CN208521187U - A kind of military turn of civilian concentrating type weather intervention antiaircraft gun control device - Google Patents
A kind of military turn of civilian concentrating type weather intervention antiaircraft gun control device Download PDFInfo
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- CN208521187U CN208521187U CN201820950537.8U CN201820950537U CN208521187U CN 208521187 U CN208521187 U CN 208521187U CN 201820950537 U CN201820950537 U CN 201820950537U CN 208521187 U CN208521187 U CN 208521187U
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Abstract
A kind of military turn of civilian concentrating type weather intervention antiaircraft gun control device, it is related to civilian hail-proof rain-increasing equipment, military equipment civil nature security management and control technical field, specifically a kind of military turn of civilian concentrating type weather intervenes antiaircraft gun control device, including steering motor group, gyroscope, fire electromagnet, gyroscope is mounted on antiaircraft gun gun tube, steering motor group is used to control the steering of antiaircraft gun, inclination angle, percussion electromagnet is used to control the percussion of antiaircraft gun, gyroscope is turned to for acquiring, the data at inclination angle, the course changing control end of steering motor group is connect by steering controller with main control unit, the pitch angle control end of steering motor group is connect by pitch angle control device with main control unit, gyroscope signal output end is connected with main control unit by gyroscope signal decoder 12, percussion electromagnet control terminal is connect by arming signal transmitter with main control unit, Main control module chain is connected to integrated signal decoder, and the first signal input of integrated signal decoder is connected with pulse button.
Description
Technical field
The utility model relates to civilian hail-proof rain-increasing equipment, military equipment civil nature security management and control technical field, specifically
A kind of military turn of civilian concentrating type weather intervention antiaircraft gun control device.
Background technique
In China's rain making working equipment, 37mm antiaircraft gun is key operation equipment.Existing many 37mm antiaircraft guns are
Military turn civilian, and various operations, which also need to rely on manually work pattern, to be had for operation safety relying primarily in the past
Being transferred to civilian work or restoring soldier for antiaircraft gun operating experience operates antiaircraft gun, but as my army's modernization step is constantly accelerated, 37mm
Antiaircraft gun is using gradually being replaced by automatic equipment, and the people with antiaircraft gun operating experience is fewer and fewer, so in this 2 years artificial
Accident, main cause are exactly that amateur's misoperation leads to bombing bore, and then injures industry personnel frequent occurrence in rainfall operation.For
This problem is solved, domestic more factories have carried out reformation of electric control to antiaircraft gun, and devise hand held controller, pass through the side of cable
Formula controls antiaircraft gun.Currently, this quasi-controller is only capable of realizing the control at the azimuth to antiaircraft gun, the angle of site and shooting percussion
System, the function of collecting and transmit without information, can not achieve the information system management to antiaircraft gun operation, while can not effectively record reality
Border fires quantity, i.e. ammunition service condition, this issue concerns needs additionally to arrange manpower to ammunition administration safety, scene confirmation,
If frequent operation, it may occur that omit, ammunition is caused artificially to lose.
Utility model content
The technical problem to be solved by the utility model is to provide a kind of military turn of civilian concentrating type weathers to intervene antiaircraft gun control
It is not strong to the management of antiaircraft gun job information and the safe dynamics of ammunition to have solved the problems, such as that existing equipment can not achieve for device processed.
A kind of technical solution of the utility model solution technical problem are as follows: military turn of civilian concentrating type weather intervention antiaircraft gun control
Device processed, including steering motor group, gyroscope, percussion electromagnet, gyroscope are mounted on antiaircraft gun gun tube, and steering motor group is used for
Steering, the inclination angle of antiaircraft gun are controlled, percussion electromagnet is used to control the percussion of antiaircraft gun, and gyroscope is used to acquire the number of steering, inclination angle
According to the course changing control end of steering motor group is connect by steering controller 10 with main control unit 0, the pitch angle control of steering motor group
End is connect by pitch angle control device 11 with main control unit 0, and gyroscope signal output end is translated with main control unit 0 by gyroscope signal
Code device 12 is connected, and percussion electromagnet control terminal is connect by arming signal transmitter 13 with main control unit 0, and main control unit 0 links
There is integrated signal decoder 14,14 first signal input of integrated signal decoder is connected with pulse button;Steering motor group,
Gyroscope, percussion electromagnet, pulse button power supply port be connected by forceful electric power switch with the forceful electric power delivery outlet of power supply module 1,
The power supply port of main control unit 0 is switched by light current to be connected with the weak current delivery outlet of power supply module 1;Main control unit 0 is connected with
GPRS module 2, locating module, full data storage 7, arming signal counter 15;Emission parameter and firing order pass through GPRS
2 remote transmission of module;The button inputted firing order priority of pulse is higher than the firing order of GPRS module 2.
Main control unit 0 is connected with wifi module 3, bluetooth module 4, and 2 priority of GPRS module is higher than wifi module 3, wifi
3 priority of module is higher than bluetooth module 4, and emission parameter and firing order pass through GPRS module 2, wifi module 3 or bluetooth module 4
Input.
Main control unit 0 connect locating module be GPS navigation module 5, Beidou navigation module 6, GPS navigation module 5 it is excellent
First grade be lower than Beidou navigation module 6, GPS navigation module 5, Beidou navigation module 6 be equipped with it is independent start switch, when corresponding
It starts switch one of them Beidou navigation module 6 of GPS navigation module 5 after one of them is closed to stop working, when corresponding starting
Switch is all turned on, and adopts information according to priority.
Full data storage 7 is equipped with usb outside access interface, and the usb outside access interface of full data storage 7 is single
To interface is read, pass through hardware circuit, restricted information write-in.
Main control unit 0 is connected with external data referring to memory 8, data comparator 9, and external data is referring to memory 8
Interface is read in individual event, passes through hardware circuit, restricted information write-in;Data comparator 9 is with external data referring to the ginseng in memory 8
It is bound according to numerical value, geographic position data, inclination angle, steering data is verified, is more than bound, then stops to emit.
Main control unit 0 is connected with recuperator means reseting sensor 16, percussion confirmation comparator 17, recuperator means reseting sensor 16
Signal input part is connected with recuperator means reseting sensor, and recuperator means reseting sensor issues a pulse signal, works as integrated signal
14 first signal input of decoder is connected with after pulse button is pressed, and percussion electromagnet drives cannon percussion, hits simultaneously
Signalling counter 15, which counts, adds one, and while the counting of arming signal counter 15 adds one, recuperator means reseting sensor 16 is received
Signal, the percussion confirmation confirmation of comparator 17 this time fires successfully, when percussion confirmation comparator 17 only receives arming signal counter
15 countings plus a signal, do not receive 16 signal of recuperator means reseting sensor, then assert and this time emit, ammunition is duds, system lock
Extremely, it removes barriers after restarting, restores normal.
14 second signal input port of integrated signal decoder is connected with Touch Screen, and Touch Screen carries decoder, touch-control
Screen is inputted for being manually entered emission parameter, emission parameter by Touch Screen, and the priority of Touch Screen is higher than GPRS mould
2 priority of block.
The utility model has the beneficial effects that: gyroscope is cannon direction, inclination angle provides data, reference index, when
Angle is fired, direction is fired, fires place, firing quantity can be according to need after percussion confirmation data are input to main control unit 0
It fires shells.All antiaircraft guns are unified by controlling by GPRS module 2, wifi module 3 or bluetooth module 4 and network connection
Center control, control centre can be according to the data of weather bureau, and the antiaircraft gun being given only in disaster region emits permission.
External data fires angle for loading antiaircraft gun in specific region referring to memory 8, fires the bound number in direction
According to external data is made of referring to memory 8 u disk and usb reader, u disk is written by special purpose interface in related data, u
After disk is inserted into usb reader, the external data that can only read data is just constituted referring to memory 8, external data is referring to storage
Device 8 provides percussion angle for antiaircraft gun and fires the bound data in direction, to guarantee the Fall Of Shot and flight path of antiaircraft gun
Always it is in safety zone.
Arming signal counter 15, recuperator means reseting sensor 16, percussion confirmation comparator 17, can effectively count ammunition
Actual use amount after that is, each successful launch or bombing bore, can all cause the loss of shell, and the normal loss certainty companion of shell
It is resetted with recuperator means, after percussion order is assigned, after thering is recuperator means to reset generation, it was demonstrated that shell is lost, and command number is fired
Value is consistent with recuperator means reset values, just calculates and fires successfully, by this way, can monitor the service condition of shell at the first time,
Guarantee is provided for safety management.
It is managed collectively by network, percussion parameter is adjusted according to position, can efficiently monitor shell actual use situation, this is
The maximum advantage of the technical program.The data such as parameter, geodata, ammunition consumption are fired by collecting, reference further evaluation,
The scheme of taking precautions against natural calamities can be targetedly improved, is artificial hail-proof rain-increasing, hail protection, effective big data is provided and is supported.
Detailed description of the invention
FIG. 1 is a schematic structural view of the utility model.
Fig. 2 is that the utility model antiaircraft gun is shot towards schematic diagram.
Fig. 3 is that the utility model antiaircraft gun shoots angle schematic diagram.
Specific embodiment
The utility model is described further with reference to embodiments.
A kind of military turn of civilian concentrating type weather intervention antiaircraft gun control device, including steering motor group, gyroscope, electrical turning
Magnet, gyroscope are mounted on antiaircraft gun gun tube, and steering motor group is used to control steering, the inclination angle of antiaircraft gun, and percussion electromagnet is used for
The percussion of antiaircraft gun is controlled, gyroscope is used to acquire the data of steering, inclination angle, and the course changing control end of steering motor group is by turning to control
Device 10 processed is connect with main control unit 0, and the pitch angle control end of steering motor group is connect by pitch angle control device 11 with main control unit 0,
Gyroscope signal output end is connected with main control unit 0 by gyroscope signal decoder 12, and percussion electromagnet control terminal is by hitting
Signalling transmitter 13 is connect with main control unit 0, and 0 chain of main control unit is connected to integrated signal decoder 14, integrated signal decoder
14 first signal inputs are connected with pulse button;Steering motor group, gyroscope, the confession for firing electromagnet, pulse button
Power port is switched by forceful electric power to be connected with the forceful electric power delivery outlet of power supply module 1, and the power supply port of main control unit 0 is switched and supplied by light current
The weak current delivery outlet of electric module 1 is connected;Main control unit 0 is connected with GPRS module 2, locating module, full data storage 7, hits
Signalling counter 15;Emission parameter and firing order pass through 2 remote transmission of GPRS module;The button inputted transmitting life of pulse
Priority is enabled to be higher than the firing order of GPRS module 2.
Main control unit 0 is connected with wifi module 3, bluetooth module 4, and 2 priority of GPRS module is higher than wifi module 3, wifi
3 priority of module is higher than bluetooth module 4, and emission parameter and firing order pass through GPRS module 2, wifi module 3 or bluetooth module 4
Input.
Main control unit 0 connect locating module be GPS navigation module 5, Beidou navigation module 6, GPS navigation module 5 it is excellent
First grade be lower than Beidou navigation module 6, GPS navigation module 5, Beidou navigation module 6 be equipped with it is independent start switch, when corresponding
It starts switch one of them Beidou navigation module 6 of GPS navigation module 5 after one of them is closed to stop working, when corresponding starting
Switch is all turned on, and adopts information according to priority.
Full data storage 7 is equipped with usb outside access interface, and the usb outside access interface of full data storage 7 is single
To interface is read, pass through hardware circuit, restricted information write-in.
Main control unit 0 is connected with external data referring to memory 8, data comparator 9, and external data is referring to memory 8
Interface is read in individual event, passes through hardware circuit, restricted information write-in;Data comparator 9 is with external data referring to the ginseng in memory 8
It is bound according to numerical value, geographic position data, inclination angle, steering data is verified, is more than bound, then stops to emit.
Main control unit 0 is connected with recuperator means reseting sensor 16, percussion confirmation comparator 17, recuperator means reseting sensor 16
Signal input part is connected with recuperator means reseting sensor, and recuperator means reseting sensor issues a pulse signal, works as integrated signal
14 first signal input of decoder is connected with after pulse button is pressed, and percussion electromagnet drives cannon percussion, hits simultaneously
Signalling counter 15, which counts, adds one, and while the counting of arming signal counter 15 adds one, recuperator means reseting sensor 16 is received
Signal, the percussion confirmation confirmation of comparator 17 this time fires successfully, when percussion confirmation comparator 17 only receives arming signal counter
15 countings plus a signal, do not receive 16 signal of recuperator means reseting sensor, then assert and this time emit, ammunition is duds, system lock
Extremely, it removes barriers after restarting, restores normal.
14 second signal input port of integrated signal decoder is connected with Touch Screen, and Touch Screen carries decoder, touch-control
Screen is inputted for being manually entered emission parameter, emission parameter by Touch Screen, and the priority of Touch Screen is higher than GPRS mould
2 priority of block.
In practical operation, according to meteorological data, the antiaircraft gun and its control system in specific region are activated, with an antiaircraft gun
For.
After antiaircraft gun activation, real data is put into external data referring to memory 8, for height as needed by operator
Big gun installation provision quantity shell opens the switch on power supply module 1, activation system, according to GPRS module 2 after system starting later
The activation signal of transmission according to circumstances fires shells after unlocking.
Transmitting, which can be, remotely sends a signal to the operation of GPRS module 2, is also possible to site operation personnel according to manipulator
Volume fires manually after being manually entered emission parameter.
When taking precautions against hail, need to want batch input parameter using ladder or fan-shaped emission, based on remotely controlling, people
Supplemented by work operation.
In hail-proof rain-increasing, launch accuracy, tranmitting frequency is of less demanding, by gunner's experience, based on manual operation, far
Supplemented by journey operation.
After the completion of operation, the time emitted every time, inclination angle, direction, geographical location, percussion situation are by main control unit 0
It is no successfully to fire and always fire number, it fires the successfully data such as number and uploads network.
After upload, antiaircraft gun is locked, antiaircraft gun can not just emit at this time, be activated until next time.
It, can induction and conclusion most effective Artificial Hail Suppression increasing rain side by the accumulation combination weather information of long-time data
Case prevents and treats hail scheme, solves the problem of that hail-proof rain-increasing amount is not achieved expected requirement and cannot effectively prevent hail, while also tight
Lattice supervise shell, in the case where guaranteeing safety, by military equipment civil nature, allow military equipment to be modernization construction, benefit ground
Fang Jingji improves people life and contributes.
Claims (7)
1. a kind of military turn of civilian concentrating type weather intervenes antiaircraft gun control device, including steering motor group, gyroscope, percussion electromagnetism
Iron, gyroscope are mounted on antiaircraft gun gun tube, and the steering motor group is used to control steering, the inclination angle of antiaircraft gun, the percussion electromagnetism
Iron is used to control the percussion of antiaircraft gun, and the gyroscope is used to acquire the data of steering, inclination angle, it is characterised in that: the steering electricity
The course changing control end of unit is connect by steering controller (10) with main control unit (0), the pitch angle control of the steering motor group
End is connect by pitch angle control device (11) with main control unit (0), and the gyroscope signal output end and main control unit (0) pass through top
Spiral shell instrument signal decoder (12) is connected, and the percussion electromagnet control terminal passes through arming signal transmitter (13) and main control unit
(0) it connects, main control unit (0) chain is connected to integrated signal decoder (14), and the integrated signal decoder (14) first is believed
Number input port is connected with pulse button;The steering motor group, gyroscope, the power supply port for firing electromagnet, pulse button
It is switched by forceful electric power and is connected with the forceful electric power delivery outlet of power supply module (1), the power supply port of the main control unit (0) is switched by light current
It is connected with the weak current delivery outlet of power supply module (1);The main control unit (0) is connected with GPRS module (2), locating module, complete
Data storage (7), arming signal counter (15);Emission parameter and firing order pass through GPRS module (2) remote transmission;Institute
State the firing order that the button inputted firing order priority of pulse is higher than GPRS module (2).
2. military turn of one kind civilian concentrating type weather according to claim 1 intervenes antiaircraft gun control device, it is characterised in that:
The main control unit (0) is connected with wifi module (3), bluetooth module (4), and GPRS module (2) priority is higher than wifi module
(3), wifi module (3) priority is higher than bluetooth module (4), emission parameter and firing order by GPRS module (2),
Wifi module (3) or bluetooth module (4) input.
3. military turn of one kind civilian concentrating type weather according to claim 2 intervenes antiaircraft gun control device, it is characterised in that:
The locating module of main control unit (0) connection is GPS navigation module (5), Beidou navigation module (6), the GPS navigation module
(5) priority is lower than Beidou navigation module (6), and the GPS navigation module (5), Beidou navigation module (6) are equipped with independent
It starts switch, starts switch one of GPS navigation module (5) Beidou navigation module (6) after one of them is closed when corresponding
It stops working, when corresponding start switch is all turned on, information is adopted according to priority.
4. military turn of one kind civilian concentrating type weather according to claim 3 intervenes antiaircraft gun control device, it is characterised in that:
The full data storage (7) is equipped with usb outside access interface, the usb outside access interface of the full data storage (7)
Unidirectionally to read interface, pass through hardware circuit, restricted information write-in.
5. military turn of one kind civilian concentrating type weather according to claim 4 intervenes antiaircraft gun control device, it is characterised in that:
The main control unit (0) is connected with external data referring to memory (8), data comparator (9), and the external data is referring to storage
Device (8) is that interface is read in individual event, passes through hardware circuit, restricted information write-in;The data comparator (9) is with external data reference
Reference numerical value in memory (8) is bound, verifies to geographic position data, inclination angle, steering data, is more than up and down
Limit, then stop to emit.
6. military turn of one kind civilian concentrating type weather according to claim 5 intervenes antiaircraft gun control device, it is characterised in that:
The main control unit (0) is connected with recuperator means reseting sensor (16), percussion confirmation comparator (17), and the recuperator means, which resets, to be passed
Sensor (16) signal input part is connected with recuperator means reseting sensor, and the recuperator means reseting sensor issues a pulse letter
Number, after (14) first signal input of integrated signal decoder, which is connected with pulse button, to be pressed, percussion electromagnet is driven
Cannon percussion, while arming signal counter (15) counts and adds one, while arming signal counter (15) counting adds one,
Recuperator means reseting sensor (16) receives signal, and percussion confirmation comparator (17) confirmation this time fires successfully, when percussion is true
Recognize comparator (17) and only receive arming signal counter (15) counting plus a signal, does not receive recuperator means reseting sensor (16) letter
Number, then assert and this time emit, ammunition is duds, and system is locked, is removed barriers after restarting, and restores normal.
7. military turn of one kind civilian concentrating type weather according to claim 6 intervenes antiaircraft gun control device, it is characterised in that:
Integrated signal decoder (14) the second signal input port is connected with Touch Screen, and the Touch Screen carries decoder, institute
It states Touch Screen and is inputted for being manually entered emission parameter, emission parameter by Touch Screen, the priority of the Touch Screen
Higher than GPRS module (2) priority.
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CN201820950537.8U CN208521187U (en) | 2018-06-20 | 2018-06-20 | A kind of military turn of civilian concentrating type weather intervention antiaircraft gun control device |
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CN201820950537.8U CN208521187U (en) | 2018-06-20 | 2018-06-20 | A kind of military turn of civilian concentrating type weather intervention antiaircraft gun control device |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
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CN110307747A (en) * | 2019-06-21 | 2019-10-08 | 随州大方精密机电工程有限公司 | A kind of DF37 millimeters of antiaircraft gun elevating mechanism locking device and control method |
CN110658534A (en) * | 2019-11-15 | 2020-01-07 | 辽宁工程技术大学 | ARM-based artificial rainfall cannonball launching position calculating instrument and using method thereof |
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2018
- 2018-06-20 CN CN201820950537.8U patent/CN208521187U/en active Active
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110307747A (en) * | 2019-06-21 | 2019-10-08 | 随州大方精密机电工程有限公司 | A kind of DF37 millimeters of antiaircraft gun elevating mechanism locking device and control method |
CN110658534A (en) * | 2019-11-15 | 2020-01-07 | 辽宁工程技术大学 | ARM-based artificial rainfall cannonball launching position calculating instrument and using method thereof |
CN110658534B (en) * | 2019-11-15 | 2023-01-17 | 辽宁工程技术大学 | ARM-based artificial rainfall cannonball launching position calculating instrument and using method thereof |
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