JPS5940200U - Decoupling device for core rocket and auxiliary booster rocket - Google Patents
Decoupling device for core rocket and auxiliary booster rocketInfo
- Publication number
- JPS5940200U JPS5940200U JP13654282U JP13654282U JPS5940200U JP S5940200 U JPS5940200 U JP S5940200U JP 13654282 U JP13654282 U JP 13654282U JP 13654282 U JP13654282 U JP 13654282U JP S5940200 U JPS5940200 U JP S5940200U
- Authority
- JP
- Japan
- Prior art keywords
- rocket
- locking
- ball
- bracket
- ball receiving
- 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
- Compressors, Vaccum Pumps And Other Relevant Systems (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図は従来のコアロケットと補助ブースタロケットと
の分離機構を示す説明図、第2図は来者、案の一実施例
を示す一部切欠した分解斜視図、第3図は第2図に示す
部材の組付状態を示す横断面図、第4図は第2図に示す
部材の組付状態を示す縦断面図、第5図はブラケツF−
10と連結用部材20との結合解除状態を示す断面説明
図である。
1・・・・・・コアロケット、2・・・・・・補助ブー
スタロケット、3・・・・・・スラストチューブ、4・
・・・・・前側ブレーズ、5・・・・・・後側ブレーズ
、10・・・・・・ブラケット、11・・・・・・基板
、12.13・・・・・・突片、12a。
13a・・・・・・ボール受孔、20・・・・・・連結
用部材、21・・・・・・段付シリンダ部、21a・・
・・・・小径シリンダ部、21b・・・・・・大径シリ
ンダ部、22・・・・・・ボール収容孔、23a、 2
3b・・・・・・拘止用ボール、24・・・・・・ピス
トン部材、25・・・・・・ガス発生器支持部、25a
・・・・・・ガス噴出口、27・・・・・・ガス発生器
、28・・・・・・シェアビン、30・・・・・・ロッ
ド、31・・・・・・エア抜き孔、32・・・・・・ガ
ス送入室。Figure 1 is an explanatory diagram showing a conventional separation mechanism between a core rocket and an auxiliary booster rocket, Figure 2 is a partially cutaway exploded perspective view showing an embodiment of the visitor's plan, and Figure 3 is 4 is a longitudinal sectional view showing the assembled state of the members shown in FIG. 2, FIG. 5 is a vertical sectional view showing the assembled state of the members shown in FIG.
10 is an explanatory cross-sectional view showing a state in which the coupling member 10 and the coupling member 20 are released. FIG. 1...Core rocket, 2...Auxiliary booster rocket, 3...Thrust tube, 4.
...Front blaze, 5...Rear blaze, 10...Bracket, 11...Platform, 12.13...Protrusion piece, 12a . 13a...Ball receiving hole, 20...Connecting member, 21...Stepped cylinder part, 21a...
...Small diameter cylinder part, 21b...Large diameter cylinder part, 22...Ball accommodation hole, 23a, 2
3b...Retaining ball, 24...Piston member, 25...Gas generator support part, 25a
......Gas outlet, 27...Gas generator, 28...Share bin, 30...Rod, 31...Air vent hole, 32... Gas supply chamber.
Claims (1)
2つの突片間に形成される凹部内に開口したボール受部
を上記各突片に形成したブラケットと、シリンダ構造を
有し、一端部が補助ブースタロケットに連結される一方
、他端部が上記凹部内に嵌挿されると共に、上記ボール
受部に両端が近接して開口するボール収容孔を有する連
結用部材と、上記ボール収容孔内から上記ブラケットの
ボール受部に一部を突出してブラケットと連結用部すと
を連結する係止位置乃びこの係止位置から後退して連結
を解除する解除位置の間を移動可能にボール収容孔内に
配置した2個の拘止用ボールと、上記連結用部材のシリ
ンダ内に配置され、上゛ 記2個の拘止用ボールの間に
押入って各拘止用ボールを上記係止位置に押圧支持する
ピストン部材と、上記連結用部材に付設され、作動時に
シリンダ内にガスを送入して、各拘止用ボールの係止位
置への押圧支持を解除する方向に上記ピストン部材を移
動させるガス発生器とを有するこ、とを特徴とするコア
ロケットと補助ブースタロケットとの結合解除装置。A bracket consisting of two protruding pieces protruding from the core rocket, each of the protruding pieces having a ball receiving part opened in a recess formed between the two protruding pieces, and a cylinder structure, one end of which is formed. is connected to the auxiliary booster rocket, and the other end thereof is fitted into the recess, and the connecting member has a ball receiving hole with both ends opening close to the ball receiving portion; A ball housing is movable between a locking position where a part of the bracket protrudes from the ball receiving part of the bracket to connect the bracket and the connecting part, and a release position where the connection is released by retreating from the locking position. Two restraining balls arranged in the hole and a cylinder of the connecting member, which is inserted between the two restraining balls and locking each of the restraining balls as described above. a piston member that presses and supports each locking ball in a locking position; and a piston member attached to the connecting member that feeds gas into the cylinder during operation to release the locking ball from the locking position. and a gas generator for moving the core rocket and the auxiliary booster rocket.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP13654282U JPS5940200U (en) | 1982-09-10 | 1982-09-10 | Decoupling device for core rocket and auxiliary booster rocket |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP13654282U JPS5940200U (en) | 1982-09-10 | 1982-09-10 | Decoupling device for core rocket and auxiliary booster rocket |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS5940200U true JPS5940200U (en) | 1984-03-14 |
Family
ID=30306973
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP13654282U Pending JPS5940200U (en) | 1982-09-10 | 1982-09-10 | Decoupling device for core rocket and auxiliary booster rocket |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS5940200U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0655605A (en) * | 1991-03-08 | 1994-03-01 | Elf Atochem Sa | Extruder device for coating at least two core materials with material of the same kind and coating method |
KR100315260B1 (en) * | 1999-08-19 | 2001-11-26 | 신용구 | Automatic separating apparatus using difference of pressure |
-
1982
- 1982-09-10 JP JP13654282U patent/JPS5940200U/en active Pending
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0655605A (en) * | 1991-03-08 | 1994-03-01 | Elf Atochem Sa | Extruder device for coating at least two core materials with material of the same kind and coating method |
KR100315260B1 (en) * | 1999-08-19 | 2001-11-26 | 신용구 | Automatic separating apparatus using difference of pressure |
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