JPH02101000U - - Google Patents
Info
- Publication number
- JPH02101000U JPH02101000U JP1020589U JP1020589U JPH02101000U JP H02101000 U JPH02101000 U JP H02101000U JP 1020589 U JP1020589 U JP 1020589U JP 1020589 U JP1020589 U JP 1020589U JP H02101000 U JPH02101000 U JP H02101000U
- Authority
- JP
- Japan
- Prior art keywords
- metal fitting
- holding device
- pressing
- receiving
- receiving metal
- 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
- 239000002184 metal Substances 0.000 claims description 8
- 230000006835 compression Effects 0.000 claims description 2
- 238000007906 compression Methods 0.000 claims description 2
- 239000002360 explosive Substances 0.000 description 1
Landscapes
- Clamps And Clips (AREA)
Description
第１図は本考案の保持装置の拡大縦断面図、第
２図は第１図の保持装置を適用した展開構造物の
保持構造の正面図、第３図は従来の保持装置のみ
を用いた展開構造物の保持構造の正面図、第４図
は従来の保持装置の一例の正面図、第５図は従来
の保持装置の他の例の縦断面図である。
１……宇宙航行体本体、２……展開構造物、３
……支持台、４……押圧金具、５……圧縮ばね、
６……係止ピン、７……受け金具、１０，１１…
…金具、１２……プーリ、１３……ワイヤ、１４
……爆発ボルト。
Fig. 1 is an enlarged vertical sectional view of the holding device of the present invention, Fig. 2 is a front view of the holding structure of a deployable structure to which the holding device of Fig. 1 is applied, and Fig. 3 is a view of the holding structure using only the conventional holding device. FIG. 4 is a front view of a holding structure for a deployable structure, FIG. 4 is a front view of an example of a conventional holding device, and FIG. 5 is a longitudinal sectional view of another example of a conventional holding device. 1... Spacecraft body, 2... Deployment structure, 3
...Support stand, 4...Press metal fitting, 5...Compression spring,
6... Locking pin, 7... Receiving metal fitting, 10, 11...
...Metal fitting, 12...Pulley, 13...Wire, 14
...Explosive bolt.
Claims (1)
ねにより突出方向に付勢された押圧金具と、この
金具に対向して展開構造物に設けられた受け金具
とを備え、前記押圧金具を圧縮ばね力により受け
金具に弾接可能に構成したことを特徴とする宇宙
展開構造物の保持装置。 It includes a pressing metal fitting that is biased in the protruding direction by a compression spring against a support base provided on the spacecraft main body, and a receiving metal fitting that is provided on the deployable structure opposite to this metal fitting, and the pressing metal fitting is compressed. A holding device for a space deployment structure, characterized in that it is configured to be able to come into elastic contact with a receiving metal fitting by a spring force.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1020589U JPH02101000U (en) | 1989-01-31 | 1989-01-31 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1020589U JPH02101000U (en) | 1989-01-31 | 1989-01-31 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH02101000U true JPH02101000U (en) | 1990-08-10 |
Family
ID=31217653
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP1020589U Pending JPH02101000U (en) | 1989-01-31 | 1989-01-31 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH02101000U (en) |
-
1989
- 1989-01-31 JP JP1020589U patent/JPH02101000U/ja active Pending