JPS59143900U - Deployment structure - Google Patents
Deployment structureInfo
- Publication number
- JPS59143900U JPS59143900U JP3777383U JP3777383U JPS59143900U JP S59143900 U JPS59143900 U JP S59143900U JP 3777383 U JP3777383 U JP 3777383U JP 3777383 U JP3777383 U JP 3777383U JP S59143900 U JPS59143900 U JP S59143900U
- Authority
- JP
- Japan
- Prior art keywords
- basic structure
- trapezoidal
- flat plate
- hinge
- deployment structure
- 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
Landscapes
- Aerials With Secondary Devices (AREA)
- Details Of Aerials (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) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
第1図は従来の三角形平板を用いた展開型アンテナ反射
鏡を示す図、第2図はこの考案の一実施1 例の展開時
太陽電池パネルを示す図、第3図は第2図にて示される
太陽電池パネルの収納時を示す図である。図中1は展開
構造物の基本構造要素、 ・2、 5. 6はヒンジ
、3は衛星、4は伸展マスト、7は太陽電池パネル面を
示す。なお、図中間−或は相当部分には同一符号を付し
て示しである。Figure 1 is a diagram showing a conventional deployable antenna reflector using a triangular flat plate, Figure 2 is a diagram showing an example of the solar cell panel when deployed as an example of this invention, and Figure 3 is the same as in Figure 2. It is a figure which shows the time of the storage of the solar cell panel shown. In the figure, 1 is the basic structural element of the deployed structure; ・2, 5. 6 is a hinge, 3 is a satellite, 4 is an extension mast, and 7 is a solar panel surface. In addition, the same reference numerals are given to the middle part of the figure or corresponding parts.
Claims (1)
相パターンを形成するように上記台形平板相互間を回動
可能なヒンジで結合してなる基本構造体と、上記基本構
造体と衛星本体とを結合し、上記台形平板に展開力を与
える機構とを備え、基本構造体の使用前は上記台形平板
を上記ヒンジを介して折畳んだ状態で保持し、基本構造
体の使用時は上記機構の作用により上記台形平板全部を
展開するように構成したことを特徴とする展開構造物。A basic structure formed by connecting a plurality of trapezoidal plates with a rotatable hinge so as to form an auspicious pattern that is one of the axial compression modes of a cylinder, and the basic structure and a satellite. and a mechanism that applies an unfolding force to the trapezoidal flat plate, and holds the trapezoidal flat plate in a folded state via the hinge before using the basic structure, and when the basic structure is in use. A deployable structure characterized in that the entire trapezoidal plate is deployed by the action of the mechanism.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP3777383U JPS59143900U (en) | 1983-03-16 | 1983-03-16 | Deployment structure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP3777383U JPS59143900U (en) | 1983-03-16 | 1983-03-16 | Deployment structure |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS59143900U true JPS59143900U (en) | 1984-09-26 |
Family
ID=30168463
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP3777383U Pending JPS59143900U (en) | 1983-03-16 | 1983-03-16 | Deployment structure |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS59143900U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2001081821A1 (en) * | 2000-04-20 | 2001-11-01 | Taketoshi Nojima | Structure with folding lines, folding line forming mold, and folding line forming method |
-
1983
- 1983-03-16 JP JP3777383U patent/JPS59143900U/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2001081821A1 (en) * | 2000-04-20 | 2001-11-01 | Taketoshi Nojima | Structure with folding lines, folding line forming mold, and folding line forming method |
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