CN110285707A - A kind of firearms rocket percussion ignition controller - Google Patents
A kind of firearms rocket percussion ignition controller Download PDFInfo
- Publication number
- CN110285707A CN110285707A CN201910615420.3A CN201910615420A CN110285707A CN 110285707 A CN110285707 A CN 110285707A CN 201910615420 A CN201910615420 A CN 201910615420A CN 110285707 A CN110285707 A CN 110285707A
- Authority
- CN
- China
- Prior art keywords
- ignition
- output
- power supply
- ignition controller
- current
- 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
- 238000009527 percussion Methods 0.000 title abstract description 9
- 238000000691 measurement method Methods 0.000 claims abstract description 16
- 238000010304 firing Methods 0.000 claims abstract description 11
- 230000006641 stabilisation Effects 0.000 claims description 5
- 238000011105 stabilization Methods 0.000 claims description 5
- 230000000087 stabilizing effect Effects 0.000 claims description 5
- 230000005611 electricity Effects 0.000 claims description 4
- 238000005259 measurement Methods 0.000 claims description 4
- 230000013011 mating Effects 0.000 description 3
- 230000033228 biological regulation Effects 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 235000015842 Hesperis Nutrition 0.000 description 1
- 235000012633 Iberis amara Nutrition 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A19/00—Firing or trigger mechanisms; Cocking mechanisms
- F41A19/58—Electric firing mechanisms
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Ignition Installations For Internal Combustion Engines (AREA)
Abstract
A kind of firearms rocket percussion ignition controller, including DC power supply and ignition controller, the front panel top of DC power supply have electric current show and voltage show, the positive high current binding post of output, the negative high current binding post of output, the positive low current binding post of output, the negative low current binding post of output, current adjusting knob, voltage adjusting knob and air switch are arranged at the front panel lower part of DC power supply, the rear panel of DC power supply has output port of power source and plant-grid connection socket, and plant-grid connection socket connects corresponding power by connecting line；The front panel top of ignition controller has resistance to show, countdown is adjusted and display, the duration of ignition adjust and display, button ignition switch and scram button, the front panel lower part of ignition controller has igniter head lead input port, measurement method/sparking mode switching switch, external trigger output one, external trigger output two and initial firing current feedback output, the rear panel of ignition controller to have safety device and power input.The application can guarantee that igniting is stablized, and the time is controllable, and easy to operate.
Description
Technical field
The present invention relates to firearms rockets to fire corollary equipment field, fires ignition control more particularly to a kind of firearms rocket
Device.
Background technique
As current weapon the degree of automation is higher and higher, traditional controller is no longer satisfied corresponding control and needs
It wants, therefore in order to guarantee that igniting is stablized, the time is controllable, is user-friendly for operating, guarantees each operation control in place, and
Consider various governing factors in practical operation, it is therefore desirable to the Aided design firearms rocket percussion with D.C. regulated power supply accordingly
Ignition controller.
Summary of the invention
In order to solve problem above, the present invention provides a kind of firearms rocket percussion ignition controller, firearms percussion igniting
Controller includes ignition controller main body and DC power supply, is provided by DC power supply and stablizes output, thus guarantee that igniting is stablized, and
And consider that practical firearms fire the mating corresponding control button of igniting factor, facilitate operator to operate, for this purpose, the present invention mentions
Ignition controller, including DC power supply and ignition controller, the power supply output of the DC power supply are fired for a kind of firearms rocket
Port connects the power input of ignition controller by connecting line:
The front panel top of the DC power supply has that electric current is shown and voltage show, and there is current stabilization instruction in electric current display side
Lamp, the voltage show that there is a pressure stabilizing indicator light in side, the front panel lower part of the DC power supply have the positive high current binding post of output,
Export negative high current binding post, the positive low current binding post of output, the negative low current binding post of output, current adjusting knob, voltage tune
Section knob and air switch, the rear panel of the DC power supply have output port of power source and plant-grid connection socket, and the power supply connects
Enter socket and corresponding power is connect by connecting line；
The front panel top of the ignition controller has resistance to show, countdown is adjusted and display, the duration of ignition are adjusted and shown,
Igniter head lead input port, measurement method/igniting are arranged at button ignition switch and scram button, the front panel lower part of the ignition controller
Mode switches switch, external trigger exports one, external trigger output two and initial firing current feedback output, behind the ignition controller
Plate has safety device and power input；
The ignition controller is adjusted the setting time that input adjusts countdown module by countdown, is adjusted and is inputted by the duration of ignition
The ignition duration of igniting time module is adjusted, then power management module is controlled by tune voltage, tune electric current and scram button, by
Signal is issued Ignition Logic control module in ignition controller by countdown module, duration of ignition module and power management module,
Ignition Logic control module is controlled the input to ignition coil by button ignition switch；Coil resistance measurement display module can be shown a little
The resistance value of firewire circle；Measurement method/sparking mode switching switch switches over control to measurement method and sparking mode.
Further improvement of the present invention, the rear panel of the DC power supply is there are also a pair of of power supply fan, and fan is for cooling down.
Further improvement of the present invention, the safety device is interior to match 20A fuse, and 20A guarantor is needed to configure in actual use
Dangerous silk.
Further improvement of the present invention, the DC supply input voltage be alternating current 220V ± 10%, output voltage be 0~
60V, output electric current are 0~20A, display mode LED, and the application is carried out in practice with DC power supply relevant parameter
As above.
Further improvement of the present invention, the ignition voltage of the ignition controller are 0-60V, initial firing current 0-20A, are surveyed
Measuring resistance range is 0-20 ohm, measures resistor current < 10mA, and the application is carried out in practice with ignition controller phase
It is as above to close parameter.
A kind of firearms rocket of the application fires ignition controller, and operation is following first to supply to DC power supply and ignition controller
Electricity, it is ensured that instrument is in power-up state；Ignition circuit connecting line is connected to resistance input port again, resistance display window is answered at this time
There is display ignition circuit resistance value, if non-resistance show value (> 20 ohm), should check whether ignition circuit is intact；Again wait need
When lighting a fire, operational mode switch is switched into sparking mode gear, waits ignition order；After preferably receiving ignition order, press
Button ignition switch, starts countdown, and timing is lighted a fire after.Scram button can be pressed at any time carries out emergency stop.The application passes through straight
It flows guarantee of power controller to stablize, and mating corresponding control button is needed according to practical control.
Detailed description of the invention
Fig. 1 the application DC power supply front panel schematic diagram；
Fig. 2 the application DC power supply rear panel schematic diagram；
Fig. 3 the application ignition controller front panel；
Fig. 4 the application ignition controller rear panel；
Fig. 5 the application ignition controller schematic internal view；
Appended drawing reference therein are as follows: 1. electric currents are shown；2. voltage is shown；3. current stabilization indicator light；4. pressure stabilizing indicator light；5. defeated
Positive high current binding post out；6. exporting negative high current binding post；7. exporting positive low current binding post；8. exporting negative low current to connect
Terminal；
9. current adjusting knob；10. voltage adjusting knob；11. air switch；12. power supply fan；13. power output end
Mouthful；14. plant-grid connection socket；1 ', resistance is shown；2 ', countdown is adjusted and is shown；3 ', the duration of ignition adjusts and shows；
4 ', button ignition switch；5 ', scram button；6 ', igniter head lead input port；7 ', measurement method/sparking mode switching switch；8'.
External trigger output one；9 ', external trigger exports；10 ', initial firing current feedback output；11 ', safety device；12 ', power input.
Specific embodiment
Present invention is further described in detail with specific embodiment with reference to the accompanying drawing:
The present invention provides a kind of firearms rocket percussion ignition controller, and it includes ignition controller master which, which fires ignition controller,
Body and DC power supply are provided by DC power supply and stablize output, to guarantee that igniting is stablized, and consider practical firearms percussion igniting
The mating corresponding control button of factor, facilitates operator to operate.
As an embodiment of the present invention, the present invention provides a kind of firearms rocket percussion ignition controller, including direct current
Source and ignition controller, the output port of power source 13 of the DC power supply connect the power input of ignition controller by connecting line
12 ':
The front panel top of herein described DC power supply have electric current show 1 and voltage show 2, the electric current shows that 1 side has
Current stabilization indicator light 3, the voltage show that there are pressure stabilizing indicator light 4 in 2 sides, and the front panel lower part of the DC power supply has output honest
Electric current binding post 5, the negative high current binding post 6 of output, the positive low current binding post 7 of output, the negative low current binding post 8 of output, electric current
Adjusting knob 9, voltage adjusting knob 10 and air switch 11, the rear panel of the DC power supply have output port of power source 13 and electricity
Socket 14 is accessed in source, and the plant-grid connection socket 14 connects corresponding power by connecting line；
The front panel top of herein described ignition controller has resistance to show that 1 ', countdown adjusts and show 2 ', the duration of ignition
Adjust and show 3 ', button ignition switch 4 ' and scram button 5 ', the front panel lower part of the ignition controller has igniter head lead defeated
Entrance 6 ', measurement method/sparking mode switching switch 7 ', external trigger output one 8 ', external trigger output 29 ' and initial firing current are anti-
Feedback output 10 ', the rear panel of the ignition controller has safety device 11 ' and power input 12 '；
Herein described ignition controller is adjusted the setting time that input adjusts countdown module by countdown, by duration of ignition tune
Section input adjusts the ignition duration of igniting time module, then controls power management by tune voltage, tune electric current and scram button
Signal is issued Ignition Logic control in ignition controller by countdown module, duration of ignition module and power management module by module
Molding block, Ignition Logic control module are controlled the input to ignition coil by button ignition switch；Coil resistance measures display module can
To show the resistance value of ignition coil；Measurement method/sparking mode switching switch switches over control to measurement method and sparking mode
System.
As a kind of specific embodiment of the present invention, the present invention provides a kind of firearms rocket as shown in Figs. 1-5 and fires igniting
The output port of power source 13 of controller, including DC power supply and ignition controller, the DC power supply passes through connecting line contact fire
The power input 12 ' of controller:
The front panel top of herein described DC power supply have electric current show 1 and voltage show 2, the electric current shows that 1 side has
Current stabilization indicator light 3, the voltage show that there are pressure stabilizing indicator light 4 in 2 sides, and the front panel lower part of the DC power supply has output honest
Electric current binding post 5, the negative high current binding post 6 of output, the positive low current binding post 7 of output, the negative low current binding post 8 of output, electric current
Adjusting knob 9, voltage adjusting knob 10 and air switch 11, the rear panel of the DC power supply have output port of power source 13 and electricity
Socket 14 is accessed in source, and the plant-grid connection socket 14 connects corresponding power by connecting line, and the rear panel of the DC power supply is also
A pair of of power supply fan 12, fan is for cooling down；
The front panel top of herein described ignition controller has resistance to show that 1 ', countdown adjusts and show 2 ', the duration of ignition
Adjust and show 3 ', button ignition switch 4 ' and scram button 5 ', the front panel lower part of the ignition controller has igniter head lead defeated
Entrance 6 ', measurement method/sparking mode switching switch 7 ', external trigger output one 8 ', external trigger output 9 ' and initial firing current are fed back
Output 10 ', the rear panel of the ignition controller has safety device 11 ' and power input 12 ', matches in the safety device
20A fuse needs to configure 20A fuse in actual use；
Herein described ignition controller is adjusted the setting time that input adjusts countdown module by countdown, by duration of ignition tune
Section input adjusts the ignition duration of igniting time module, then controls power management by tune voltage, tune electric current and scram button
Signal is issued Ignition Logic control in ignition controller by countdown module, duration of ignition module and power management module by module
Molding block, Ignition Logic control module are controlled the input to ignition coil by button ignition switch；Coil resistance measures display module can
To show the resistance value of ignition coil；Measurement method/sparking mode switching switch switches over control to measurement method and sparking mode
System.
Herein described DC supply input voltage is alternating current 220V ± 10%, and output voltage is 0~60V, and output electric current is
0~20A, display mode LED, the application carry out as above with DC power supply relevant parameter in practice.
The ignition voltage of herein described ignition controller is 0-60V, initial firing current 0-20A, and measurement resistance range is
0-20 ohm, resistor current < 10mA is measured, the application carries out as above with ignition controller relevant parameter in practice.
The application voltage of direct-flow voltage regulation, which operates with, to be described as follows；
By current regulation to maximum clockwise before booting, adjusting voltage knob to required voltage value after booting (can be according to institute
Need resistance mutually multiplied adjusting voltage of the initial firing current with institute survey time road).
The application ignition controller panel operation operation instruction is as follows；
(1) igniter head resistance display；
Ignition circuit inspection switch when having resistance display, illustrates that ignition circuit connection is intact when measurement method shelves, can
To light a fire.
(2) count down time；
Count down time can be set before ignition, and timing then starts to light a fire.
(3) duration of ignition；
Igniting can be set before ignition to last long.
(4) button ignition switch；
Ignition control switch starts countdown when pressing.
(5) scram button；
In countdown period, emergency stop can be carried out at any time.After scram button restores, light a fire by button ignition switch.
(6) resistance inputs；
Ignition circuit Wiring port.
(7) igniter head detection switch；
Before externally being lighted a fire, first ignition circuit is checked, to ensure reliable ignition.(note: under normality, this button
It should be at measurement method gear).
(8) external trigger output port；
This port provides two road rising edge Transistor-Transistor Logic levels, externally provides synchronous triggering signal.
(9) feedback output；
Voltage output is converted into after initial firing current is acquired.
(10) safety device；
This safety device is used to protect the internal relay of ignition controller, and to prevent, electric current is excessive and is burned.
(11) power input；
This port provides working power for ignition controller, is accessed by D.C. regulated power supply.
The above described is only a preferred embodiment of the present invention, being not the limit for making any other form to the present invention
System, and made any modification or equivalent variations according to the technical essence of the invention, still fall within present invention model claimed
It encloses.
Claims (5)
1. a kind of firearms rocket fires ignition controller, including DC power supply and ignition controller, the power supply of the DC power supply
Output port (13) connects the power input (12 ') of ignition controller by connecting line, it is characterised in that:
The front panel top of the DC power supply has electric current to show that (1) and voltage are shown (2), and the electric current shows that (1) side has
Current stabilization indicator light (3), the voltage show that (2) side has pressure stabilizing indicator light (4), and the front panel lower part of the DC power supply has defeated
Positive high current binding post (5), the negative high current binding post (6) of output, the positive low current binding post (7) of output, the negative low current of output out
Binding post (8), current adjusting knob (9), voltage adjusting knob (10) and air switch (11), the rear panel of the DC power supply
There are output port of power source (13) and plant-grid connection socket (14), the plant-grid connection socket (14) connects corresponding electricity by connecting line
Source；
The front panel top of the ignition controller has resistance to show that (1 '), countdown adjust and show (2 '), duration of ignition tune
Section and display (3 '), button ignition switch (4 ') and scram button (5 '), the front panel lower part of the ignition controller have igniter head to draw
Line input port (6 '), measurement method/sparking mode switching switch (7 '), external trigger exports one (8 '), external trigger exports two (9 ')
With initial firing current feedback output (10 '), the rear panel of the ignition controller has safety device (11 ') and power input
(12 ')；
The ignition controller is adjusted the setting time that input adjusts countdown module by countdown, is adjusted and is inputted by the duration of ignition
The ignition duration of igniting time module is adjusted, then power management module is controlled by tune voltage, tune electric current and scram button, by
Signal is issued Ignition Logic control module in ignition controller by countdown module, duration of ignition module and power management module,
Ignition Logic control module is controlled the input to ignition coil by button ignition switch；Coil resistance measurement display module can be shown a little
The resistance value of firewire circle；Measurement method/sparking mode switching switch switches over control to measurement method and sparking mode.
2. a kind of firearms rocket according to claim 1 fires ignition controller, it is characterized in that: after the DC power supply
There are also a pair of of power supply fans (12) for panel.
3. a kind of firearms rocket according to claim 1 fires ignition controller, it is characterized in that: the safety device
Match fuse in (11 ').
4. a kind of firearms rocket according to claim 1 fires ignition controller, it is characterized in that: the DC supply input
Voltage is alternating current 220V ± 10%, and output voltage is 0~60V, and output electric current is 0~20A, display mode LED.
5. a kind of firearms rocket according to claim 1 fires ignition controller, it is characterized in that: the ignition controller
Ignition voltage is 0-60V, initial firing current 0-20A, and measurement resistance range is 0-20 ohm, measures resistor current < 10mA.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910615420.3A CN110285707A (en) | 2019-07-09 | 2019-07-09 | A kind of firearms rocket percussion ignition controller |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910615420.3A CN110285707A (en) | 2019-07-09 | 2019-07-09 | A kind of firearms rocket percussion ignition controller |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110285707A true CN110285707A (en) | 2019-09-27 |
Family
ID=68021013
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910615420.3A Pending CN110285707A (en) | 2019-07-09 | 2019-07-09 | A kind of firearms rocket percussion ignition controller |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110285707A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113804052A (en) * | 2021-10-12 | 2021-12-17 | 中国兵器装备集团上海电控研究所 | Percussion control box system and vehicle |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0071734A2 (en) * | 1981-08-11 | 1983-02-16 | Wegmann & Co. GmbH | Electric-firing mechanism for a launching apparatus |
| CN101769701A (en) * | 2008-12-31 | 2010-07-07 | 吉林市北华航天科技有限公司 | Multifunctional remote electronic ignition system |
| CN102072817A (en) * | 2010-11-25 | 2011-05-25 | 西北工业大学 | Device and method for controlling ignition by constant-current time sequence |
| CN106523189A (en) * | 2016-10-20 | 2017-03-22 | 南京理工大学 | Rocket firing control system |
| CN206894518U (en) * | 2017-06-30 | 2018-01-16 | 青岛博瑞电气有限公司 | A kind of control dc source manually |
| CN210346469U (en) * | 2019-07-09 | 2020-04-17 | 南京华剑兵科智能装备有限公司 | Firing ignition controller for gun and rocket firing |
-
2019
- 2019-07-09 CN CN201910615420.3A patent/CN110285707A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0071734A2 (en) * | 1981-08-11 | 1983-02-16 | Wegmann & Co. GmbH | Electric-firing mechanism for a launching apparatus |
| CN101769701A (en) * | 2008-12-31 | 2010-07-07 | 吉林市北华航天科技有限公司 | Multifunctional remote electronic ignition system |
| CN102072817A (en) * | 2010-11-25 | 2011-05-25 | 西北工业大学 | Device and method for controlling ignition by constant-current time sequence |
| CN106523189A (en) * | 2016-10-20 | 2017-03-22 | 南京理工大学 | Rocket firing control system |
| CN206894518U (en) * | 2017-06-30 | 2018-01-16 | 青岛博瑞电气有限公司 | A kind of control dc source manually |
| CN210346469U (en) * | 2019-07-09 | 2020-04-17 | 南京华剑兵科智能装备有限公司 | Firing ignition controller for gun and rocket firing |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113804052A (en) * | 2021-10-12 | 2021-12-17 | 中国兵器装备集团上海电控研究所 | Percussion control box system and vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US5283516A (en) | Low voltage dimmer with no load protection | |
| CN108402525B (en) | Infrared temperature control system of electronic heating device and control method thereof | |
| CN110285707A (en) | A kind of firearms rocket percussion ignition controller | |
| CN106523189A (en) | Rocket firing control system | |
| CN102685998B (en) | Pulse xenon lamp controller | |
| CN205433413U (en) | Temperature rise control circuit of electric oven | |
| CN104102143A (en) | Control method and device of electronic cigarette with multiple voltage output modes | |
| CN206419918U (en) | A kind of light source controller | |
| CN108776449A (en) | A kind of general priming system simulation system | |
| CN210346469U (en) | Firing ignition controller for gun and rocket firing | |
| CN110068777B (en) | Portable light supplement lamp signal generator | |
| CN204611836U (en) | A kind of Remote Firing Unit | |
| CN114199087B (en) | Emission control device of electronic fuze | |
| CN104500233B (en) | A kind of portable airspace engine igniter | |
| CN108803412B (en) | Digital control system and method for blasting in movie and television shooting | |
| CN208506212U (en) | Capacitance-resistance load regulation test fixture | |
| US7948184B2 (en) | Vehicle testing lamp apparatus, system, and method | |
| US20210341146A1 (en) | Push-out portable arc igniter | |
| CN213527433U (en) | Novel electronic firecracker | |
| CN208548876U (en) | Tandem machine of smoke-screen trigger control device | |
| CN108717281A (en) | A kind of programmable machine vision controller | |
| CN205408044U (en) | Modified vehicle radar intelligent monitoring trigger mechanism | |
| CN206739998U (en) | A kind of new priming system opens quick-fried controller | |
| CN219914884U (en) | Boiler control function testing device | |
| CN210573292U (en) | Intelligent measurement and control device for switch cabinet |
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 | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190927 |
|
| RJ01 | Rejection of invention patent application after publication |