JPS60165700U - Fuse safety device for flying bodies - Google Patents
Fuse safety device for flying bodiesInfo
- Publication number
- JPS60165700U JPS60165700U JP5219584U JP5219584U JPS60165700U JP S60165700 U JPS60165700 U JP S60165700U JP 5219584 U JP5219584 U JP 5219584U JP 5219584 U JP5219584 U JP 5219584U JP S60165700 U JPS60165700 U JP S60165700U
- Authority
- JP
- Japan
- Prior art keywords
- piston
- diaphragm
- chamber
- safety device
- fuse safety
- 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
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) [Abstract] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
第１図、第２図及び第３図は従来の飛しよう体用信管安
全装置を示す図、第４図はこの考案の飛しよう体の信管
安全装置の概略構成要素図である。
図において、６はチャンバー、７はダイヤフラム、８，
９は室、１０は推進剤、１１は燃焼室、１２は遅延フィ
ルタ、１３はピストンシリンダ、１４はピ不トン、１５
は切換スイッチ部、１６はピストン軸、１７はバネであ
る。1, 2, and 3 are views showing conventional fuse safety devices for flying objects, and FIG. 4 is a schematic diagram of the components of the fuse safety device for flying objects according to the present invention. In the figure, 6 is a chamber, 7 is a diaphragm, 8,
9 is a chamber, 10 is a propellant, 11 is a combustion chamber, 12 is a delay filter, 13 is a piston cylinder, 14 is a piston, 15
16 is a piston shaft, and 17 is a spring.
Claims (1)
を燃焼室に連通させ、かつ他室をピストンシリンダに連
通ずると共に、前記ビス下ンシリンダにダイヤフラム側
へ付勢されるピストンと、このピストンに連接するピス
トン軸を介し、前記ダイヤフラムとピストンとの間に遅
延フィルタを配設し、前記ピストン軸の端部と接触する
一位置に切換スイッチ部を配し、燃焼ガスの圧力により
、前記ダイヤフラムを駆動させると共に、前記ダイヤフ
ラムの動作に応じて前記ピストンが動作し、このピスト
ンと連接するピストン軸が前記切換スイッチ部を駆動さ
せることによって解除命令を発生することを特徴とする
飛しよう体用信管安全装置。One chamber of the chamber divided into two chambers by the diaphragm is communicated with the combustion chamber, and the other chamber is communicated with the piston cylinder, and the piston is urged toward the diaphragm side by the screw-under cylinder, and the piston is connected to the piston. A delay filter is disposed between the diaphragm and the piston via the piston shaft, a changeover switch is disposed at a position in contact with an end of the piston shaft, and the diaphragm is driven by the pressure of the combustion gas. The fuse safety device for a flying object is characterized in that the piston operates in response to the operation of the diaphragm, and a piston shaft connected to the piston generates a release command by driving the changeover switch section.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP5219584U JPS60165700U (en) | 1984-04-10 | 1984-04-10 | Fuse safety device for flying bodies |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP5219584U JPS60165700U (en) | 1984-04-10 | 1984-04-10 | Fuse safety device for flying bodies |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS60165700U true JPS60165700U (en) | 1985-11-02 |
Family
ID=30571931
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP5219584U Pending JPS60165700U (en) | 1984-04-10 | 1984-04-10 | Fuse safety device for flying bodies |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS60165700U (en) |
-
1984
- 1984-04-10 JP JP5219584U patent/JPS60165700U/en active Pending
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