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JPS5953866B2 - sandwich panel - Google Patents
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JPS5953866B2 - sandwich panel - Google Patents

sandwich panel

Info

Publication number
JPS5953866B2
JPS5953866B2 JP8306378A JP8306378A JPS5953866B2 JP S5953866 B2 JPS5953866 B2 JP S5953866B2 JP 8306378 A JP8306378 A JP 8306378A JP 8306378 A JP8306378 A JP 8306378A JP S5953866 B2 JPS5953866 B2 JP S5953866B2
Authority
JP
Japan
Prior art keywords
face
sandwich panel
core material
core
spherical
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.)
Expired
Application number
JP8306378A
Other languages
Japanese (ja)
Other versions
JPS559866A (en
Inventor
慶次 大村
秀明 蒲原
澄生 奥野
稔 田中
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.)
Hitachi Ltd
Original Assignee
Hitachi 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 Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP8306378A priority Critical patent/JPS5953866B2/en
Publication of JPS559866A publication Critical patent/JPS559866A/en
Publication of JPS5953866B2 publication Critical patent/JPS5953866B2/en
Expired legal-status Critical Current

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  • Panels For Use In Building Construction (AREA)
  • Laminated Bodies (AREA)

Description

【発明の詳細な説明】 本発明は面材と芯材で構成されるサンドイッチパネルに
係り、特に面材を軽量化するに好適な断面形状を有する
サンドイッチパネルに関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a sandwich panel composed of a face material and a core material, and particularly to a sandwich panel having a cross-sectional shape suitable for reducing the weight of the face material.

従来からサンドイッチパネルは軽量で薄いにもかかわら
ず強靭であるという特性のため、航空機、車両、船舶及
び建築などの分野において、それぞれ用いられている。
以下、これらのサンドイッチパネルについて図面を用い
て説明する。第1図乃至第4図は従来の代表的なサンド
イッチパネルについて示したものである。図において、
1及び1’は平板の面材、2〜6は芯材でそれぞれハニ
カム、波板、パルサ材、発泡材及び球材である。一般に
サンドイッチパネルの強度並びに防音、断熱などの特性
は、前記の芯材の材質、構造により異なる。芯材として
第1図及び第2図゜に示すような金属性のハニカム2及
び波板3を使用したものは、強度面からの問題はほとん
ど生じないが、上、下の面材1及び1’が金属間の接触
状態となり、断熱に対して不利である。また、一般的に
高価である。i−方、第3図及び第4図に示すように芯
材としてパルサ材4及び発泡材5を使用した・ものは、
逆に防音、断熱特性は優れているが強度特性が低下する
Sandwich panels have traditionally been used in fields such as aircraft, vehicles, ships, and architecture because of their characteristics of being strong despite being lightweight and thin.
These sandwich panels will be described below with reference to the drawings. 1 to 4 show typical conventional sandwich panels. In the figure,
1 and 1' are flat plate face materials, and 2 to 6 are core materials, which are honeycomb, corrugated sheet, pulsar material, foamed material, and spherical material, respectively. In general, properties such as strength, soundproofing, and heat insulation of a sandwich panel vary depending on the material and structure of the core material. Those using the metallic honeycomb 2 and corrugated plate 3 as shown in FIGS. 1 and 2 as the core material have almost no problems in terms of strength, but the upper and lower facing materials 1 and 1 ' becomes a contact state between metals, which is disadvantageous for heat insulation. They are also generally expensive. The i-way, as shown in Figures 3 and 4, uses pulsar material 4 and foam material 5 as core materials,
Conversely, it has excellent soundproofing and heat insulation properties, but its strength properties deteriorate.

特に発泡材5を利用した場合は、芯材が非弾性で硬度も
ほとんどなあことから面材に局部的な集中荷重が作用し
た場合、面材は板厚の減少にともない、局所的な変形を
生じやすくなる。このため、局所的変形すなわちへこみ
量が厳しく制限される設計仕様、たとえば車両の床材な
どに使用する場合は、他の芯材のサンドイツチパネルに
比較して面材の板厚が増加し、軽量化の面で不利となる
。またバルサ材4の場合は芯材の重量が大きく、全体の
重量が増加する欠点がある。第5a,b図は前記第1図
乃至第4図に示すサンドイツチパネルの個々の特徴を含
む構造として最近検討されているもので、芯材に弾性を
有する軽量、安価な高分子材料製の中空の球材6を使用
している。この球材6は第6図に示すような荷重Pが作
用した場合、図示するように弾性変形を生ずるため、面
材1全体では第7図に示す弾性床材梁のような変形挙動
となる。しかし、この場合も第7図のD部に示すように
荷重点が隣接する球材6の中点に位置したときには、前
記の発泡材5に比較すると,改善されてはいるがこの球
材間で局部的な変形を生じやすい。このため、面材の薄
肉化すなわちサンドイツチパネルの一層の軽量化には困
難があつ〜 本発明の目的は、面材の材料強度特性を効果的二に発揮
させることにより局所的剛性を向上させ、面材を薄肉化
し、軽量で強度的に十分満足するサンドイツチパネルを
提供することにある。
In particular, when foam material 5 is used, the core material is inelastic and has almost no hardness, so when a localized concentrated load is applied to the facing material, the facing material will undergo local deformation as the plate thickness decreases. more likely to occur. For this reason, when using design specifications that severely limit local deformation, or the amount of denting, such as vehicle flooring, the thickness of the face material is increased compared to sanderch panels with other core materials. This is disadvantageous in terms of weight reduction. Moreover, in the case of balsa wood 4, the weight of the core material is large, which has the drawback of increasing the overall weight. Figures 5a and 5b show a structure that has recently been studied that incorporates the individual features of the sanderch panels shown in Figures 1 to 4, and is made of lightweight, inexpensive polymeric material with elastic core material. A hollow ball 6 is used. When this ball material 6 is subjected to a load P as shown in FIG. 6, it undergoes elastic deformation as shown in the figure, so the surface material 1 as a whole exhibits a deformation behavior similar to that of an elastic flooring beam shown in FIG. . However, in this case as well, when the load point is located at the midpoint of the adjacent balls 6, as shown in section D of FIG. tends to cause local deformation. For this reason, it is difficult to make the face material thinner, that is, to further reduce the weight of the sandwich panel.The purpose of the present invention is to improve local rigidity by effectively demonstrating the material strength characteristics of the face material. The object of the present invention is to provide a sanderch panel that is lightweight and has sufficient strength by reducing the thickness of the facing material.

本発明の特徴とするところは芯材に中空の球材を利用し
たサンドイツチパネルにおいて、面材にこ作用する面外
からの荷重を受ける面材の断面形状を、球形の芯材に一
部そわせて波形とすることにより、面内力に近いものと
し、面材の局所的剛性を向上させ、薄肉化できるように
したことである。
A feature of the present invention is that in a sanderch panel that uses a hollow spherical material as the core material, the cross-sectional shape of the face material that receives an out-of-plane load that acts on the face material is partially attached to the spherical core material. In addition, by creating a corrugated shape, the in-plane force can be approximated, improving the local rigidity of the face material and making it possible to reduce the thickness of the face material.

次に本発明の一実施例であるサンドイツチパネルを図面
を用いて詳細に説明する。
Next, a sandwich panel which is an embodiment of the present invention will be described in detail using the drawings.

第8a,b図は本発明を適用したサンドイツチパネルを
示したものである。図において、球材6及び接着剤7は
従前の通りであり、面材9及び9″は該球材6の4曲面
形状に適合する凹凸状の彼型断面を有する面材(以後、
波型面材と称す)である。サンドイツチパネルは基本的
にはこのような部品で構成され、波型面材9及び9″と
中空の球材6とはそれぞれ接着剤7で結合する。球材6
は弾性を有し、かつ防音、断熱特性が優れた高分子材料
で製作する。このようなサンドイツチパネルに面外から
の荷重が作用した場合、全体的には第7図に示すように
個々の球材6が弾性の変形挙動を示し、面材全体で荷重
を分担する。
Figures 8a and 8b show a sandwich panel to which the present invention is applied. In the figure, the ball 6 and the adhesive 7 are the same as before, and the face materials 9 and 9'' have an uneven cross section that matches the four-curved shape of the ball 6 (hereinafter referred to as
(referred to as wavy surface material). The sanderch panel is basically composed of such parts, and the corrugated panels 9 and 9'' and the hollow spheres 6 are each bonded with an adhesive 7.The spheres 6
is made of a polymeric material that is elastic and has excellent sound and heat insulation properties. When a load from outside the plane is applied to such a sanderch panel, the individual balls 6 exhibit elastic deformation behavior as shown in FIG. 7, and the load is shared by the entire panel.

一方、永久変形にもとづくへこみ量に大きく影響する波
形面材9の球材6間のいわゆる局所的変形は、第9図に
示すように球状6に囲まれた範囲を半球面とし、分布荷
重が作用したとしてモデル化すると膜変位となり弾性範
囲内では(1)式で示すようになる。
On the other hand, the so-called local deformation between the spheres 6 of the corrugated surface material 9, which greatly affects the amount of indentation due to permanent deformation, is caused by the area surrounded by the spheres 6 being a hemispherical surface as shown in Fig. 9, and the distributed load is When modeled as acting, it becomes membrane displacement as shown by equation (1) within the elastic range.

比較のため従来の平板の場合(以後、平型面材と称す)
も同様に、第10図に示すようにモデル化すると最大変
形量は(2)式となる。そこで彼型と′T′至凹材T及
ひjについてK1=Rと仮定し、(1),(2)式を単
位変形量当りの荷重P/δで表わし比較すると、(3)
式のようになる。
For comparison, the case of conventional flat plate (hereinafter referred to as flat plate)
Similarly, when modeled as shown in FIG. 10, the maximum deformation amount becomes equation (2). Therefore, assuming K1=R for the He type and 'T' concave material T and hj, and comparing equations (1) and (2) by expressing the load P/δ per unit deformation, we get (3)
It becomes like the expression.

ここで、K,:波型面材の(P/δ)/平型面材の(P
/δ)(3)式において、サンドイツチパネルではR2
〉2t2となり、K,〉1である。
Here, K,: (P/δ) of the corrugated surface material/(P of the flat surface material)
/δ) In formula (3), R2 for the Sanderch panel
〉2t2, and K,〉1.

換言すれば、波型面材の場合が平型面材に比較して、同
一荷重に対する変形量は小さくなる。また、最大応力は
それぞれ(4),(5)式で表わされる。ここで゛、σ
W,σp:応力(Kg/Mm2)前記の変形量の場合と
同様に比較すると(6)式となる。
In other words, in the case of a corrugated panel, the amount of deformation for the same load is smaller than that of a flat panel. Further, the maximum stress is expressed by equations (4) and (5), respectively. Here ゛, σ
W, σp: Stress (Kg/Mm2) When compared in the same manner as in the case of the amount of deformation described above, equation (6) is obtained.


ここで、KO:波型面材の応力/平型面材の応力(6)
式において、2t〈3Rであり、KOく1となる。
Here, KO: stress of corrugated surface material/stress of flat surface material (6)
In the formula, 2t<3R, and KO×1.

すなわち、彼型面材の場合が平型面材に比較して応力は
小さくなる。このような両者の変形量及び応力の関係は
、第11図から明らかなように面材9と球材6の接着面
で波型面材9に凸部を形成して、球材6と同一の曲率半
径をもたせることにより面材と球材の非接触部の長さが
短くなりR〉R1となるため、それぞれR4/R2←1
,R1/R倍助長されることとなる。このような波型と
平型面材の変形量及び応力の関係は、集中荷重が作用し
た場合にもほぼ同様の傾向となる。以上の結果から明ら
かなように、面材に球形に近い曲率半径を有する波型形
状を設けることにより、面材に作用する面外からの荷重
は面内力となり、永久変形にもとづくへこみ量並びに応
力は小さくなる。
In other words, the stress is smaller in the case of a rectangular plate than in the case of a flat plate. As is clear from FIG. 11, the relationship between the amount of deformation and the stress between the two is such that a convex portion is formed on the corrugated surface material 9 at the bonding surface between the surface material 9 and the ball material 6, and the surface material is the same as the ball material 6. By giving a radius of curvature of
, R1/R times. The relationship between the amount of deformation and the stress between the corrugated and flat face members tends to be almost the same even when a concentrated load is applied. As is clear from the above results, by providing the face material with a wave-like shape with a radius of curvature close to a spherical shape, the load from outside the plane acting on the face material becomes an in-plane force, and the amount of denting and stress due to permanent deformation are reduced. becomes smaller.

したがつて、サンドイツチパネル全体で重量割合の大き
い面材の板厚を小さくすることができ、軽量化が可能と
なる。また、防音及び断熱特性も中空の球材6を使用し
、上、下の面材間に空気層を設けており、従来の発泡材
と芯材とした場合とほぼ同等となる。第12a,b図は
、本発明の他の応用例を示したもので、前記の第8a,
b図と異なるのは、波型面材9の凹部9a及び9″aと
球材6″を接触させたもので、このため球材6″の外面
には面材9との接触部6aを凹型にしている。
Therefore, it is possible to reduce the thickness of the face material having a large weight ratio in the entire sanderch panel, thereby making it possible to reduce the weight. In addition, the soundproofing and heat insulating properties are almost the same as in the case of using a conventional foam material and core material, since the hollow sphere material 6 is used and an air layer is provided between the upper and lower face materials. Figures 12a and 12b show other application examples of the present invention;
What differs from Figure b is that the ball 6'' is in contact with the recesses 9a and 9''a of the corrugated panel 9, and therefore the outer surface of the ball 6'' has a contact portion 6a with the panel 9. It is concave.

また、第13図は本発明の更に他の変形例を示したもの
で、芯材10として半球形のものを用いた場合において
も、波型面材9の凹部が半球10の非球面部10,aに
位置し、凸部が球面部10bと接触するように組合せる
。このような面材と芯材の組合せでも、前記と同一の効
果を有する。本発明によれば、面材の球材との非接触部
の剛性をあげるため、サンドイツチパネルの全体重量の
大部分を占める面材の板厚を薄肉にすることができ、軽
量化できるという効果がある。
Further, FIG. 13 shows still another modification of the present invention, in which even when a hemispherical core material 10 is used, the concave portion of the corrugated surface material 9 is the aspherical portion 10 of the hemispherical surface 10. , a, and are assembled so that the convex portion is in contact with the spherical portion 10b. Such a combination of face material and core material also has the same effect as described above. According to the present invention, in order to increase the rigidity of the non-contact part of the face material with the ball material, the thickness of the face material, which accounts for most of the overall weight of the sanderch panel, can be made thinner, resulting in weight reduction. effective.

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

第1図乃至第4図は従来の代表的なサンドイツチパネル
を示したもので、第1図は芯材にハニカム、第2図は芯
材に波板、第3図は芯材にバルサ材、第4図は芯材に発
泡材をそれぞれれ使用した場合の概略構造図、第5a図
は現在考えられている芯材に球材を使用したサンドイツ
チパネルの構造図、第5b図は第5a図のA−A断面図
、第6図は第5図に表わす球材の弾性変形状態を示す説
明図、第7図は第5図に示すサンドイツチパネルに面外
からの荷重が作用した場合の面材の変形状態を示す説明
図、第8a図は本発明の一実施例であり、面材が波型の
断面形状であるサンドイツチパネルを示す構造図、第8
b図は第8a図のB一B断面図、第9図及び第10図は
本発明及び従来の面材に面外からの荷重が作用した場合
を局所的”にモデル化した説明図、第11図は本発明に
おける波型面材と球製芯材の結合状態の詳細を示す説明
図、第12a図及び第13図はそれぞれ本発明の応用例
であるサンドイツチパネルを示したもので、第12a図
は波型面材と球材の接触位置を変・化させた状態を、第
13図は芯材が半球材の場合を示す構造図、12b図は
第12a図のC−C断面図である。 1,1″・・・面材、6・・・中空の球材、9,9″・
・・波型面材、10・・・半球材。
Figures 1 to 4 show typical conventional sanderch panels. Figure 1 has a honeycomb core, Figure 2 has a corrugated core, and Figure 3 has a balsa core. , Fig. 4 is a schematic structural diagram of the case where foam material is used as the core material, Fig. 5a is a structural diagram of the currently considered sanderch panel using spherical material as the core material, and Fig. 5b is the Figure 5a is a sectional view taken along line A-A, Figure 6 is an explanatory diagram showing the state of elastic deformation of the ball shown in Figure 5, and Figure 7 is an illustration of the sanderch panel shown in Figure 5 when an out-of-plane load is applied. Fig. 8a is an explanatory diagram showing the deformed state of the facing plate in the case of the present invention, and Fig. 8a is a structural diagram showing a sanderch panel in which the facing plate has a corrugated cross-sectional shape.
Figure b is a B-B sectional view of Figure 8a, Figures 9 and 10 are explanatory diagrams locally modeling the case where an out-of-plane load is applied to the inventive and conventional surface materials, FIG. 11 is an explanatory diagram showing details of the bonding state of the corrugated panel and the spherical core material in the present invention, and FIGS. 12a and 13 each show a sandwich panel which is an application example of the present invention. Fig. 12a shows the state in which the contact position between the corrugated surface material and the ball material is changed, Fig. 13 is a structural diagram showing the case where the core material is a hemispherical material, and Fig. 12b is the C-C cross section of Fig. 12a. It is a figure. 1,1″...Face material, 6...Hollow ball material, 9,9″・
...Corrugated surface material, 10...Semispherical material.

Claims (1)

【特許請求の範囲】 1 相対する金属あるいは複合材料からなる面材と、該
面材間にはさまれる複数個の球状の芯材からなるサンド
イッチパネルにおいて、前記面材の断面形状を波型形状
にしたことを特徴とするサンドイッチパネル。 2 特許請求の範囲第1項記載のサンドイッチパネルに
おいて、面材の波型形状の凸部が球状の芯材と接触し同
じく面材の凹部が隣接した芯材との中間点に位置するよ
うに前記面材と芯材を組合せさたことを特徴とするサン
ドイッチパネル。 3 特許請求の範囲第1項記載のサンドイッチパネルに
おいて、球状の芯材の外面に任意の大きさの凹部を設け
、この芯材の凹部に面材の凹部をそわせて接触させ、か
つ面材の凸部が隣接した芯材との中間点に位置するよう
に面材と芯材を組合せたことを特徴とするサンドイッチ
パネル。 4 特許請求の範囲第3項記載のサンドイッチパネルに
おいて、形状の凹部を大きく形成して該芯材を半球状に
し、面材の凹部が該半球の芯材の非球面部に位置し、同
じく面材の凸部が半球状の芯材の球面部と接触するよう
に面材と芯材を組合せたことを特徴とするサンドイッチ
パネル。 5 特許請求の範囲第1項又は第2項又は第3項又は第
4項記載のサンドイッチパネルにおいて、前記芯材を中
空にすると共に高分子材料で形成したことを特徴とする
サンドイッチパネル
[Scope of Claims] 1. In a sandwich panel consisting of opposing face plates made of metal or composite materials and a plurality of spherical core members sandwiched between the face plates, the cross-sectional shape of the face plates is wave-shaped. A sandwich panel characterized by: 2. In the sandwich panel according to claim 1, the wavy convex portion of the face material is in contact with the spherical core material, and the concave portion of the face material is located at the midpoint between the adjacent core material. A sandwich panel characterized by combining the above-mentioned face material and core material. 3. In the sandwich panel according to claim 1, a concave portion of an arbitrary size is provided on the outer surface of the spherical core material, and the concave portion of the face material is aligned and in contact with the concave portion of the core material, and the face material A sandwich panel characterized in that a face material and a core material are combined so that the convex portion of the panel is located at a midpoint between two adjacent core materials. 4. In the sandwich panel according to claim 3, the core material is made into a hemispherical shape by forming a large recessed portion, and the recessed portion of the face material is located on the aspherical surface portion of the hemispherical core material, and A sandwich panel characterized in that a face material and a core material are combined so that a convex part of the material contacts a spherical part of a hemispherical core material. 5. A sandwich panel according to claim 1, 2, 3, or 4, characterized in that the core material is hollow and made of a polymeric material.
JP8306378A 1978-07-10 1978-07-10 sandwich panel Expired JPS5953866B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP8306378A JPS5953866B2 (en) 1978-07-10 1978-07-10 sandwich panel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP8306378A JPS5953866B2 (en) 1978-07-10 1978-07-10 sandwich panel

Publications (2)

Publication Number Publication Date
JPS559866A JPS559866A (en) 1980-01-24
JPS5953866B2 true JPS5953866B2 (en) 1984-12-27

Family

ID=13791718

Family Applications (1)

Application Number Title Priority Date Filing Date
JP8306378A Expired JPS5953866B2 (en) 1978-07-10 1978-07-10 sandwich panel

Country Status (1)

Country Link
JP (1) JPS5953866B2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2408015A (en) * 2003-11-14 2005-05-18 Intelligent Engineering Structural sandwich plate members with forms
CN105459932A (en) * 2015-11-23 2016-04-06 天津华夏联盛汽车部件有限公司 Bumper with buffering function

Also Published As

Publication number Publication date
JPS559866A (en) 1980-01-24

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