CN107144189B - It is a kind of can safe on-line checking in-line arrangement fuse - Google Patents

It is a kind of can safe on-line checking in-line arrangement fuse Download PDF

Info

Publication number
CN107144189B
CN107144189B CN201710511997.0A CN201710511997A CN107144189B CN 107144189 B CN107144189 B CN 107144189B CN 201710511997 A CN201710511997 A CN 201710511997A CN 107144189 B CN107144189 B CN 107144189B
Authority
CN
China
Prior art keywords
component
high pressure
test
safety control
control circuit
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.)
Active
Application number
CN201710511997.0A
Other languages
Chinese (zh)
Other versions
CN107144189A (en
Inventor
沈德璋
叶海福
宋睿
赵昕
赵紫正
张中才
刘炜
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.)
Institute of Electronic Engineering of CAEP
Original Assignee
Institute of Electronic Engineering of CAEP
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 Institute of Electronic Engineering of CAEP filed Critical Institute of Electronic Engineering of CAEP
Priority to CN201710511997.0A priority Critical patent/CN107144189B/en
Publication of CN107144189A publication Critical patent/CN107144189A/en
Application granted granted Critical
Publication of CN107144189B publication Critical patent/CN107144189B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42CAMMUNITION FUZES; ARMING OR SAFETY MEANS THEREFOR
    • F42C21/00Checking fuzes; Testing fuzes

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuses (AREA)

Abstract

The present invention provides it is a kind of can safe on-line checking in-line arrangement fuse, the program includes shell, safety control circuit component, high pressure detonation component, detonator assembly, electric interfaces and test interface;Safety control circuit component, high pressure detonation component, detonator assembly, electric interfaces and test interface are each attached on shell;Safety control circuit component is electrically connected with electric interfaces and high pressure detonation component respectively;High pressure detonation component is also electrically connected with detonator assembly;Test interface is electrically connected with the interface of safety control circuit component and the inter-module of high pressure detonation component respectively.The program is connect using setting test interface with the key point of each internal component interface, by measuring each core wire of test interface resistance value over the ground, judge safety control circuit component and high pressure detonation component with the presence or absence of hardware fault, count the test value of each normal product, as the foundation for formulating test passes criterion, test point and test physical quantity can select according to actual needs.

Description

It is a kind of can safe on-line checking in-line arrangement fuse
Technical field
The present invention relates to in-line arrangement fuse, especially it is a kind of can safe on-line checking in-line arrangement fuse.
Background technique
In-line arrangement fuse refers to using electronic safety and arming device and the Slapper detonator based on insensitiveness powder charge, is formed Fuze system without flame proof explosive train.
In-line arrangement fuse is relative to tradition machinery fuse and mechanical-electrical fuze, other than high security, high reliability, Ling Yichong Wanting feature is to have good testability.Tradition machinery fuse or mechanical-electrical fuze, since solution guarantor's process is irreversible, production assembly The test of the workflows such as complete solution guarantor, triggering is not can be carried out after the completion.In-line arrangement fuse, will be removable before producing and shooting Slapper detonator is unloaded to be substituted for after simulation detonator sub-assembly, it can be achieved that comprehensive test of fuse performance.
But install in fuse to body, since what is installed on fuse is actual primer, and do not have the mould that changes the outfit generally The operating condition of quasi- detonator, it is contemplated that safety cannot be powered up test.I.e. various fuses are once installed to body at present Afterwards, it not can be carried out on-line testing.
And for some guided missile class high value ammunitions, have under the conditions of self-contained before transmission each component of total system is carried out it is complete The demand of face test, to guarantee that system function is normal, it is ensured that be reliably completed strike task.Fuze system becomes online survey before transmitting The blind spot of examination.
The paper that Shen Bo of Xi'an Electro-mechanical Information Inst. et al. was delivered in 2010 " increases CAN for electronic time fuze Bus selftest module " in, propose that one kind can be measured for four class measurement points such as voltage value, resistance value, time value and switching signals, The scheme of electronic time fuze functional test is completed when setting by CAN module.The program has certain novelty, but also deposits Some insufficient: one, since mechanical-electrical fuze solution is protected, process is irreversible, and inquiry solution guarantor's state is not to vital safety System function is tested;Two, detonator inner walkway just can be carried out after transmitting, and practical significance is little;Three, selftest module increases The requirement such as system bulk, cost, power consumption reflects volume, power consumption since electronic time fuze security system is not tested in text Etc. costs it is little, if tested fuse comprehensively, increased volume, power consumption etc. may be larger.
Summary of the invention
The purpose of the present invention, aiming at deficiency of the prior art, and provide it is a kind of can safe on-line checking In-line arrangement fuse, the program is connect using setting test interface with the key point of each internal component interface, due to electronics member device Impedance can generate variation after part failure, and then influence the impedance of the test point of component interface, therefore after fuse is packed into guided missile, lead Control system is played by the testing impedance of fuse test interface, can determine whether most of device (not being isolated device) state whether Normally, and then judge fuse state and performance.Why inter-module interface testing point is used rather than the external electric interfaces of fuse Impedance measurement is since the external electric interfaces of fuse are typically provided with various isolating devices, to the anti-of internal device parameters variation Reflect unobvious, test effect is bad.
This programme is achieved by the following technical measures:
It is a kind of can safe on-line checking in-line arrangement fuse, include shell, safety control circuit component, high pressure detonation group Part, detonator assembly, electric interfaces and test interface;Safety control circuit component, detonator assembly, electrically connects high pressure detonation component Mouth and test interface are each attached on shell;Safety control circuit component is electrically connected with electric interfaces and high pressure detonation component respectively It connects;High pressure detonation component is also electrically connected with detonator assembly;Test interface respectively with safety control circuit component and high pressure detonation group The interface of the inter-module of part is electrically connected.
As the preferred of this programme: the outside of housing tip is arranged in electric interfaces.
As the preferred of this programme: the outside of housing tip is arranged in test interface.
As the preferred of this programme: enclosure interior is provided with bracket;The safety control circuit component and high pressure detonation group Part is arranged on bracket.
As the preferred of this programme: the bottom end of detonator assembly setting inside housings.
As the preferred of this programme: the electrical connection carrier between each component is cable.
The beneficial effect of this programme can according to the description of the above program, due to using test interface in this scenario The component interface for being connected to safety control circuit component and high pressure detonation component powers on connection, fuse system when can satisfy test System does not work, and can not dismantle detonator and carry out on-line testing;Test interface is connected to component interface, passes through testing impedance detection system It whether normal unites, is studied through preliminary test, can effectively find most of hardware fault problem;Using independent test interface, do not change Become the original electric interfaces of fuse, does not increase detection circuit in the product, do not increase product power consumption, cost, volume substantially.
It can be seen that compared with prior art, the present invention having substantive features and progress, the beneficial effect implemented It is obvious.
Detailed description of the invention
Fig. 1 is the structural diagram of the present invention.
Fig. 2 is the circuit relationships deployed configuration schematic diagram of Fig. 1.
In figure, 1 is shell, and 2 be safety control circuit component, and 3 be high pressure detonation component, and 4 be detonator assembly, and 5 be support Frame, 6 be cable, and 7 be electric interfaces, and 8 be test interface.
Specific embodiment
All features disclosed in this specification or disclosed all methods or in the process the step of, in addition to mutually exclusive Feature and/or step other than, can combine in any way.
Any feature disclosed in this specification (including any accessory claim, abstract and attached drawing), except non-specifically chatting It states, can be replaced by other alternative features that are equivalent or have similar purpose.That is, unless specifically stated, each feature is only It is an example in a series of equivalent or similar characteristics.
As shown, this programme include shell, it is safety control circuit component, high pressure detonation component, detonator assembly, electrical Interface and test interface;Safety control circuit component, high pressure detonation component, detonator assembly, electric interfaces and test interface are solid It is scheduled on shell;Safety control circuit component is electrically connected with electric interfaces and high pressure detonation component respectively;High pressure detonates component also It is electrically connected with detonator assembly;Test interface is electric with the interface of safety control circuit component and the inter-module of high pressure detonation component respectively Connection.The outside of housing tip is arranged in electric interfaces.The outside of housing tip is arranged in test interface.Enclosure interior is provided with Bracket;The safety control circuit component and high pressure detonation component are arranged on bracket.Detonator assembly is arranged inside housings Bottom end.Electrical connection carrier between each component is cable.
Test interface can by its testing impedance realize fuse hardware state detection, test interface connection test point, Testing physical quantity can determine according to component design, including but not limited to the listed peace control component of embodiment 1 and high pressure detonation component Interface resistance value over the ground, acceptable criterion depends on product accounting data.
The present embodiment judges that safety control circuit component and high pressure rise by measuring each core wire of test interface resistance value over the ground Quick-fried component whether there is hardware fault, the test value of each normal product of statistical test interface, as formulation test passes criterion Foundation, test point and test physical quantity can select according to actual needs.
The invention is not limited to specific embodiments above-mentioned.The present invention, which expands to, any in the present specification to be disclosed New feature or any new combination, and disclose any new method or process the step of or any new combination.

Claims (4)

1. one kind can safe on-line checking in-line arrangement fuse, it is characterized in that: including shell, safety control circuit component, height Pressure detonation component, detonator assembly, electric interfaces and test interface;The safety control circuit component, high pressure detonation component, detonator Component, electric interfaces and test interface are each attached on shell;The safety control circuit component respectively with electric interfaces and height Pressure detonation component electrical connection;The high pressure detonation component is also electrically connected with detonator assembly;The test interface respectively with safety control The interface electrical connection of the inter-module of circuit unit processed and high pressure detonation component;The outer of housing tip is arranged in the electric interfaces Portion;The outside of housing tip is arranged in the test interface.
2. one kind according to claim 1 can safe on-line checking in-line arrangement fuse, it is characterized in that: enclosure interior be arranged There is bracket;The safety control circuit component and high pressure detonation component are arranged on bracket.
3. one kind according to claim 1 can safe on-line checking in-line arrangement fuse, it is characterized in that: the detonator assembly Bottom end inside housings is set.
4. one kind according to claim 1 can safe on-line checking in-line arrangement fuse, it is characterized in that: between each component Electrical connection carrier is cable.
CN201710511997.0A 2017-06-29 2017-06-29 It is a kind of can safe on-line checking in-line arrangement fuse Active CN107144189B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710511997.0A CN107144189B (en) 2017-06-29 2017-06-29 It is a kind of can safe on-line checking in-line arrangement fuse

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710511997.0A CN107144189B (en) 2017-06-29 2017-06-29 It is a kind of can safe on-line checking in-line arrangement fuse

Publications (2)

Publication Number Publication Date
CN107144189A CN107144189A (en) 2017-09-08
CN107144189B true CN107144189B (en) 2019-03-26

Family

ID=59785749

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710511997.0A Active CN107144189B (en) 2017-06-29 2017-06-29 It is a kind of can safe on-line checking in-line arrangement fuse

Country Status (1)

Country Link
CN (1) CN107144189B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107478112B (en) * 2017-09-21 2023-07-04 中国工程物理研究院电子工程研究所 High-reliability in-line fuse and control method thereof
CN107765045B (en) * 2017-11-15 2023-06-23 中国工程物理研究院电子工程研究所 Electronic product safety testing device with redundant safety control
CN108398062A (en) * 2018-03-21 2018-08-14 中国工程物理研究院电子工程研究所 Detachable protecting against shock fuse

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN204963688U (en) * 2015-09-30 2016-01-13 中国人民解放军军械工程学院 Embedded guided missile signal acquisition and switching device
CN206862221U (en) * 2017-06-29 2018-01-09 中国工程物理研究院电子工程研究所 It is a kind of can safe on-line checking in-line arrangement fuse

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS63236238A (en) * 1987-03-25 1988-10-03 桑野電機株式会社 Fuse disconnection detector

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN204963688U (en) * 2015-09-30 2016-01-13 中国人民解放军军械工程学院 Embedded guided missile signal acquisition and switching device
CN206862221U (en) * 2017-06-29 2018-01-09 中国工程物理研究院电子工程研究所 It is a kind of can safe on-line checking in-line arrangement fuse

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
基于总线控制的直列式点火系统;欧阳丽娥;《测控与控制学报》;20140430;第36卷(第2期);全文

Also Published As

Publication number Publication date
CN107144189A (en) 2017-09-08

Similar Documents

Publication Publication Date Title
CN107144189B (en) It is a kind of can safe on-line checking in-line arrangement fuse
CN104198850B (en) Initiating explosive device parallel type bypass testing method in ignition experiment
US8136448B2 (en) Networked electronic ordnance system
US10890426B2 (en) Detonator
CN110399691A (en) A kind of the all-electronin fuze safety Logic control module and its software timing design method of high security
US11105600B1 (en) Identification method in a detonator network
US9243877B2 (en) Detonator ignition protection and detection circuit
CN103256868B (en) Integrated grounding piezoelectric fuze
US3500747A (en) Safe-arm initiator
CN206862221U (en) It is a kind of can safe on-line checking in-line arrangement fuse
CN104764371A (en) Adapter compatible to electronic detonator, detonating system and detonating method for exploration electronic detonator
KR102294831B1 (en) Apparatus for measuring detonation shock of tandem-charge types of missile and method for the same
CN111964542B (en) Initiating explosive device detonating circuit, stratospheric airship and nondestructive testing method
CN109425269A (en) A kind of fuse electronic security(ELSEC) orientation multipoint priming control circuit
CN207716970U (en) A kind of all-electronin contact fuze tester
KR101865778B1 (en) Measuring apparatus for fire-time of fuze and method thereof
KR101339081B1 (en) Triggering apparatus of nonelectric detonator using the sparker device and electric blasting machine and triggering method using thereof
CN212458149U (en) Initiating explosive device detonation circuit and stratospheric airship
KR101341396B1 (en) an electronic time fuze
CN108871132A (en) A kind of explosion self-desttruction equipment for cylinder test
CN110133712B (en) Synchronous trigger device for mine seismic exploration time-delay explosive source
CN104315931A (en) Piezoresistance type efficient electrostatic protection bridge-wire electric detonator
CN212806775U (en) High-reliability electronic detonator initiator system
CN209357958U (en) Multipoint priming fuse tester safety test load plug
CN207423007U (en) A kind of contact fuze of sensor redundancy formula design

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant