are pressurized and heated to be cured, And the third step is performed after the fourth step and before the final step. Therefore, when forming the aileron 10, the trailing edge silicon is formed. After the core-making mold 51 is pulled out, a tube bag 86 is inserted into which the outer release film 54 remaining inside the trailing edge prepreg molding 28 is inserted into the trailing edge prepreg molding 28 during pressurization and heating. This is used for a release film for release treatment. As a result, release is facilitated, and at the same time, the release cost can be greatly reduced when the aileron 10 is molded.

尚、本実施形態では、中空構造用プリプレグ成形体の成形方法及び複合材成形品の成形方法を図1に示したエルロン10に適用したが、これに限らず、航空機の他の部分に適用してもよい。   In the present embodiment, the molding method of the hollow structure prepreg molded body and the molding method of the composite material molded product are applied to the aileron 10 shown in FIG. 1, but the present invention is not limited to this and is applied to other parts of the aircraft. May be.

本発明の中空構造用プリプレグ成形体の成形方法及び複合材成形品の成形方法は、航空機の製造に好適である。   The method for forming a hollow structure prepreg molded body and the method for molding a composite molded article according to the present invention are suitable for aircraft production.

10…複合材成形品(エルロン)、21…下型、22a…下側外皮用プリプレグ(下側プリプレグ)、22d…上側外皮用プリプレグ(上側プリプレグ)、28…中空構造用プリプレグ成形体(後縁用プリプレグ成形体)、28P…中空構造用プリプレグ(後縁用プリプレグ)、35,51…シリコン製中子型(前中間用シリコン製中子型、後縁用シリコン製中子型)、36,52…第1離型フィルム(内側離型フィルム)、37,54…第2離型フィルム(外側離型フィルム)。   DESCRIPTION OF SYMBOLS 10 ... Composite material molded product (aileron), 21 ... Lower mold, 22a ... Lower skin prepreg (lower prepreg), 22d ... Upper skin prepreg (upper prepreg), 28 ... Hollow structure prepreg molded body (rear edge) Prepreg molded body), 28P ... hollow structure prepreg (rear edge prepreg), 35, 51 ... silicon core mold (front intermediate silicon core mold, rear edge silicon core mold), 36, 52 ... 1st release film (inner release film), 37, 54 ... 2nd release film (outside release film).

Claims (2)

長尺状で三次元形状からなる複合材成形品を形成する中空構造用プリプレグ成形体の成形方法において、
シリコン製中子型上に第1離型フィルムを被覆し、この第1離型フィルム上に第2離型フィルムを被覆する第1工程と、
前記第2離型フィルム上に中空構造用プリプレグを積層した後に、前記中空構造用プリプレグに圧力を加えて前記シリコン製中子型に第1離型フィルム、第2離型フィルムを介して中空構造用プリプレグを密着させて中空構造用プリプレグ成形体を得る第2工程と、
前記シリコン製中子型を前記第1離型フィルムと共に長尺方向から脱型する第3工程と、
を含むことを特徴とする中空構造用プリプレグ成形体の成形方法。
In the molding method of a hollow structure prepreg molded body that forms a long and three-dimensional composite molded article,
A first step of coating a first mold release film on a silicon core mold, and coating a second mold release film on the first mold release film;
After laminating the hollow structure prepreg on the second release film, pressure is applied to the hollow structure prepreg to form a hollow structure via the first release film and the second release film on the silicon core mold. A second step of obtaining a hollow structure prepreg molded body by closely attaching the prepreg for use;
A third step of releasing the silicon core mold from the longitudinal direction together with the first release film;
A method for forming a hollow structure prepreg molded body, comprising:
請求項1記載の中空構造用プリプレグ成形体の成形方法により複合材成形品を成形する複合材成形品の成形方法であって、
前記第1工程及び前記第2工程で得られるシリコン製中子型付き中空構造物用プリプレグ成形体を、下型に載せた下側外皮用プリプレグ上に配置する第4工程と、
前記中空構造物用プリプレグ成形体上に上側外皮用プリプレグを積層する第5工程と、
その後、前記下側外皮用プリプレグ、中空構造物用プリプレグ成形体及び上側外皮用プリプレグを加圧・加熱して硬化させ、前記複合材成形品を得る最終工程と、からなり、
前記第4工程より後で且つ前記最終工程より前までに、前記第3工程を実施することを特徴とする複合材成形品の成形方法。
A molding method of a composite material molded product, wherein the composite material molded product is molded by the molding method of the hollow structure prepreg molded body according to claim 1,
A fourth step of disposing the prepreg molded body for a hollow structure with a silicon core mold obtained in the first step and the second step on a prepreg for the lower outer skin placed on the lower die; and
A fifth step of laminating the upper skin prepreg on the hollow structure prepreg molded body,
Thereafter, pressurizing and heating the prepreg for the lower skin, the prepreg molded body for the hollow structure and the prepreg for the upper skin, and curing, to obtain the composite material molded product,
A method for molding a composite molded article, wherein the third step is performed after the fourth step and before the final step.
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Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011011473A (en) * 2009-07-02 2011-01-20 Honda Motor Co Ltd Method for molding wing structure
JP2011152753A (en) * 2010-01-28 2011-08-11 Honda Motor Co Ltd Method for molding aircraft wing structure
WO2014136255A1 (en) 2013-03-08 2014-09-12 株式会社エーゼット Peri-implantitis therapy device
WO2015033625A1 (en) 2013-09-05 2015-03-12 三菱重工業株式会社 Core box and method for producing hollow structure
JP2018083305A (en) * 2016-11-21 2018-05-31 陸子 赤沼 Manufacturing method of hollow shaped structure
CN108622371A (en) * 2018-06-12 2018-10-09 精功(绍兴)复合材料有限公司 Unmanned aerial vehicle composite material rudder and preparation method
JP2020029088A (en) * 2018-08-22 2020-02-27 ザ・ボーイング・カンパニーThe Boeing Company Flexible mandrel for forming composite structures
CN113146809A (en) * 2021-05-17 2021-07-23 吉林建筑大学设计研究院有限责任公司 Core-pulling mold of hollow concrete wallboard, preparation method and application
CN114083812A (en) * 2021-11-12 2022-02-25 江苏亨睿航空工业有限公司 Composite material multi-rotor unmanned aerial vehicle integrated forming die and method

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6325023A (en) * 1986-07-18 1988-02-02 Showa Aircraft Ind Co Ltd Molding of fiber reinforced plastic tube
JPH01247123A (en) * 1988-03-29 1989-10-03 Ube Ind Ltd Preparation of hollow product
JPH04107129A (en) * 1990-08-28 1992-04-08 Kubota Corp Method for molding reinforced plastic pipe
JPH04265714A (en) * 1991-02-21 1992-09-21 Kawasaki Heavy Ind Ltd Manufacture of hollow composite member
JPH08290431A (en) * 1995-04-21 1996-11-05 Olympus Optical Co Ltd Casting core
JPH09201836A (en) * 1996-11-28 1997-08-05 Jiyousou Koshitsu Chrome:Kk Rubber molded product
JPH10146406A (en) * 1996-11-18 1998-06-02 Somar Corp Golf club shaft, golf club and how to manufacture them
JP2011011473A (en) * 2009-07-02 2011-01-20 Honda Motor Co Ltd Method for molding wing structure
JP2011011474A (en) * 2009-07-02 2011-01-20 Honda Motor Co Ltd Method for molding lengthy molding

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6325023A (en) * 1986-07-18 1988-02-02 Showa Aircraft Ind Co Ltd Molding of fiber reinforced plastic tube
JPH01247123A (en) * 1988-03-29 1989-10-03 Ube Ind Ltd Preparation of hollow product
JPH04107129A (en) * 1990-08-28 1992-04-08 Kubota Corp Method for molding reinforced plastic pipe
JPH04265714A (en) * 1991-02-21 1992-09-21 Kawasaki Heavy Ind Ltd Manufacture of hollow composite member
JPH08290431A (en) * 1995-04-21 1996-11-05 Olympus Optical Co Ltd Casting core
JPH10146406A (en) * 1996-11-18 1998-06-02 Somar Corp Golf club shaft, golf club and how to manufacture them
JPH09201836A (en) * 1996-11-28 1997-08-05 Jiyousou Koshitsu Chrome:Kk Rubber molded product
JP2011011473A (en) * 2009-07-02 2011-01-20 Honda Motor Co Ltd Method for molding wing structure
JP2011011474A (en) * 2009-07-02 2011-01-20 Honda Motor Co Ltd Method for molding lengthy molding

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011011473A (en) * 2009-07-02 2011-01-20 Honda Motor Co Ltd Method for molding wing structure
JP2011152753A (en) * 2010-01-28 2011-08-11 Honda Motor Co Ltd Method for molding aircraft wing structure
WO2014136255A1 (en) 2013-03-08 2014-09-12 株式会社エーゼット Peri-implantitis therapy device
US10322529B2 (en) 2013-09-05 2019-06-18 Mitsubishi Heavy Industries, Ltd. Assembled mandrel and method for producing hollow structure
WO2015033625A1 (en) 2013-09-05 2015-03-12 三菱重工業株式会社 Core box and method for producing hollow structure
JP2018083305A (en) * 2016-11-21 2018-05-31 陸子 赤沼 Manufacturing method of hollow shaped structure
CN108622371A (en) * 2018-06-12 2018-10-09 精功(绍兴)复合材料有限公司 Unmanned aerial vehicle composite material rudder and preparation method
CN108622371B (en) * 2018-06-12 2024-03-19 绍兴宝旌复合材料有限公司 Unmanned aerial vehicle composite rudder and preparation method thereof
JP2020029088A (en) * 2018-08-22 2020-02-27 ザ・ボーイング・カンパニーThe Boeing Company Flexible mandrel for forming composite structures
JP7355529B2 (en) 2018-08-22 2023-10-03 ザ・ボーイング・カンパニー Flexible mandrel for forming composite structures
CN113146809A (en) * 2021-05-17 2021-07-23 吉林建筑大学设计研究院有限责任公司 Core-pulling mold of hollow concrete wallboard, preparation method and application
CN113146809B (en) * 2021-05-17 2022-11-08 吉林建筑大学 Core-pulling mold of hollow concrete wallboard, preparation method and application
CN114083812A (en) * 2021-11-12 2022-02-25 江苏亨睿航空工业有限公司 Composite material multi-rotor unmanned aerial vehicle integrated forming die and method
CN114083812B (en) * 2021-11-12 2024-05-24 江苏亨睿航空工业有限公司 Integrated forming die and method for composite material multi-rotor unmanned aerial vehicle

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