CN105652123A - Testing method of pulse ignition voltage of electric explosive device - Google Patents

Testing method of pulse ignition voltage of electric explosive device Download PDF

Info

Publication number
CN105652123A
CN105652123A CN201610090870.1A CN201610090870A CN105652123A CN 105652123 A CN105652123 A CN 105652123A CN 201610090870 A CN201610090870 A CN 201610090870A CN 105652123 A CN105652123 A CN 105652123A
Authority
CN
China
Prior art keywords
tested
electric spark
type electric
pulse
spark workpiece
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
Application number
CN201610090870.1A
Other languages
Chinese (zh)
Inventor
张高强
徐剑
易水华
李贺
蔡仕存
吴乐
梅欢
张睿纯
谢强
郑宏海
高欣
徐玮
万蒋亮
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Jiangxi Hongdu Aviation Industry Group Co Ltd
Original Assignee
Jiangxi Hongdu Aviation Industry Group Co Ltd
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 Jiangxi Hongdu Aviation Industry Group Co Ltd filed Critical Jiangxi Hongdu Aviation Industry Group Co Ltd
Priority to CN201610090870.1A priority Critical patent/CN105652123A/en
Publication of CN105652123A publication Critical patent/CN105652123A/en
Pending legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01RMEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R31/00Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Testing Electric Properties And Detecting Electric Faults (AREA)

Abstract

The invention provides a testing method of pulse ignition voltage of an electric explosive device. According to the testing method, an output positive electrode of a direct-current stabilized voltage power supply is connected with an input end of a solid relay; an output end of the solid relay is connected with one end of a pulse ignition type electric explosive device to be tested; a triggering end of the solid relay is connected with a DO (Defense Order) interface of an industrial control computer; the other end of the pulse ignition type electric explosive device to be tested is connected with an output negative electrode of the direct-current stabilized voltage power supply; the industrial control computer is internally provided with a pulse width testing procedure, and a high-speed on/off control signal is transmitted to the triggering end of the solid relay through programming the pulse width testing procedure, so that ignition voltage can be provided for the pulse ignition type electric explosive device to be tested; the pulse width testing procedure has good commonality, and only can carry out corresponding setting on pulse width according to different pulse width requirements on the ignition voltage of the pulse ignition type electric explosive device to be tested, so that related testing verification work can be carried out; and the electric explosive device can be repeatedly used, is low in cost and has a long-term use value.

Description

A kind of method of testing of electric spark workpiece impulse ignition voltage
Technical field
The present invention relates to electric spark workpiece pulse firing technical field of measurement and test, particularly relate to the method for testing of a kind of electric spark workpiece impulse ignition voltage.
Background technology
Priming system is equipped with gunpowder or explosive, is stimulated after-combustion or blast by the less energy in the external world, for the gunpowder that ignites, ignition charge, do the predetermined functions such as mechanic once to the general name of the element used or device; It is detonate and igniting most sensitive originate the energy, the starting property of its function and susceptible determine its status in the system of weapon and effect, as the most sensitive part in armament systems, its safety, reliability directly affect the safety and reliability of armament systems.
The optimization design needs developed rapidly with aircraft electric power system along with priming system firing technique; aircraft subsystem has been selected pulse firing type electric spark workpiece quite a lot; and the priming system of the type is higher to the width requirement of firing pulse; pulse width is less be easily caused this type of pulse firing type electric spark workpiece can not normal ignition; and then reduce the reliability of pulse firing type electric spark workpiece work; pulse width is bigger than normal, crosses long-time energising, increase ignition circuit short-circuit risks further after the fusing that is easily caused in firing circuit current limiting safeguard resistor.
Therefore, this type of electric spark workpiece pulse firing performance must be carried out test checking, at present, conventional solution be buy a fast response time, artificial mains that control accuracy is high, utilize the voltage pulse output that its program control host setting needs, then carry out verification experimental verification; This scheme is feasible (its control accuracy can only control at more than 1ms) to a certain extent, but it is in the input excessive (such as the price of chrysanthemum water artificial mains PCR4000LA mono-is about 300,000 RMB) of early stage.
Summary of the invention
Technical problem solved by the invention is in that to provide the method for testing of a kind of electric spark workpiece impulse ignition voltage, to solve the shortcoming in above-mentioned background technology.
Technical problem solved by the invention realizes by the following technical solutions:
A kind of method of testing of electric spark workpiece impulse ignition voltage, including D.C. regulated power supply, solid-state relay, industrial control computer and pulse firing type electric spark workpiece to be tested, wherein, D.C. regulated power supply output cathode is connected with solid-state relay input, solid-state relay outfan is connected with pulse firing type electric spark workpiece one end to be tested, solid-state relay triggers end and is connected with the DO interface of industrial control computer, and the pulse firing type electric spark workpiece other end to be tested is connected with the negative level of D.C. regulated power supply output;Pulse width test program it is provided with, by working out pulse width test program to send break-make control signal at a high speed to solid-state relay triggering end, thus realizing providing ignition voltage to pulse firing type electric spark workpiece to be tested in industrial control computer; Carrying out practically mode is as follows:
A, solid-state relay input is connected with D.C. regulated power supply output cathode, again the outfan of solid-state relay is connected with pulse firing type electric spark workpiece one end to be tested, the pulse firing type electric spark workpiece other end to be tested is connected with the negative level of D.C. regulated power supply output simultaneously, finally solid-state relay is triggered end and is connected with the DO interface of industrial control computer;
B, treat that each parts of step a) assemble after, two ends have been connected complete pulse firing type electric spark workpiece to be tested and have put into priming system igniting protective housing;
C, unlatching D.C. regulated power supply, after D.C. regulated power supply self-inspection is normal, then be configured the basic voltage that pulse firing type electric spark workpiece igniting to be tested is required;
D, unlatching industrial control computer, enter pulse width test program, the pulsewidth of pulse firing type electric spark workpiece to be tested be configured;
E, treating that the pulsewidth of pulse firing type electric spark workpiece to be tested in step d) is after setting completed, clicking pulse width test program, thus completing pulse firing type electric spark workpiece ignition performance checking to be tested;
F, as to carry out test of many times, repeated execution of steps a��e many times.
In the present invention, in step a), in industrial control computer, it is configured with DO board, equipped with multiple DO interfaces on DO board.
In the present invention, in step e), pulse width test program is provided with output button, by clicking output button, thus completing pulse firing type electric spark workpiece ignition performance checking to be tested.
Beneficial effect:
1) present inventive concept is novel, form simple, easy to use, reliable operation;
2) present invention has good versatility, can according to the pulse width requirement of different electric spark workpiece ignition voltages, only by pulse width test program, pulsewidth need to be carried out the verification experimental verification work that relative set can be correlated with, optimize test method, be effectively increased testing efficiency;
3) in the present invention, most ingredients belong to common apparatus, reusable, with low cost.
Accompanying drawing explanation
Fig. 1 is the flow chart of presently preferred embodiments of the present invention.
Detailed description of the invention
For the technological means making the present invention realize, creation characteristic, reach purpose and effect and be easy to understand, below in conjunction with being specifically illustrating, the present invention is expanded on further.
Method of testing referring to a kind of electric spark workpiece impulse ignition voltage of Fig. 1, including D.C. regulated power supply, solid-state relay, industrial control computer and pulse firing type electric spark workpiece to be tested, wherein, D.C. regulated power supply (such as Agilent6653), its major function is to provide the basic DC voltage needed for pulse firing type electric spark workpiece to be tested; Solid-state relay (such as 1JG20-1), its major function is that the input voltage of input is carried out quickly switching accordingly and from outfan output, belonging to executive component by the switching triggering command received according to triggering termination; Industrial control computer (as grinding China UNO3072), its major function is to utilize DO programming pulse width test program that is built-in in industrial computer or that embed, again through establishment pulse width test program to send break-make control signal at a high speed to solid-state relay triggering end, thus realizing providing ignition voltage to pulse firing type electric spark workpiece to be tested; Carrying out practically mode is as follows:
A, shown in Fig. 1, the input of solid-state relay is connected with the output cathode of D.C. regulated power supply, again the outfan of solid-state relay is connected with pulse firing type electric spark workpiece one end to be tested, negative with the output of D.C. regulated power supply for the pulse firing type electric spark workpiece other end to be tested level is connected simultaneously, finally the end that triggers of solid-state relay is connected with the DO interface of industrial control computer;
B, treat that each parts of step a) assemble after, two ends have been connected complete pulse firing type electric spark workpiece to be tested and have put into priming system igniting protective housing;
C, unlatching D.C. regulated power supply, after D.C. regulated power supply self-inspection is normal, then be configured the basic voltage that pulse firing type electric spark workpiece igniting to be tested is required;
D, unlatching industrial control computer, enter pulse width test program, the pulsewidth of pulse firing type electric spark workpiece to be tested be configured;
E, the output button clicked on pulse width test program, thus completing pulse firing type electric spark workpiece ignition performance checking to be tested;
F, as to carry out test of many times, repeatable execution step a��e many times.
In the present embodiment, pulse width test program has good versatility, according to the pulse width requirement of difference pulse firing type electric spark workpiece ignition voltages to be tested, only by pulse width test program, pulsewidth can need to be carried out the verification experimental verification work that relative set can be correlated with; Reusable, with low cost, there is the value of life-time service.
The ultimate principle of the present invention and principal character and advantages of the present invention have more than been shown and described. Skilled person will appreciate that of the industry; the present invention is not restricted to the described embodiments; described in above-described embodiment and description is that principles of the invention is described; without departing from the spirit and scope of the present invention; the present invention also has various changes and modifications, and these changes and improvements both fall within the claimed scope of the invention. Claimed scope is defined by appending claims and equivalent thereof.

Claims (3)

1. the method for testing of an electric spark workpiece impulse ignition voltage, including D.C. regulated power supply, solid-state relay, industrial control computer and pulse firing type electric spark workpiece to be tested, it is characterized in that, D.C. regulated power supply output cathode is connected with solid-state relay input, solid-state relay outfan is connected with pulse firing type electric spark workpiece one end to be tested, solid-state relay triggers end and is connected with the DO interface of industrial control computer, and the pulse firing type electric spark workpiece other end to be tested is connected with the negative level of D.C. regulated power supply output; Pulse width test program it is provided with, by working out pulse width test program to send break-make control signal at a high speed to solid-state relay triggering end, thus realizing providing ignition voltage to pulse firing type electric spark workpiece to be tested in industrial control computer; Carrying out practically mode is as follows:
A, solid-state relay input is connected with D.C. regulated power supply output cathode, again the outfan of solid-state relay is connected with pulse firing type electric spark workpiece one end to be tested, the pulse firing type electric spark workpiece other end to be tested is connected with the negative level of D.C. regulated power supply output simultaneously, finally solid-state relay is triggered end and is connected with the DO interface of industrial control computer;
B, treat that each parts of step a) assemble after, two ends have been connected complete pulse firing type electric spark workpiece to be tested and have put into priming system igniting protective housing;
C, unlatching D.C. regulated power supply, after D.C. regulated power supply self-inspection is normal, then be configured the basic voltage that pulse firing type electric spark workpiece igniting to be tested is required;
D, unlatching industrial control computer, enter pulse width test program, the pulsewidth of pulse firing type electric spark workpiece to be tested be configured;
E, treating that the pulsewidth of pulse firing type electric spark workpiece to be tested in step d) is after setting completed, clicking pulse width test program, thus completing pulse firing type electric spark workpiece ignition performance checking to be tested;
F, as to carry out test of many times, repeated execution of steps a��e many times.
2. the method for testing of a kind of electric spark workpiece impulse ignition voltage according to claim 1, it is characterised in that in step a), be configured with DO board in industrial control computer, equipped with multiple DO interfaces on DO board.
3. the method for testing of a kind of electric spark workpiece impulse ignition voltage according to claim 1, it is characterized in that, in step e), pulse width test program is provided with output button, by clicking output button, thus completing pulse firing type electric spark workpiece ignition performance checking to be tested.
CN201610090870.1A 2016-02-18 2016-02-18 Testing method of pulse ignition voltage of electric explosive device Pending CN105652123A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610090870.1A CN105652123A (en) 2016-02-18 2016-02-18 Testing method of pulse ignition voltage of electric explosive device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610090870.1A CN105652123A (en) 2016-02-18 2016-02-18 Testing method of pulse ignition voltage of electric explosive device

Publications (1)

Publication Number Publication Date
CN105652123A true CN105652123A (en) 2016-06-08

Family

ID=56488441

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610090870.1A Pending CN105652123A (en) 2016-02-18 2016-02-18 Testing method of pulse ignition voltage of electric explosive device

Country Status (1)

Country Link
CN (1) CN105652123A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108761139A (en) * 2018-06-19 2018-11-06 上海微小卫星工程中心 One kind can successively initiated and the adjustable priming system simulator of resistance value
CN118427565A (en) * 2024-07-04 2024-08-02 浙江永联民爆器材有限公司 Method and system for testing ignition of electric initiating explosive device after no-ignition load

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030116048A1 (en) * 1998-03-30 2003-06-26 George Bossarte Precision pyrotechnic display system and method having increased safety and timing accuracy
CN103499244A (en) * 2013-09-24 2014-01-08 中国空间技术研究院 Firer device detonation control system for control through MOSFET
CN203445612U (en) * 2013-09-06 2014-02-19 北京航天长征飞行器研究所 Multipath continuous heavy current pulse output control circuit
CN203551684U (en) * 2013-09-30 2014-04-16 中国航天科技集团公司川南机械厂 Initiating explosive device electrical property comprehensive tester
CN104090234A (en) * 2014-07-28 2014-10-08 珠海格力电器股份有限公司 Test circuit and method for arc fault circuit interrupter

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030116048A1 (en) * 1998-03-30 2003-06-26 George Bossarte Precision pyrotechnic display system and method having increased safety and timing accuracy
CN203445612U (en) * 2013-09-06 2014-02-19 北京航天长征飞行器研究所 Multipath continuous heavy current pulse output control circuit
CN103499244A (en) * 2013-09-24 2014-01-08 中国空间技术研究院 Firer device detonation control system for control through MOSFET
CN203551684U (en) * 2013-09-30 2014-04-16 中国航天科技集团公司川南机械厂 Initiating explosive device electrical property comprehensive tester
CN104090234A (en) * 2014-07-28 2014-10-08 珠海格力电器股份有限公司 Test circuit and method for arc fault circuit interrupter

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
赵金芳: "火工品多参数测试系统设计", 《中国优秀硕士学位论文全文数据库 工程科技Ⅱ辑》 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108761139A (en) * 2018-06-19 2018-11-06 上海微小卫星工程中心 One kind can successively initiated and the adjustable priming system simulator of resistance value
CN108761139B (en) * 2018-06-19 2020-11-10 上海微小卫星工程中心 Initiating explosive device equivalent device capable of continuously detonating and adjusting resistance value
CN118427565A (en) * 2024-07-04 2024-08-02 浙江永联民爆器材有限公司 Method and system for testing ignition of electric initiating explosive device after no-ignition load

Similar Documents

Publication Publication Date Title
CN102278924B (en) Intelligent detonation control system and method
US3610153A (en) Self-contained delay squib
CN109470094B (en) Safety ignition circuit with short-circuit safety function
CN109341448B (en) Initiating explosive device safety ignition circuit capable of overcoming ignition signal abnormality
CN105652123A (en) Testing method of pulse ignition voltage of electric explosive device
CN111366045B (en) Initiating explosive device equivalent device and device
CN106523189A (en) Rocket firing control system
CN105403112A (en) Detonating tube electronic delay detonator and method for detonating detonator under double control of light and shock waves
WO2011014892A2 (en) Detonator firing circuit
CN109297375B (en) Method for igniting side input/output electronic excitation conductive material of circuit board
CN217032216U (en) Safe type electron detonator control module
CN112179202B (en) Electric ignition circuit of ammunition fuse
CN114740077A (en) Ion flame detection method for heating furnace burner
CN212364828U (en) Multifunctional trigger device
KR20220155417A (en) Triggering apparatus controlled by mcu for nonelectric detonator and triggering method and system of nonelectric detonator using thereof
JP2016121845A (en) Burner controller and combustion control device
CN108803412B (en) Digital control system and method for blasting in movie and television shooting
CN214095782U (en) Cascade control detonating device of detonator
CN113589201A (en) Intelligent testing device and method for initiating explosive device passage
CN209459520U (en) The Initiator Safety firing circuit of ignition signal exception can be overcome
CN103490604A (en) Hysteresis protective circuit of device power source
CN205375058U (en) Optimizing apparatus of control current output
CN210741273U (en) Remote control type multi-path time-delay detonating system
CN202514234U (en) Device for preventing mistaken explosion caused by electromagnetic interference in explosion relevant operation
CN104677197A (en) Explosion starter safety control device and method used for underwater robot

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication

Application publication date: 20160608

RJ01 Rejection of invention patent application after publication