JPH04329125A - Monolithic molding method of composite - Google Patents

Monolithic molding method of composite

Info

Publication number
JPH04329125A
JPH04329125A JP3098733A JP9873391A JPH04329125A JP H04329125 A JPH04329125 A JP H04329125A JP 3098733 A JP3098733 A JP 3098733A JP 9873391 A JP9873391 A JP 9873391A JP H04329125 A JPH04329125 A JP H04329125A
Authority
JP
Japan
Prior art keywords
molding
jig
molded
autoclave
foam
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Withdrawn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
JP3098733A
Other languages
Japanese (ja)
Inventor
Hiroshi Mizuno
宏 水野
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 JP3098733A priority Critical patent/JPH04329125A/en
Publication of JPH04329125A publication Critical patent/JPH04329125A/en
Withdrawn legal-status Critical Current

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Abstract

PURPOSE:To materialise monolithic molding method where the number of molding jigs to be used and working hours are a few and securing of accuracy is easy. CONSTITUTION:Other molding jig for exclusive use of one molding element 2 is made unnecessary and securing of accuracy of the molding element 2 is made easy, by laminating a prepreg material on the surface of a molding jig having a recessed part in the same form as an external form of the molding element 2. Then a foam 3 is filled into a space between the one and other molding elements 2, 4 and autoclave heating and pressurizing molding is performed, through which the title composite can be molded by an individual molding process and a monolithic molded product which is superior in molding quality can be made manufacturable at a low cost.

Description

【発明の詳細な説明】[Detailed description of the invention]

【0001】0001

【産業上の利用分野】本発明は、樹脂系複合材料製品に
適用される複合材料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 composite material integral molding method applied to resin-based composite material products.

【0002】0002

【従来の技術】樹脂系複合材料の一体成形方法は、成形
する部品の形状等によって種々あるが、ここではハット
型ストリンガと外板より成る補強外板を一体で成形する
場合について述べる。
2. Description of the Related Art There are various methods for integrally molding resin-based composite materials depending on the shape of the parts to be molded, but here we will discuss the case of integrally molding a reinforced outer panel consisting of a hat-shaped stringer and an outer panel.

【0003】従来のこのような構造の成形品を成形する
場合を図4により説明する。先ず、図4(a)に示すよ
うに一体成形組付け時の成形部品の取扱い性や部品の形
態保持性等を考慮して、一方の成形要素(ストリンガ)
02をオートクレーブで予備成形(マトリックス樹脂を
半硬化状態にする)する。具体的には、成形治具01に
成形治具10をセットし、その上に成形要素02を成形
するためのプリプレグ材料を所定の積層構成でレイアッ
プする。次に、オートクレーブ成形するためにブリーザ
クロス05、バキュームシーラント06、バキュームフ
ィルム07を適用し、真空引き口08より真空引きして
バキュームフィルム07内を真空状態にし、オートクレ
ーブで加熱・加圧(必要に応じて)成形する。他方の成
形要素(外板)04についても図4(b)に示すように
図4(a)と同様の方法で、オートクレーブで予備成形
する。
A conventional method of molding a molded product having such a structure will be explained with reference to FIG. First, as shown in Fig. 4(a), one of the molded elements (stringer) is assembled in consideration of the ease of handling the molded parts and the shape retention of the parts during integral molding assembly.
02 is preformed in an autoclave (the matrix resin is semi-cured). Specifically, the molding jig 10 is set on the molding jig 01, and a prepreg material for molding the molding element 02 is laid up thereon in a predetermined laminated configuration. Next, in order to perform autoclave molding, Breather Cloth 05, Vacuum Sealant 06, and Vacuum Film 07 are applied, vacuum is drawn from the vacuum port 08 to create a vacuum inside the vacuum film 07, and heated and pressurized in the autoclave (as necessary). ) according to the shape. The other molded element (outer plate) 04 is also preformed in an autoclave in the same manner as in FIG. 4(a), as shown in FIG. 4(b).

【0004】上記予備成形された成形要素02と成形要
素04は一体成形されるが、その工程は図4(c)に示
すように成形治具01に予備成形された成形要素04を
セットし、その上の所定位置に成形治具11と予備成形
された成形要素02を組付けたものをセットする。その
後は、図4(a)の場合と同様にブリーザクロス05、
バキュームシーラント06、バキュームフィルム07を
適用し、真空引き口08より真空引きしてバキュームフ
ィルム07内を真空状態にしてから、オートクレーブで
加熱・加圧成形を行う。上記成形後は一体成形品より成
形治具11を取除き図4(d)に示す一体成形品を得て
いた。
The above-mentioned preformed molding element 02 and molding element 04 are integrally molded, and the process involves setting the preformed molding element 04 in a molding jig 01 as shown in FIG. 4(c). The molding jig 11 and the preformed molding element 02 assembled thereon are set at a predetermined position. After that, as in the case of FIG. 4(a), the breather cloth 05,
Vacuum sealant 06 and vacuum film 07 are applied, and the inside of vacuum film 07 is evacuated by drawing a vacuum through vacuum port 08, and then heating and pressure molding is performed in an autoclave. After the above molding, the molding jig 11 was removed from the integrally molded product to obtain the integrally molded product shown in FIG. 4(d).

【0005】[0005]

【発明が解決しようとする課題】前記ストリンガと外板
の一体成形について示した従来の方法においては、次の
ような課題を有していた。 (1)実際の部品を成形する場合、特に複曲面構造にお
いては、ストリンガはそれぞれ取付けられる位置によっ
て曲率が異なってくるため、それぞれの曲率に適合した
成形治具が必要となり、多くの成形治具を必要とする。 (2)従来の方法では、大別すると予備成形と一体成形
の2工程が必要であり、予備成形においては外板とスト
リンガ成形の2工程が別々に必要となるなど成形作業、
オートクレーブ操作作業に多大な作業時間を必要とする
。 (3)一方の成形治具の上に外板と成形治具に組付けら
れたストリンガとが単に乗せてあるだけのため、オート
クレーブ硬化中にマトリックス樹脂の低粘度化に伴う成
形要素間の滑りが生じ、そのままの状態では成形後の位
置寸法を確保するのが困難である。仮に、外部拘束構造
による位置寸法の確保を行う場合、その位置決め治具は
相当複雑なものとなり、また高価なものとなる。
Problems to be Solved by the Invention The conventional method described above for integrally molding the stringer and the outer panel had the following problems. (1) When molding actual parts, especially in multi-curved structures, each stringer has a different curvature depending on its mounting position, so a molding jig that matches each curvature is required, and many molding jigs are required. Requires. (2) Conventional methods require two processes, roughly divided into preforming and integral molding, and preforming requires two separate processes of outer plate and stringer molding, etc.
Autoclave operation requires a large amount of time. (3) Because the outer panel and the stringer assembled to the molding jig are simply placed on one molding jig, slippage between the molding elements occurs due to the low viscosity of the matrix resin during autoclave curing. occurs, and in that state it is difficult to secure the positional dimensions after molding. If the positional dimensions were to be secured using an external restraint structure, the positioning jig would be quite complex and expensive.

【0006】本発明は、以上の課題を解消させ、成形品
の位置決め精度の確保が容易で単一の成形工程で高品質
の一体成形品を得ることのできる成形方法を提供するこ
とを目的とする。
An object of the present invention is to provide a molding method that solves the above-mentioned problems, makes it easy to ensure the positioning accuracy of a molded product, and allows a high-quality integral molded product to be obtained in a single molding process. do.

【0007】[0007]

【課題を解決するための手段】本発明の複合材料一体成
形方法は、一方の成形要素の外形形状と同一形状の凹み
部を有する成形治具の面にプリプレグ材料を積層して上
記一方の成形要素を形成し、同形成された一方の成形要
素の凹み部に発泡体を充填し、同一方の成形要素と発泡
体の上面にプリプレグ材料を積層して他方の成形要素を
形成し、同他方の成形要素をカバーにより包んで真空引
きした後、オートクレーブにより加熱・加圧して成形す
ることを特徴としている。
[Means for Solving the Problems] The method for integrally molding a composite material of the present invention involves laminating a prepreg material on the surface of a molding jig having a concave portion having the same external shape as the external shape of one of the molding elements. forming a molded element, filling the recessed part of one molded element with a foam, laminating a prepreg material on the upper surface of the molded element and the foam to form the other molded element, and forming the other molded element. The molding element is wrapped in a cover and evacuated, and then heated and pressurized in an autoclave for molding.

【0008】[0008]

【作用】上記において、一方の成形要素は、成形治具の
凹み部を有する面にプリプレグ材料を積層することによ
り、他の成形治具を必要とせずに精度よく形成すること
ができる。
[Operation] In the above, one of the molding elements can be formed with high precision without requiring another molding jig by laminating the prepreg material on the surface of the molding jig having the recessed portion.

【0009】また、オートクレーブによる加熱・加圧成
形においては、成形治具と接触する一方と他方の成形要
素の外面には所定のオートクレーブ圧が加わり、一方と
他方の成形要素により囲まれた部分では、プリプレグ材
料と共に硬化する発泡体を介してオートクレーブ圧が伝
達されて加圧されるため、良好な品質の一体成形品が得
られる。
[0009] In addition, in heat and pressure molding using an autoclave, a predetermined autoclave pressure is applied to the outer surfaces of one molding element and the other molding element that come into contact with the molding jig, and the area surrounded by the molding elements of one and the other is Since the autoclave pressure is transmitted and pressurized through the foam that hardens together with the prepreg material, an integrally molded product of good quality is obtained.

【0010】上記により、単一のオートクレーブ加熱・
加圧成形工程による成形品の一体成形を可能としたため
、良好な品質の成形品を低コストで製作することが可能
となる。
[0010] According to the above, a single autoclave heating
Since it is possible to integrally mold a molded product using a pressure molding process, it is possible to produce a molded product of good quality at low cost.

【0011】[0011]

【実施例】本発明の第1実施例を図1(a),(b)を
参照しながら説明する。図1(a),(b)に示す本実
施例は、ハット型ストリンガ(成形要素)2と外板(成
形要素)4の一体成形例を示すもので、まず、成形治具
1の内側に成形要素2を形成するためのプリプレグ材料
を所定の積層構成でレイアップする。次に、成形要素2
の凹みの部分に発泡体3を所定量充てんし、その上に成
形要素4を形成するプリプレグ材料を所定の積層構成で
レイアップする。次に、オートクレーブ成形に必要なブ
リーザクロス5、バキュームシーラント6、バキューム
フィルム7よりなるカバーを適用し、真空引き口8より
真空引きしてバキュームフィルム7内を真空にしてオー
トクレーブで加熱・加圧成形を行う。
Embodiment A first embodiment of the present invention will be described with reference to FIGS. 1(a) and 1(b). The present embodiment shown in FIGS. 1(a) and 1(b) shows an example of integral molding of a hat-shaped stringer (molding element) 2 and an outer plate (molding element) 4. The prepreg material for forming the molding element 2 is laid up in a predetermined layered configuration. Next, forming element 2
A predetermined amount of the foam 3 is filled into the concave portion, and a prepreg material forming the molded element 4 is laid up thereon in a predetermined laminated configuration. Next, a cover consisting of a breather cloth 5, a vacuum sealant 6, and a vacuum film 7 necessary for autoclave molding is applied, and a vacuum is drawn from the vacuum opening 8 to evacuate the inside of the vacuum film 7, which is then heated and pressure molded in an autoclave. I do.

【0012】上記において、成形治具1にはストリンガ
2と同一外形形状の溝が施してあるため、その成形治具
1上で直接ストリンガ2のレイアップが可能であり、ス
トリンガ2の成形のための専用の成形治具を不要とする
と共に、成形後のストリンガ2の位置決め精度も確保さ
れる。
In the above, since the forming jig 1 is provided with a groove having the same external shape as the stringer 2, it is possible to lay up the stringer 2 directly on the forming jig 1. This eliminates the need for a dedicated molding jig, and also ensures the positioning accuracy of the stringer 2 after molding.

【0013】上記ストリンガ2のレイアップ後は、同ス
トリンガ2の凹みの部分に発泡体3が充填され、その上
に外板4がレイアップされ、同外板4はブリーザクロス
5、バキュームシーラント6、バキュームフィルム7で
包まれ、真空引きが行われる。
After the stringer 2 is laid up, the concave portion of the stringer 2 is filled with the foam 3, and the outer panel 4 is laid up on top of it, and the outer panel 4 is coated with breather cloth 5 and vacuum sealant 6. , wrapped in a vacuum film 7, and evacuated.

【0014】上記真空引き後に行われるオートクレーブ
加熱・加圧成形時においては、成形治具1と投影面で接
触するストリンガ2及び外板4部分には所定のオートク
レーブ圧が加わり、ストリンガ2と外板4とで囲まれた
部分では、プリプレグ材料と共に硬化する発泡体3を介
してオートクレーブ圧が伝達されて加圧され、図1(b
)に示すような良好な品質の一体成形品が得られる。
During the autoclave heating and pressure forming performed after the vacuum evacuation, a predetermined autoclave pressure is applied to the stringer 2 and outer plate 4 portions that contact the forming jig 1 on the projection surface, and the stringer 2 and outer plate In the area surrounded by 4, autoclave pressure is transmitted and pressurized through the foam 3 that hardens together with the prepreg material.
) An integrally molded product of good quality can be obtained.

【0015】上記により、単一のオートクレーブ加熱・
加圧成形工程で成形品の一体成形ができるため、良好な
品質の成形品を低コストで成形することが可能となった
[0015] According to the above, a single autoclave heating
Since the molded product can be molded in one piece during the pressure molding process, it has become possible to produce molded products of good quality at low cost.

【0016】なお、本実施例に用いる発泡体は、成形に
必要な圧力条件、成形品として要求される重量等によっ
て適正密度を選択することによって、従来のものに比べ
てほとんど重量増加せず、軽量かつ低コストの一体成形
品が得られる。
[0016] The foam used in this example has almost no weight increase compared to conventional foams by selecting an appropriate density depending on the pressure conditions required for molding, the weight required for the molded product, etc. A lightweight and low-cost integrally molded product can be obtained.

【0017】本発明の第2実施例を図2(a),(b)
を参照しながら説明する。図2(a),(b)に示す本
実施例では、第1実施例より更に高圧成形を要する場合
、あるいは、ストリンガ部分に高い面圧強度が要求され
る場合に適用されるものであり、第1実施例における発
泡体3にはアラミド繊維強化プラスチックハニカムコア
、ガラス繊維強化プラスチックハニカムコア、アルミウ
ムハニカムコアなどのハニカムコア9が併用されて成形
されるものである。成形方法は第1実施例と同様に行い
、第1実施例よりも高強度の成形品が得られる。
A second embodiment of the present invention is shown in FIGS. 2(a) and 2(b).
This will be explained with reference to. The present embodiment shown in FIGS. 2(a) and 2(b) is applied when higher pressure molding is required than in the first embodiment, or when high surface pressure strength is required for the stringer portion. The foam 3 in the first embodiment is molded using a honeycomb core 9 such as an aramid fiber-reinforced plastic honeycomb core, a glass fiber-reinforced plastic honeycomb core, or an aluminum honeycomb core. The molding method is the same as in the first example, and a molded product with higher strength than in the first example is obtained.

【0018】本発明の第3実施例を図3(a),(b)
を参照しながら説明する。図3(a),(b)に示す本
実施例は半円型ストリンガの場合を示すもので、成形し
ようとするストリンガ(成形要素)2aと同一外形形状
を施した成形治具1aを用い、第1実施例と同様の成形
工程により図3(b)に示す形状の成形品が得られる。 これはストリンガの形状選択の自由度が大きいことを示
している。
A third embodiment of the present invention is shown in FIGS. 3(a) and 3(b).
This will be explained with reference to. The present embodiment shown in FIGS. 3(a) and 3(b) shows the case of a semicircular stringer, and uses a forming jig 1a having the same outer shape as the stringer (molding element) 2a to be formed. A molded article having the shape shown in FIG. 3(b) is obtained by the same molding process as in the first example. This shows that there is a large degree of freedom in selecting the shape of the stringer.

【0019】[0019]

【発明の効果】本発明の複合材料一体成形方法は、一方
の成形要素の外形形状と同一形状の凹み部を有する成形
治具の面にプリプレグ材料を積層することによって、一
方の成形要素専用の他の成形治具を不要とすると共に、
一方の成形要素の精度確保を容易とし、また、一方と他
方の成形要素の間に発泡体を充填してオートクレーブ加
熱・加圧成形を行うことによって、単一のオートクレー
ブ成形工程で成形できるものとし、成形品質の優れた一
体成形品を低コストで製造可能とする。
Effects of the Invention The method for integrally molding a composite material of the present invention has a method for integrally molding a composite material by laminating a prepreg material on the surface of a molding jig having a concave portion having the same external shape as that of one molding element. In addition to eliminating the need for other molding jigs,
It is easy to ensure the accuracy of one molding element, and it can be molded in a single autoclave molding process by filling a foam between one molding element and the other molding element and performing autoclave heating and pressure molding. , it is possible to manufacture integrally molded products with excellent molding quality at low cost.

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

【図1】本発明の第1実施例の説明図で、(a)は成形
方法の説明図、(b)は成形品の説明図である。
FIG. 1 is an explanatory diagram of a first embodiment of the present invention, in which (a) is an explanatory diagram of a molding method, and (b) is an explanatory diagram of a molded product.

【図2】本発明の第2実施例の説明図で、(a)は成形
方法の説明図、(b)は成形品の説明図である。
FIG. 2 is an explanatory diagram of a second embodiment of the present invention, in which (a) is an explanatory diagram of a molding method, and (b) is an explanatory diagram of a molded product.

【図3】本発明の第3実施例の説明図で、(a)は成形
方法の説明図、(b)は成形品の説明図である。
FIG. 3 is an explanatory diagram of a third embodiment of the present invention, in which (a) is an explanatory diagram of a molding method, and (b) is an explanatory diagram of a molded product.

【図4】従来の成形方法の説明図である。FIG. 4 is an explanatory diagram of a conventional molding method.

【符号の説明】[Explanation of symbols]

1    成形治具 2,2a    成形要素 3    発泡体 4    成形要素 5    ブリーザクロス 6    バキュームシーラント 7    バキュームフィルム 8    真空引き口 9    ハニカムコア 1 Molding jig 2, 2a Molding element 3 Foam 4 Molding elements 5 Breather Cross 6 Vacuum sealant 7 Vacuum film 8 Vacuum port 9 Honeycomb core

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】  一方の成形要素の外形形状と同一形状
の凹み部を有する成形治具の面にプリプレグ材料を積層
して上記一方の成形要素を形成し、同形成された一方の
成形要素の凹み部に発泡体を充填し、同一方の成形要素
と発泡体の上面にプリプレグ材料を積層して他方の成形
要素を形成し、同他方の成形要素をカバーにより包んで
真空引きした後、オートクレーブにより加熱・加圧して
成形することを特徴とする複合材料一体成形方法。
Claim 1: One molding element is formed by laminating a prepreg material on the surface of a molding jig having a concave portion having the same external shape as the outer shape of the one molding element, and Fill the recess with foam, layer the prepreg material on top of the molded element and the foam to form the other molded element, wrap the other molded element with a cover, evacuate it, and then autoclave. A composite material integral molding method characterized by molding by heating and pressurizing.
JP3098733A 1991-04-30 1991-04-30 Monolithic molding method of composite Withdrawn JPH04329125A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3098733A JPH04329125A (en) 1991-04-30 1991-04-30 Monolithic molding method of composite

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3098733A JPH04329125A (en) 1991-04-30 1991-04-30 Monolithic molding method of composite

Publications (1)

Publication Number Publication Date
JPH04329125A true JPH04329125A (en) 1992-11-17

Family

ID=14227717

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3098733A Withdrawn JPH04329125A (en) 1991-04-30 1991-04-30 Monolithic molding method of composite

Country Status (1)

Country Link
JP (1) JPH04329125A (en)

Cited By (12)

* Cited by examiner, † Cited by third party
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JP2003039566A (en) * 2001-07-27 2003-02-13 Fuji Heavy Ind Ltd Method for manufacturing reinforced panel
JP2007176050A (en) * 2005-12-28 2007-07-12 Toho Tenax Co Ltd Molding method for frp molded article with foam core
JP2010058418A (en) * 2008-09-05 2010-03-18 Japan Aircraft Mfg Co Ltd Method of manufacturing hollow product
WO2010065330A1 (en) * 2008-11-25 2010-06-10 The Boeing Company Reinforced foam-filled composite stringer
US7861969B2 (en) 2007-05-24 2011-01-04 The Boeing Company Shaped composite stringers and methods of making
US7879276B2 (en) 2007-11-08 2011-02-01 The Boeing Company Foam stiffened hollow composite stringer
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