JP2002292772A - Manufacturing method for curved-surface sandwich structure - Google Patents

Manufacturing method for curved-surface sandwich structure

Info

Publication number
JP2002292772A
JP2002292772A JP2001097137A JP2001097137A JP2002292772A JP 2002292772 A JP2002292772 A JP 2002292772A JP 2001097137 A JP2001097137 A JP 2001097137A JP 2001097137 A JP2001097137 A JP 2001097137A JP 2002292772 A JP2002292772 A JP 2002292772A
Authority
JP
Japan
Prior art keywords
curved
core
sandwich structure
curved surface
face plate
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.)
Granted
Application number
JP2001097137A
Other languages
Japanese (ja)
Other versions
JP3482525B2 (en
Inventor
Atsushi Goto
淳 後藤
Kazuhiro Nishi
一洋 西
Sayaka Shimizu
さやか 清水
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.)
Kawasaki Heavy Industries Ltd
Original Assignee
Kawasaki 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 Kawasaki Heavy Industries Ltd filed Critical Kawasaki Heavy Industries Ltd
Priority to JP2001097137A priority Critical patent/JP3482525B2/en
Publication of JP2002292772A publication Critical patent/JP2002292772A/en
Application granted granted Critical
Publication of JP3482525B2 publication Critical patent/JP3482525B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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  • Laminated Bodies (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)

Abstract

PROBLEM TO BE SOLVED: To easily and precisely manufacture a curved-surface-shaped sandwich structure having a uniform thickness and high accuracy, a curved-surface sandwich structure having a small curvature in particular and also a sandwich structure having a complicated shape. SOLUTION: In the present manufacturing method of the curved-surface sandwich structure, one side of a block of a polyether imide resin foamed material is machined to be formed into a three-dimensional curved surface, and then a face plate made of FRP and molded in the same curved-surface shape is adhered to the above curved surface, or a face plate of an uncured fiber-reinforced resin prepreg is disposed thereat and joined thereto by heat curing molding. Next, the other side of the block is so machined along the above three-dimensional curved surface as to have a required thickness and to be formed into a three-dimensional curved surface, so that a core be formed. The face plate made of the FRP and molded in the same curved-surface shape is adhered thereafter to the three-dimensional curved surface inside the core of the polyether imide resin foamed material having the required thickness, or the face plate of the uncured fiber-reinforced resin prepreg is disposed thereat and joined thereto by heat curing molding.

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、航空機に用いる曲
面サンドイッチ構造体の製造方法に関する。
The present invention relates to a method for manufacturing a curved sandwich structure used for an aircraft.

【0002】[0002]

【従来の技術】従来より航空機の機体構造材としては、
一般的に図8に示すようにノーメックス、アルミ、GF
RP等より成るハニカムコア30を、2枚の複合材面板
31で挾み、フィルム接着材32を介在して接着結合し
たサンドイッチ構造体33が使用されている。また、一
部には、ポリメタクリルイミド発泡材をコアとするサン
ドイッチ構造体も使用されている。これらのサンドイッ
チ構造体は、主に厚肉が必要な動翼類(補助翼、フラッ
プ、昇降舵、スポイラー等)、ドア、点検口のカバーお
よびレドーム等に使用されていて、機体構造重量に占め
る割合は多くないが、機体表面積については広い割合を
占めている。
2. Description of the Related Art Conventionally, as an aircraft structural material,
Generally, as shown in FIG. 8, Nomex, aluminum, GF
A sandwich structure 33 is used in which a honeycomb core 30 made of RP or the like is sandwiched between two composite material face plates 31 and bonded together with a film adhesive 32 interposed therebetween. In some cases, a sandwich structure having a polymethacrylimide foam material as a core is also used. These sandwich structures are mainly used for rotor blades (auxiliary wings, flaps, elevators, spoilers, etc.), doors, inspection door covers, radomes, etc., which require a thick wall, and occupy the weight of the body structure. Although the ratio is not large, it accounts for a large proportion of the aircraft surface area.

【0003】従来のハニカムコアを使用したサンドイッ
チ構造体は、以下に述べる数多くの問題点があった。 サンドイッチ構造体は、オートクレーブ中での成形
中のハニカムのセル壁以外の部分は加圧されないので、
図8のA部拡大図である図9に示すように複合材面板3
1内の気泡34が残留して強度が低く、航空機の繰り返
し使用中に樹脂層35に微小な亀裂36が発生すること
が多い。 航空機が地上と成層圏を往復する間に、大きな気圧
と気温(1気圧、プラス40℃から1/10気圧、マイ
ナス54℃)の変動を受け、複合材面板31に生じた亀
裂36を通じて外気がハニカムコア30の内部に出入り
する。 外部からハニカムコア30の内部に進入した大気の
中に含まれていた湿気が、航空機の上昇による気圧・気
温の変化により、ハニカムコア30の内部で凝結し、水
滴37として残留する。この過程の繰り返しによりハニ
カムコア30の内部に次第に水分が蓄積され、機体構造
重量が増大する。その重量増加は、ボーイング747ク
ラスの大型旅客機では数100Kgにも達するといわれ
ている。 このハニカムコア30の内部の水分は高空で凍結
し、その体積膨張によりハニカムコア30と複合材面板
31の接着接合を破壊して複合材面板31を剥離させ
る。その結果、構造強度が低下し、飛行安全性が損なわ
れるという大きな問題が発生する。従って、複合材サン
ドイッチ構造体は軽量かつ高剛性であるという理由で、
従来の航空機では機体構造材として多用されてきたが、
徐々に金属構造体に置換されつつあるのが現状である。
A sandwich structure using a conventional honeycomb core has a number of problems described below. Since the sandwich structure is not pressurized except for the cell walls of the honeycomb being formed in the autoclave,
As shown in FIG. 9 which is an enlarged view of a portion A in FIG.
The strength of the air bubbles 34 remaining in 1 is low, and minute cracks 36 often occur in the resin layer 35 during repeated use of the aircraft. As the aircraft makes round trips between the ground and the stratosphere, it undergoes large atmospheric pressure and temperature fluctuations (1 atm, plus 40 ° C to 1/10 atm, minus 54 ° C), and the outside air passes through the cracks 36 formed in the composite material face plate 31 and the honeycomb It goes in and out of the core 30. Moisture contained in the atmosphere that has entered the inside of the honeycomb core 30 from outside is condensed inside the honeycomb core 30 due to changes in air pressure and temperature due to the rise of the aircraft, and remains as water droplets 37. By repeating this process, moisture is gradually accumulated inside the honeycomb core 30, and the body structure weight increases. It is said that the weight increase will reach several hundred kilograms in a large Boeing 747 class passenger aircraft. Moisture inside the honeycomb core 30 freezes in the high sky, and its volume expansion breaks the adhesive bonding between the honeycomb core 30 and the composite material face plate 31 to peel the composite material face plate 31. As a result, there is a serious problem that the structural strength is reduced and the flight safety is impaired. Therefore, because the composite sandwich structure is lightweight and highly rigid,
Although it has been widely used as a fuselage structural material in conventional aircraft,
At present, it is gradually being replaced by metal structures.

【0004】このような問題を解決するために、ハニカ
ムコアを発泡プラスチックに置き換えたサンドイッチ構
造体も提案された。この場合に発泡コアに独立気泡を含
むものを採用すれば、ハニカムコアで問題となったコア
内部への湿気の進入を防ぐことができるという利点があ
る。これは、従来のハニカムコアサンドイッチ構造体の
改良となる魅力的な提案であった。この場合には、複合
材面板の成形とコアとのサンドイッチ化を同一工程で行
うため、その温度と圧力に耐えるコアが必要であること
から、ポリメタクリルイミド発泡材がコアとして使用さ
れた。しかし、このポリメタクリルイミド発泡材コアに
も以下のような問題点があった。 吸湿により強度が大幅に低下する。 運用中の吸湿による変形、体積収縮が生じ、これら
に基づく面積との剥離が発生した。 面板との接合強度が弱く、工具の落下や雹との衝突
による衝撃にて、面板が剥離する。 室温・大気中の放置でも、早く多量に吸湿してしま
うため、シビアな保管条件が要求されると共に、使用前
の乾燥処理が必要となることから、その取り扱いには費
用と手間がかかる。 室温での変形性能が極めて低く、部品形状の成形用
の型に沿わせることがことができず、型とコアを高温に
保持した後に成形を行う必要がある。 これは、専用の治具/設備と手間を必要とすると共
に、設備内の高温の状態で成形型に沿わせるため、基本
的には成形型に正確に沿ったかどうかを確認することが
できず、不具合が発生する場合があり、コアの成形コス
トを引き上げる要因となっている。
In order to solve such a problem, a sandwich structure in which the honeycomb core is replaced with a foamed plastic has been proposed. In this case, if a foamed core containing closed cells is employed, there is an advantage that it is possible to prevent moisture from entering the inside of the core which is a problem in the honeycomb core. This was an attractive proposal to improve the conventional honeycomb core sandwich structure. In this case, since the molding of the composite material face plate and the sandwiching of the core are performed in the same step, a core that can withstand the temperature and pressure is required. Therefore, a polymethacrylimide foam material was used as the core. However, this polymethacrylimide foam core also has the following problems. Strength is greatly reduced by moisture absorption. Deformation and volume shrinkage due to moisture absorption during operation occurred, and peeling from the area based on these occurred. The bonding strength with the face plate is weak, and the face plate is peeled off by the impact due to the drop of the tool or the collision with the hail. Even when left at room temperature and in the air, it absorbs a large amount of moisture quickly, so that severe storage conditions are required and a drying treatment before use is required, so that handling is expensive and troublesome. Deformation performance at room temperature is extremely low, so that it cannot be conformed to a mold for forming a part shape, and it is necessary to perform molding after holding the mold and the core at a high temperature. This requires special jigs / equipment and labor, and since it follows the mold at a high temperature in the equipment, it is basically impossible to check whether the mold has been accurately followed. In some cases, inconveniences occur, which is a factor that increases the molding cost of the core.

【0005】さらに、上記ポリメタクリルイミド発泡材
をコアとするサンドイッチ構造体の欠点を改良するた
め、ポリエーテルイミド発泡材が検討された。ポリエー
テルイミド発泡材は、ポリメタクリルイミド発泡材と比
較して図10に示すように吸湿量が小さいばかりでな
く、吸湿による特性劣化が無いため、厳密な保管条件の
管理や脱湿処理等の作業も全く不要である。また、ポリ
エーテルイミド発泡材は、独立気泡から成るものであ
り、サンドイッチ構造体のコアとしても浸水が無いこ
と、及び重量や強度特性もほぼポリメタクリルイミド発
泡材と同等であることから、サンドイッチ構造体用のコ
アとして適しているものと考えられる。
Further, in order to improve the drawbacks of the sandwich structure having the polymethacrylimide foam as a core, a polyetherimide foam has been studied. As shown in FIG. 10, the polyetherimide foam material has not only a small amount of moisture absorption as compared to the polymethacrylimide foam material, but also has no characteristic deterioration due to moisture absorption. No work is required. In addition, the polyetherimide foam material is composed of closed cells, and has no water intrusion as the core of the sandwich structure, and the weight and strength characteristics are almost the same as those of the polymethacrylimide foam material. It is considered to be suitable as a body core.

【0006】上記のように利点の多いポリエーテルイミ
ド発泡材であるが、これをコアにしたサンドイッチ構造
体の図11に示す製造工程において、以下に述べるよう
な問題点があった。 ポリエーテルイミド樹脂そのものは熱可塑性であ
り、200℃近傍の温度で荷重を与えることにより永久
変形を与えることが可能である。しかし今回使用したい
ポリエーテルイミド発泡材は密度を下げるために多量の
空隙(発泡)を含んでいることから、元々圧縮強度が低
い。特にコアの成形に必要な200℃近傍では、より圧
縮強度が下がることから、従来は温度と圧力を多段階に
制御可能な特殊な設備を用いてコア成形を行う必要があ
った。 また、このポリエーテルイミド発泡材を用いても、
例えば航空機の翼端の如き袋状の曲率の小さい部品形状
に成形することは不可能であった。
As described above, the polyetherimide foamed material having many advantages, however, has the following problems in the manufacturing process shown in FIG. 11 of the sandwich structure using this as a core. The polyetherimide resin itself is thermoplastic, and can be permanently deformed by applying a load at a temperature near 200 ° C. However, since the polyetherimide foam material to be used this time contains a large amount of voids (foaming) to reduce the density, the compression strength is originally low. In particular, at around 200 ° C. necessary for molding the core, the compressive strength is further reduced. Therefore, conventionally, it has been necessary to perform the core molding using special equipment capable of controlling the temperature and pressure in multiple stages. Also, using this polyetherimide foam,
For example, it has been impossible to form a bag-shaped part having a small curvature, such as a wing tip of an aircraft.

【0007】[0007]

【発明が解決しようとする課題】そこで本発明は、従来
のポリエーテルイミド発泡材コアとFRP製面板とより
成るサンドイッチ構造体の製造方法について、上記問題
点を解決し、とりわけポリエーテルイミド発泡材コアの
加工方法を改善し、従来の製造方法では実現できなかっ
た曲面形状のサンドイッチ構造体を精度よく製造できる
方法を提供しようとするものである。
SUMMARY OF THE INVENTION The present invention solves the above-mentioned problems with a conventional method for producing a sandwich structure comprising a polyetherimide foam core and an FRP face plate. It is an object of the present invention to improve a method of processing a core and to provide a method for accurately manufacturing a sandwich structure having a curved shape, which cannot be realized by a conventional manufacturing method.

【0008】[0008]

【課題を解決するための手段】上記課題を解決するため
の本発明の曲面サンドイッチ構造体の製造方法の1つ
は、ポリエーテルイミド樹脂発泡材を曲面板に加工して
コアとなし、このコアの両面に同じ曲面に成形したFR
P製面板を接着するか、又は未硬化繊維強化樹脂プリプ
レグ面板を配し加熱硬化成形して接合することを特徴と
するものである。
One of the methods for manufacturing a curved sandwich structure according to the present invention for solving the above-mentioned problems is to form a core by processing a polyetherimide resin foam material into a curved plate and forming the core. FR molded on the same curved surface on both sides
The method is characterized in that a P-made face plate is bonded or an uncured fiber reinforced resin prepreg face plate is arranged, heat-cured, and joined.

【0009】上記の曲面サンドイッチ構造体の製造方法
において、コアの曲面状の加工の1つは、所要厚のポリ
エーテルイミド樹脂発泡材の平板を、170℃〜210
℃の温度範囲で真空吸引による圧力にて三次元の曲面に
成形加工するものであり、コアの曲面状の加工の他の1
つは、ポリエーテルイミド樹脂発泡材のブロックを、所
要厚の三次元の曲面板に機械加工するものである。
In the above-mentioned method for manufacturing a curved sandwich structure, one of the processes of forming the curved surface of the core is to form a flat plate of a polyetherimide resin foam material having a required thickness from 170 ° C. to 210 ° C.
It is to form a three-dimensional curved surface with the pressure of vacuum suction in a temperature range of ° C.
First, a block of a polyetherimide resin foam is machined into a three-dimensional curved plate having a required thickness.

【0010】本発明の曲面サンドイッチ構造体の製造方
法の他の1つは、ポリエーテルイミド樹脂発泡材のブロ
ックの一側を機械加工して、三次元の曲面を形成し、次
にこの曲面に、同じ曲面形状に成形したFRP製面板を
接着するか、又は未硬化繊維強化樹脂プリプレグ面板を
配し加熱硬化成形して接合し、次いで前記ポリエーテル
イミド樹脂発泡材のブロックの他側を、前記三次元の曲
面に沿って所要厚となるように機械加工して三次元の曲
面を形成しコアとなし、然る後所要厚となったポリエー
テルイミド樹脂発泡材コアの内側の三次元の曲面に、同
じ曲面形状に成形したFRP製面板を接着するか、又は
未硬化繊維強化樹脂プリプレグ面板を配し加熱硬化成形
して接合することを特徴とするものである。
Another method of manufacturing a curved sandwich structure according to the present invention is to machine one side of a block of a polyetherimide resin foam material to form a three-dimensional curved surface, and then apply the curved surface to the curved surface. Adhering a FRP face plate molded into the same curved shape, or disposing an uncured fiber reinforced resin prepreg face plate, heat-curing molding and joining, then the other side of the polyetherimide resin foam material block, A three-dimensional curved surface is machined to the required thickness along the three-dimensional curved surface to form a three-dimensional curved surface to form a core, and then the three-dimensional curved surface inside the polyetherimide resin foam core having the required thickness. Then, an FRP face plate formed into the same curved shape is bonded thereto, or an uncured fiber reinforced resin prepreg face plate is disposed, and then heat-cured and joined.

【0011】[0011]

【発明の実施の形態】本発明の曲面サンドイッチ構造体
の製造方法の実施形態を説明する。先ずその1つを図に
よって説明すると、図1のaに示すようにポリエーテル
イミド樹脂発泡材を曲面板に加工してコア1となし、次
にこのコア1の両面に図1のbに示すように夫々同じ曲
面に成形したFRP製面板2,2′を接着するか、又は
コア1の両面に図1のcに示すように未硬化繊維強化樹
脂プリプレグ面板3,3′を配し、これを加熱硬化成形
して接合し、曲面サンドイッチ構造体4を得る。
DESCRIPTION OF THE PREFERRED EMBODIMENTS An embodiment of a method for manufacturing a curved sandwich structure according to the present invention will be described. First, one of them will be described with reference to the drawings. As shown in FIG. 1A, a polyetherimide resin foam material is processed into a curved plate to form a core 1, and then both sides of the core 1 are shown in FIG. FRP face plates 2 and 2 'molded to the same curved surface as described above, respectively, or uncured fiber reinforced resin prepreg face plates 3 and 3' as shown in FIG. Are heat-cured and joined to obtain a curved sandwich structure 4.

【0012】この曲面サンドイッチ構造体4の製造方法
において、曲面板のコア1の加工方法には、2つの方法
がある。その1つは成形加工である。コア1の成形は、
ポリエーテルイミド樹脂発泡材に温度と圧力を負荷する
ことによって行う。従って、上下の型のマッチドダイ方
式でも成形できるが、型費を安くできることから図2に
示すように三次元の曲面成形用型治具5の型面6に所要
厚のポリエーテルイミド樹脂発泡材の平板7を載せ、そ
の上から変形性のある樹脂フィルム8を覆い、曲面成形
用型治具5の基板9上に装着したシール材10にてシー
ルして設置し、樹脂フィルム8内に温度と圧力を負荷す
る方法が好ましい。この方法では圧力を特別に制御する
ことなく、樹脂フィルム8に装備した口金11から単純
に図示せぬ真空ポンプ等にて樹脂フィルム8内を吸引す
る圧力を、ポリエーテルイミド樹脂発泡材の平板7に負
荷することにより、このポリエーテルイミド樹脂発泡材
の平板7をある程度曲面成形用型治具5の型面6に沿わ
せた状態で、図3に示す170℃〜210℃の温度を、
温度が高い側では数分、温度が低い側では数時間かける
ことにより、図4に示すように熱可塑性材料であるポリ
エーテルイミド発泡材の平板7に型面6に沿った永久変
形を与えて三次元の曲面板のコア1に成形加工できる。
この成形加工における温度測定は、図2に示すようにポ
リエーテルイミド樹脂発泡材の平板7の表裏に設置した
複数個の熱電対12によって行われる。
In the method of manufacturing the curved sandwich structure 4, there are two methods for processing the core 1 of the curved plate. One of them is molding. The molding of the core 1
This is performed by applying temperature and pressure to the polyetherimide resin foam. Therefore, although the molding can be performed by a matched die method of the upper and lower dies, since the cost of the die can be reduced, the required thickness of the polyetherimide resin foam material is formed on the mold surface 6 of the three-dimensional curved surface molding jig 5 as shown in FIG. A flat plate 7 is placed, a deformable resin film 8 is covered therefrom, and the resin film 8 is sealed with a sealing material 10 mounted on a substrate 9 of a curved surface forming jig 5. A method of applying pressure is preferred. In this method, the pressure for sucking the inside of the resin film 8 from the base 11 mounted on the resin film 8 by a vacuum pump or the like, which is not shown, is applied to the flat plate 7 made of polyetherimide resin foam without special control of the pressure. In a state where the flat plate 7 made of the polyetherimide resin foam material is somewhat along the mold surface 6 of the mold jig 5 for curved surface molding, the temperature of 170 ° C. to 210 ° C. shown in FIG.
By taking several minutes on the high temperature side and several hours on the low temperature side, permanent deformation along the mold surface 6 is given to the flat plate 7 of the polyetherimide foam material which is a thermoplastic material as shown in FIG. The core 1 can be formed into a three-dimensional curved plate core.
The temperature measurement in this molding process is performed by a plurality of thermocouples 12 installed on the front and back of the flat plate 7 made of a polyetherimide resin foam material as shown in FIG.

【0013】上記の曲面板のコア1の成形加工におい
て、温度範囲を170℃〜210℃とした理由は、ポリ
エーテルイミド樹脂が高温曲げでの荷重たわみ温度が1
74℃、ガラス転移温度が217℃であり、それら近傍
の温度範囲にて成形する必要性から、実際のコア1の曲
面成形における成形温度と成形結果から決定したもので
ある。即ち、真空吸引下において、170℃未満の成形
温度では、図5のaに示すようにスプリングバッグが起
こり、コア1に所定の曲面形状を与えることができなか
った。また、210℃を超える成形温度では、図5のb
に示すようにコア1が応力に耐えきれず塑性変形が起き
てしまい、表面に凹凸が生じたりして非常に荒れ、減厚
した成形体しか得られなかった。然るに、170℃〜2
10℃の成形温度では、図5のcに示すようにコア1が
所定の曲面形状に、且つ所定の板厚に成形できた。
The reason why the temperature range is set to 170 ° C. to 210 ° C. in the above-mentioned forming process of the core 1 of the curved plate is that the polyetherimide resin has a deflection temperature under load of 1 at high temperature bending.
It is 74 ° C., the glass transition temperature is 217 ° C., and it is determined from the molding temperature and the molding result in the actual curved surface molding of the core 1 from the necessity of molding in a temperature range near them. That is, at a molding temperature of less than 170 ° C. under vacuum suction, a spring bag occurred as shown in FIG. 5A, and the core 1 could not be given a predetermined curved shape. Further, at a molding temperature exceeding 210 ° C., b in FIG.
As shown in (1), the core 1 could not withstand the stress and plastic deformation occurred, and the surface became uneven, resulting in a very rough molded article. However, 170 ℃ ~ 2
At a molding temperature of 10 ° C., as shown in FIG.

【0014】尚、上記の曲面板のコア1の成形加工にお
いて、熱源はオーブンの他に、ヒートブランケット、型
治具設置ヒーター、ヒートガン(熱可塑性であるため部
分的に変形成形することができるため)を選択すること
ができる。また、圧力を真空ポンプで与えることから、
工場内のみでなく任意の場所でコア1の成形作業を行う
ことができる。
In the above-mentioned forming process of the core 1 of the curved plate, the heat source is not only an oven but also a heat blanket, a mold jig installation heater, and a heat gun (because it is thermoplastic, it can be partially deformed and formed. ) Can be selected. Also, since pressure is given by a vacuum pump,
The molding operation of the core 1 can be performed not only in the factory but also in any place.

【0015】曲面板のコア1の加工方法の他の1つは、
機械加工である。この機械加工は、図6のaに示すポリ
エーテルイミド樹脂発泡材のブロック13の上面を機械
加工して、図6のbに示すように三次元の曲面14を形
成し、次にこの曲面14に沿って所要厚となるようにポ
リエーテルイミド樹脂発泡材のブロック13の下面を機
械加工して、図6のcに示すように三次元の曲面15を
形成して、三次元の曲面板のコア1を得るものである。
Another method of processing the core 1 of the curved plate is as follows.
Machine processing. In this machining, the upper surface of the polyetherimide resin foam block 13 shown in FIG. 6A is machined to form a three-dimensional curved surface 14 as shown in FIG. The lower surface of the block 13 of the polyetherimide resin foam material is machined so as to have a required thickness along with a three-dimensional curved surface 15 as shown in FIG. The core 1 is obtained.

【0016】次に本発明の曲面サンドイッチ構造体の製
造方法の他の1つについて説明する。これまで説明して
きた本発明の曲面サンドイッチ構造体の製造方法は、比
較的大きな曲率を持つ曲面サンドイッチ構造体の製造に
適するものである。ところで、航空機の翼端等の小さな
曲率を持つ曲面サンドイッチ構造体は、コアが袋形形状
のため現状では成形不可能であることから、幾つかの分
割コアにして成形後、接着処理して組み立てによる一体
のコア部品とすることが行われるが、非常に手間と費用
がかかる。さらに、この小さな曲率のコア部品にFRP
製面板を接着するのも非常に難しく、結局小さな曲率を
持つ曲面サンドイッチ構造体の製造は困難なものとなっ
ている。そこで本発明は、ポリエーテルイミド樹脂発泡
材の優れた機械加工性に着目して、コアの曲面を機械加
工により形成すると共にその曲面に面板を接着して曲面
サンドイッチ構造体を作る方法を見い出した。即ち、本
発明の曲面サンドイッチ構造体の製造方法の他の1つ
は、先ず図7のaに示すようにポリエーテルイミド樹脂
発泡材のブロック16の一側を機械加工して、図7のb
に示すように曲率の小さな三次元の曲面17を形成し、
次にこの曲面17に、図7のcに示すように同じ曲面形
状に成形したFRP製面板18を接着するか、又は未硬
化繊維強化樹脂プリプレグ面板を配し加熱硬化成形して
接合し、次いで前記ポリエーテルイミド樹脂発泡材のブ
ロック16の他側を、前記三次元の曲面17に沿って所
要厚となるように機械加工して、図7のdに示すように
三次元の曲面19を形成しコア20と成し、然る後所要
厚となったコア20の内側の三次元の曲面19に、図7
のeに示すように同じ曲面形状に成形したFRP製面板
21を接着するか、又は未硬化繊維強化樹脂プリプレグ
面板を配し加熱硬化成形して接合し、曲面サンドイッチ
構造体22を得るものである。
Next, another method for manufacturing a curved sandwich structure of the present invention will be described. The method for manufacturing a curved sandwich structure according to the present invention described above is suitable for manufacturing a curved sandwich structure having a relatively large curvature. By the way, a curved sandwich structure with a small curvature, such as an aircraft wing tip, cannot be molded at present because the core is a bag-like shape. However, it is very troublesome and expensive. In addition, the FRP
It is also very difficult to bond the face plate, which makes it difficult to produce a curved sandwich structure having a small curvature. Therefore, the present invention has focused on the excellent machinability of the polyetherimide resin foam material, and has found a method of forming a curved surface of a core by machining and bonding a face plate to the curved surface to form a curved sandwich structure. . That is, another method of manufacturing a curved sandwich structure of the present invention is to first machine one side of a block 16 of a polyetherimide resin foam material as shown in FIG.
A three-dimensional curved surface 17 having a small curvature is formed as shown in FIG.
Next, an FRP face plate 18 molded into the same curved shape as shown in FIG. 7C is adhered to the curved surface 17 or an uncured fiber reinforced resin prepreg face plate is arranged, heat-cured and joined, and then The other side of the block 16 of the polyetherimide resin foam material is machined to a required thickness along the three-dimensional curved surface 17 to form a three-dimensional curved surface 19 as shown in FIG. 7 is formed on the three-dimensional curved surface 19 inside the core 20 which has been formed into a core 20 and then has a required thickness.
As shown in (e), the FRP face plate 21 formed into the same curved shape is adhered, or an uncured fiber reinforced resin prepreg face plate is arranged, heat-cured and joined to obtain a curved sandwich structure 22. .

【0017】上記のように本発明の曲面サンドイッチ構
造体の製造方法の他の1つは、ポリエーテルイミド樹脂
発泡材のブロック16の一側に、機械加工により曲率の
小さな曲面17を形成するので、ポリエーテルイミド樹
脂発泡材は機械加工による変形は無く、エキセス部分に
パイロットホールをあけて基準を作ることができる。ま
た、曲率の小さな曲面17に、同じ曲面形状に成形した
FRP製面板18を接着する際、又は未硬化繊維強化樹
脂プリプレグ面板を配し加熱硬化成形して接合する際、
曲面17が固い表面であるため、治具代りとなって面板
18は安定して精度よくポリエーテルイミド樹脂発泡材
と一体化できる。さらに一側の曲面17に面板18を接
着した状態で、ポリエーテルイミド樹脂発泡材のブロッ
ク16の他側を前記曲面17に沿って所要厚となるよう
に機械加工して曲面19を形成するので、ずれや歪が無
く、厚さの均一な精度の高いコア20を形成できる。そ
して、この精度の高いコア20の他側の曲面19に、同
じ曲面形状に成形したFRP製面板21を接着するか、
又は未硬化繊維強化樹脂プリプレグ面板を配し加熱硬化
成形して接合するので、面板21は安定して精度よくコ
ア20と一体化できる。かくして、従来の製造方法では
実現不可能であった小さな曲率を持つ曲面サンドイッチ
構造体22は勿論のこと、複雑な形状を持つサンドイッ
チ構造体も容易に精度よく製造できるようになる。
As described above, another method of manufacturing a curved sandwich structure according to the present invention is to form a curved surface 17 having a small curvature on one side of a block 16 of a polyetherimide resin foam material by machining. The polyetherimide resin foam is not deformed by machining, and a reference hole can be formed by opening a pilot hole in an excess portion. Also, when bonding the FRP face plate 18 molded into the same curved shape to the curved surface 17 having a small curvature, or when arranging an uncured fiber reinforced resin prepreg face plate and joining by heating and curing,
Since the curved surface 17 is a hard surface, the face plate 18 can be stably and accurately integrated with the polyetherimide resin foam material instead of a jig. Further, with the face plate 18 adhered to one curved surface 17, the other side of the block 16 of the polyetherimide resin foam is machined so as to have a required thickness along the curved surface 17 to form the curved surface 19. The core 20 having a uniform thickness and high precision can be formed without displacement or distortion. Then, an FRP face plate 21 formed into the same curved shape is bonded to the curved surface 19 on the other side of the core 20 with high accuracy,
Alternatively, since an uncured fiber reinforced resin prepreg face plate is provided, heat-cured molding and joining are performed, the face plate 21 can be integrated with the core 20 stably and accurately. Thus, not only the sandwich structure 22 having a small curvature, which cannot be realized by the conventional manufacturing method, but also the sandwich structure having a complicated shape can be easily and accurately manufactured.

【0018】[0018]

【発明の効果】以上の説明で判るように本発明の曲面サ
ンドイッチ構造体の製造方法の1つによれば、ポリエー
テルイミド樹脂発泡材のコアを、加熱・真空圧による成
形加工或いは機械加工により曲面板にするので、精度の
高いコアの製作が容易で、特別な温度・圧力制御装置は
必要とせず、専用設備は不要である。従って、この曲面
板のコアに、同じ曲面に成形したFRP製面板を接着又
は未硬化繊維強化樹脂プリプレグ面板を配して加熱硬化
成形により接合して得る曲面サンドイッチ構造体は均一
な厚さで、精度の高い曲面形状となる。
As can be seen from the above description, according to one of the methods for manufacturing a curved sandwich structure of the present invention, a core of a polyetherimide resin foam material is formed by heating or vacuum pressure forming or machining. Since it is a curved plate, it is easy to manufacture a highly accurate core, no special temperature / pressure control device is required, and no special equipment is required. Therefore, the curved sandwich structure obtained by bonding the uncured fiber reinforced resin prepreg face plate to the core of the curved plate, bonding the uncured fiber reinforced resin prepreg face plate to the core of the same curved surface, and bonding by heat-curing molding has a uniform thickness, A highly accurate curved surface shape is obtained.

【0019】また、本発明の曲面サンドイッチ構造体の
製造方法の他の1つによれば、ポリエーテルイミド樹脂
発泡材のブロックを機械加工して曲率の小さな曲面を外
側及び内側に順次形成していくので、機械加工による変
形がなく、しかもその曲率の小さな曲面を形成後直ちに
同じ曲面に成形したFRP製面板を接着する際又は未硬
化繊維強化樹脂プリプレグを配して加熱硬化成形により
接合する際、コアとなるポリエーテルイミド樹脂発泡材
の曲面が固い表面であるため、治具代りとなって、面板
は安定して精度よくコアと一体化できる。従って、従来
の製造方法では実現不可能であった小さな曲率を持つ曲
面サンドイッチ構造体は勿論のこと、複雑な形状を持つ
サンドイッチ構造体も容易に精度よく製造できる。
According to another method of manufacturing a curved sandwich structure of the present invention, a block of a polyetherimide resin foam is machined to sequentially form curved surfaces having small curvatures on the outside and inside. Since there is no deformation due to mechanical processing, and when bonding a FRP face plate molded to the same curved surface immediately after forming a curved surface with a small curvature, or when disposing an uncured fiber reinforced resin prepreg and joining by heat curing molding Since the curved surface of the polyetherimide resin foam material serving as the core is a hard surface, the face plate can be stably and accurately integrated with the core instead of a jig. Therefore, not only a sandwich structure having a small curvature which cannot be realized by a conventional manufacturing method but also a sandwich structure having a complicated shape can be easily and accurately manufactured.

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

【図1】a,b,cは本発明の曲面サンドイッチ構造体
の製造方法の1つを示す工程図である。
FIGS. 1a, 1b and 1c are process diagrams showing one method of manufacturing a curved sandwich structure of the present invention.

【図2】図1の曲面サンドイッチ構造体の製造方法にお
いて、ポリエーテルイミド樹脂発泡材を曲面板のコアに
加工する方法の1つである成形加工方法を示す図であ
る。
FIG. 2 is a view showing a molding method which is one of methods for processing a polyetherimide resin foam material into a core of a curved plate in the method of manufacturing the curved sandwich structure of FIG.

【図3】ポリエーテルイミド樹脂発泡材を曲面板のコア
に成形する条件を示す図である。
FIG. 3 is a diagram showing conditions for molding a polyetherimide resin foam material into a core of a curved plate.

【図4】図2の成形加工方法と図3の成形条件により曲
面板のコアを成形した状態を示す図である。
4 is a view showing a state in which a core of a curved plate is formed by the forming method of FIG. 2 and the forming conditions of FIG. 3;

【図5】図3の成形条件の内の温度範囲を170℃〜2
10℃と限定した理由の説明図で、aは170℃未満で
の成形状態、bは210℃を超えた場合の成形状態、c
は170℃〜210℃での適正な成形状態を示す。
FIG. 5 shows a temperature range of 170 ° C. to 2 in the molding conditions of FIG.
Explanatory drawing of the reason why the temperature is limited to 10 ° C., a is a molded state at less than 170 ° C., b is a molded state at a temperature exceeding 210 ° C., c
Indicates an appropriate molding state at 170 ° C to 210 ° C.

【図6】a,b,cは図1の曲面サンドイッチ構造体の
製造方法において、ポリエーテルイミド樹脂発泡材を曲
面板のコアに加工する方法の他の1つである機械加工方
法の工程を示す図である。
FIGS. 6A, 6B and 6C show steps of a machining method which is another method of processing a polyetherimide resin foam material into a core of a curved plate in the method of manufacturing the curved sandwich structure of FIG. FIG.

【図7】a〜eは本発明の曲面サンドイッチ構造体の製
造方法の他の1つを示す工程図である。
7A to 7E are process diagrams showing another method of manufacturing a curved sandwich structure of the present invention.

【図8】従来のハニカムコアサンドイッチ構造体の概要
を示す図である。
FIG. 8 is a diagram showing an outline of a conventional honeycomb core sandwich structure.

【図9】図12のA部拡大断面図である。FIG. 9 is an enlarged sectional view of a portion A in FIG.

【図10】ポリエーテルイミド発泡材とポリメタクリル
イミド発泡材の吸湿特性を示す図である。
FIG. 10 is a diagram showing the moisture absorption characteristics of a polyetherimide foam and a polymethacrylimide foam.

【図11】ポリエーテルイミド発泡材をコアとしたサン
ドイッチ構造体の製造工程を示すフロー図である。
FIG. 11 is a flowchart showing a manufacturing process of a sandwich structure having a polyetherimide foam as a core.

【符号の説明】[Explanation of symbols]

1,20 コア 2,2′,18,21 FRP製面板 3,3′ 未硬化繊維強化樹脂プリプレグ面板 4,22 曲面サンドイッチ構造体 5 曲面成形用型治具 6 型面 7 ポリエーテルイミド樹脂発泡材の平板 8 樹脂フィルム 9 曲面成形用型治具の基板 10 シール材 11 口金 12 熱電対 13,16 ポリエーテルイミド樹脂発泡材のブロック 14,15,17,19 三次元の曲面 1,20 core 2,2 ', 18,21 FRP face plate 3,3' uncured fiber reinforced resin prepreg face plate 4,22 Curved sandwich structure 5 Curved mold die 6 Mold surface 7 Polyetherimide resin foam 8 Plate of resin 8 Resin film 9 Substrate of mold jig for curved surface forming 10 Sealing material 11 Cap 12 Thermocouple 13,16 Block of polyetherimide resin foam material 14,15,17,19 Three-dimensional curved surface

───────────────────────────────────────────────────── フロントページの続き (51)Int.Cl.7 識別記号 FI テーマコート゛(参考) // B29K 79:00 B29K 79:00 (72)発明者 清水 さやか 岐阜県各務原市川崎町1番地 川崎重工業 株式会社岐阜工場内 Fターム(参考) 4F100 AK49A AK49K BA03 BA06 BA10B BA10C BA13 CB00 DH01B DH01C DH02B DH02C DJ01A EC052 EC182 EJ082 EJ281 EJ422 GB31 JL02 4F201 AA32 AA40 AD05 AD16 AD17 AD20 AG03 AG20 BA03 BC12 BD07 BM04 BM13 4F211 AA32 AA40 AD05 AD16 AD17 AD20 AG03 AG20 TA03 TA13 TC06 TD11 TH02 TH18 TN44 4F213 AA32 AA40 AD05 AD16 AD17 AD20 AG03 AG20 WA08 WA09 WA15 WA43 WA52 WA53 WA72 WA74 WA87 WB01 ──────────────────────────────────────────────────の Continued on the front page (51) Int.Cl. 7 Identification FI FI Theme Court ゛ (Reference) // B29K 79:00 B29K 79:00 (72) Inventor Sayaka Shimizu 1 Kawasaki-cho, Kakamigahara-shi, Gifu Prefecture Kawasaki Heavy Industries F-term in Gifu Plant Co., Ltd. (Reference) 4F100 AK49A AK49K BA03 BA06 BA10B BA10C BA13 CB00 DH01B DH01C DH02B DH02C DJ01A EC052 EC182 EJ082 EJ281 EJ422 GB31 JL02 4F201 AA32 AA40 AD05 AD16 AD17 AD20 AMB0320 AD17 AD20 AG03 AG20 TA03 TA13 TC06 TD11 TH02 TH18 TN44 4F213 AA32 AA40 AD05 AD16 AD17 AD20 AG03 AG20 WA08 WA09 WA15 WA43 WA52 WA53 WA72 WA74 WA87 WB01

Claims (4)

【特許請求の範囲】[Claims] 【請求項1】 ポリエーテルイミド樹脂発泡材を曲面板
に加工してコアとなし、このコアの両面に同じ曲面に成
形したFRP製面板を接着するか、又は未硬化繊維強化
樹脂プリプレグ面板を配し加熱硬化成形して接合するこ
とを特徴とする曲面サンドイッチ構造体の製造方法。
1. A polyetherimide resin foam material is processed into a curved surface plate to form a core, and an FRP surface plate formed into the same curved surface is adhered to both surfaces of the core, or an uncured fiber reinforced resin prepreg face plate is provided. A method for producing a curved sandwich structure, comprising: heat-curing molding; and joining.
【請求項2】 請求項1記載の曲面サンドイッチ構造体
の製造方法において、コアの曲面状の加工が、所要厚の
ポリエーテルイミド樹脂発泡材の平板を、170℃〜2
10℃の温度範囲で真空吸引による圧力にて三次元の曲
面に成形加工するものであることを特徴とする曲面サン
ドイッチ構造体の製造方法。
2. The method for manufacturing a curved sandwich structure according to claim 1, wherein the processing of the curved surface of the core comprises the step of forming a flat plate of a polyetherimide resin foam material having a required thickness from 170 ° C. to 2 ° C.
A method for producing a curved sandwich structure, wherein a three-dimensional curved surface is formed by a pressure of vacuum suction in a temperature range of 10 ° C.
【請求項3】 請求項1記載の曲面サンドイッチ構造体
の製造方法において、コアの曲面状の加工が、ポリエー
テルイミド樹脂発泡材のブロックを、所要厚の三次元の
曲面板に機械加工するものであることを特徴とする曲面
サンドイッチ構造体の製造方法。
3. The method for manufacturing a curved sandwich structure according to claim 1, wherein the curved surface of the core is formed by machining a block of a polyetherimide resin foam into a three-dimensional curved plate having a required thickness. A method for producing a curved sandwich structure.
【請求項4】 ポリエーテルイミド樹脂発泡材のブロッ
クの一側を機械加工して、三次元の曲面を形成し、次に
この曲面に、同じ曲面形状に成形したFRP製面板を接
着するか、又は未硬化繊維強化樹脂プリプレグ面板を配
し加熱硬化成形して接合し、次いで前記ポリエーテルイ
ミド樹脂発泡材のブロックの他側に、前記三次元の曲面
に沿って所要厚となるように機械加工して三次元の曲面
を形成しコアとなし、然る後所要厚となったポリエーテ
ルイミド樹脂発泡材のコアの内側の三次元の曲面に、同
じ曲面形状に成形したFRP製面板を接着するか、又は
未硬化繊維強化樹脂プリプレグ面板を配し加熱硬化成形
して接合することを特徴とする曲面サンドイッチ構造体
の製造方法。
4. One side of the block of the polyetherimide resin foam is machined to form a three-dimensional curved surface, and then an FRP face plate molded into the same curved shape is bonded to the curved surface, or Alternatively, an uncured fiber reinforced resin prepreg face plate is arranged, heat-cured and bonded, and then machined on the other side of the polyetherimide resin foam material so as to have a required thickness along the three-dimensional curved surface. A three-dimensional curved surface is formed to form a core, and an FRP face plate molded into the same curved shape is bonded to the three-dimensional curved surface inside the polyetherimide resin foam material core having a required thickness. Or a method of manufacturing a curved sandwich structure, comprising arranging an uncured fiber reinforced resin prepreg face plate, heat-curing molding, and joining.
JP2001097137A 2001-03-29 2001-03-29 Method of manufacturing curved sandwich structure Expired - Lifetime JP3482525B2 (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2015123694A (en) * 2013-12-26 2015-07-06 川崎重工業株式会社 Laminated structure and method for producing the same

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2015123694A (en) * 2013-12-26 2015-07-06 川崎重工業株式会社 Laminated structure and method for producing the same

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