JPH09131817A - End face treating method for honeycomb panel - Google Patents

End face treating method for honeycomb panel

Info

Publication number
JPH09131817A
JPH09131817A JP29399295A JP29399295A JPH09131817A JP H09131817 A JPH09131817 A JP H09131817A JP 29399295 A JP29399295 A JP 29399295A JP 29399295 A JP29399295 A JP 29399295A JP H09131817 A JPH09131817 A JP H09131817A
Authority
JP
Japan
Prior art keywords
honeycomb panel
honeycomb
end surface
panel
surface material
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
Application number
JP29399295A
Other languages
Japanese (ja)
Inventor
Fumiaki Saku
文昭 佐久
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.)
Jamco Corp
Original Assignee
Jamco Corp
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 Jamco Corp filed Critical Jamco Corp
Priority to JP29399295A priority Critical patent/JPH09131817A/en
Publication of JPH09131817A publication Critical patent/JPH09131817A/en
Pending legal-status Critical Current

Links

Abstract

PROBLEM TO BE SOLVED: To provide a method for treating the end face of a honeycomb panel having a structure that surface materials are adhered to both the surfaces of a honeycomb member by utilizing the surface materials. SOLUTION: The honeycomb panel 1 has a structure that surface materials 20a, 20b are adhered to both the surfaces of a honeycomb member 10. The surface material is formed of a flexible material such as FRP or the like. The one material 20a is formed by extending from the end face of the panel to form an extended part 22a. The panel 1 is disposed on a flat table 100 with the material 20a disposed thereunder. The one end of the panel is stopped by an end plate 110, and the other end is pressed by a pressing plate 120 via a channel material 130. The part 22a is coated with hot-melt type adhesive 50, and adhered to the end face of the panel.

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】本発明はハニカムコア部材の
両面に表面材を貼着してつくられるハニカムパネルの端
面部の処理方法を提供するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention provides a method for treating an end face portion of a honeycomb panel, which is produced by attaching a surface material to both surfaces of a honeycomb core member.

【0002】[0002]

【従来の技術】ハニカム材を内部にサンドイッチしたハ
ニカムパネル材は、建築材等に普及しているが、特にプ
ラスチック複合材によるハニカムサンドイッチパネル
(以下、ハニカムパネルと称する)は、軽量でかつ高い
強度を持つ特性を利用して、航空機の床材、壁材、ギャ
レー、ラバトリーモジュール等の内装用材料をはじめと
して、操縦翼面、ドア、ダクト、フェアリング等の外装
用材料としても広く使用されている。
2. Description of the Related Art Honeycomb panel materials having a honeycomb material sandwiched therein are widely used in construction materials and the like. Especially, a honeycomb sandwich panel made of a plastic composite material (hereinafter referred to as a honeycomb panel) is lightweight and has high strength. It is widely used for interior materials such as aircraft flooring materials, wall materials, galleys, lavatory modules, etc., as well as exterior materials such as control surfaces, doors, ducts, fairings, etc. There is.

【0003】図17はハニカムパネルの一般的な構造を
示すもので、サンドイッチ材であるハニカムコア部材1
0の両面に表面材(スキンと称される)20a,20b
を接着し、必要に応じて表面材20a,20bの両方又
は片方の表面に化粧材30を張付けて最終製品としてい
る。ハニカムコア部材10は、紙、プラスチック、アル
ミニウム等の材料でつくられるが、航空機用の材料とし
ては、芳香属ポリアミド短繊維を紙状にしてフェノール
樹脂を含浸させてハニカム状に成形したコア部材が用い
られる。
FIG. 17 shows a general structure of a honeycomb panel, which is a honeycomb core member 1 which is a sandwich material.
Surface materials (referred to as skins) 20a, 20b on both sides of 0
Is adhered, and the decorative material 30 is attached to both or one of the surfaces of the surface materials 20a and 20b as required to obtain the final product. The honeycomb core member 10 is made of a material such as paper, plastic and aluminum. As a material for aircraft, a core member formed by forming aromatic polyamide short fibers into a paper shape and impregnating it with a phenol resin to form a honeycomb shape is used. Used.

【0004】表面材20a,20bは、板材、アルミニ
ウム等も用いられるが、航空機用の材料としては、ガラ
ス、アラミド、カーボン等の織物や単繊維にフェノール
やエポキシ樹脂を含浸させてシート状にしたプリプレグ
材が用いられている。プリプレグ材の表面材20a,2
0bは、熱硬化性の樹脂を含み、常温では可塑性を有す
る。そこで、ハニカムコア部材10の両面に表面材20
a,20bを積層し、可圧、加熱すると、表面材20
a,20bに含浸された樹脂が熱硬化してハニカムコア
部材と接着し、ハニカムパネル1が成形される。必要に
応じて、表面材の上面に化粧材30を接着フィルム等に
より張付けて最終製品とする。
As the surface materials 20a and 20b, plate materials, aluminum and the like are used, but as materials for aircraft, woven fabrics such as glass, aramid, carbon, etc. or single fibers are impregnated with phenol or epoxy resin to form a sheet. Prepreg material is used. Surface material 20a, 2 of prepreg material
0b contains a thermosetting resin and has plasticity at normal temperature. Therefore, the surface material 20 is provided on both surfaces of the honeycomb core member 10.
When a and 20b are laminated, and pressure and heat are applied, the surface material 20
The resin impregnated in a and 20b is thermoset and adheres to the honeycomb core member, and the honeycomb panel 1 is formed. If necessary, the decorative material 30 is attached to the upper surface of the surface material with an adhesive film or the like to obtain a final product.

【0005】図18は従来の端面処理方法の一例を示
し、ハニカムパネル1の端面70を平坦面に整形し、整
形部材であるチャンネル部材80の内面に接着剤82を
塗布してハニカムパネル1の端面を整形するものであ
る。チャンネル部材80は、例えばアルミ合金を枠状に
整形したものが利用できる。図19は従来の端面処理方
法の他の例を示し、端部のコアをとり除き、凹部74を
形成する。この凹部に接着剤82を充填し、硬化後に表
面84を研削加工等により整形し、所望の端面を得る。
FIG. 18 shows an example of a conventional end surface treatment method. The end surface 70 of the honeycomb panel 1 is shaped into a flat surface, and an adhesive 82 is applied to the inner surface of a channel member 80, which is a shaping member. The end face is shaped. As the channel member 80, for example, an aluminum alloy shaped like a frame can be used. FIG. 19 shows another example of the conventional end surface processing method, in which the core at the end is removed and the recess 74 is formed. The concave portion is filled with the adhesive 82, and after curing, the surface 84 is shaped by grinding or the like to obtain a desired end face.

【0006】[0006]

【発明が解決しようとする課題】上述した端面処理にあ
っては、整形部材(通常アルミニウムの整形)を必要と
し、この整形部材はハニカムパネルの厚さ寸法に応じて
専用の部材を用意する必要があるので、部品点数の増加
と軽量化の難しいところであり、加工工数を要してい
た。また、接着剤等を充填し、硬化後に表面を加工する
必要があった。本発明は以上の不具合を解消するハニカ
ムパネルの端面処理方法を提供するものである。
The above-mentioned end surface treatment requires a shaping member (usually aluminum shaping), and this shaping member requires a dedicated member prepared according to the thickness dimension of the honeycomb panel. Therefore, it is difficult to increase the number of parts and reduce the weight, which requires processing man-hours. Further, it is necessary to fill the surface with an adhesive or the like and process the surface after curing. The present invention provides a method for treating an end surface of a honeycomb panel, which solves the above problems.

【0007】[0007]

【課題を解決するための手段】本発明のハニカムパネル
の端面処理方法は、ハニカムパネルを構成する表面材を
端面から延長させ、この延長部に接着剤を塗布して端面
に接着させることを基本的な手段とする。そして、この
延長部を端面から更に突出させることで、他のハニカム
パネルと接合させて端面の処理を行うことができるもの
である。
A method for treating an end surface of a honeycomb panel according to the present invention is basically such that a surface material constituting a honeycomb panel is extended from an end surface, and an adhesive is applied to the extension portion to adhere to the end surface. As an effective means. Then, by further projecting this extension from the end face, the end face can be treated by being joined to another honeycomb panel.

【0008】[0008]

【発明の実施の形態】図1〜図4は、本発明のハニカム
パネルの端面処理方法の概要を示す説明図である。ハニ
カムパネル1は、ハニカムコア部材10の両面に表面材
20a,20bが接着された構造を有し、その一側の端
面70を処理対象とする。図2に示すように、一方の表
面材20aが端面70を覆うに足る長さだけ延長された
状態に加工する。この加工は、表面材20aをハニカム
コア部材10に接着する際に、予めその長さだけ表面材
20aの寸法を大きくとっておくことにより達成され
る。また、既製のハニカムパネルにあっては、ルーター
等の加工機械によって、反対側の表面材20bとハニカ
ムコア部材10を切削して所定の寸法だけ表面材20a
を延長させることができる。さらに、図4に示すよう
に、表面材22aに延長部24aを設けることもでき
る。
BEST MODE FOR CARRYING OUT THE INVENTION FIGS. 1 to 4 are explanatory views showing an outline of a method for treating an end surface of a honeycomb panel of the present invention. The honeycomb panel 1 has a structure in which the surface materials 20a and 20b are adhered to both surfaces of the honeycomb core member 10, and one end surface 70 of the honeycomb material is treated. As shown in FIG. 2, the one surface material 20 a is processed into a state in which it is extended by a length sufficient to cover the end surface 70. This processing is achieved by preliminarily increasing the dimension of the surface material 20a by the length when the surface material 20a is bonded to the honeycomb core member 10. In the case of a ready-made honeycomb panel, the surface material 20b and the honeycomb core member 10 on the opposite side are cut by a processing machine such as a router to cut the surface material 20a by a predetermined dimension.
Can be extended. Further, as shown in FIG. 4, the surface material 22a may be provided with an extension 24a.

【0009】図8〜図10は、この端面処理に使用する
装置の概要を示す説明図である。処理装置のテーブル1
00は、平坦な上面を有し、このテーブル100上に延
長された表面材20aがテーブル100に接するように
載置する。テーブルの一端部にはエンドプレート110
に対向して配設される押圧プレート120は、油圧ジャ
ッキ150等のアクチュエータによってテーブル100
上を移動する。押圧プレート120は、適宜のガイドレ
ール等によってエンドプレート110に対して平行を保
って案内される。押圧プレート120の前面は、アング
ル部材130が置かれる。
8 to 10 are explanatory views showing the outline of an apparatus used for this end face processing. Table 1 of processing equipment
00 has a flat upper surface, and the surface material 20 a extended on the table 100 is placed so as to be in contact with the table 100. One end of the table has an end plate 110
The pressing plate 120 disposed so as to face the table 100 is mounted on the table 100 by an actuator such as a hydraulic jack 150.
Move up. The pressing plate 120 is guided in parallel with the end plate 110 by an appropriate guide rail or the like. An angle member 130 is placed on the front surface of the pressing plate 120.

【0010】表面材20aの延長部22aとハニカムパ
ネル1の端面の間に熱可塑性(ホットメルトタイプ)の
接着剤50を塗布して、押圧プレート120を押し進め
る。アングル部材130は、表面材の延長部22aをハ
ニカムパネルの端面に押圧する。接着剤50が硬化する
と、延長部22aは、端面を覆った状態で固着される。
以上の処理によって、良好な外観をもつ端面を形成する
ことができる。端面のコーナー部25の曲率半径は、使
用するアングル部材130によって任意に選択すること
ができる。
A thermoplastic (hot melt type) adhesive 50 is applied between the extension 22a of the surface member 20a and the end face of the honeycomb panel 1, and the pressing plate 120 is pushed forward. The angle member 130 presses the extension portion 22a of the surface material against the end surface of the honeycomb panel. When the adhesive 50 hardens, the extension 22a is fixed while covering the end face.
By the above processing, an end face having a good appearance can be formed. The radius of curvature of the corner portion 25 of the end face can be arbitrarily selected depending on the angle member 130 used.

【0011】図5,図6は、以上の手段によって端面処
理を施した薄いハニカムコア部材12を有する第2のハ
ニカムパネル2を用いて、厚いハニカムコア部材10を
有する第1のハニカムパネル1の端面70を処理する手
段を示す。第1のハニカムパネル1の端面70に対して
接着剤で固着された第2のハニカムパネル2は第1のハ
ニカムパネル1の縁部に突出部を形成することとなる。
そこで、図7に示すように、このハニカムパネルでつく
られたパネル製品5は、中央部5aが低い表面を有す
る。そこで、このパネル製品5は、ドアパネルや間仕切
り用のパネルとすることで、エッジ部が軽量で剛性の高
い枠の機能を備え、利用価値が高い製品を得ることがで
きる。
FIGS. 5 and 6 show a first honeycomb panel 1 having a thick honeycomb core member 10 by using the second honeycomb panel 2 having the thin honeycomb core member 12 end-face-treated by the above means. A means for treating the end face 70 is shown. The second honeycomb panel 2 fixed to the end surface 70 of the first honeycomb panel 1 with an adhesive forms a protruding portion at the edge of the first honeycomb panel 1.
Therefore, as shown in FIG. 7, the panel product 5 made of this honeycomb panel has a low central portion 5a. Therefore, by using this panel product 5 as a door panel or a panel for partitioning, it is possible to obtain a product having a high utility value, which has a frame function with a light edge portion and high rigidity.

【0012】図13、図14は、表面延長部24aを有
するハニカムパネル1cと、端面を未処理しないハニカ
ムパネル1とを突き合わせて、コーナー部を加工する実
施例を示す。突き合せ面にホットメルトタイプ又は通常
の接着剤50を塗布し、適宜の治具で両者を保持するこ
とで、コーナー部を形成するとともに端面処理すること
ができる。
13 and 14 show an embodiment in which a honeycomb panel 1c having a surface extension 24a and a honeycomb panel 1 whose end face is not treated are butted against each other to process a corner portion. By applying a hot-melt type or normal adhesive 50 to the abutting surfaces and holding the both with an appropriate jig, it is possible to form a corner portion and perform edge treatment.

【0013】図15、図16は、表面材の延長部を有さ
ない端面処理を施したハニカムパネル1Aと、一方の表
面材に延長部26aを加工したハニカムパネル1Dを用
意し、突き合せ面に接着剤50を塗布して、コーナー部
を構成するものである。コーナー部の外側は、2枚の表
面材が重合される構造となり、剛性はより高くなる。
FIGS. 15 and 16 show a honeycomb panel 1A having an end surface treatment having no extension of the surface material and a honeycomb panel 1D having one surface material processed with the extension portion 26a. The adhesive 50 is applied to the above to form the corner portion. The outside of the corner portion has a structure in which two surface materials are polymerized, and the rigidity becomes higher.

【0014】図11は、直尺のハニカムパネル200の
一方の表面材200bを直線状の端面202から延長す
る延長部210bを設け、この延長部210bが成形ロ
ーラ310,320,330を通過する間に、連続して
端部を覆うように折り曲げ加工する方法を示す。第1の
成形ローラ310の近傍において、折り曲げ部にホット
メルトタイプの接着剤50を適下して塗布する。長尺の
ハニカムパネル200は、上面を押圧ロール340で押
圧して、浮き上がりを防止する。
In FIG. 11, an extension 210b is provided to extend one surface material 200b of the straight honeycomb panel 200 from the straight end surface 202, and while the extension 210b passes through the forming rollers 310, 320, 330. Shows a method of continuously bending so as to cover the end portion. In the vicinity of the first molding roller 310, a hot-melt type adhesive 50 is appropriately applied and applied to the bent portion. The long honeycomb panel 200 presses the upper surface with the pressing roll 340 to prevent the floating.

【0015】図15は、端面222が曲率を有するハニ
カムパネル220の端面を表面材で覆う場合の処理方法
を示す。表面材220bは端面222から一定の長さ突
出する延長部230bを有し、この延長部230bを成
形ロール310,32,330で順次折り曲げて端部を
覆う。第1の成形ロール310の近傍において、ホット
メルトタイプの接着剤50を適下、塗布することは、先
の実施例と同様である。端面222が常時成形ロール側
に押しつけられるようにハニカムパネル220を移動さ
せることで、曲率をもつ端面の処理を達成する。
FIG. 15 shows a processing method when the end surface of the honeycomb panel 220 having an end surface 222 having a curvature is covered with a surface material. The surface material 220b has an extension portion 230b protruding from the end surface 222 by a certain length, and the extension portion 230b is sequentially bent by the forming rolls 310, 32, 330 to cover the end portion. Applying the hot-melt type adhesive 50 appropriately in the vicinity of the first molding roll 310 is the same as in the previous embodiment. By moving the honeycomb panel 220 such that the end surface 222 is always pressed against the forming roll, the treatment of the end surface having a curvature is achieved.

【0016】[0016]

【発明の効果】本発明は以上のように、ハニカムコア部
材の両面に表面材を接着してつくられたハニカムパネル
の端面を表面材の延長部を折り曲げて覆うとともに、ホ
ットメルトタイプの接着剤で接合して端面処理を行なう
もので、端面の整形部材を用いることなく、外観に優
れ、かつ剛性の高い端面処理を施すことができる。
As described above, according to the present invention, an end face of a honeycomb panel formed by adhering a surface material to both surfaces of a honeycomb core member is covered by bending an extension portion of the surface material, and a hot-melt type adhesive agent. Since the end surface treatment is performed by joining with, the end surface treatment having excellent appearance and high rigidity can be performed without using a shaping member for the end surface.

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

【図1】本発明を適用するハニカムパネルの側面図。FIG. 1 is a side view of a honeycomb panel to which the present invention is applied.

【図2】本発明により端面処理されたハニカムパネルの
一実施例を示す側面図。
[Fig. 2] Fig. 2 is a side view showing an embodiment of a honeycomb panel subjected to an end surface treatment according to the present invention.

【図3】本発明により端面処理されたハニカムパネルの
他の実施例を示す側面図。
[Fig. 3] Fig. 3 is a side view showing another embodiment of the honeycomb panel end-face-treated according to the present invention.

【図4】本発明により端面処理されたハニカムパネルの
更に他の実施例を示す側面図。
FIG. 4 is a side view showing still another embodiment of the honeycomb panel having the end surface treated according to the present invention.

【図5】2枚のハニカムパネルを用いて端面処理する実
施例を示す側面図。
FIG. 5 is a side view showing an embodiment in which an end face treatment is performed using two honeycomb panels.

【図6】2枚のハニカムパネルを用いて端面処理する実
施例を示す側面図。
FIG. 6 is a side view showing an embodiment in which the end face treatment is performed using two honeycomb panels.

【図7】本発明の端面処理によりつくられたパネルの斜
視図。
FIG. 7 is a perspective view of a panel made by the edge treatment of the present invention.

【図8】本発明に使用する装置の一実施例を示す斜視
図。
FIG. 8 is a perspective view showing an embodiment of an apparatus used in the present invention.

【図9】本発明に使用する装置の一実施例を示す断面
図。
FIG. 9 is a sectional view showing an embodiment of the apparatus used in the present invention.

【図10】本発明に使用する装置の一実施例を示す断面
図。
FIG. 10 is a sectional view showing an embodiment of the apparatus used in the present invention.

【図11】本発明に使用する装置の他の実施例を示す斜
視図。
FIG. 11 is a perspective view showing another embodiment of the device used in the present invention.

【図12】本発明に使用する装置の更に他の実施例を示
す斜視図。
FIG. 12 is a perspective view showing still another embodiment of the apparatus used in the present invention.

【図13】2枚のハニカムパネルを用いて端面を処理す
る実施例を示す側面図。
FIG. 13 is a side view showing an example in which an end face is processed by using two honeycomb panels.

【図14】2枚のハニカムパネルを用いて端面を処理す
る実施例を示す側面図。
[Fig. 14] Fig. 14 is a side view showing an example in which an end face is processed by using two honeycomb panels.

【図15】2枚のハニカムパネルを用いて端面を処理す
る他の実施例を示す側面図。
FIG. 15 is a side view showing another embodiment in which the end face is treated by using two honeycomb panels.

【図16】2枚のハニカムパネルを用いて端面を処理す
る他の実施例を示す側面図。
FIG. 16 is a side view showing another embodiment in which the end face is treated by using two honeycomb panels.

【図17】ハニカムパネルの一般的な構造を示す斜視
図。
FIG. 17 is a perspective view showing a general structure of a honeycomb panel.

【図18】従来のハニカムパネルの端面処理に示す側面
図。
FIG. 18 is a side view showing an end surface treatment of a conventional honeycomb panel.

【図19】従来のハニカムパネルの端面処理に示す側面
図。
FIG. 19 is a side view showing an end surface treatment of a conventional honeycomb panel.

【符号の説明】[Explanation of symbols]

1,2 ハニカムパネル 5 製品 10,12 ハニカムコア部材 20a,20b 表面材 22a,24a 延長部 25 コーナー部 50 熱可塑性接着剤 70 端面 100 テーブル 110 エンドプレート 120 押圧プレート 130 アングル部材 310,320,330 成形ロール 340 押圧ロール 1, 2 Honeycomb panel 5 Product 10, 12 Honeycomb core member 20a, 20b Surface material 22a, 24a Extension part 25 Corner part 50 Thermoplastic adhesive 70 End surface 100 Table 110 End plate 120 Pressing plate 130 Angle member 310, 320, 330 Forming Roll 340 Press roll

Claims (7)

【特許請求の範囲】[Claims] 【請求項1】 ハニカムコア部材と、ハニカムコア部材
のコア開口部の両面に接着される表面材とを有するハニ
カムパネルの端面処理方法において、 ハニカムパネルの第1の表面材を端面から延長する延長
部を加工する工程と、 表面材の延長部とハニカムパネルの間に熱可塑性の接着
剤を塗布する工程と、 表面材の延長部をハニカムパネルの端面に押圧して接着
する工程と、 を備えるハニカムパネルの端面処理方法。
1. A method for treating an end surface of a honeycomb panel having a honeycomb core member and a surface material adhered to both surfaces of a core opening of the honeycomb core member, the extension comprising extending a first surface material of the honeycomb panel from the end surface. And a step of applying a thermoplastic adhesive between the extension portion of the surface material and the honeycomb panel, and a step of pressing and adhering the extension portion of the surface material to the end surface of the honeycomb panel. A method for treating an end surface of a honeycomb panel.
【請求項2】 ハニカムパネルの第1の表面材に形成さ
れる延長部は、ハニカムパネルの端面を覆うとともに第
2の表面材から突出する寸法を有する請求項1記載のハ
ニカムパネルの端面処理方法。
2. The method for treating an end surface of a honeycomb panel according to claim 1, wherein the extension portion formed on the first surface material of the honeycomb panel has a dimension that covers the end surface of the honeycomb panel and projects from the second surface material. .
【請求項3】 ハニカムコア部材と、ハニカムコア部材
のコア開口部の両面に接着される表面材とを有するハニ
カムパネルの端面処理方法において、 第1のハニカムパネルの端部に、表面材の延長部を有す
る第2のハニカムパネルを重ねる工程と、 第2のハニカムパネルの表面材の延長部と第1のハニカ
ムパネルの端面との間に熱可塑性の接着剤を塗布する工
程と、 第2のハニカムパネルの表面材の延長部を第1のハニカ
ムパネルの端面に押圧して接着する工程と、 を備えるハニカムパネルの端面処理方法。
3. A method for treating an end surface of a honeycomb panel having a honeycomb core member and a surface material adhered to both surfaces of a core opening of the honeycomb core member, wherein the surface material is extended to an end portion of the first honeycomb panel. Stacking a second honeycomb panel having a portion, applying a thermoplastic adhesive between the extension of the surface material of the second honeycomb panel and the end surface of the first honeycomb panel, And a step of adhering the extended portion of the surface material of the honeycomb panel to the end surface of the first honeycomb panel by adhering the same to the end surface of the first honeycomb panel.
【請求項4】 ハニカムコア部材と、ハニカムコア部材
のコア開口部の両面に接着される表面材とを有するハニ
カムパネルの端面処理方法において、 第1のハニカムパネルの端部に表面材の延長部を有する
第2のハニカムパネルを直交して配置する工程と、 第1のハニカムパネルと第2のハニカムパネルの接触部
に熱可塑性の接着剤を塗布する工程と、 第1のハニカムパネルと第2のハニカムパネルを押圧し
て接着する工程と、 を備えるハニカムパネルの端面処理方法。
4. A method for treating an end surface of a honeycomb panel having a honeycomb core member and a surface material adhered to both surfaces of a core opening of the honeycomb core member, wherein an extension portion of the surface material is provided at an end portion of the first honeycomb panel. Arranging the second honeycomb panel having the above at right angles, applying a thermoplastic adhesive to the contact portion between the first honeycomb panel and the second honeycomb panel, and the first honeycomb panel and the second honeycomb panel And a step of adhering the honeycomb panel by pressing the honeycomb panel.
【請求項5】 ハニカムコア部材と、ハニカムコア部材
のコア開口部の両面に接着される表面材とを有するハニ
カムパネルの端面処理方法において、 端面から延長する表面材の延長部を有する長尺のハニカ
ムパネルを用意する工程と、 ハニカムパネルを連続的に搬送する間に表面材の延長部
を複数のロールによって順次ハニカムパネルの端面に向
けて折り曲げる工程と、 表面材の折り曲げ部とハニカムパネルの端面の間に熱可
塑性の接着剤を塗布する工程と、 表面材の折り曲げ部をハニカムパネルの端面に押圧して
接着する工程と、 を備えるハニカムパネルの端面処理方法。
5. A method for treating an end surface of a honeycomb panel having a honeycomb core member and a surface material adhered to both surfaces of a core opening of the honeycomb core member, the method comprising a long member having an extension portion of the surface material extending from the end surface. The step of preparing the honeycomb panel, the step of sequentially bending the extension part of the surface material toward the end surface of the honeycomb panel by a plurality of rolls while continuously conveying the honeycomb panel, and the bending part of the surface material and the end surface of the honeycomb panel. A method for treating an end face of a honeycomb panel, which comprises: applying a thermoplastic adhesive between the two; and pressing the bent portion of the surface material to the end face of the honeycomb panel to adhere it.
【請求項6】 ハニカムパネルの端面が直線である請求
項5記載のハニカムパネルの端面処理方法。
6. The method for treating an end surface of a honeycomb panel according to claim 5, wherein the end surface of the honeycomb panel is a straight line.
【請求項7】 ハニカムパネルの端面が曲線である請求
項5記載のハニカムパネルの端面処理方法。
7. The method for treating an end surface of a honeycomb panel according to claim 5, wherein the end surface of the honeycomb panel is a curved line.
JP29399295A 1995-11-13 1995-11-13 End face treating method for honeycomb panel Pending JPH09131817A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP29399295A JPH09131817A (en) 1995-11-13 1995-11-13 End face treating method for honeycomb panel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP29399295A JPH09131817A (en) 1995-11-13 1995-11-13 End face treating method for honeycomb panel

Publications (1)

Publication Number Publication Date
JPH09131817A true JPH09131817A (en) 1997-05-20

Family

ID=17801848

Family Applications (1)

Application Number Title Priority Date Filing Date
JP29399295A Pending JPH09131817A (en) 1995-11-13 1995-11-13 End face treating method for honeycomb panel

Country Status (1)

Country Link
JP (1) JPH09131817A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011523588A (en) * 2008-05-23 2011-08-18 ノードソン コーポレーション Method and apparatus for processing the surrounding area of a sandwich part
WO2014097619A1 (en) * 2012-12-19 2014-06-26 横浜ゴム株式会社 Joining structure for interior panel for aeroplane
JP2017518902A (en) * 2014-05-28 2017-07-13 ザ・ボーイング・カンパニーThe Boeing Company Sandwich panel joint and method for joining sandwich panels

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011523588A (en) * 2008-05-23 2011-08-18 ノードソン コーポレーション Method and apparatus for processing the surrounding area of a sandwich part
WO2014097619A1 (en) * 2012-12-19 2014-06-26 横浜ゴム株式会社 Joining structure for interior panel for aeroplane
JP2014118091A (en) * 2012-12-19 2014-06-30 Yokohama Rubber Co Ltd:The Connecting structure of aircraft interior panel
US9440726B2 (en) 2012-12-19 2016-09-13 The Yokohama Rubber Co., Ltd. Joining structure for interior panel for aircraft
JP2017518902A (en) * 2014-05-28 2017-07-13 ザ・ボーイング・カンパニーThe Boeing Company Sandwich panel joint and method for joining sandwich panels

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