CN207817495U - Shadow aircraft airborne flame bullet launch control unit - Google Patents
Shadow aircraft airborne flame bullet launch control unit Download PDFInfo
- Publication number
- CN207817495U CN207817495U CN201820308690.0U CN201820308690U CN207817495U CN 207817495 U CN207817495 U CN 207817495U CN 201820308690 U CN201820308690 U CN 201820308690U CN 207817495 U CN207817495 U CN 207817495U
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- China
- Prior art keywords
- module
- control unit
- microprocessor
- launch control
- flame bullet
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Abstract
The utility model is related to flame bullet emission control monitoring technology fields, it is a kind of shadow aircraft airborne flame bullet launch control unit, it includes video monitoring apparatus, launch control unit and execution control device, launch control unit includes babinet, first microprocessor, power module, voltage isolated location and control module, the first display module and the first keyboard input module are separately installed on babinet, video monitoring apparatus is electrically connected with first microprocessor, power module is electrically connected with first microprocessor and voltage isolated location respectively, voltage isolated location and first microprocessor are electrically connected with control module；It includes the second microprocessor, detection module, drive module, the second display module, ignition module and second keyboard input module etc. to execute control unit.The utility model has the characteristics that monitor in real time, failure rate is low, simple installation, operating efficiency are high, and compensating for current shadow aircraft airborne and sowing operation can not carry out monitoring in real time and the not high defect of operating efficiency.
Description
Technical field
The utility model is related to flame bullet emission control monitoring technology fields, are a kind of shadow aircraft airborne flame bullet emission control
Device.
Background technology
The method and apparatus of existing Weather modification operation mainly have：1, ground cigarette stove operation, it is to use ground cigarette stove
Device is increased rain artificially by the method for the plume that burns to realize, uprush and diffusion of the catalyst particles such as AgI by burning
It is admitted to High aititude, alpine region landform cloud layer carries out influence operation；Its main feature is that job safety, cost is relatively low；It is insufficient
It is：By landform cloud layer meteorologic parameter is influenced, coverage is more narrow, is not suitable with large area Weather modification operation；2、
Rocket or antiaircraft gun operation, it is that a large amount of high-efficiency artificial nucleus are quickly and effectively sent into target cloud layer by rocket or antiaircraft gun,
Feature is not limited by weather condition, can all-weather operation, shortcoming is limited by road, orographic condition etc., operation
It is less efficient, influence area is smaller.
Existing flame bullet mission controller uses mechano-electronic structure, and often transmitting is primary to be needed to reset, and setting is complicated,
Reliability is low, does not also have the function of display, execute control instruction it is complete after, can not accurately judge whether flame bullet lights a fire transmitting,
It is not high because often resulting in operation accuracy rate at this time.
Invention content
The utility model provides a kind of shadow aircraft airborne flame bullet launch control unit, overcome the above-mentioned prior art it
Deficiency can be solved the problems, such as effectively that flame bullet emission process can not be monitored in real time, further solve flame bullet and shoot
Afterwards because there is poor contact, staff cannot check out in time, the problem to cause flame bullet launcher reliability low and
Complicated, the inconvenient for use problem of launch control unit setting.
The technical solution of the utility model is realized by following measures：A kind of shadow aircraft airborne flame bullet transmitting control
Device processed, including video monitoring apparatus, launch control unit and execution control device, launch control unit include babinet, setting
First microprocessor, power module, voltage isolated location in babinet and control module, pacify respectively on the lateral surface of babinet
Equipped with the first display module and the first keyboard input module, video monitoring apparatus is electrically connected with first microprocessor, power module
It is electrically connected respectively with first microprocessor and voltage isolated location, voltage isolated location and first microprocessor are and control module
Electrical connection；Execute control unit include the second microprocessor, detection module, drive module, the second display module, ignition module and
Second keyboard input module, control module are connected with the second microprocessor communication, and detection module, drive module and the second button are defeated
Enter module to be electrically connected with the second microprocessor, drive module is electrically connected with ignition module and the second display module respectively.
Here is the further optimization and/or improvements to above-mentioned utility model technical solution：
Above-mentioned further includes wireless communication module, control module and the second microprocessor module communication link by radio communication
It connects.
Above-mentioned further includes RS485 interface modules, and control module passes through RS485 interface module communication links with the second microprocessor
It connects.
Above-mentioned video monitoring apparatus includes at least one low temperature camera, each low temperature camera with the first microcontroller
It is electrically connected with the second microprocessor.
Above-mentioned low temperature camera is four.
Above-mentioned first display module and the second display module are four split screen liquid crystal displays.
The utility model is by mutually tying current steady, ripe integrated circuit technique with Video Supervision Technique two parts
It closes, by the way that the video monitoring apparatus for monitoring flame bullet is arranged on shadow aircraft, realizes to the real-time of flame bullet emission process
Monitoring provides the overall process of flame bullet transmitting to staff in real time, effectively prevents the error of flame bullet transmitting.First key-press input
Module is provided with eight groups of buttons, and the intellectualized operation of flame bullet control way is realized for combination to be arranged；First keyboard input module
It after being provided with, clicks and confirms button, you can complete setting operation；Meanwhile detection module has the detection side of 400 road flame bullets
Formula is solved the problems, such as not determining whether poor contact after flame bullet is shot, be improved work efficiency.Execute control device with
Launch control unit communicates, and the second microcontroller output interface is electrically connected with drive module, passes through drive module drive ignition mould
Block is, it can be achieved that control ignition module.The utility model has the spies such as low monitoring in real time, failure rate, simple installation, operating efficiency height
Point compensates for current shadow aircraft airborne and sows operation and there was only single emission mode and can not carry out monitoring in real time and operation effect
The not high defect of rate.
Description of the drawings
Attached drawing 1 is the circuit control block diagram of the best embodiment of the utility model.
Specific implementation mode
The utility model is not limited by following embodiments, can technical solution according to the present utility model and actual conditions
Determine specific embodiment.
The utility model is further described with reference to embodiment and attached drawing：
As shown in Fig. 1, which includes video monitoring apparatus, emission control dress
Set and execute control device, launch control unit includes babinet, the first microprocessor, power module, the electricity that are arranged in babinet
Isolated location and control module are pressed, the first display module and the first key-press input mould are separately installed on the lateral surface of babinet
Block, the video monitoring apparatus are electrically connected with first microprocessor, and power module is isolated with first microprocessor and voltage respectively
Unit is electrically connected, and voltage isolated location and first microprocessor are electrically connected with control module；It includes second to execute control unit
Microprocessor, detection module, drive module, the second display module, ignition module and the second keyboard input module, control module and
Second microprocessor communication connects, and detection module, drive module and the second keyboard input module are electrically connected with the second microprocessor
It connects, drive module is electrically connected with ignition module and the second display module respectively.
By the way that video monitoring apparatus is arranged, the moving image of the flame bullet of monitoring is sent to first microprocessor, then pass through
First display module is shown, the transmitting situation of flame bullet is observed for staff.
Here detection module and ignition module is electrically connected with the launching tube of flame bullet, and detection module is for detecting flame bullet
No to install successfully and testing result is sent to the second microprocessor, if detection module detects flame, bullet is fitted without success,
Then the second microprocessor does not send ignition control instruction to ignition module, to reduce the fault rate of flame bullet transmitting.Here
Ignition module includes ignition relay and its peripheral circuit, and the second microprocessor is by drive module drive ignition relay to flame
Snap into row igniting emission control.
The utility model is by mutually tying current steady, ripe integrated circuit technique with Video Supervision Technique two parts
It closes, by the way that the video monitoring apparatus for monitoring flame bullet is arranged on shadow aircraft, realizes to the real-time of flame bullet emission process
Monitoring provides the overall process of flame bullet transmitting to staff in real time, effectively prevents the error of flame bullet transmitting.First key-press input
Module is provided with eight groups of buttons, and the intellectualized operation of flame bullet control way is realized for combination to be arranged；First keyboard input module
It after being provided with, clicks and confirms button, you can complete setting operation；Meanwhile detection module has the detection side of 400 road flame bullets
Formula avoids occurring poor contact after being shot there are flame bullet because of launch control unit, and staff cannot check out in time, to
The problem for causing flame bullet launcher reliability low effectively increases working efficiency by the way that detection module is arranged.Execute control device with
Launch control unit communicates, and the second microcontroller output interface is electrically connected with drive module, passes through drive module drive ignition mould
Block is, it can be achieved that control ignition module.The utility model has the spies such as low monitoring in real time, failure rate, simple installation, operating efficiency height
Point compensates for current shadow aircraft airborne and sows operation and there was only single emission mode and can not carry out monitoring in real time and operation effect
The not high defect of rate.
Above-mentioned shadow aircraft airborne flame bullet launch control unit can be advanced optimized or/and be changed according to actual needs
Into：
As shown in Fig. 1, further include wireless communication module, control module and the second microprocessor module by radio communication
Communication connection.
As shown in Fig. 1, further include RS485 interface modules, control module and the second microprocessor pass through RS485 interface moulds
Block communicates to connect.In the actual course of work, it is unstable network signal often occur, the case where influencing flame bullet normal transmission, leads to
It is more stable to cross the control signal transmission sent to the second microprocessor using the control module of technical grade RS485 bus communications, really
Flame bullet normal transmission is protected, the accident for occurring to reduce working efficiency is avoided.
As shown in Fig. 1, video monitoring apparatus includes at least one low temperature camera, and each low temperature camera is with first
Microcontroller and the electrical connection of the second microprocessor.Here camera uses low temperature camera, can also make at a temperature of -40 spend
With, it is reliable and stable by way of wired connection, it is easy for installation.
As shown in Fig. 1, low temperature camera is four.
As shown in Fig. 1, the first display module and the second display module are four split screen liquid crystal displays.Here low temperature
Camera may be provided with four, can check the image of each low temperature camera acquisition simultaneously using four split screen liquid crystal displays,
It is convenient to facilitate, and saves the time.
The above technical characteristic constitutes the most preferred embodiment of the utility model, with stronger adaptability and best implementation
Effect can increase and decrease non-essential technical characteristic, to meet the needs of different situations according to actual needs.
Claims (10)
1. a kind of shadow aircraft airborne flame bullet launch control unit, it is characterised in that filled including video monitoring apparatus, emission control
Set and execute control device, launch control unit includes babinet, the first microprocessor, power module, the electricity that are arranged in babinet
Isolated location and control module are pressed, the first display module and the first key-press input mould are separately installed on the lateral surface of babinet
Block, video monitoring apparatus are electrically connected with first microprocessor, power module respectively with first microprocessor and voltage isolated location
Electrical connection, voltage isolated location and first microprocessor are electrically connected with control module；It includes second micro- place to execute control unit
Manage device, detection module, drive module, the second display module, ignition module and the second keyboard input module, control module and second
Microprocessor communication connects, and detection module, drive module and the second keyboard input module are electrically connected with the second microprocessor, drives
Dynamic model block is electrically connected with ignition module and the second display module respectively.
2. shadow aircraft airborne flame bullet launch control unit according to claim 1, it is characterised in that further include channel radio
Believe module, module communicates to connect control module by radio communication with the second microprocessor.
3. shadow aircraft airborne flame bullet launch control unit according to claim 1 or 2, it is characterised in that further include
RS485 interface modules, control module are communicated to connect with the second microprocessor by RS485 interface modules.
4. shadow aircraft airborne flame bullet launch control unit according to claim 1 or 2, it is characterised in that video monitoring fills
It sets including at least one low temperature camera, each low temperature camera is electrically connected with the first microcontroller and the second microprocessor.
5. shadow aircraft airborne flame bullet launch control unit according to claim 3, it is characterised in that video monitoring apparatus
Including at least one low temperature camera, each low temperature camera is electrically connected with the first microcontroller and the second microprocessor.
6. shadow aircraft airborne flame bullet launch control unit according to claim 4, it is characterised in that the low temperature camera shooting
Head is four.
7. shadow aircraft airborne flame bullet launch control unit according to claim 5, it is characterised in that the low temperature camera shooting
Head is four.
8. the shadow aircraft airborne flame bullet launch control unit according to claims 1 or 2 or 5 or 6 or 7, it is characterised in that
First display module and the second display module are four split screen liquid crystal displays.
9. shadow aircraft airborne flame bullet launch control unit according to claim 3, it is characterised in that the first display module
It is four split screen liquid crystal displays with the second display module.
10. shadow aircraft airborne flame bullet launch control unit according to claim 4, it is characterised in that the first display module
It is four split screen liquid crystal displays with the second display module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820308690.0U CN207817495U (en) | 2018-03-07 | 2018-03-07 | Shadow aircraft airborne flame bullet launch control unit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820308690.0U CN207817495U (en) | 2018-03-07 | 2018-03-07 | Shadow aircraft airborne flame bullet launch control unit |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207817495U true CN207817495U (en) | 2018-09-04 |
Family
ID=63321266
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820308690.0U Expired - Fee Related CN207817495U (en) | 2018-03-07 | 2018-03-07 | Shadow aircraft airborne flame bullet launch control unit |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207817495U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109725581A (en) * | 2019-01-22 | 2019-05-07 | 北京电子工程总体研究所 | A kind of Intelligent unattended launch control system based on 4G technology |
-
2018
- 2018-03-07 CN CN201820308690.0U patent/CN207817495U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109725581A (en) * | 2019-01-22 | 2019-05-07 | 北京电子工程总体研究所 | A kind of Intelligent unattended launch control system based on 4G technology |
| CN109725581B (en) * | 2019-01-22 | 2020-09-18 | 北京电子工程总体研究所 | Intelligent unmanned emission control system based on 4G technology |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180904 Termination date: 20210307 |