JPH03122000U - - Google Patents
Info
- Publication number
- JPH03122000U JPH03122000U JP3205990U JP3205990U JPH03122000U JP H03122000 U JPH03122000 U JP H03122000U JP 3205990 U JP3205990 U JP 3205990U JP 3205990 U JP3205990 U JP 3205990U JP H03122000 U JPH03122000 U JP H03122000U
- Authority
- JP
- Japan
- Prior art keywords
- panel
- frame structure
- reinforced composite
- equipment mounting
- thin plates
- 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
- 239000003733 fiber-reinforced composite Substances 0.000 claims 4
- 229910000838 Al alloy Inorganic materials 0.000 claims 2
- 239000011162 core material Substances 0.000 claims 2
- 239000000463 material Substances 0.000 claims 2
- 230000003014 reinforcing effect Effects 0.000 claims 2
- 238000010586 diagram Methods 0.000 description 4
- 210000002615 epidermis Anatomy 0.000 description 2
- 238000009434 installation Methods 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
Landscapes
- Support Of Aerials (AREA)
Description
第１図はこの考案の機器搭載パネルの構成図、
第２図は第１図に示すものの断面図、第３図は骨
組構造体に取り付けられた状態を示す図、第４図
〜第６図はこの考案の他の実施例を示す図、第７
図及び第８図は従来の機器搭載パネルの図、第７
図は構成図、第８図は骨組構造体に取り付けられ
た状態を示す図である。
図において、１は表皮、２はハニカムコア、３
は端部補強部材、４は機器取付ネジ穴、５はパネ
ル固定用ボルト穴、６は縦フレーム、７は横フレ
ーム、８は継手、９はパネル固定ボルト、１０は
搭載機器、１１は機器取付ボルト、１２はパネル
結合継手、１３は単板パネルである。なお、図中
、同一あるいは相当部分には同一符号を付してあ
る。
Figure 1 is a configuration diagram of the device mounting panel of this invention.
FIG. 2 is a sectional view of what is shown in FIG. 1, FIG. 3 is a view showing the state in which it is attached to a frame structure, FIGS. 4 to 6 are views showing other embodiments of this invention, and FIG.
Figures 7 and 8 are diagrams of conventional equipment mounting panels.
The figure is a configuration diagram, and FIG. 8 is a diagram showing a state where it is attached to a frame structure. In the figure, 1 is the epidermis, 2 is the honeycomb core, and 3 is the epidermis.
is the end reinforcement member, 4 is the device mounting screw hole, 5 is the panel fixing bolt hole, 6 is the vertical frame, 7 is the horizontal frame, 8 is the joint, 9 is the panel fixing bolt, 10 is the installed equipment, 11 is the equipment installation Bolts, 12 are panel joints, and 13 is a single panel. In addition, in the drawings, the same or corresponding parts are given the same reference numerals.
Claims (1)
置される機器搭載パネルにおいて、アルミニウム
合金薄板あるいは繊維強化複合材薄板で形成され
たパネルと繊維強化複合材で形成され、かつ上記
パネル周辺の両面に接着固定されると共に上記パ
ネルが骨組構造体に取付けられた際にはその骨組
構造体の荷重経路として作用する中央部には厚み
を増した薄肉三角形断面をもつ端部補強部材とで
構成したことを特徴とする人工衛星用の機器搭載
パネル。 (2) 人工衛星搭載用のアンテナタワーなどに設
置される機器搭載パネルにおいて、心材にはハニ
カムコアを使用し、両面の表皮にはアルミニウム
合金薄板あるいは繊維強化複合材薄板を使用して
形成されたハニカムサンドウイツチパネルと、繊
維強化複合材から成り上記パネル周辺の両面に接
着固定されると共にパネルが骨組構造体に取付け
られた際にはその骨組構造体の荷重経路として作
用する中央部には厚みを増した薄肉三角形断面を
もつ端部補強部材とで構成したことを特徴とする
人工衛星用の機器搭載パネル。[Scope of Claim for Utility Model Registration] (1) In equipment mounting panels installed on antenna towers for use in satellites, panels formed of aluminum alloy thin plates or fiber reinforced composite thin plates and fiber reinforced composite materials. , and an edge having a thin triangular cross section with increased thickness in the center part which is adhesively fixed to both sides around the panel and acts as a load path for the frame structure when the panel is attached to the frame structure. An equipment mounting panel for an artificial satellite, characterized by comprising a reinforcing member. (2) For equipment mounting panels installed on satellite antenna towers, etc., honeycomb core is used as the core material, and aluminum alloy thin plates or fiber reinforced composite thin plates are used for the skins on both sides. It consists of a honeycomb sandwich panel and a fiber-reinforced composite material, which is adhesively fixed on both sides around the panel and has a thickness in the center that acts as a load path for the frame structure when the panel is attached to the frame structure. 1. An equipment mounting panel for an artificial satellite, characterized by comprising an end reinforcing member having a thin triangular cross section with increased thickness.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3205990U JPH03122000U (en) | 1990-03-28 | 1990-03-28 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP3205990U JPH03122000U (en) | 1990-03-28 | 1990-03-28 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH03122000U true JPH03122000U (en) | 1991-12-12 |
Family
ID=31534911
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP3205990U Pending JPH03122000U (en) | 1990-03-28 | 1990-03-28 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH03122000U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2010502516A (en) * | 2006-09-12 | 2010-01-28 | ジーケイエヌ エアロスペース サービシイズ リミテッド | Rib post |
-
1990
- 1990-03-28 JP JP3205990U patent/JPH03122000U/ja active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2010502516A (en) * | 2006-09-12 | 2010-01-28 | ジーケイエヌ エアロスペース サービシイズ リミテッド | Rib post |
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