JPS6334015B2 - - Google Patents
Info
- Publication number
- JPS6334015B2 JPS6334015B2 JP1660182A JP1660182A JPS6334015B2 JP S6334015 B2 JPS6334015 B2 JP S6334015B2 JP 1660182 A JP1660182 A JP 1660182A JP 1660182 A JP1660182 A JP 1660182A JP S6334015 B2 JPS6334015 B2 JP S6334015B2
- Authority
- JP
- Japan
- Prior art keywords
- honeycomb
- blocks
- shape
- honeycomb core
- curved surface
- 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
Links
- 238000004519 manufacturing process Methods 0.000 claims description 5
- 239000000463 material Substances 0.000 claims description 5
- 238000000034 method Methods 0.000 claims description 4
- 239000011162 core material Substances 0.000 claims 1
- 239000004576 sand Substances 0.000 claims 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 5
- 229910052782 aluminium Inorganic materials 0.000 description 5
- 238000005452 bending Methods 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 102000055510 ATP Binding Cassette Transporter 1 Human genes 0.000 description 1
- 108700005241 ATP Binding Cassette Transporter 1 Proteins 0.000 description 1
- 101100161481 Homo sapiens ABCA1 gene Proteins 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
Landscapes
- Laminated Bodies (AREA)
- Aerials With Secondary Devices (AREA)
Description
【発明の詳細な説明】
この発明は表皮材とハニカムコアにより曲面形
状をしたサンドイツチパネルの製造法に関し、特
に容易な方法で寸法精度が高く、かつ剛性の大き
なパネルを製作することを目的としたものであ
る。[Detailed Description of the Invention] The present invention relates to a method for manufacturing a sandwich panel having a curved surface using a skin material and a honeycomb core, and an object of the present invention is to manufacture a panel with high dimensional accuracy and high rigidity using a particularly easy method. This is what I did.
従来の方法は、ハニカムコアをロールにより曲
げたり小さな帯状に裁断し、それを並べて曲面の
パネルを製造していた。このためハニカムコアの
厚さが大きくなるとハニカムコアが座屈したり切
れたりし、曲面に曲げることが困難になるためハ
ニカムコアをより小さな形状に裁断し組み合わせ
て製造しなければならなかつた。このためハニカ
ムコアの継ぎ目が多くなり、ハニカムコア間にす
き間が生じ強度的な問題を生じたり規定の寸法精
度が得られなかつたりする等の欠点があつた。 Conventional methods involve bending honeycomb cores with rolls or cutting them into small strips, which are then lined up to produce curved panels. For this reason, when the thickness of the honeycomb core becomes large, the honeycomb core buckles or breaks, making it difficult to bend into a curved surface, so the honeycomb core has to be cut into smaller shapes and assembled. For this reason, there are many seams between the honeycomb cores, and gaps are created between the honeycomb cores, resulting in problems in terms of strength and failure to obtain specified dimensional accuracy.
この発明はこれらの欠点を解決しようとするも
のであり、その実施例を図面によつて詳細に説明
する。 The present invention aims to solve these drawbacks, and embodiments thereof will be described in detail with reference to the drawings.
第1図はシート状のアルミハニカムコアを六角
形の形状に裁断し、そのハニカムコアの片面に格
子状の切り込み3を入れたアルミハニカムブロツ
ク1の斜視図である。なお、第1図ではハニカム
ブロツク1の中の詳細なハニカム形状は省略して
示してある。 FIG. 1 is a perspective view of an aluminum honeycomb block 1 in which a sheet-like aluminum honeycomb core is cut into a hexagonal shape and grid-like cuts 3 are made on one side of the honeycomb core. In FIG. 1, the detailed honeycomb shape of the honeycomb block 1 is omitted.
第2図は格子状の切り込みを入れたアルミハニ
カムブロツク1を多数個並べ両面にCERP等から
なる表皮材2を接着し、曲面構造となしたサンド
イツチパネルの断面図である。 FIG. 2 is a cross-sectional view of a sandwich panel in which a large number of aluminum honeycomb blocks 1 having lattice-like cuts are arranged and a skin material 2 made of CERP or the like is adhered to both sides to form a curved structure.
アルミハニカムコアをこのような形状のブロツ
クに製作するためには、従来の機械加工によるも
のより放電加工により製作すれば寸法精度がすぐ
れ均一な形状なものが容易に得られ、しかも外周
切り込み加工を同時に行うことができる。 In order to manufacture aluminum honeycomb cores into blocks with this shape, it is easier to produce blocks with excellent dimensional accuracy and uniform shapes by using electric discharge machining rather than conventional machining. Can be done at the same time.
曲面の形状および必要な設計条件によりアルミ
ハニカムコアの厚さを定め、それにより切り込み
の間隔および深さを適当な寸法に選びハニカムコ
アを曲げることにより厚いハニカムコアでも容易
に曲面になじますことができる。 The thickness of the aluminum honeycomb core is determined based on the shape of the curved surface and the necessary design conditions, and by selecting the appropriate cut interval and depth and bending the honeycomb core, even thick honeycomb cores can easily conform to the curved surface. can.
なお、ハニカムブロツクの形状は三角形でも四
角形でもよいが、結合部が一直線にならないこと
から六角形が強度的にすぐれている。 The shape of the honeycomb block may be either triangular or square, but a hexagonal shape is superior in terms of strength because the joints are not in a straight line.
このような方法により製作されたサンドイツチ
構造のパネルは鏡面精度がすぐれしかも軽く剛性
の大きなものが得られる等の効果を有する。した
がつて、大形のアンテナ等に適用可能である。 A panel having a sanderch structure manufactured by such a method has the advantage of having excellent mirror surface precision, being lightweight, and having high rigidity. Therefore, it is applicable to large antennas, etc.
第1図および第2図はこの発明の実施例を示
し、第1図は格子状の切り込みを入れたハニカム
ブロツクの概略斜視図、第2図は格子状の切り込
みを入れたハニカムブロツクを多数個並べ両面に
表皮材を接着し製作した曲面サンドイツチパネル
の断面図である。
図中の符号1はハニカムブロツク、2は表皮
材、3は切込みである。なお図中同一あるいは相
当部分には同一符号を示してある。
1 and 2 show an embodiment of the present invention, FIG. 1 is a schematic perspective view of a honeycomb block with lattice-shaped cuts, and FIG. 2 shows a honeycomb block with many lattice-shaped cuts. FIG. 2 is a cross-sectional view of a curved sanderch panel manufactured by arranging and bonding skin materials to both sides. In the figure, numeral 1 is a honeycomb block, 2 is a skin material, and 3 is a notch. Note that the same or corresponding parts in the figures are denoted by the same reference numerals.
Claims (1)
断し、そのハニカムブロツクに格子状の切り込み
を入れたものを多数個並べ、それに表皮材を接着
し曲面を構成することを特徴とするハニカムサン
ドイツチパネルの製造法。 2 ハニカムブロツクの形状を六角形としたこと
を特徴とする特許請求の範囲第1項記載のハニカ
ムサンドイツチパネルの製造法。[Claims] 1. A honeycomb core material is cut into blocks of a certain shape, a large number of the honeycomb blocks are lined up with grid-like cuts, and a skin material is adhered to the blocks to form a curved surface. A manufacturing method for honeycomb sand germanchi panels. 2. The method for manufacturing a honeycomb sanderboard panel according to claim 1, wherein the honeycomb block has a hexagonal shape.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1660182A JPS58134736A (en) | 1982-02-04 | 1982-02-04 | Manufacture of honeycomb sandwich panel |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1660182A JPS58134736A (en) | 1982-02-04 | 1982-02-04 | Manufacture of honeycomb sandwich panel |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS58134736A JPS58134736A (en) | 1983-08-11 |
JPS6334015B2 true JPS6334015B2 (en) | 1988-07-07 |
Family
ID=11920810
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP1660182A Granted JPS58134736A (en) | 1982-02-04 | 1982-02-04 | Manufacture of honeycomb sandwich panel |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS58134736A (en) |
-
1982
- 1982-02-04 JP JP1660182A patent/JPS58134736A/en active Granted
Also Published As
Publication number | Publication date |
---|---|
JPS58134736A (en) | 1983-08-11 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CA2359924C (en) | Noise reduction sandwich panel, notably for aircraft turbojet engine | |
US5894045A (en) | Cellular core structure building component | |
US5262220A (en) | High strength structure assembly and method of making the same | |
EP0491277B1 (en) | A honeycomb member and a honeycomb | |
GB2182703A (en) | Improvements relating to structural sandwich sheet material comprising two face sheets and two core sheets | |
US3881338A (en) | Method of bending a metal sheet and a corner produced thereby | |
US3093370A (en) | Workholder with means for thermal compensation | |
JPS6334015B2 (en) | ||
US4020542A (en) | Sandwich panel fabrication | |
JP2000301365A (en) | Production of structural body and structural body | |
US3205109A (en) | Method of making a honeycomb type structure | |
JPS6326683B2 (en) | ||
JP3010925B2 (en) | Brazed laminated panel and method of manufacturing the same | |
US3635070A (en) | Method of working cellular material | |
JPH067866A (en) | Honeycomb panel | |
JP2579503B2 (en) | Honeycomb core | |
GB2153408A (en) | Foam boards | |
JP2001205526A (en) | Method of honeycomb core cutting and fixture for honeycomb core cutting | |
US3563840A (en) | Honeycomb having equal shear strength properties | |
JPH06316012A (en) | Honeycomb panel | |
JPS5917948B2 (en) | Manufacturing method of honeycomb sand germanchi panel | |
JPH02136408A (en) | Manufacturing of resonator type soundproof panel | |
JP2000141350A (en) | Production of alc corner panel | |
JPH06246855A (en) | Rigid board | |
JPH0882024A (en) | Bed panel and manufacture thereof |