CN201463760U - Drive-by-wire type initiating system - Google Patents
Drive-by-wire type initiating system Download PDFInfo
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- CN201463760U CN201463760U CN2009201095982U CN200920109598U CN201463760U CN 201463760 U CN201463760 U CN 201463760U CN 2009201095982 U CN2009201095982 U CN 2009201095982U CN 200920109598 U CN200920109598 U CN 200920109598U CN 201463760 U CN201463760 U CN 201463760U
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- initiator
- control
- percussion
- initiation system
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Abstract
The utility model discloses a drive-by-wire type initiating system which comprises a shell of an initiator and a control circuit board of the initiator arranged in the shell, wherein the shell is provided with a plug, a control switch and an indicating lamp; one side of the shell is provided with a battery box; and the plug, the control switch, the indicating lamp and the battery box are all electrically connected with the control circuit board of the initiator. The drive-by-wire type initiating system is specially used for initiating a special electric detonator, solves the technical problems that the existing electrically initiating operation has generally heavier equipment, inconvenient installation of leads, accidentally static occurrence of connection status of the leads and complicated power sources. The drive-by-wire type initiating system has convenient carrying, firmness and endurance, convenient installation, simple operation, static resistance, adoption of common 7th batteries and good electricity saving performance, and can know whether every step of initiating is normal by the initiating system and ensure the life safety of people.
Description
Technical field
The utility model relates to a kind of explosive, specifically, relates to a kind of wire control initiation system.
Background technology
In bursting work, methods of printing commonly used detonates powder charge (cartridge bag), and methods of printing has fuse cord methods of printing, detonator methods of printing and electric ignition method.
The fuse cord methods of printing is with the continue method of the ignitron detonating charge that forms of fuse cord and detonator.Fuse cord is used pull igniter, sparking pipe, match etc. always and is lighted, and its flame reaches detonator with stable combustion speed, makes it blast.A plurality of powder charges but it can not detonate simultaneously are difficult for the accurately control burst time, weather and environmental requirement height, the unstable properties of detonating.
The detonator methods of printing is the method with detonator detonating primer detonating charge.It is connected with detonator and forms the detonator non-electric initiation system.Detonator is a kind of plastics small hose, and inwall scribbles very thin one deck high explosive.It is with exciting element (percussion rifle and igniter cap, percussion pen, detonator etc.) to excite, and its shortcoming is a detonator preservation condition harshness, very easily damages, and blasting circuit can not be used meter check, and the cost height detonates.
Electric ignition method is to utilize electric current to ignite the method for electric detonator initiation powder charge.Its a plurality of powder charge of constantly detonating simultaneously accurately; Can the detection by instrument guarantee the reliability of detonating; Can carry out superquick action, also can use delay electric detonator, millisecond electric detonator to carry out order and detonate.Wired electric ignition method is to utilize conductor wire to ignite the method for electric detonator initiation powder charge by electric current.Its priming supply can be selected dynamo exploder, portable power station and illumination, power line etc. for use.The preceding two kinds of methods of comparing, it is safe and reliable to detonate, low to environmental requirement, preserves easily.But equipment is generally relatively heavier now, and inconvenience is installed, and the lead connection status can't be judged, produces static sometimes and causes the electric cap unintended detonation.
Summary of the invention
The utility model technical issues that need to address just are to overcome the defective that existing wired electric ignition method exists, and a kind of wire control initiation system is provided, and it is specifically designed to the extraordinary electric cap that detonates.It is generally relatively heavier to have solved in the present electric initiating operation equipment, and lead is installed inconvenient, lead connection status, unexpected static and power supply source complicated technology problem.
For addressing the above problem, the utility model adopts following technical scheme:
A kind of wire control initiation system of the utility model, described initiation system comprise initiator shell and are installed on the interior initiator control circuit board of shell; Described shell is provided with plug, gauge tap and an indicator lamp, and a side of shell is provided with battery compartment, the equal and initiator control circuit board electrical connection of described plug, gauge tap and indicator lamp and battery compartment.
Described initiator control circuit board comprises the central microprocessor module, is used for the sequential control and the display driver of overall process; Voltage control module, be used for voltage ratio, voltage amplification and voltage judges; The percussion control module, the percussion control that is used to detonate, described voltage control module, percussion control module all insert the central microprocessor module.
Described initiator control circuit board adopts the PCB IC design.
Described plug is a FQ type aviation plug.
Described indicator lamp has three, is respectively power supply indicator, test indicator lamp and percussion indicator lamp.
Described gauge tap has three, is respectively power control switch, test gauge tap and percussion gauge tap.
The utility model adopts the PCB IC design; enclosure volume is small and exquisite; be convenient for carrying. what power supply adopted is No. 7 batteries of popularizing on the market; only need 4 batteries; can when percussion, produce voltage up to 24V; can guarantee the ignition requirement of electric cap fully; under the situation of not changing battery; can guarantee normally to pull the trigger more than 100 times. the interface of instrument and lead adopts FQ type aviation plug; its profile is circular waterproof plug seat; it is little to have volume, waterproof be connected and separate and durable characteristics fast, during connection as long as two ends aviation plug aligning is screwed.
Three indicator lamps are arranged on housing face-plate described in the utility model, be respectively power supply indication, test indication and percussion indication.Whether power supply indicator can allow operating personnel understand the power supply power supply normal, whether the test indicator lamp can indicate lead to connect normal, the percussion indicator lamp can indicate whether percussion, and whether make operating personnel watch this equipment can understand each operating process at safe distance normal.In structural design of the present utility model, by insulating surfaces and the air gap are set, not only satisfied the requirement of ignition instrument insulating properties, also reached the antistatic requirement.
In the work of detonating of special duty, use the utility model can, carry out the task of detonating fast, convenient and safely.Characteristics of the present utility model are easy to carry, and are durable, easy for installation, simple to operate, antistatic, adopt that common No. 7 batteries, electricity saving performance are good, whether can understand each step of detonating by the utility model normal, guarantee personnel's life security.
Operating procedure of the present utility model is simple and easy to use.The connecting line of will lighting a fire in the safe distance place combines with line wheel, initiator.Afterwards lead is moved to fire point, lead is connected with extraordinary electric cap.When detonating operation, the utility model power switch is placed " ON " position, the green power supply indicator lamp should be lighted, and blue percussion indicator lamp is also lighted after about 8 seconds, presses " test " button, and white indicating light is lighted and is illustrated that the connection status of detonating is normal.At this moment, can instruct, press " percussion " button, finish demolition duty according to the commander.
Description of drawings
Fig. 1 is the utility model structural representation.
Fig. 2 is an initiation system workflow diagram described in the utility model.
Fig. 3 is initiation system circuit theory diagrams described in the utility model.
The specific embodiment
As shown in Figure 1, a kind of wire control initiation system of the utility model, described initiation system comprises initiator shell 1 and is installed on the interior initiator control circuit board 2 of shell; Described shell is provided with plug 3, gauge tap and an indicator lamp, and a side of shell is provided with battery compartment 6, the equal and initiator control circuit board electrical connection of described plug, gauge tap and indicator lamp and battery compartment.
Described initiator control circuit board comprises the central microprocessor module, is used for the sequential control and the display driver of overall process; Voltage control module, be used for voltage ratio, voltage amplification and voltage judges; The percussion control module, the percussion control that is used to detonate, described voltage control module, percussion control module all insert the central microprocessor module.
Described initiator control circuit board adopts the PCB IC design.
Described plug is a FQ type aviation plug.
As shown in Figure 1, described indicator lamp has three, is respectively power supply indicator 4-1, test indicator lamp 4-2 and percussion indicator lamp 4-3.
Described gauge tap has three, is respectively power control switch 5-1, test gauge tap 5-2 and percussion gauge tap 5-3.
The utility model adopts the PCB IC design; enclosure volume is long; wide and height only is respectively 14cm; 9cm and 3.5cm; volume is small and exquisite; be convenient for carrying. what power supply adopted is No. 7 batteries of popularizing on the market; only need 4 batteries; can when percussion, produce voltage up to 24V; can guarantee the ignition requirement of electric cap fully; under the situation of not changing battery; can guarantee normally to pull the trigger more than 100 times. the interface of instrument and lead adopts FQ type aviation plug, and its profile is circular waterproof plug seat, and it is little to have a volume; waterproof be connected and separate and durable characteristics fast, during connection as long as two ends aviation plug aligning is screwed.
Three indicator lamps are arranged on housing face-plate described in the utility model, be respectively power supply indication, test indication and percussion indication.Whether power supply indicator can allow operating personnel understand the power supply power supply normal, whether the test indicator lamp can indicate lead to connect normal, the percussion indicator lamp can indicate whether percussion, and whether make operating personnel watch this equipment can understand each operating process at safe distance normal.In structural design of the present utility model, by insulating surfaces and the air gap are set, not only satisfied the requirement of ignition instrument insulating properties, also reached the antistatic requirement.
In the work of detonating of special duty, use the utility model can, carry out the task of detonating fast, convenient and safely.Characteristics of the present utility model are easy to carry, and are durable, easy for installation, simple to operate, antistatic, adopt that common No. 7 batteries, electricity saving performance are good, whether can understand each step of detonating by the utility model normal, guarantee personnel's life security.
Operating procedure of the present utility model is simple and easy to use.The connecting line of will lighting a fire in the safe distance place combines with line wheel, initiator.Afterwards lead is moved to fire point, lead is connected with extraordinary electric cap.When detonating operation, the utility model power switch is placed " ON " position, the green power supply indicator lamp should be lighted, and blue percussion indicator lamp is also lighted after about 8 seconds, presses " test " button, and white indicating light is lighted and is illustrated that the connection status of detonating is normal.At this moment, can instruct, press " percussion " button, finish demolition duty according to the commander.
Described initiation system workflow diagram as shown in Figure 2, by power supply input 6V voltage, voltage control module carry out voltage ratio, voltage amplification is connected with judgement, when circuit connects just often, normal percussion, output 24V voltage, assurance electric detonator initiation.
Initiation system circuit theory diagrams described in the utility model as shown in Figure 3.
It should be noted that at last: above embodiment only in order to the explanation the utility model and and the described technical scheme of unrestricted the utility model; Therefore, although this specification has been described in detail the utility model with reference to each above-mentioned embodiment,, those of ordinary skill in the art should be appreciated that still and can make amendment or be equal to replacement the utility model; And all do not break away from the technical scheme and the improvement thereof of spirit and scope of the present utility model, all should be encompassed in the claim scope of the present utility model.
Claims (6)
1. wire control initiation system is characterized in that: described initiation system comprises initiator shell and is installed on initiator control circuit board in the shell; Described shell is provided with plug, gauge tap and an indicator lamp, and a side of shell is provided with battery compartment, the equal and initiator control circuit board electrical connection of described plug, gauge tap and indicator lamp and battery compartment.
2. wire control initiation system as claimed in claim 1 is characterized in that: described initiator control circuit board comprises the central microprocessor module, is used for the sequential control and the display driver of overall process; Voltage control module, be used for voltage ratio, voltage amplification and voltage judges; The percussion control module, the percussion control that is used to detonate, described voltage control module, percussion control module all insert the central microprocessor module.
3. wire control initiation system as claimed in claim 1 or 2 is characterized in that: described plug is a FQ type aviation plug.
4. wire control initiation system as claimed in claim 3 is characterized in that: described initiator control circuit board adopts the PCB IC design.
5. wire control initiation system as claimed in claim 4 is characterized in that: described indicator lamp has three, is respectively power supply indicator, test indicator lamp and percussion indicator lamp.
6. wire control initiation system as claimed in claim 5 is characterized in that: described gauge tap has three, is respectively power control switch, test gauge tap and percussion gauge tap.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2009201095982U CN201463760U (en) | 2009-07-03 | 2009-07-03 | Drive-by-wire type initiating system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2009201095982U CN201463760U (en) | 2009-07-03 | 2009-07-03 | Drive-by-wire type initiating system |
Publications (1)
Publication Number | Publication Date |
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CN201463760U true CN201463760U (en) | 2010-05-12 |
Family
ID=42391111
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN2009201095982U Expired - Fee Related CN201463760U (en) | 2009-07-03 | 2009-07-03 | Drive-by-wire type initiating system |
Country Status (1)
Country | Link |
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CN (1) | CN201463760U (en) |
-
2009
- 2009-07-03 CN CN2009201095982U patent/CN201463760U/en not_active Expired - Fee Related
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C17 | Cessation of patent right | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20100512 Termination date: 20100703 |