JPS618122U - Honeycomb core reinforcement structure - Google Patents
Honeycomb core reinforcement structureInfo
- Publication number
- JPS618122U JPS618122U JP9030084U JP9030084U JPS618122U JP S618122 U JPS618122 U JP S618122U JP 9030084 U JP9030084 U JP 9030084U JP 9030084 U JP9030084 U JP 9030084U JP S618122 U JPS618122 U JP S618122U
- Authority
- JP
- Japan
- Prior art keywords
- honeycomb core
- appropriate
- reinforcement structure
- core reinforcement
- length
- 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.)
- Granted
Links
Landscapes
- Laminated Bodies (AREA)
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Abstract] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
第１図乃至第６図は本考案の実施例を示すもので、第１
図は第１の実施例の斜視図、．第２図乃至第５図はそれ
ぞれ他の実施例の斜視図、第６図ａ， ｂは補強板のそ
れぞれ他の実施例の斜視図、第７図は本考案の溝部の形
成工程を示す斜視説明図、第８図はハニカムコアの斜視
図、第９図は従来の大形整流板の斜視説明図、第１０図
は従来の散光板の取付状態を示す要部の断面説明図であ
る。
図中１はハニカムコア、２はセル、３は溝部、４は補強
板、５は取付部、６は斜視部、７は末展張状態のハニカ
ムコア、Ｗは展張方向、Ｌはリボン方向もある。Figures 1 to 6 show embodiments of the present invention.
The figure is a perspective view of the first embodiment. 2 to 5 are perspective views of other embodiments, FIGS. 6a and 6b are perspective views of other embodiments of the reinforcing plate, and FIG. 7 is a perspective view showing the groove forming process of the present invention. FIG. 8 is a perspective view of a honeycomb core, FIG. 9 is a perspective view of a conventional large rectifier plate, and FIG. 10 is a cross-sectional view of a main part of a conventional light diffuser plate showing how it is attached. In the figure, 1 is the honeycomb core, 2 is the cell, 3 is the groove, 4 is the reinforcing plate, 5 is the attachment part, 6 is the perspective part, 7 is the honeycomb core in the end tension state, W is the expansion direction, and L is the ribbon direction. .
Claims (1)
ムコアの展張方向に沿い展張力向全長に亙って形成され
た所定数の適宜深さを有する溝部における所定位置に、
適宜長さを有し、かつ、適宜幅に形成された帯状補強板
を嵌着してなることを特徴とするハニカムコアの補強構
造。At a predetermined position in a predetermined number of grooves having an appropriate depth formed along the entire length of the honeycomb core in the expansion tension direction at an appropriate position on one cell end surface of the honeycomb core,
A reinforcing structure for a honeycomb core, characterized in that it is formed by fitting a band-shaped reinforcing plate formed to have an appropriate length and an appropriate width.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9030084U JPS618122U (en) | 1984-06-19 | 1984-06-19 | Honeycomb core reinforcement structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9030084U JPS618122U (en) | 1984-06-19 | 1984-06-19 | Honeycomb core reinforcement structure |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS618122U true JPS618122U (en) | 1986-01-18 |
| JPH0239793Y2 JPH0239793Y2 (en) | 1990-10-24 |
Family
ID=30645167
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP9030084U Granted JPS618122U (en) | 1984-06-19 | 1984-06-19 | Honeycomb core reinforcement structure |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS618122U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2011517635A (en) * | 2008-03-12 | 2011-06-16 | エアバス オペラツィオンス ゲゼルシャフト ミット ベシュレンクテル ハフツング | Manufacturing method of integrated fiber composite parts |
| JP2014012467A (en) * | 2012-07-04 | 2014-01-23 | Japan Aircraft Mfg Co Ltd | Member for airplane |
-
1984
- 1984-06-19 JP JP9030084U patent/JPS618122U/en active Granted
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2011517635A (en) * | 2008-03-12 | 2011-06-16 | エアバス オペラツィオンス ゲゼルシャフト ミット ベシュレンクテル ハフツング | Manufacturing method of integrated fiber composite parts |
| JP2014012467A (en) * | 2012-07-04 | 2014-01-23 | Japan Aircraft Mfg Co Ltd | Member for airplane |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0239793Y2 (en) | 1990-10-24 |
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