JP4285854B2 - Detonator - Google Patents
Detonator Download PDFInfo
- Publication number
- JP4285854B2 JP4285854B2 JP25826799A JP25826799A JP4285854B2 JP 4285854 B2 JP4285854 B2 JP 4285854B2 JP 25826799 A JP25826799 A JP 25826799A JP 25826799 A JP25826799 A JP 25826799A JP 4285854 B2 JP4285854 B2 JP 4285854B2
- Authority
- JP
- Japan
- Prior art keywords
- explosive
- optical fiber
- chamber
- ignition
- holder
- 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.)
- Expired - Lifetime
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B3/00—Blasting cartridges, i.e. case and explosive
- F42B3/10—Initiators therefor
- F42B3/113—Initiators therefor activated by optical means, e.g. laser, flashlight
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- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Laser Beam Processing (AREA)
- Feeding, Discharge, Calcimining, Fusing, And Gas-Generation Devices (AREA)
Description
【0001】
【発明が属する技術分野】
本発明は、例えば二段式軽ガス銃のような高速飛行体発射装置の初期駆動に用いられる火薬の起爆装置に関する。
【0002】
【従来技術】
この種高速飛行体発射装置の初期駆動には従来、高圧気体と共に火薬が用いられている。火薬の起爆装置としては、電気点火装置によって起爆薬を点火する点火玉が用いられ、一般の発破の初期点火には電気雷管がよく用いられる。
【0003】
【発明が解決しようとする課題】
瞬発電気雷管は、通電から着火するまでの着火遅れ時間が2〜3m秒で、バラ付きが大きい。着火遅れ時間のバラ付きが小さい高秒時精度電気雷管でも公差が±0.2m秒である。本発明の目的は、レーザ光を用いて起爆する高速飛行体発射装置の初期駆動に用いられる火薬の起爆装置において、レーザ光を通す光ファイバーの挿入口から発生するガス洩れを防止しようとするものである。
【0004】
【課題の解決手段】
請求項1記載の発明は、レーザ発生装置と、ホルダーに裸線で通されてホルダーとは接触面全体が接着剤にて固着され、レーザ発生装置で発生したレーザ光を火薬室に導入する光ファイバーとからなり、火薬室には無煙火薬が装薬されると共に、火薬室の前側に伝火薬を、更にその前に光ファイバーの先端に接する点火薬が配されることを特徴とする。
【0005】
本発明によると、レーザ照射から着火するまでの着火遅れ時間を数m秒、着火遅れ時間のバラ付きの公差を数十μ秒に抑えることができる。また本発明者らの実験によると、樹脂で被覆した光ファイバーを用い、ホルダーに通して光ファイバー挿入口の1か所を接着剤にて固定した状態で起爆したところ、火薬の量によっては光ファイバー挿入口からガス洩れを生ずることがあったが、本発明による場合、ガス洩れを生ずることがなかった。
【0006】
【発明の実施の形態】
図1は、高速飛翔体発射装置としての小型二段式軽ガス銃について示すもので、火薬室1と加速管2は厚さ0.5mmのステンレス製隔膜3で仕切ってある。この隔膜3の静的破断圧力は20MPa±15%である。火薬室1の前側部には、日本油脂株式会社製の無煙火薬4が3〜10g装薬され、その前側には、伝火薬としての黒色火薬5が0.5g、更にその前に点火薬として中国化薬株式会社製のアジ化銀ペレット6が10mg配されている。
【0007】
アジ化銀ペレット6は被覆樹脂を剥ぎ取ってホルダー7に取着された金属製のスリーブ8に通し、かつ該スリーブ8と接触面全体がグレースジャパン株式会社製の二液性の接着剤で固定した光ファイバーとしてのフジクラ株式会社製のグラスファイバー9(コア径0.6mm)の先端に接し、グラスファイバー9はトリガ信号を発生するハンディタイプの軽量のYAGレーザ発生装置(図示省略)に接続され、レーザ照射時の出力信号がデジタルストレンジスコープ(図示省略)で検出されるようになっている。
【0008】
火薬室1にはまた、圧力変換器10が取付けられ、起爆時における圧力の時間変化を測定できるようになっている。
【0009】
【実施例】
無煙火薬4を5g用い、YAGレーザ光(パルス幅7ns、エネルギー25mj)を用いて起爆させた。そしてレーザ照射時の出力信号をデジタルストレンジスコープで検出すると共に、火薬室内の圧力を圧力変換器11で測定した。そして同じ条件でこの実験を3回繰返して行った。このときの最高圧力は71.9±1.1MPaであった。またレーザ照射から着火するまでの時間(着火遅れ時間)t1、最高圧力に到達するまでの時間t2、着火が終了するまでの時間t3はそれぞれ、2835±47μ秒、3758±31μ秒、4648±121μ秒であった。
【0010】
図2にレーザ照射時の出力信号と火薬室内の圧力履歴を示す。同図に見られるように、本起爆方法によると、圧力履歴の再現性もよく、着火遅れ時間のバラ付きの公差も少なく、高精度の着火性能を有する。なお、上述の実験では3回共、光ファイバー挿入口からのガス洩れは目視では観察されなかった。
【0011】
因みにグラスファイバーを樹脂で被覆したままスリーブ8に通し、光ファイバー挿入口を上記と同じ接着剤を用いて固定した場合、無煙火薬4の量が5gを越えると、ガス洩れを生じた。
【0012】
【発明の効果】
請求項1記載の発明の高速飛行体発射装置の初期駆動用火薬の起爆装置によると、レーザ起爆により高精度のトリガ信号が得られ、着火遅れ時間のバラ付きも小さく、現象の光学可視化、圧力計測、速度計測等を効率よく簡単に行うことができ、また圧力履歴の再現性もよい。更に起爆させたときの点火部後方からのガス洩れを簡単な方法で防止することができ、爆発エネルギーを有効利用することができると共に、着火遅れ時間のバラ付きもより小さくでき、圧力履歴の再現性も向上する。
【図面の簡単な説明】
【図1】小型二段式ガス銃の要部の概略断面図。
【図2】レーザ照射時の出力信号と火薬室内の圧力履歴を示す図。
【符号の説明】
1・・火薬室
2・・加速管
3・・隔膜
4・・無煙火薬
5・・黒色火薬
6・・アジ化銀ペレット
7・・ホルダー
8・・スリーブ
9・・グラスファイバー
10・・圧力変換器[0001]
[Technical field to which the invention belongs]
The present invention relates to an explosive explosive device used for initial driving of a high-speed flying object launcher such as a two-stage light gas gun.
[0002]
[Prior art]
Conventionally, explosives are used together with high-pressure gas for the initial drive of this type of high-speed flying object launcher. As the explosive detonator, an ignition ball that ignites the explosive with an electric ignition device is used, and an electric detonator is often used for the initial ignition of general blasting.
[0003]
[Problems to be solved by the invention]
The instantaneous electric detonator has a large variation in ignition delay time of 2 to 3 milliseconds from energization to ignition. Even with high-second precision electric detonators with small variations in the ignition delay time, the tolerance is ± 0.2 ms. An object of the present invention is to prevent gas leakage generated from an insertion port of an optical fiber through which a laser beam passes in an explosive detonator used for initial driving of a high-speed flying object launching device that uses a laser beam to detonate. is there.
[0004]
[Means for solving problems]
According to the first aspect of the present invention, there is provided a laser generating device and an optical fiber which is passed through a holder with a bare wire, the entire contact surface of the holder is fixed with an adhesive, and a laser beam generated by the laser generating device is introduced into an explosive chamber. It is characterized by the fact that smokeless gunpowder is charged in the gunpowder chamber, a charge transfer agent is disposed on the front side of the gunpowder chamber, and an igniter in contact with the front end of the optical fiber is disposed in front of it.
[000 5 ]
According to the present invention, it is possible to suppress the ignition delay time from laser irradiation to ignition to several milliseconds and the tolerance of variation in the ignition delay time to several tens of microseconds. In addition , according to the experiments by the present inventors, when an optical fiber coated with resin was used, and the explosion was started in a state where one portion of the optical fiber insertion port was fixed with an adhesive through a holder, depending on the amount of explosive, the optical fiber insertion port However, in the case of the present invention, no gas leak occurred .
[000 6 ]
DETAILED DESCRIPTION OF THE INVENTION
FIG. 1 shows a small two-stage light gas gun as a high-speed projectile launching apparatus. An explosive chamber 1 and an acceleration tube 2 are separated by a stainless steel diaphragm 3 having a thickness of 0.5 mm. The static breaking pressure of the diaphragm 3 is 20 MPa ± 15%. The front side of the explosive chamber 1 is charged with 3 to 10 g of smokeless gunpowder 4 manufactured by Nippon Oil & Fats Co., Ltd. 10 mg of silver azide pellet 6 manufactured by Chuka Kayaku Co., Ltd. is provided.
[000 7 ]
The silver azide pellet 6 is peeled off from the coating resin and passed through a metal sleeve 8 attached to the
[000 8 ]
The explosive chamber 1 is also provided with a
[00 09 ]
【Example】
5 g of smokeless explosive 4 was used and detonated using YAG laser light (
[00 10 ]
FIG. 2 shows an output signal at the time of laser irradiation and a pressure history in the explosive chamber. As shown in the figure, according to this initiation method, the reproducibility of the pressure history is good, the tolerance of variation in the ignition delay time is small, and the ignition performance is highly accurate. In the above experiment, gas leakage from the optical fiber insertion port was not visually observed three times.
[001 1 ]
Incidentally, when the glass fiber was covered with resin and passed through the sleeve 8 and the optical fiber insertion port was fixed using the same adhesive as described above, gas leakage occurred when the amount of the smokeless gunpowder 4 exceeded 5 g.
[001 2 ]
【The invention's effect】
According to the explosive device for explosives for initial drive of the high-speed flying object launching device according to the first aspect of the invention, a highly accurate trigger signal can be obtained by laser initiation, the variation in ignition delay time is small, optical visualization of the phenomenon, pressure Measurement, speed measurement, etc. can be performed efficiently and easily, and the reproducibility of pressure history is also good. Further leakage gas from the igniter rear of the feeder and was detonated can be prevented in a simple manner, it is possible to effectively use the explosive energy, also smaller with roses ignition delay time, reproduction of the pressure history Also improves.
[Brief description of the drawings]
FIG. 1 is a schematic cross-sectional view of a main part of a small two-stage gas gun.
FIG. 2 is a diagram showing an output signal at the time of laser irradiation and a pressure history in the explosive chamber.
[Explanation of symbols]
1 .... explosive chamber 2 .... acceleration tube 3 .... diaphragm 4 ....
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP25826799A JP4285854B2 (en) | 1999-09-13 | 1999-09-13 | Detonator |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP25826799A JP4285854B2 (en) | 1999-09-13 | 1999-09-13 | Detonator |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2001082900A JP2001082900A (en) | 2001-03-30 |
JP4285854B2 true JP4285854B2 (en) | 2009-06-24 |
Family
ID=17317873
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP25826799A Expired - Lifetime JP4285854B2 (en) | 1999-09-13 | 1999-09-13 | Detonator |
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JP (1) | JP4285854B2 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2009008325A (en) * | 2007-06-28 | 2009-01-15 | Ihi Aerospace Co Ltd | Disposal method of explosive |
DE202009014949U1 (en) | 2009-01-26 | 2010-10-07 | Oao Znjj "Burevestnik" | Device for the ignition of the charge in the projectile chamber of a shellless artillery system |
KR101740620B1 (en) * | 2015-02-27 | 2017-05-26 | 부산대학교 산학협력단 | Nano Energetic Material Composites with Explosion via Optical Ignition and Method for fabricating the same |
KR101736410B1 (en) * | 2015-08-07 | 2017-05-16 | 부산대학교 산학협력단 | Method for controlling Door Breaching based on Remote Ignition and Explosion of Light Sensitized Material Composites via Low Power Laser Pointer Beam Irradiation |
-
1999
- 1999-09-13 JP JP25826799A patent/JP4285854B2/en not_active Expired - Lifetime
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Publication number | Publication date |
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JP2001082900A (en) | 2001-03-30 |
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