JPH01106399U - - Google Patents
Info
- Publication number
- JPH01106399U JPH01106399U JP88788U JP88788U JPH01106399U JP H01106399 U JPH01106399 U JP H01106399U JP 88788 U JP88788 U JP 88788U JP 88788 U JP88788 U JP 88788U JP H01106399 U JPH01106399 U JP H01106399U
- Authority
- JP
- Japan
- Prior art keywords
- equipment mounting
- reinforced composite
- thin sheets
- fiber
- core
- 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
- 239000011162 core material Substances 0.000 claims 2
- 239000003733 fiber-reinforced composite Substances 0.000 claims 2
- 229910000838 Al alloy Inorganic materials 0.000 claims 1
- 239000000463 material Substances 0.000 claims 1
- 230000003014 reinforcing effect Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 5
- 210000002615 epidermis Anatomy 0.000 description 2
- 230000002787 reinforcement Effects 0.000 description 1
Landscapes
- Laminated Bodies (AREA)
- Support Of Aerials (AREA)
Description
第1図、第2図及び第3図は一実施例であり、
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
構造体に設置された状態を示す図。第4図及び第
5図は従来の機器搭載パネルの図であり、第4図
は構成図、第5図は骨組構造体に設置された状態
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は簡易継手、5は機器取付ネ
ジ穴、6はパネル固定用ボルト穴、7は縦フレー
ム、8は横フレーム、9は継手、10はパネル固
定ボルト、11は搭載機器、12は機器取付ボル
ト、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。
FIG. 1, FIG. 2, and FIG. 3 are one example,
FIG. 1 is a configuration diagram of the equipment mounting panel of this invention, FIG. 2 is a sectional view of the device shown in FIG. 1, and FIG. 3 is a diagram showing the state installed on a frame structure. 4 and 5 are diagrams of a conventional equipment mounting panel, with FIG. 4 being a configuration diagram and FIG. 5 being a diagram showing the state installed on a frame structure. In the figure, 1 is the epidermis, 2 is the honeycomb core, and 3 is the epidermis.
is an end reinforcement member, 4 is a simple joint, 5 is a device mounting screw hole, 6 is a panel fixing bolt hole, 7 is a vertical frame, 8 is a horizontal frame, 9 is a joint, 10 is a panel fixing bolt, 11 is installed equipment , 12 is a device mounting bolt, and 13 is a single panel. Note that the same or corresponding parts in the figures are given the same reference numerals.
Claims (1)
れる機器搭載パネルにおいて、心材にハニカムコ
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成形し
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、中央部には厚みを増したI型断面
形状を有する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。 For equipment mounting panels installed on satellite antenna towers, etc., we use honeycomb sandwich panels, which are formed using a honeycomb core for the core material and aluminum alloy thin sheets or fiber reinforced composite thin sheets for the skins on both sides. An equipment mounting panel for an artificial satellite, comprising a fiber-reinforced composite material and an end reinforcing member having a thickened I-shaped cross section in the center.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP88788U JPH01106399U (en) | 1988-01-08 | 1988-01-08 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP88788U JPH01106399U (en) | 1988-01-08 | 1988-01-08 |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH01106399U true JPH01106399U (en) | 1989-07-18 |
Family
ID=31200294
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP88788U Pending JPH01106399U (en) | 1988-01-08 | 1988-01-08 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH01106399U (en) |
-
1988
- 1988-01-08 JP JP88788U patent/JPH01106399U/ja active Pending
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