JP4285854B2 - Detonator - Google Patents

Detonator Download PDF

Info

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
Application number
JP25826799A
Other languages
Japanese (ja)
Other versions
JP2001082900A (en
Inventor
和喜 高山
伸生 永易
信武 大坪
Original Assignee
中国化薬株式会社
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by 中国化薬株式会社 filed Critical 中国化薬株式会社
Priority to JP25826799A priority Critical patent/JP4285854B2/en
Publication of JP2001082900A publication Critical patent/JP2001082900A/en
Application granted granted Critical
Publication of JP4285854B2 publication Critical patent/JP4285854B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B3/00Blasting cartridges, i.e. case and explosive
    • F42B3/10Initiators therefor
    • F42B3/113Initiators therefor activated by optical means, e.g. laser, flashlight

Landscapes

  • 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。
【000
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
【000
【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。
【000
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。
【000
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。
【001
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。
【001
【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 holder 7, and the sleeve 8 and the entire contact surface are fixed with a two-component adhesive made by Grace Japan Co., Ltd. The glass fiber 9 is in contact with the tip of a glass fiber 9 (core diameter 0.6 mm) manufactured by Fujikura Corporation as an optical fiber, and is connected to a handy type lightweight YAG laser generator (not shown) that generates a trigger signal. An output signal at the time of laser irradiation is detected by a digital strange scope (not shown).
[000 8 ]
The explosive chamber 1 is also provided with a pressure transducer 10 so that the time change of pressure at the time of detonation can be measured.
[00 09 ]
【Example】
5 g of smokeless explosive 4 was used and detonated using YAG laser light (pulse width 7 ns, energy 25 mj). And the output signal at the time of laser irradiation was detected with the digital strange scope, and the pressure in the gunpowder chamber was measured with the pressure transducer 11. This experiment was repeated three times under the same conditions. The maximum pressure at this time was 71.9 ± 1.1 MPa. Also, the time from laser irradiation to ignition (ignition delay time) t 1 , the time t 2 until reaching the maximum pressure, and the time t 3 until the ignition ends are 2835 ± 47 μsec, 3758 ± 31 μsec, It was 4648 ± 121 μsec.
[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 .... smokeless powder 5 .... black powder 6 .... silver azide pellet 7 .... holder 8 ... sleeve 9 ... glass fiber 10 ... pressure transducer

Claims (1)

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であって、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火薬の起爆装置。An explosive explosive device used for the initial drive of a high-speed flying object launcher. The laser generator is passed through the holder with a bare wire, and the entire contact surface of the holder is fixed with an adhesive. the laser beam generated Ri Do from an optical fiber for introducing the explosive chamber, with the explosive chamber smokeless powder is charge, the transfer charge in front of the explosive chamber, ignition charge further contact with the tip of the optical fiber in front Gunpowder detonator characterized by being arranged .
JP25826799A 1999-09-13 1999-09-13 Detonator Expired - Lifetime JP4285854B2 (en)

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

Country Status (1)

Country Link
JP (1) JP4285854B2 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
JP2001082900A (en) 2001-03-30

Similar Documents

Publication Publication Date Title
US4957027A (en) Versatile nonelectric dearmer
US3724383A (en) Lasser stimulated ordnance initiation device
US6272996B1 (en) In-line initiator and firing device assembly
US4892037A (en) Self consumable initiator
US5415105A (en) Tandem warhead with piezoelectric percussion fuses
US4606272A (en) Initiation delay system for warheads with tandem mounted shaped charges
CN109631678B (en) Method for reducing laser initiation energy
US5107766A (en) Follow-thru grenade for military operations in urban terrain (MOUT)
US7752972B1 (en) Low reaction rate, high blast shaped charge waveshaper
US4126955A (en) High velocity tapered bore gun and ammunition
US4930421A (en) Partitioned, fluid supported, high efficiency traveling charge for hyper-velocity guns
US5092243A (en) Propellant pressure-initiated piezoelectric power supply for an impact-delay projectile base-mounted fuze assembly
US2592623A (en) Primer assembly for artillery ammunition
JP4285854B2 (en) Detonator
US4726295A (en) Grenade arrangement for screening cloud
USH1214H (en) Multiple point laser detonation system for explosive charges
US4714022A (en) Warhead with tandem shaped charges
FI112702B (en) DDT-type laser lighter
US6269747B1 (en) Training rocket for smoke development
JP2921573B2 (en) Pyrotechnic ignition device
US6202560B1 (en) Explosively started projectile gun ammunition
US5000094A (en) Shotgun cartridge with explosive shell
US6279480B1 (en) Firing pin assembly for a warhead detonator
RU2408833C1 (en) Ignition method of powder charge onboard moving missile train and device for its realisation
US5044282A (en) Tapered disc and jacketed explosive device for projecting high velocity metal jets

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20060616

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20080925

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20081014

A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20081215

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20090317

A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20090324

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20120403

Year of fee payment: 3

R150 Certificate of patent or registration of utility model

Free format text: JAPANESE INTERMEDIATE CODE: R150

Ref document number: 4285854

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20120403

Year of fee payment: 3

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20150403

Year of fee payment: 6

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

EXPY Cancellation because of completion of term