JPS63121300U - - Google Patents
Info
- Publication number
- JPS63121300U JPS63121300U JP1106287U JP1106287U JPS63121300U JP S63121300 U JPS63121300 U JP S63121300U JP 1106287 U JP1106287 U JP 1106287U JP 1106287 U JP1106287 U JP 1106287U JP S63121300 U JPS63121300 U JP S63121300U
- Authority
- JP
- Japan
- Prior art keywords
- igniter
- detonation
- initiator
- signal
- pressure gas
- 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
- 238000005474 detonation Methods 0.000 claims description 9
- 239000003999 initiator Substances 0.000 claims description 6
- 238000001514 detection method Methods 0.000 claims description 3
- 238000010586 diagram Methods 0.000 description 2
- 239000002360 explosive Substances 0.000 description 2
- 230000007274 generation of a signal involved in cell-cell signaling Effects 0.000 description 1
Landscapes
- Radar Systems Or Details Thereof (AREA)
Description
第１図は、この考案による機能ブロツク図、第
２図は従来の起爆装置の機能ブロツク図である。
図中１はラツチ回路、２はＡＮＤ回路、３は駆
動部、４は、距離検知装置、５は起爆信号発生部
、６はイニシエータ、７はセーフ／アーム切換部
、８はイグナイター、９は弾頭の炸薬、１０は、
起爆信号発生部、１１はイニシエータ、１２はセ
ーフ／アーム切換部、１３はイグナイター、１４
は弾頭の炸薬である。なお、図中同一あるいは相
当部分には同一符号を付して示してある。
FIG. 1 is a functional block diagram of this invention, and FIG. 2 is a functional block diagram of a conventional detonator. In the figure, 1 is a latch circuit, 2 is an AND circuit, 3 is a drive unit, 4 is a distance detection device, 5 is a detonation signal generator, 6 is an initiator, 7 is a safe/arm switching unit, 8 is an igniter, and 9 is a warhead. The explosive charge, 10, is
Detonation signal generation section, 11 is an initiator, 12 is a safe/arm switching section, 13 is an igniter, 14
is the explosive charge of the warhead. It should be noted that the same or corresponding parts in the drawings are designated by the same reference numerals.
Claims (1)
用パルスにより、起爆信号を出力する起爆信号発
生器と、上記起爆信号を印加することにより、点
火動作を行うイニシエータと、上記イニシエータ
で発生した高温高圧ガスにより、点火動作を行う
イグナイターと、一端を上記イニシエータと接合
し、他の一端を上記イグナイターに接合され、上
記高温高圧ガスを通す火路と、上記イニシエータ
とイグナイターの間に位置し、上記火路の開閉を
行う、セーフ／アーム切換部と、上記イグナイタ
ーで発生した高温高圧ガスにより爆発し、目標を
破壊する弾頭からなる飛しよう体において、発射
後、母機とミサイル間の距離が弾頭の有効範囲外
になると信号を出す距離検知装置、ミサイル発射
信号を保持しておく、ラツチ回路、上記ラツチ回
路の出力と、距離検知装置の出力が一致を判定す
るＡＮＤ回路、近接信管よりの起爆パルスにより
起爆信号を発生する起爆信号発生器を備えたこと
を特徴とする起爆装置。 A detonation signal generator that outputs a detonation signal using a detonation pulse from a guiding part of a flying object or a proximity fuse, an initiator that performs an ignition operation by applying the detonation signal, and a high temperature generated by the initiator. an igniter that performs an ignition operation using high-pressure gas; an igniter having one end connected to the initiator and the other end connected to the igniter and passing the high-temperature high-pressure gas; and a fire path located between the initiator and the igniter; In a flying vehicle consisting of a safe/arm switching section that opens and closes the fire path, and a warhead that explodes and destroys the target with high-temperature, high-pressure gas generated by the igniter, after launch, the distance between the mother aircraft and the missile is A distance detection device that issues a signal when it is out of the effective range, a latch circuit that holds the missile launch signal, an AND circuit that determines whether the output of the latch circuit and the output of the distance detection device match, and a detonation pulse from the proximity fuze. A detonator characterized by comprising a detonation signal generator that generates a detonation signal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1106287U JPS63121300U (en) | 1987-01-28 | 1987-01-28 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1106287U JPS63121300U (en) | 1987-01-28 | 1987-01-28 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS63121300U true JPS63121300U (en) | 1988-08-05 |
Family
ID=30797938
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP1106287U Pending JPS63121300U (en) | 1987-01-28 | 1987-01-28 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS63121300U (en) |
-
1987
- 1987-01-28 JP JP1106287U patent/JPS63121300U/ja active Pending
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| FI870876A (en) | SPRAENGKAPSEL. | |
| US3973499A (en) | Safe rocket motor igniter using sequenced initiation to an explosive logic network | |
| US3854401A (en) | Thermal ignition device | |
| GB1197347A (en) | A Fuze for an Explosive Device | |
| US9273939B2 (en) | Ignition system for scalable munitions system | |
| JPS58119095U (en) | secondary warhead released from the bullet | |
| US3968945A (en) | Shaped mini charge round | |
| ES8103369A1 (en) | Non-electric delay detonator and assembly of a detonating cord and a delay detonator. | |
| US4831932A (en) | Detonator | |
| JPS63121300U (en) | ||
| US3547033A (en) | Ignitor for explosive charge with means for preventing inadvertent ignition | |
| US3641938A (en) | Percussion or vibration fuse for explosive charge | |
| JP2921573B2 (en) | Pyrotechnic ignition device | |
| US4938141A (en) | Shock initiator device for initiating a percussion primer | |
| JPH03121400U (en) | ||
| US3306205A (en) | Fin stabilized projectile | |
| JPH0167500U (en) | ||
| CN214666412U (en) | Digital electronic detonator initiator with positioning function | |
| JPH0216158Y2 (en) | ||
| US4281600A (en) | Subprojectile to be expelled from a projectile | |
| US3688700A (en) | Ignition device for rocket motors | |
| JPH04198696A (en) | Liner for hollow cone charge warhead | |
| JPS6139300U (en) | detonator | |
| FR2368009A1 (en) | Time delay munitions fuse - has movable arming device actuated automatically on detonation of charge on input side | |
| JPS62228899A (en) | Triggering device |