JPH07180281A - Honeycomb sandwich panel and manufacture thereof - Google Patents
Honeycomb sandwich panel and manufacture thereofInfo
- Publication number
- JPH07180281A JPH07180281A JP32878893A JP32878893A JPH07180281A JP H07180281 A JPH07180281 A JP H07180281A JP 32878893 A JP32878893 A JP 32878893A JP 32878893 A JP32878893 A JP 32878893A JP H07180281 A JPH07180281 A JP H07180281A
- Authority
- JP
- Japan
- Prior art keywords
- sandwich panel
- reinforced resin
- honeycomb
- fiber
- fiber reinforced
- 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.)
- Pending
Links
Abstract
Description
【０００１】[0001]
【産業上の利用分野】この発明は、ハニカムサンドイッ
チパネル及びその製造方法に係わり、更に詳しくは一方
向に剛性を強化し、軽量化したハニカムサンドイッチパ
ネル及びその製造方法に関するものである。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a honeycomb sandwich panel and a method for manufacturing the same, and more particularly to a honeycomb sandwich panel which is unidirectionally reinforced to reduce weight and a method for manufacturing the same.
【０００２】[0002]
【従来の技術】従来、電車用床板，航空機用床板，カー
テンウォール等には、一定の剛性を維持し、かつ軽量化
を図るためにアルミハニカムサンドイッチパネルが使用
されている。これらのハニカムサンドイッチパネルは、
一般的には曲げ剛性が設計の標定になっており、特に床
板の場合は、曲げ剛性と、ハイヒール強度（局部荷重）
が標定になっている。2. Description of the Related Art Conventionally, aluminum honeycomb sandwich panels have been used for floorboards for trains, floorboards for aircraft, curtain walls, etc. in order to maintain a certain rigidity and reduce the weight. These honeycomb sandwich panels
Generally, the bending rigidity is the standard of the design. Especially in the case of floor boards, the bending rigidity and high heel strength (local load)
Is the orientation.
【０００３】従って、表面板に使用されているアルミ板
の引張弾性率が7,100Kgf/mm 2 程度と小さいので、パネ
ルに荷重が加わった時に撓み易いため、表面板の板厚を
厚くしたり、または芯材（コア）の厚さを厚くしたりし
てサンドイッチパネルを構成している。Therefore, since the tensile elastic modulus of the aluminum plate used for the surface plate is as small as about 7,100 Kgf / mm 2 , since the panel easily bends when a load is applied to the panel, the thickness of the surface plate is increased, Alternatively, the sandwich panel is configured by increasing the thickness of the core material (core).
【０００４】[0004]
【発明が解決しようとする問題点】然しながら、表面板
の板厚を厚くするとサンドイッチパネルの重量が増加し
て全体の重量が大きくなると言う問題があり、また表面
板の板厚を薄目にして芯材の厚さを厚くした場合、軽量
化を図ることは出来るが、ハイヒール強度が弱いと言う
問題があった。この発明は、かかる従来の課題に着目し
て案出されたもので、サンドイッチパネルをスパン方向
に一方向に繊維を配列した繊維強化樹脂層で補強するこ
とにより、サンドイッチパネルの剛性を増大させること
が出来ると共に、板厚を薄いものにして軽量化を図るこ
とが出来るハニカムサンドイッチパネル及びその製造方
法を提供することを目的とするものである。However, when the thickness of the surface plate is increased, the weight of the sandwich panel is increased and the overall weight is increased, and the thickness of the surface plate is reduced to make the core thin. If the material is made thicker, the weight can be reduced, but there is a problem that the high heel strength is weak. The present invention was devised in view of such conventional problems, and increases the rigidity of a sandwich panel by reinforcing the sandwich panel with a fiber-reinforced resin layer in which fibers are arranged in one direction in the span direction. It is an object of the present invention to provide a honeycomb sandwich panel and a method for manufacturing the same, which is capable of achieving the above-mentioned effects and can be made lighter by reducing the plate thickness.
【０００５】[0005]
【課題を解決するための手段】この発明は上記目的を達
成するため、ハニカムコアと表面板との間に一方向に繊
維を配列した繊維強化樹脂層を一体的に形成したことを
要旨とするものである。また、前記表面板は、アルミニ
ウム板であり、繊維強化樹脂層の繊維がカーボン繊維で
あり、樹脂がエポキシ樹脂等の熱硬化性樹脂により構成
する。SUMMARY OF THE INVENTION In order to achieve the above object, the gist of the present invention is to integrally form a fiber-reinforced resin layer in which fibers are arranged in one direction between a honeycomb core and a surface plate. It is a thing. The surface plate is an aluminum plate, the fibers of the fiber-reinforced resin layer are carbon fibers, and the resin is a thermosetting resin such as an epoxy resin.
【０００６】[0006]
【発明の作用】この発明は上記のように構成され、ハニ
カムコアの両面に一方向に繊維を配列したプリプレグ材
等の繊維強化樹脂層を介して表面板を積層させ、この積
層体を加圧下で加熱してハニカムコアと繊維強化樹脂層
と表面板とを一体的に成形することで、繊維強化樹脂層
により曲げ剛性が増加した分ハニカムサンドイッチパネ
ルの板厚を薄くすることができ、また軽量化も図ること
が出来るものである。The present invention is constructed as described above, and a face plate is laminated on both sides of a honeycomb core through a fiber reinforced resin layer such as a prepreg material in which fibers are arranged in one direction, and the laminated body is pressed. The honeycomb core, the fiber-reinforced resin layer, and the surface plate are integrally molded by heating with the, and the plate thickness of the honeycomb sandwich panel can be reduced by the amount that the bending rigidity is increased by the fiber-reinforced resin layer, and the weight is also light. It can also be realized.
【０００７】[0007]
【発明の実施例】以下、添付図面に基づき、この発明の
実施例を説明する。図１は、この発明を実施したハニカ
ムサンドイッチパネル１の一部拡大断面図、図２は支柱
２に設置されたハニカムサンドイッチパネル１の平面
図、図３は図２のＡーＡ矢視側面図を示し、前記ハニカ
ムサンドイッチパネル１は、アルミニウムのハニカムコ
ア３の両面に、予め一方向、即ち、図３に示すスパン方
向（図３の左右方向）に繊維６を配列したプリプレグ材
等の加熱硬化前の繊維強化樹脂シートを貼合わせた表面
板５ａ，５ｂを、前記ハニカムコア３側に加熱硬化前の
繊維強化樹脂シートが位置するように配設して、ホット
プレス法，オートクレーブまたはバキュームによる真空
バッグ法により、加圧下で加熱して一体的に成形するこ
とで、ハニカムコア３と表面板５ａ，５ｂとの間に一方
向に繊維を配列した繊維強化樹脂層４を一体的に形成し
たものである。Embodiments of the present invention will be described below with reference to the accompanying drawings. 1 is a partially enlarged cross-sectional view of a honeycomb sandwich panel 1 embodying the present invention, FIG. 2 is a plan view of the honeycomb sandwich panel 1 installed on a column 2, and FIG. 3 is a side view taken along the line AA of FIG. The honeycomb sandwich panel 1 is formed by heat-curing a prepreg material or the like in which fibers 6 are arranged in advance in one direction, that is, in the span direction shown in FIG. 3 (left-right direction in FIG. 3) on both surfaces of an aluminum honeycomb core 3. Surface plates 5a, 5b to which the previous fiber-reinforced resin sheet is attached are arranged so that the fiber-reinforced resin sheet before heat curing is located on the honeycomb core 3 side, and vacuum is applied by a hot press method, autoclave or vacuum. By the bag method, the fiber-reinforced resin layer 4 in which the fibers are arranged in one direction is formed between the honeycomb core 3 and the surface plates 5a and 5b by heating under pressure and integrally molding. It is obtained by the body formed.
【０００８】なお、前記繊維強化樹脂層４の繊維６はカ
ーボン繊維であり、また樹脂はエポキシ樹脂またはポリ
エステル樹脂等の熱硬化性樹脂を使用するものであり、
ハニカムコアとしては、アルミハニカムコア等の金属製
またはペーパーハニカム等の非金属製，或いはウレタン
発泡材等の樹脂系発泡材等の芯材である。次に、上記の
ような一方向に剛性を強化したハニカムサンドイッチパ
ネル１の製造方法を具体的に説明する。The fibers 6 of the fiber-reinforced resin layer 4 are carbon fibers, and the resin is thermosetting resin such as epoxy resin or polyester resin.
The honeycomb core is a core made of metal such as aluminum honeycomb core or non-metal such as paper honeycomb, or resin foam such as urethane foam. Next, a method for manufacturing the honeycomb sandwich panel 1 whose rigidity is strengthened in one direction as described above will be specifically described.
【０００９】まず、アルミ板等から成る表面板５ａ，５
ｂの接着前処理工程として、表面板５ａ，５ｂを酸エッ
チング法，リン酸アノダイズ法等で、一般的なアルミ板
の接着前処理を行う。次に、表面板５ａ，５ｂの長さ，
幅寸法に合わせて、プリプレグ材から成る加熱硬化前の
繊維強化樹脂シート（この実施例では、高弾性型一方向
カーボン繊維入りのエポキシ樹脂プリプレグ，以下、ハ
イモジュラス型一方向性プリプレグと言う）を裁断し、
この繊維強化樹脂シートを前記表面板５ａ，５ｂに、カ
ーボン繊維の方向が剛性を強化しようとする方向になる
ように貼り合わせる。First, the surface plates 5a, 5 made of an aluminum plate or the like.
As the bonding pretreatment step of b, the surface plates 5a and 5b are subjected to general bonding pretreatment of an aluminum plate by an acid etching method, a phosphoric acid anodizing method or the like. Next, the length of the surface plates 5a and 5b,
According to the width dimension, a fiber reinforced resin sheet made of prepreg material before heat curing (in this embodiment, an epoxy resin prepreg containing a highly elastic type unidirectional carbon fiber, hereinafter referred to as a high modulus type unidirectional prepreg) is used. Cut,
This fiber reinforced resin sheet is attached to the front plates 5a and 5b so that the direction of the carbon fibers is the direction in which the rigidity is reinforced.
【００１０】なお、繊維強化樹脂シートとして、上記の
ようにカーボン繊維を使用する場合には、アルミ表面板
と直接接触すると電食が発生し易いため、カーボンハイ
モジュラス型一方向性プリプレグとアルミ表面板との間
に、薄いガラス布プリプレグのように非電導性の材料を
貼り合わせる。次に、ハニカムコア３と維強化樹脂シー
トを貼り合わせた表面板５ａ，５ｂとの接着組付け作業
を説明すると、まず、接着組立治具を準備し、その上に
繊維強化樹脂シートを貼付けた表面板５ａ，ハニカムコ
ア３，表面板５ｂを順次重ね合わせて置く。この時、繊
維強化樹脂シートがハニカムコア３に接するように置
き、ハニカムコア３を挟んだ状態で組付ける。When carbon fiber is used as the fiber reinforced resin sheet as described above, electrolytic corrosion is likely to occur when it comes into direct contact with the aluminum surface plate. Therefore, carbon high modulus type unidirectional prepreg and aluminum surface plate are used. A non-conducting material such as a thin glass cloth prepreg is attached to the face plate. Next, the operation of bonding and attaching the honeycomb core 3 and the surface plates 5a and 5b to which the fiber-reinforced resin sheet is bonded will be described. First, a bonding and assembling jig is prepared, and the fiber-reinforced resin sheet is bonded thereon. The surface plate 5a, the honeycomb core 3, and the surface plate 5b are sequentially stacked and placed. At this time, the fiber-reinforced resin sheet is placed so as to be in contact with the honeycomb core 3, and the honeycomb core 3 is sandwiched and assembled.
【００１１】そして、このように組付けた積層体をホッ
トプレス法，オートクレーブまたはバキュームによる真
空バッグ法等の加熱硬化装置（図示せず）により、加圧
下で加熱して、前記繊維強化樹脂シートの樹脂を溶解
し、ハニカムコア３と表面板５ａ，５ｂとに接着させて
一体硬化させることで、一体的に接着させるものであ
る。その後、加熱硬化装置から一体接着したハニカムサ
ンドイッチパネル１を取り出して、清掃仕上げして完成
させるものである。 〔比較例１〕次に、図４に示すように、厚さ18.7mmのハ
ニカムコア３の両面に、一方向に繊維を配列したプリプ
レグ材等の厚さ0.2 mmの繊維強化樹脂層４を介して厚さ
0.6mmの表面板５ａ，５ｂを積層させて一体的に成形し
たパネル全厚が20.3mmのこの発明にかかるハニカムサン
ドイッチパネル１と、図５に示すように、厚さ25.4mmの
ハニカムコア１３の両面に、接着剤１４を介して厚さ0.
8 mmのアルミ板から成る表面板15a,15b を一体的に接着
して成形したパネル全厚が27.0mmの従来のハニカムサン
ドイッチパネル１０とのパネル厚さ，パネル重量を比較
すると、以下の表ー１のようになる。Then, the laminated body thus assembled is heated under pressure by a heat curing device (not shown) such as a hot press method, an autoclave or a vacuum bag method using a vacuum, to heat the fiber-reinforced resin sheet. The resin is melted and adhered to the honeycomb core 3 and the surface plates 5a and 5b and integrally cured, thereby integrally adhering. After that, the integrally bonded honeycomb sandwich panel 1 is taken out from the heating and curing device, and is cleaned and finished to complete. Comparative Example 1 Next, as shown in FIG. 4, a fiber-reinforced resin layer 4 having a thickness of 0.2 mm, such as a prepreg material in which fibers are arranged in one direction, is provided on both surfaces of a honeycomb core 3 having a thickness of 18.7 mm. Thickness
A honeycomb sandwich panel 1 according to the present invention having a total thickness of 20.3 mm, which is integrally formed by laminating surface plates 5a and 5b having a thickness of 0.6 mm, and a honeycomb core 13 having a thickness of 25.4 mm, as shown in FIG. Both sides have a thickness of 0.
The following table compares the panel thickness and panel weight with the conventional honeycomb sandwich panel 10 with the total thickness of 27.0 mm, which is formed by integrally bonding the surface plates 15a and 15b made of 8 mm aluminum plate. It becomes like 1.
【００１２】なお、この場合に両パネルの曲げ剛性を同
等にすると仮定する。 〔比較例２〕この発明にかかるハイモジュラス型一方向
性プリプレグパネルと、従来のアルミハニカムサンドイ
ッチパネルの厚さを同じにした場合、ハイモジュラス型
一方向性プリプレグパネルの方が曲げ剛性が大きいの
で、支柱２の間隔（スパン）を大きく出来る。このた
め、パネル自身の軽量化に加えて、支柱２の施工本数も
減らすことが出来るので更に軽量化が可能である。即
ち、電車の車内に床板（床面積３ｍ×２５ｍ）を施工す
る場合、図５に示すような従来のアルミサンドイッチパ
ネルを施工すると、支柱２のスパンは５００mmピッチで
あった。In this case, it is assumed that both panels have the same bending rigidity. Comparative Example 2 When the high modulus type unidirectional prepreg panel according to the present invention and the conventional aluminum honeycomb sandwich panel have the same thickness, the high modulus type unidirectional prepreg panel has a higher bending rigidity. The interval (span) between the columns 2 can be increased. Therefore, in addition to reducing the weight of the panel itself, it is possible to reduce the number of struts 2 to be constructed, and thus it is possible to further reduce the weight. That is, when a floor board (floor area: 3 m × 25 m) is installed in the train, a conventional aluminum sandwich panel as shown in FIG. 5 is installed, and the span of the columns 2 is 500 mm pitch.
【００１３】この代わりに、図４に示すハイモジュラス
型一方向性プリプレグパネルで、ハニカムコアの厚さ２
５．０mm，プリプレグ材の厚さ0.2 mm，表面板５ａ，５
ｂの厚さ0.6 mm，パネル全厚が27.0mm施工すると、バネ
ルの曲げ剛性は、従来のパネルが1.95×106 Kg／mmに対
して、この実施例のパネルの曲げ剛性は、3.52×106Kg
／mmと大きいため、同じ撓み量にするには、支柱２のス
パンは580 mmで十分である。従って、パネルそのものの
軽量化と支柱の減少により、従来の床構造に比較して、
約１６％の軽量化が可能である。この軽量化の内容を以
下の表ー２に示す。Alternatively, the high modulus type unidirectional prepreg panel shown in FIG.
5.0 mm, prepreg material thickness 0.2 mm, surface plates 5a, 5
When the thickness of b is 0.6 mm and the total thickness of the panel is 27.0 mm, the bending rigidity of the panel is 1.95 × 10 6 Kg / mm, whereas the bending rigidity of the panel of this embodiment is 3.52 × 10 5. 6 Kg
Since it is as large as / mm, a span of 580 mm is sufficient for the strut 2 to achieve the same amount of deflection. Therefore, due to the weight reduction of the panel itself and the reduction of columns, compared to the conventional floor structure,
Weight reduction of about 16% is possible. The contents of this weight reduction are shown in Table 2 below.
【００１４】 この発明は、上記のようにハニカムコアの両面に一方向
に繊維を配列したプリプレグ材等の繊維強化樹脂層４を
介して表面板５ａ，５ｂを積層させ、この積層体を加圧
下で加熱してハニカムコアと繊維強化樹脂層４と表面板
５ａ，５ｂとを一体的に成形することで、繊維強化樹脂
層４により曲げ剛性が増加した分ハニカムサンドイッチ
パネル１の板厚を薄くすることができ、また軽量化も図
ることが出来るものである。[0014] According to the present invention, surface plates 5a and 5b are laminated via a fiber reinforced resin layer 4 such as a prepreg material in which fibers are arranged in one direction on both surfaces of a honeycomb core as described above, and the laminated body is heated under pressure. By integrally molding the honeycomb core, the fiber-reinforced resin layer 4, and the surface plates 5a and 5b, the honeycomb sandwich panel 1 can be thinned by the increase in bending rigidity due to the fiber-reinforced resin layer 4. Moreover, the weight can be reduced.
【００１５】[0015]
【発明の効果】この発明は、上記のようにハニカムコア
の両面に表面板を配設して一体的に成形して成るハニカ
ムサンドイッチパネルにおいて、前記ハニカムコアと表
面板との間に一方向に繊維を配列した繊維強化樹脂層を
一体的に形成したので、サンドイッチパネルの剛性を増
大させることが出来ると共に、板厚を薄いものにして軽
量化を図ることが出来る効果がある。As described above, according to the present invention, in a honeycomb sandwich panel formed by integrally disposing surface plates on both sides of a honeycomb core as described above, the honeycomb core and the surface plate are unidirectionally arranged. Since the fiber reinforced resin layer in which the fibers are arranged is integrally formed, it is possible to increase the rigidity of the sandwich panel and to reduce the thickness by reducing the plate thickness.
【図１】この発明を実施したハニカムサンドイッチパネ
ルの一部拡大断面図である。FIG. 1 is a partially enlarged sectional view of a honeycomb sandwich panel embodying the present invention.
【図２】支柱に設置されたハニカムサンドイッチパネル
の平面図である。FIG. 2 is a plan view of a honeycomb sandwich panel installed on columns.
【図３】図２のＡーＡ矢視側面図である。FIG. 3 is a side view taken along the line AA of FIG.
【図４】この発明にかかるハイモジュラス型一方向性プ
リプレグ補強パネルの説明図である。FIG. 4 is an explanatory view of a high modulus type unidirectional prepreg reinforcing panel according to the present invention.
【図５】従来のアルミハニカムサンドイッチパネルの説
明図である。FIG. 5 is an explanatory view of a conventional aluminum honeycomb sandwich panel.
１ ハニカムサンドイッチパネル ２ 支柱 ３ ハニカムコア ４ 繊維
強化樹脂シート ５ａ，５ｂ 表面板 ６ 繊維1 Honeycomb Sandwich Panel 2 Struts 3 Honeycomb Core 4 Fiber Reinforced Resin Sheets 5a, 5b Surface Plate 6 Fibers
Claims (4)
一体的に成形して成るハニカムサンドイッチパネルにお
いて、前記ハニカムコアと表面板との間に一方向に繊維
を配列した繊維強化樹脂層を一体的に形成したことを特
徴とするハニカムサンドイッチパネル。1. A honeycomb sandwich panel formed by integrally disposing surface plates on both sides of a honeycomb core, wherein a fiber reinforced resin layer in which fibers are arranged in one direction between the honeycomb core and the surface plate. A honeycomb sandwich panel characterized by being integrally formed.
600Kgf/mm 2 のアルミニウム板であり、繊維強化樹脂層
の繊維がカーボン繊維であり、樹脂がエポキシ樹脂等の
熱硬化性樹脂であり、炭素繊維強化プリプレグとして、
硬化後の状態で引張弾性率が18,000Kgf/mm2 以上である
請求項１に記載のハニカムサンドイッチパネル。2. The surface plate has a tensile elastic modulus of 7,000 to 7,
It is an aluminum plate of 600 Kgf / mm 2 , the fiber of the fiber reinforced resin layer is carbon fiber, the resin is a thermosetting resin such as epoxy resin, as a carbon fiber reinforced prepreg,
The honeycomb sandwich panel according to claim 1, which has a tensile elastic modulus of 18,000 Kgf / mm 2 or more after being cured.
列した繊維強化樹脂層を介して表面板を積層させ、この
積層体を加圧下で加熱してハニカムコアと繊維強化樹脂
層と表面板とを一体的に成形するハニカムサンドイッチ
パネルの製造方法。3. A surface plate is laminated on both sides of a honeycomb core via a fiber reinforced resin layer in which fibers are arranged in one direction, and the laminated body is heated under pressure to heat the honeycomb core, the fiber reinforced resin layer and the surface plate. A method for manufacturing a honeycomb sandwich panel, which comprises integrally molding and.
請求項３に記載のハニカムサンドイッチパネルの製造方
法。4. The method for manufacturing a honeycomb sandwich panel according to claim 3, wherein a prepreg material is used for the fiber reinforced resin layer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP32878893A JPH07180281A (en) | 1993-12-24 | 1993-12-24 | Honeycomb sandwich panel and manufacture thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP32878893A JPH07180281A (en) | 1993-12-24 | 1993-12-24 | Honeycomb sandwich panel and manufacture thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH07180281A true JPH07180281A (en) | 1995-07-18 |
Family
ID=18214126
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP32878893A Pending JPH07180281A (en) | 1993-12-24 | 1993-12-24 | Honeycomb sandwich panel and manufacture thereof |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH07180281A (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009542471A (en) * | 2006-06-27 | 2009-12-03 | ヘクセル コーポレイション | Corrosion resistant honeycomb |
| US8025954B2 (en) | 2006-11-30 | 2011-09-27 | Jamco Corporation | Sandwich panel |
| JP2012126133A (en) * | 2010-12-14 | 2012-07-05 | Shinyoung Co Ltd | Multiple bonding material |
| US8383231B2 (en) | 2006-11-30 | 2013-02-26 | Jamco Corporation | Sandwich panel |
| KR101247311B1 (en) * | 2010-12-20 | 2013-03-25 | 한화엘앤씨 주식회사 | Backboard assembly of three column type seat back frame |
| JP2017524582A (en) * | 2014-06-04 | 2017-08-31 | ブライト ライト ストラクチャーズ エルエルシー | Multi-element polymer resin, coating method thereof, and composite laminate structure including the same |
| CN112297535A (en) * | 2020-11-20 | 2021-02-02 | 长春珑鑫新材料有限公司 | Composite automobile cab sleeping plank and preparation method thereof |
| US10967583B2 (en) | 2015-04-03 | 2021-04-06 | Bright Lite Structures Llc | Apparatus for controllably cutting fibers and related methods |
| WO2021132321A1 (en) | 2019-12-27 | 2021-07-01 | 三井化学株式会社 | Multilayer body and method for producing same |
-
1993
- 1993-12-24 JP JP32878893A patent/JPH07180281A/en active Pending
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2009542471A (en) * | 2006-06-27 | 2009-12-03 | ヘクセル コーポレイション | Corrosion resistant honeycomb |
| US8025954B2 (en) | 2006-11-30 | 2011-09-27 | Jamco Corporation | Sandwich panel |
| US8383231B2 (en) | 2006-11-30 | 2013-02-26 | Jamco Corporation | Sandwich panel |
| JP2012126133A (en) * | 2010-12-14 | 2012-07-05 | Shinyoung Co Ltd | Multiple bonding material |
| KR101247311B1 (en) * | 2010-12-20 | 2013-03-25 | 한화엘앤씨 주식회사 | Backboard assembly of three column type seat back frame |
| US10399307B2 (en) | 2014-06-04 | 2019-09-03 | Bright Lite Structures Llc | Reinforced composite structure |
| JP2017524582A (en) * | 2014-06-04 | 2017-08-31 | ブライト ライト ストラクチャーズ エルエルシー | Multi-element polymer resin, coating method thereof, and composite laminate structure including the same |
| US10406789B2 (en) | 2014-06-04 | 2019-09-10 | Bright Lite Structures Llc | Multicomponent polymer resin, methods for applying the same, and composite laminate structure including the same |
| US10780677B2 (en) | 2014-06-04 | 2020-09-22 | Bright Lite Structures Llc | Composite structure exhibiting energy absorption and/or including a defect free surface |
| US10786977B2 (en) | 2014-06-04 | 2020-09-29 | Bright Lite Structures Llc | Composite sandwich having a high bending stiffness |
| US11241867B2 (en) | 2014-06-04 | 2022-02-08 | Bright Lite Structures Llc | Multicomponent polymer resin, methods for applying the same, and composite laminate structure including the same |
| US10967583B2 (en) | 2015-04-03 | 2021-04-06 | Bright Lite Structures Llc | Apparatus for controllably cutting fibers and related methods |
| WO2021132321A1 (en) | 2019-12-27 | 2021-07-01 | 三井化学株式会社 | Multilayer body and method for producing same |
| CN112297535A (en) * | 2020-11-20 | 2021-02-02 | 长春珑鑫新材料有限公司 | Composite automobile cab sleeping plank and preparation method thereof |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US6689246B2 (en) | Method of making composite airfoil structures | |
| JP4191343B2 (en) | Method for manufacturing honeycomb sandwich panel | |
| JP4890642B2 (en) | Vehicle body made of integrated composite material for transport vehicle and method for manufacturing the same | |
| KR101832301B1 (en) | Back cover for supporting display panel and method for producing the same | |
| EP1145828A2 (en) | Method for producing composite structure and composite structure produced thereby | |
| RU2366579C2 (en) | Method forming laminar material with filleted joint | |
| JPH07180281A (en) | Honeycomb sandwich panel and manufacture thereof | |
| WO2005065920A2 (en) | Method of making a window skin panel | |
| JPH0326362B2 (en) | ||
| JP4328579B2 (en) | Method for manufacturing honeycomb sandwich panel | |
| JPH08197668A (en) | Lamination structure of fiber reinforced resin | |
| EP1641611B1 (en) | Laminate with fill layer | |
| JP7034849B2 (en) | Composite material, method for manufacturing composite material, and method for curing composite material | |
| JP4396057B2 (en) | FRP laminate and FRP molding method | |
| JP3822182B2 (en) | Manufacturing method of composite material honeycomb sandwich structure | |
| JP3204529B2 (en) | Method for manufacturing curved honeycomb panel | |
| JP3004309B2 (en) | Method for producing fiber-reinforced resin laminate | |
| JP3004370B2 (en) | Multi-layer honeycomb structure | |
| WO1998058709A1 (en) | Skid plate | |
| JP3493131B2 (en) | Method for manufacturing bisect type fiber reinforced plastic honeycomb core | |
| JPS584198B2 (en) | Manufacturing method of fiber-reinforced plastic impeller | |
| JP7218043B2 (en) | honeycomb laminate | |
| WO2022260186A1 (en) | Laminate for pressing, and pressed laminate | |
| JP2740219B2 (en) | Method for manufacturing composite material structure | |
| JP7039401B2 (en) | Composite material and method of curing composite material |