JPH06226891A - Vibration-damping honeycomb panel - Google Patents
Vibration-damping honeycomb panelInfo
- Publication number
- JPH06226891A JPH06226891A JP3937693A JP3937693A JPH06226891A JP H06226891 A JPH06226891 A JP H06226891A JP 3937693 A JP3937693 A JP 3937693A JP 3937693 A JP3937693 A JP 3937693A JP H06226891 A JPH06226891 A JP H06226891A
- Authority
- JP
- Japan
- Prior art keywords
- vibration
- panel
- honeycomb
- damping
- honeycomb panel
- 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
Landscapes
- Body Structure For Vehicles (AREA)
- Laminated Bodies (AREA)
Abstract
Description
【０００１】[0001]
【産業上の利用分野】本発明は、自動車、鉄道車両、航
空機、住宅の床、壁等の制振用構造体として適用される
制振ハニカムパネルに関するものである。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a vibration-damping honeycomb panel applied as a vibration-damping structure for automobiles, railway cars, aircrafts, floors of houses, walls and the like.
【０００２】[0002]
【従来の技術】この種のハニカムパネルに関しては、実
開平３−２６５３２号公報に記載のものが知られてい
る。即ち、（ハニカムパネルの一部切断斜視図）に示す
ように、アルミハニカム１の上下面又は一方の面にアル
ミ制振板２ａ，２ｂを貼り付けてあり、かつこのアルミ
制振板２ａ，２ｂは、図６（図５の２−２矢視断面図）
に示すように厚さが等しいアルミ板３ａ，３ｂの間に合
成樹脂材料４を介在させた構成である。この構成によ
り、遮音性に優れ、さらには振動等を有効に抑えること
ができる旨開示されている。2. Description of the Related Art A honeycomb panel of this type is known from Japanese Utility Model Laid-Open No. 3-26532. That is, as shown in (partially cut perspective view of honeycomb panel), aluminum damping plates 2a and 2b are attached to the upper and lower surfaces or one surface of the aluminum honeycomb 1, and the aluminum damping plates 2a and 2b are attached. Is shown in FIG. 6 (a sectional view taken along the line 2-2 of FIG. 5).
As shown in FIG. 3, the synthetic resin material 4 is interposed between the aluminum plates 3a and 3b having the same thickness. It is disclosed that this configuration has excellent sound insulation and can effectively suppress vibration and the like.
【０００３】[0003]
【発明が解決しようとする課題】しかし、上記のハニカ
ムパネルは、アルミ制振板自体が有する公知の優れた振
動抑制効果に着目し、この公知のアルミ制振板を単にハ
ニカムコアの上下面の少なくとも一方に貼り付けた構成
であるため、アルミ板だけを貼り付けていたときに比べ
れば振動抑制効果に多少の向上はみられるが、ハニカム
パネル全体としての振動抑制効果は、アルミ制振動板を
単独で用いた場合に比較して低下するという問題点があ
った。However, in the above honeycomb panel, attention is paid to the known excellent vibration suppressing effect of the aluminum vibration damping plate itself, and this known aluminum vibration damping plate is simply used for the upper and lower surfaces of the honeycomb core. Since the structure is attached to at least one side, there is some improvement in the vibration suppression effect compared to when only the aluminum plate is adhered, but the vibration suppression effect for the honeycomb panel as a whole is There is a problem that it is lower than that when used alone.
【０００４】そこで、本発明者等は、ハニカムパネル全
体の振動抑制効果を著しく向上させるという目的を掲
げ、特にハニカムパネルが音圧加振や機械的加振を受け
て、曲げ振動が発生したときに合成樹脂等の粘弾性材料
に作用する力学的特性に着目して研究を重ね、本発明を
完成した。Therefore, the inventors of the present invention have the object of significantly improving the vibration suppressing effect of the entire honeycomb panel, and particularly when the honeycomb panel is subjected to sound pressure vibration or mechanical vibration and bending vibration occurs. The present invention has been completed by repeating the research focusing on the mechanical characteristics acting on the viscoelastic material such as synthetic resin.
【０００５】[0005]
【課題を解決するための手段】上記目的を達成し得た第
１発明の制振ハニカムパネルは、該パネルの外側から厚
み方向に沿って弾性板，ハニカムコア，弾性板，粘弾性
材料層，弾性板，ハニカムコア，弾性板の順序で一体的
に成形して構成したことを要旨とするものである。A vibration-damping honeycomb panel of the first aspect of the present invention that has achieved the above object is an elastic plate, a honeycomb core, an elastic plate, a viscoelastic material layer, which extends from the outside of the panel in the thickness direction. The gist is that the elastic plate, the honeycomb core, and the elastic plate are integrally molded in this order.
【０００６】また、第２発明の制振ハニカムパネルは、
ハニカムサンドイッチ構造の制振パネルであって、該パ
ネルの外側から厚み方向に沿って厚肉の弾性板，粘弾性
材料層，薄肉の弾性板，ハニカムコアの順序で一体的に
成形したものを含んで構成したことを要旨とするもので
ある。The vibration damping honeycomb panel of the second invention is
A vibration damping panel having a honeycomb sandwich structure, which includes a thick elastic plate, a viscoelastic material layer, a thin elastic plate, and a honeycomb core integrally formed in this order from the outside of the panel in the thickness direction The summary is that it is composed of.
【０００７】さらに、第３発明の制振ハニカムパネル
は、ハニカムサンドイッチ構造の制振パネルであって、
該パネルの厚み方向に弾性板，粘弾性材料層，弾性板，
側壁が粘弾性材料膜で被覆されたハニカムコアの順序で
一体的に成形してものを含んで構成したことを要旨とす
るものである。Further, the vibration damping honeycomb panel of the third invention is a vibration damping panel having a honeycomb sandwich structure,
An elastic plate, a viscoelastic material layer, an elastic plate, in the thickness direction of the panel,
The gist of the present invention is that the honeycomb core whose side walls are coated with the viscoelastic material film is integrally molded in the order.
【０００８】[0008]
【作用】前記第１発明によれば、粘弾性材料層は、ハニ
カムパネルの中立軸付近に位置し、この粘弾性材料層の
上側のハニカム構造体と下側のハニカム構造体の各曲げ
剛性をほぼ等しくすることができる。その結果、粘弾性
材料層には、公知のアルミ制振板を単独で使用したとき
にその中立軸に位置する合成樹脂層に働く力学的特性と
同一の作用を生ぜしめることができる。即ち、ハニカム
パネル全体が曲げ変形を受けると、このパネルの中立軸
付近に位置する粘弾性材料もせん断変形を受けるが、せ
ん断ひずみエネルギーが最大となるため、振動エネルギ
ーが熱エネルギーに変換して外気に放出される割合も最
大となり、パネル全体の振動抑制効果が最も大きくな
る。According to the first aspect of the invention, the viscoelastic material layer is located near the neutral axis of the honeycomb panel, and the bending rigidity of each of the honeycomb structure above and below the viscoelastic material layer is adjusted. Can be about equal. As a result, the viscoelastic material layer can exert the same action as the mechanical characteristic that acts on the synthetic resin layer positioned on the neutral axis when a known aluminum damping plate is used alone. That is, when the entire honeycomb panel is subjected to bending deformation, the viscoelastic material located near the neutral axis of this panel is also subjected to shear deformation, but since the shear strain energy becomes maximum, the vibration energy is converted into thermal energy and the outside air is converted. The rate of release to the maximum is also maximized, and the effect of suppressing vibration of the entire panel is maximized.
【０００９】この点は、従来技術の制振ハニカムパネル
における作用と大きく異なるところである。即ち、従来
のハニカムパネルでは、公知のアルミ制振板を単にハニ
カムコアの面材として使用するものであり、ハニカムコ
アの曲げ剛性がと大きいために、アルミ制振板の合成樹
脂は、ハニカムパネルの中立軸から大きく離れた位置に
存在することになる。その結果、その合成樹脂に生じる
せん断ひずみエネルギーは、アルミ制振板単品を使用す
る際に合成樹脂に作用するせん断ひずみエネルギーに比
べて極めて小さく、振動エネルギーが熱エネルギーに変
換する割合、つまり振動減衰率を大きくできず、ハニカ
ムパネル全体の振動抑制効果の向上につながらなかった
のである。This point is largely different from the operation of the conventional vibration damping honeycomb panel. That is, in the conventional honeycomb panel, a known aluminum damping plate is simply used as the face material of the honeycomb core, and since the bending rigidity of the honeycomb core is large, the synthetic resin of the aluminum damping plate is It will be located far away from the neutral axis. As a result, the shear strain energy generated in the synthetic resin is extremely smaller than the shear strain energy acting on the synthetic resin when using a single aluminum damping plate, and the rate at which vibration energy is converted to thermal energy, that is, vibration damping The rate could not be increased, and the effect of suppressing vibration of the entire honeycomb panel was not improved.
【００１０】次に、前記第２発明は、粘弾性材料層の非
ハニカムコア側の厚肉状弾性体の曲げ剛性をハニカムコ
ア側の薄肉状弾性体をいわば面材とするハニカムコアの
曲げ剛性に近づけることが可能である。即ち、結果とし
て、粘弾性材料を、ハニカムパネルの中立軸に近づける
ことができるので、この場合も、上記請求項１の発明と
同様にハニカムパネル全体が曲げ振動を受けた場合に粘
弾性材料に生じるせん断ひずみエネルギーは非常に大き
くなり、振動減衰率の増加により、振動抑制効果を大き
く向上させることができる。Next, in the second invention, the bending rigidity of the thick elastic body on the non-honeycomb core side of the viscoelastic material layer is the bending rigidity of the honeycomb core using the thin elastic body on the honeycomb core side as a so-called face material. It is possible to approach. That is, as a result, the viscoelastic material can be brought close to the neutral axis of the honeycomb panel. In this case as well, the viscoelastic material becomes the viscoelastic material when the entire honeycomb panel is subjected to bending vibration as in the invention of claim 1. The shear strain energy generated becomes very large, and the vibration damping effect can be greatly improved by increasing the vibration damping rate.
【００１１】次に、前記第３発明について、その作用を
説明する。まず、従来のハニカムパネルにおいて振動が
伝わる様子をみれば、該パネルが騒音源から音圧を受け
たり、或いは機械的加振を受けることにより、該パネル
に振動が生じる。このとき、ハニカムコアの側壁は面板
との接合部近傍で著しく変形する。ところが、ハニカム
コアには何らの振動抑制対策はなされておらず、面板の
振動抑制対策に頼っていた。Next, the operation of the third invention will be described. First, looking at how the vibration is transmitted in the conventional honeycomb panel, the panel is vibrated by receiving sound pressure from a noise source or mechanical vibration. At this time, the side wall of the honeycomb core is significantly deformed near the joint with the face plate. However, the honeycomb core does not take any vibration suppression measures, and relies on the face plate vibration suppression measures.
【００１２】これに対し、第３発明は、ハニカムコアの
全側壁にも粘弾性材料膜を貼り付けた構成のハニカムパ
ネルである。従ってハニカムコアの側壁に生じる曲げ
は、ハニカムコア側壁表裏面の粘弾性材料膜のところ
で、この粘弾性材料の曲げ振動に対する伸縮変形により
熱エネルギーに変換され、外気に放出される。この結
果、ハニカムパネル全体の振動抑制効果が著しく向上さ
れる。On the other hand, the third aspect of the present invention is a honeycomb panel having a structure in which a viscoelastic material film is attached to all sidewalls of a honeycomb core. Therefore, the bending generated on the side wall of the honeycomb core is converted into thermal energy at the viscoelastic material film on the front and back surfaces of the side wall of the honeycomb core by expansion and contraction of the viscoelastic material due to bending vibration, and is released to the outside air. As a result, the vibration suppressing effect of the entire honeycomb panel is significantly improved.
【００１３】[0013]
【実施例】以下、本発明の実施例を図面に基づいて説明
する。図１は、第１発明を実施した制振ハニカムパネル
の概略説明図である。このハニカムパネル１０は、パネ
ルの外側から厚み方向に沿ってアルミ板１３ａ，アルミ
ハニカムコア１２，アルミ板１３ｂ，ポリエステル樹脂
等の樹脂層１４，アルミ板１３ｂ，アルミハニカムコア
１２，アルミ板１３ａの順序で一体的に積層成形して構
成している。この構成において、図面の上下２層を占め
るハニカム構造体１１ａ，１１ｂは、夫々、同一厚みの
アルミハニカムコア１２の上下面に同一厚みのアルミ板
１３ａ，１３ｂを貼り付けて剛性パネルを成している。Embodiments of the present invention will be described below with reference to the drawings. FIG. 1 is a schematic explanatory view of a vibration damping honeycomb panel in which the first invention is implemented. This honeycomb panel 10 includes an aluminum plate 13a, an aluminum honeycomb core 12, an aluminum plate 13b, a resin layer 14 such as a polyester resin, an aluminum plate 13b, an aluminum honeycomb core 12, and an aluminum plate 13a in this order from the outside of the panel. Are integrally laminated and formed. In this structure, the honeycomb structures 11a and 11b, which occupy the upper and lower two layers in the drawing, form a rigid panel by attaching aluminum plates 13a and 13b having the same thickness to the upper and lower surfaces of the aluminum honeycomb core 12 having the same thickness, respectively. There is.
【００１４】さて、制振ハニカムパネル１０に振動が加
えられると、上下２層の剛性パネル１１ａ，１１ｂは、
曲げ振動を開始する。このとき、この２層の剛性パネル
１１ａ，１１ｂに挟まれた樹脂はせん断変形を受ける
が、樹脂層１４が制振ハニカムパネル１０の中立軸付近
に存在するので、樹脂のせん断ひずみエネルギーは最大
となり、この樹脂層１４で熱となって外部に放出される
効率が最大となる。この結果、制振ハニカムパネル１０
全体の曲げ振動抑制効果は最大となる。When vibration is applied to the damping honeycomb panel 10, the upper and lower two rigid panels 11a and 11b are
Start bending vibration. At this time, the resin sandwiched between the two rigid panels 11a and 11b undergoes shear deformation, but since the resin layer 14 exists near the neutral axis of the damping honeycomb panel 10, the shear strain energy of the resin becomes maximum. The efficiency of heat generated by the resin layer 14 and released to the outside is maximized. As a result, the damping honeycomb panel 10
The overall effect of suppressing bending vibration is maximized.
【００１５】なお、この振動抑制効果は、上下２層の剛
性パネル１１ａ，１１ｂの厚みが等しいときに最大とな
るが、その反面、樹脂のせん断弾性係数の上昇が曲げ剛
性には負の影響を及ぼし、制振ハニカムパネル１０全体
の曲げ剛性は、若干低下する傾向を示す。そこで、各産
業分野の適用に際しては、要求される曲げ剛性と所要の
振動抑制効果量との兼ね合いを考慮し、本実施例の構成
をそのまま採用したり、上下２層の剛性パネル１１ａ，
１１ｂの厚みに適切な差をつけて樹脂層１４を制振ハニ
カムパネル全体の中立軸からみて少しずれた位置とし、
必要十分な振動抑制効果を維持しつつ、十分な曲げ剛性
を確保する構成とする等、適宜選択可能であり、この場
合も本発明の技術的範囲を逸脱するものではない。The vibration suppressing effect is maximized when the upper and lower two rigid panels 11a and 11b have the same thickness. On the other hand, the increase in the shear elastic modulus of the resin has a negative effect on the bending rigidity. Therefore, the bending rigidity of the entire vibration-damping honeycomb panel 10 tends to slightly decrease. Therefore, in applying each industrial field, in consideration of the balance between the required bending rigidity and the required vibration suppression effect amount, the configuration of the present embodiment is adopted as it is, or the rigid panels 11a of the upper and lower two layers,
An appropriate difference is made in the thickness of 11b to position the resin layer 14 at a position slightly deviated from the neutral axis of the entire vibration damping honeycomb panel,
It is possible to appropriately select such a configuration as to ensure a sufficient bending rigidity while maintaining a necessary and sufficient vibration suppressing effect, and this case does not depart from the technical scope of the present invention.
【００１６】次に、図２は、第２発明を実施した制振ハ
ニカムパネルの概略説明図である。この制振ハニカムパ
ネル２０は、パネルの外側から厚み方向に沿って厚肉の
アルミ板２１ａ，樹脂層２３，薄肉のアルミ板２１ｂ，
アルミハニカムコア２２，薄肉のアルミ板２１ｂ，樹脂
層２３，厚肉のアルミ板２１ａの順序じ一体的に積層成
形して構成している。Next, FIG. 2 is a schematic explanatory view of a vibration damping honeycomb panel embodying the second invention. The vibration-damping honeycomb panel 20 includes a thick aluminum plate 21a, a resin layer 23, a thin aluminum plate 21b, which extends from the outside of the panel in the thickness direction.
The aluminum honeycomb core 22, the thin aluminum plate 21b, the resin layer 23, and the thick aluminum plate 21a are integrally laminated and formed in this order.
【００１７】この構成において、厚肉アルミ板２１ａの
厚み（ｔａ）と薄肉アルミ板２１ｂの厚み（ｔｂ）との
比（ｔａ／ｔｂ）が大きくなるほど、厚肉アルミ板２１
ａの曲げ剛性を、薄肉アルミ板２１ｂを面材とするアル
ミハニカムコア２２の曲げ剛性に近づけることができ、
結果として樹脂層２３を制振ハニカムパネル２０全体の
中立軸付近に位置させることができる。従って、制振ハ
ニカムパネル２０に曲げ振動が生じたときは、第１発明
の実施例の場合と同様に樹脂のせん断ひずみエネルギー
は非常に大きくなり、この樹脂層２３で熱となって外部
に放出される効率も非常に大きくなる。この結果、制振
ハニカムパネル２０全体の曲げ振動抑制効果を著しく高
めることができる。In this structure, the thicker the aluminum plate 21 is, the larger the ratio (ta / tb) between the thickness (ta) of the thick aluminum plate 21a and the thickness (tb) of the thin aluminum plate 21b is.
The bending rigidity of a can be made close to the bending rigidity of the aluminum honeycomb core 22 having the thin aluminum plate 21b as a surface material,
As a result, the resin layer 23 can be positioned near the neutral axis of the entire vibration damping honeycomb panel 20. Therefore, when bending vibration occurs in the vibration-damping honeycomb panel 20, the shear strain energy of the resin becomes very large as in the case of the embodiment of the first invention, and this resin layer 23 becomes heat and is released to the outside. The efficiency is also greatly increased. As a result, the effect of suppressing bending vibration of the entire vibration damping honeycomb panel 20 can be significantly enhanced.
【００１８】なお、第２発明についても、各産業分野へ
の適用に際しては、要求される振動抑制効果量との関係
で、本実施例の構成をそのまま適用したり、ハニカムコ
アの片側の面材を厚肉のアルミ板，樹脂層，薄肉のアル
ミ板の３層で構成し、反対側の面材は単なるアルミ板と
すること等、適宜選択可能である。When the second invention is applied to each industrial field, the structure of this embodiment may be applied as it is, or the face material on one side of the honeycomb core may be applied in relation to the required vibration suppression effect amount. Is composed of three layers of a thick aluminum plate, a resin layer, and a thin aluminum plate, and the face material on the opposite side is simply an aluminum plate.
【００１９】厚肉アルミ板２１ａ，樹脂層２３，薄肉ア
ルミ板２１ｂからなる３層及びアルミハニカムコア２２
の夫々の厚みを一定とした上で、厚肉アルミ板２１ａの
厚み（ｔａ）と薄肉アルミ板２１ｂの厚み（ｔｂ）の比
（ｔａ／ｔｂ）をいろいろ変えた場合について、片持ち
梁法により振動抑制効果を表すパラメータである損失係
数（ζ）を測定した。その結果を示したものが図３であ
る。なお、（ｔａ／ｔｂ）＝１の場合は、従来のハニカ
ムパネルに相当する。Three layers of a thick aluminum plate 21a, a resin layer 23, and a thin aluminum plate 21b, and an aluminum honeycomb core 22.
When the ratios (ta / tb) of the thickness (ta) of the thick aluminum plate 21a and the thickness (tb) of the thin aluminum plate 21b are variously changed while keeping the respective thicknesses constant, the cantilever method is used. The loss coefficient (ζ), which is a parameter representing the vibration suppression effect, was measured. The result is shown in FIG. The case of (ta / tb) = 1 corresponds to a conventional honeycomb panel.
【００２０】図３から明らかなように、（ｔａ／ｔｂ）
が大きくなるほどζの値が大きくなっており、特に（ｔ
ａ／ｔｂ）＝４とした場合の本発明品は、従来品に比べ
てζの値が約４倍も大きくなっており、振動抑制効果が
著しく向上することが確認できた。なお、（ｔａ／ｔ
ｂ）の値は、要求される振動抑制効果量に応じて適宜決
定することができる。しかし振動抑制効果の向上が一応
期待でき、アルミ板２１ａ，２１ｂ相互のバランスが崩
れない（ｔａ／ｔｂ）の範囲は、２〜４が好ましい。As is apparent from FIG. 3, (ta / tb)
The larger the value of, the larger the value of ζ.
In the case of a / tb) = 4, the product of the present invention has a value of ζ about 4 times larger than that of the conventional product, and it was confirmed that the vibration suppressing effect was remarkably improved. Note that (ta / t
The value of b) can be appropriately determined according to the required vibration suppression effect amount. However, the improvement of the vibration suppression effect can be expected for the time being, and the range in which the balance between the aluminum plates 21a and 21b is not disturbed (ta / tb) is preferably 2 to 4.
【００２１】次に、図４は、第３発明を実施した制振ハ
ニカムパネルの概略説明図である。この制振ハニカムパ
ネル３０は、該パネルの厚み方向に沿ってアルミ板３１
ａ，樹脂層３４，アルミ板３１ｂ，側壁３３ａが樹脂層
３３ｂで被覆されたアルミハニカムコア３３，アルミ板
３１ｂ，樹脂層３４，アルミ板３１ａの順序で一体的に
積層成形して構成している。Next, FIG. 4 is a schematic illustration of a vibration damping honeycomb panel embodying the third invention. This damping honeycomb panel 30 has an aluminum plate 31 along the thickness direction of the panel.
a, a resin layer 34, an aluminum plate 31b, and an aluminum honeycomb core 33 whose side wall 33a is covered with the resin layer 33b, an aluminum plate 31b, a resin layer 34, and an aluminum plate 31a are integrally laminated and formed in this order. .
【００２２】このような制振ハニカムパネル３０に振動
源からの振動が加わると、アルミ板３１ａ，樹脂層３
４，アルミ板３１ｂからなる面材３１が加振され、曲げ
振動を開始し、その振動エネルギーは、ハニカムコア３
３の側壁３３ａへと伝搬する。このとき、面材３１から
側壁３３ａを伝わる振動エネルギーは、側壁３３ａ表裏
面の樹脂膜３３ｂのところで、この樹脂の曲げ振動に伴
う伸縮変形により熱エネルギーに変換され、ハニカムコ
アの空間３３ｃに放出される。この結果、振動源と反対
側の面材３１に伝わる振動エネルギーは非常に小さくな
り、制振ハニカムパネル３０全体の振動抑制効果を著し
く向上させることができる。さらに、図示のように、面
材３１上の一方は又は双方を樹脂膜３２で被覆し、振動
抑制効果を更に高めることができる。When vibration from a vibration source is applied to the vibration damping honeycomb panel 30 as described above, the aluminum plate 31a and the resin layer 3 are formed.
4, the face material 31 made of the aluminum plate 31b is excited to start bending vibration, and the vibration energy is the honeycomb core 3
3 propagates to the side wall 33a. At this time, the vibration energy transmitted from the face material 31 through the side wall 33a is converted into heat energy at the resin film 33b on the front and back surfaces of the side wall 33a by expansion and contraction due to bending vibration of the resin, and is released to the space 33c of the honeycomb core. It As a result, the vibration energy transmitted to the face material 31 on the side opposite to the vibration source becomes extremely small, and the vibration suppressing effect of the entire vibration damping honeycomb panel 30 can be significantly improved. Further, as shown in the drawing, one or both of the face materials 31 can be covered with the resin film 32 to further enhance the vibration suppressing effect.
【００２３】[0023]
【発明の効果】本発明の制振ハニカムパネルは、以上の
ように構成しており、いずれもハニカムパネルが曲げ振
動するとき、パネル内に介在する樹脂等の粘弾性材料に
作用する力学的変形を有効に活用して振動エネルギーを
熱エネルギーに効率良く変換して放出できるようにした
ので、振動抑制効果を著しく高めることができるように
なった。The vibration-damping honeycomb panel of the present invention is constructed as described above, and in any case, when the honeycomb panel vibrates and vibrates, mechanical deformation acting on a viscoelastic material such as resin interposed in the panel is exerted. Since the vibration energy can be effectively utilized and efficiently converted into the heat energy and released, the vibration suppressing effect can be remarkably enhanced.
【図１】第１発明の一実施例を示す概略説明図である。FIG. 1 is a schematic explanatory view showing an embodiment of the first invention.
【図２】第２発明の一実施例を示す概略説明図である。FIG. 2 is a schematic explanatory view showing an embodiment of the second invention.
【図３】第２発明の一実施例と従来品の振動抑制効果の
比較図である。FIG. 3 is a comparison diagram of the vibration suppressing effect between the embodiment of the second invention and the conventional product.
【図４】第３発明の一実施例を示す要部断面説明図であ
る。FIG. 4 is an explanatory cross-sectional view of a main part showing an embodiment of a third invention.
【図５】従来のハニカムパネルの一部切断斜視図であ
る。FIG. 5 is a partially cut perspective view of a conventional honeycomb panel.
【図６】図５の２−２矢視断面図である。6 is a sectional view taken along the line 2-2 of FIG.
１２，２２，３３ ハニカムコア １３ａ，１３ｂ，２１ａ，２１ｂ，３１ａ，３１ｂ 弾
性板 １４，２３，３４ 粘弾性材料層 ３３ａ ハニカムコア側壁 ３３ｂ 樹脂膜12, 22, 33 Honeycomb core 13a, 13b, 21a, 21b, 31a, 31b Elastic plate 14, 23, 34 Viscoelastic material layer 33a Honeycomb core side wall 33b Resin film
───────────────────────────────────────────────────── フロントページの続き (72)発明者 畑山 直史 東京都千代田区丸の内１丁目８番２号 株 式会社神戸製鋼所東京本社内 (72)発明者 鶴野 招弘 栃木県真岡市鬼怒ヶ丘15番地 株式会社神 戸製鋼所真岡製造所内 ─────────────────────────────────────────────────── ─── Continuation of the front page (72) Naofumi Hatayama 1-8-2 Marunouchi, Chiyoda-ku, Tokyo Incorporated company Kobe Steel Ltd. Tokyo headquarters (72) Inventor Tsuruno Tsunehiro 15 Kinugaoka, Moka City, Tochigi Prefecture Address Kamido Steel Works Moka Works
Claims (3)
であって、該パネルの外側から厚み方向に沿って弾性
板，ハニカムコア，弾性板，粘弾性材料層，弾性板，ハ
ニカムコア，弾性板の順序で一体的に成形して構成した
ことを特徴とする制振ハニカムパネル。1. A vibration damping panel having a honeycomb sandwich structure, wherein an elastic plate, a honeycomb core, an elastic plate, a viscoelastic material layer, an elastic plate, a honeycomb core, and an elastic plate are arranged in this order from the outside of the panel in the thickness direction. A vibration-damping honeycomb panel characterized by being integrally molded with.
であって、該パネルの外側から厚み方向に沿って厚肉の
弾性板，粘弾性材料層，薄肉の弾性板，ハニカムコアの
順序で一体的に成形したものを含んで構成したことを特
徴とする制振ハニカムパネル。2. A vibration damping panel having a honeycomb sandwich structure, wherein a thick elastic plate, a viscoelastic material layer, a thin elastic plate, and a honeycomb core are integrally formed in this order from the outside of the panel along the thickness direction. A vibration-damping honeycomb panel characterized by being configured to include a molded product.
であって、該パネルの厚み方向に弾性板，粘弾性材料
層，弾性板，側壁が粘弾性材料膜で被覆されたハニカム
コアの順序で一体的に成形してものを含んで構成したこ
とを特徴とする制振ハニカムパネル。3. A vibration damping panel having a honeycomb sandwich structure, wherein an elastic plate, a viscoelastic material layer, an elastic plate, and a honeycomb core whose side wall is covered with a viscoelastic material film are integrated in this order in the thickness direction of the panel. A vibration-damping honeycomb panel, characterized in that it is configured to include a molded product.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3937693A JPH06226891A (en) | 1993-02-02 | 1993-02-02 | Vibration-damping honeycomb panel |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3937693A JPH06226891A (en) | 1993-02-02 | 1993-02-02 | Vibration-damping honeycomb panel |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH06226891A true JPH06226891A (en) | 1994-08-16 |
Family
ID=12551318
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP3937693A Pending JPH06226891A (en) | 1993-02-02 | 1993-02-02 | Vibration-damping honeycomb panel |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH06226891A (en) |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR980009694A (en) * | 1996-07-18 | 1998-04-30 | 부르크하르트 한스. 게르네트 자무엘 | Composite panel |
| WO2007056204A1 (en) * | 2005-11-04 | 2007-05-18 | The Boeing Company | Integrally damped composite aircraft floor panels |
| KR100868880B1 (en) * | 2007-01-29 | 2008-11-14 | 홍성산업 주식회사 | Panel for railroad car |
| JP2009241761A (en) * | 2008-03-31 | 2009-10-22 | Kinki Sharyo Co Ltd | Soundproofing method by panel for railway vehicle and soundproofing panel structure for railway vehicle used therefor |
| CZ304341B6 (en) * | 2013-02-13 | 2014-03-12 | Vysoká škola technická a ekonomická v Českých Budějovicích | Composite sandwich panel, especially panel for floors of means of conveyance |
| CN107815960A (en) * | 2017-11-01 | 2018-03-20 | 佛山科学技术学院 | A kind of pier anticollision system |
| CN108656665A (en) * | 2018-06-29 | 2018-10-16 | 贵州大学 | A kind of lightweight high-intensity PVC honeycomb aluminum plates |
| CN110001791A (en) * | 2017-12-27 | 2019-07-12 | 铃木株式会社 | Plate built in ojosa and its manufacturing method |
| JP2019531512A (en) * | 2016-07-22 | 2019-10-31 | ザ ギル コーポレーション | Structure and formation method thereof |
| JP2020152296A (en) * | 2019-03-22 | 2020-09-24 | トヨタ車体株式会社 | Vehicle floor raising member |
| JP2022535137A (en) * | 2019-06-07 | 2022-08-04 | エスエイチピーピー グローバル テクノロジーズ べスローテン フェンノートシャップ | Vehicle structure with honeycomb insert and its manufacture and use |
-
1993
- 1993-02-02 JP JP3937693A patent/JPH06226891A/en active Pending
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR980009694A (en) * | 1996-07-18 | 1998-04-30 | 부르크하르트 한스. 게르네트 자무엘 | Composite panel |
| WO2007056204A1 (en) * | 2005-11-04 | 2007-05-18 | The Boeing Company | Integrally damped composite aircraft floor panels |
| US7419031B2 (en) | 2005-11-04 | 2008-09-02 | The Boeing Company | Integrally damped composite aircraft floor panels |
| KR100868880B1 (en) * | 2007-01-29 | 2008-11-14 | 홍성산업 주식회사 | Panel for railroad car |
| JP2009241761A (en) * | 2008-03-31 | 2009-10-22 | Kinki Sharyo Co Ltd | Soundproofing method by panel for railway vehicle and soundproofing panel structure for railway vehicle used therefor |
| CZ304341B6 (en) * | 2013-02-13 | 2014-03-12 | Vysoká škola technická a ekonomická v Českých Budějovicích | Composite sandwich panel, especially panel for floors of means of conveyance |
| JP2019531512A (en) * | 2016-07-22 | 2019-10-31 | ザ ギル コーポレーション | Structure and formation method thereof |
| CN107815960A (en) * | 2017-11-01 | 2018-03-20 | 佛山科学技术学院 | A kind of pier anticollision system |
| CN110001791A (en) * | 2017-12-27 | 2019-07-12 | 铃木株式会社 | Plate built in ojosa and its manufacturing method |
| CN110001791B (en) * | 2017-12-27 | 2021-09-21 | 铃木株式会社 | Honeycomb structure built-in plate and method for manufacturing same |
| CN108656665A (en) * | 2018-06-29 | 2018-10-16 | 贵州大学 | A kind of lightweight high-intensity PVC honeycomb aluminum plates |
| JP2020152296A (en) * | 2019-03-22 | 2020-09-24 | トヨタ車体株式会社 | Vehicle floor raising member |
| JP2022535137A (en) * | 2019-06-07 | 2022-08-04 | エスエイチピーピー グローバル テクノロジーズ べスローテン フェンノートシャップ | Vehicle structure with honeycomb insert and its manufacture and use |
| US12077215B2 (en) | 2019-06-07 | 2024-09-03 | Shpp Global Technologies B.V. | Structural bodies for vehicles having honeycomb inserts and methods of making and using same |
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