JPH02115800U - - Google Patents
Info
- Publication number
- JPH02115800U JPH02115800U JP2581989U JP2581989U JPH02115800U JP H02115800 U JPH02115800 U JP H02115800U JP 2581989 U JP2581989 U JP 2581989U JP 2581989 U JP2581989 U JP 2581989U JP H02115800 U JPH02115800 U JP H02115800U
- Authority
- JP
- Japan
- Prior art keywords
- rocket motor
- flight
- groove
- flying object
- coupling device
- 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
- 230000008878 coupling Effects 0.000 claims description 5
- 238000010168 coupling process Methods 0.000 claims description 5
- 238000005859 coupling reaction Methods 0.000 claims description 5
- 238000002347 injection Methods 0.000 claims description 4
- 239000007924 injection Substances 0.000 claims description 4
- 229910000831 Steel Inorganic materials 0.000 claims description 2
- 239000010959 steel Substances 0.000 claims description 2
- 238000010586 diagram Methods 0.000 description 2
Landscapes
- Toys (AREA)
Description
第１図はこの考案の一実施例を示す飛翔体の射
出用ロケツトモータ結合装置の概略構成図、第２
図および第３図は従来技術とその問題点を説明す
るために示す図である。
１１……飛翔体、１２……射出用ロケツトモー
タ、１３……発射筒、１５……飛翔用ロケツトモ
ータ、１６……溝、１７……鋼球、１８……スプ
リング。
Fig. 1 is a schematic configuration diagram of a rocket motor coupling device for ejecting a flying object, showing one embodiment of this invention;
3 and 3 are diagrams shown to explain the prior art and its problems. 11... Flying object, 12... Rocket motor for injection, 13... Launch tube, 15... Rocket motor for flight, 16... Groove, 17... Steel ball, 18... Spring.
Claims (1)
ロケツトモータを結合する飛翔体の射出用ロケツ
トモータ結合装置において、 前記飛翔用ロケツトモータには、前記射出用ロ
ケツトモータとの結合部の外周に溝が形成され、 前記射出用ロケツトモータには、前記飛翔用ロ
ケツトモータが装着される装着部の、前記飛翔用
ロケツトモータと前記溝と対向する位置に、その
内部方向に付勢力を与えるスプリングが取付けら
れ、 前記射出用ロケツトモータの前記スプリングと
前記飛翔用ロケツトモータの前記溝との間に鋼球
を介在させた状態で、前記飛翔用ロケツトモータ
と前記射出用ロケツトモータとを結合するように
したことを特徴とする飛翔体の射出用ロケツトモ
ータ結合装置。[Scope of Claim for Utility Model Registration] In a rocket motor coupling device for a flying object, which couples a rocket motor for ejection to a flying object equipped with a rocket motor for flight, the rocket motor for flight has a structure in which the rocket motor for flight is connected to the rocket motor for ejection. A groove is formed on the outer periphery of the coupling part, and the injection rocket motor is provided with a groove in the mounting part to which the flight rocket motor is mounted, at a position facing the flight rocket motor and the groove. The flight rocket motor and the injection rocket motor are connected to each other in a state where a spring for applying force is attached and a steel ball is interposed between the spring of the injection rocket motor and the groove of the flight rocket motor. 1. A rocket motor coupling device for ejecting a flying object, characterized in that the rocket motor coupling device is adapted to couple the following.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2581989U JPH02115800U (en) | 1989-03-07 | 1989-03-07 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2581989U JPH02115800U (en) | 1989-03-07 | 1989-03-07 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH02115800U true JPH02115800U (en) | 1990-09-17 |
Family
ID=31246890
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2581989U Pending JPH02115800U (en) | 1989-03-07 | 1989-03-07 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH02115800U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2011052951A (en) * | 2009-09-03 | 2011-03-17 | Res Inst Of Natl Defence | Ejection and separation device for portable guided missile |
-
1989
- 1989-03-07 JP JP2581989U patent/JPH02115800U/ja active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2011052951A (en) * | 2009-09-03 | 2011-03-17 | Res Inst Of Natl Defence | Ejection and separation device for portable guided missile |
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