CN220701030U - Liftable aircraft detection and reaction emergency mobile command system - Google Patents
Liftable aircraft detection and reaction emergency mobile command system Download PDFInfo
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- CN220701030U CN220701030U CN202321932509.0U CN202321932509U CN220701030U CN 220701030 U CN220701030 U CN 220701030U CN 202321932509 U CN202321932509 U CN 202321932509U CN 220701030 U CN220701030 U CN 220701030U
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Abstract
The utility model provides a liftable aircraft detection and reaction emergency mobile command system, which comprises an aircraft detection and reaction system module: the reaction host adopts an industrialized design mode, and an internal integrated ring control system and an automatic alarm system are adopted; erecting an external antenna platform of a host on a lifting platform, and lifting the platform to a high degree; the equipment cabinets of the whole system are all in a separation design, the power distribution cabin, the counter-control host system cabin, the equipment cabin and the lifting platform control system cabin are mutually independent and separated on the module partition, the module systems are independently deployed and tightly combined into a complete control link, and a data acquisition unit and a control unit are arranged in the host.
Description
Technical Field
The utility model relates to the technical field of aircraft detection and countercheck, in particular to a lifting aircraft detection and countercheck emergency mobile command system.
Background
The lifting aircraft detection and reaction emergency mobile command system is deployed behind a van-type mobile command vehicle, when tasks such as emergency sudden handling or large security are carried out, the vehicle can be driven to a designated task place or a security team can be followed to execute the tasks, and when the system is used, no matter whether equipment at the rear of the vehicle body is lifted, the equipment can work normally, and the requirements of different operation scenes can be met. Most of existing aircraft detection and countercheck systems are fixedly deployed, and are limited by deployment sites, equipment often has insufficient detection capability on signals of an invading aircraft or insufficient countercheck capability on the invading aircraft during working, the equipment is deployed on an outdoor site for a long time, higher requirements are provided for waterproof, dustproof and rust-proof indexes of the equipment, and a plurality of inconvenient factors are provided for maintenance and maintenance of the equipment in the later period. For the existing mobile aircraft detection and reaction system, the existing mode is mechanical fixed installation, and the installation mode increases the overall height of the vehicle, so that the system is not beneficial to operation under multiple scene conditions. Based on the two conditions, the utility model is designed, an aircraft detection and reaction system is arranged behind the carriage of the emergency mobile command vehicle, the equipment antenna is arranged in a lifting mode, the top of the vehicle body is cut open, the cabin door is manufactured, and a rainproof mechanism is additionally arranged at the top end and the cabin door of the equipment antenna, so that the situation that water leakage and a large amount of dust accumulation can not occur in the equipment cabin in the vehicle after the equipment cabin is lifted or recovered, the functions of water prevention and dust prevention are achieved to a certain extent, and the cleaning, the reliability and the stable operation of the equipment electric cabinet in the vehicle are ensured. The stabilizing mechanism is added at the position of the lifting platform of the rear equipment, so that when the equipment is in a lifting state and the vehicle runs at a high speed, the stability problems of equipment such as jolt, shake and the like of the rear equipment can be avoided.
Disclosure of Invention
The utility model mainly provides a lifting aircraft detection and reaction emergency mobile command system which is used for solving the technical problems in the background technology.
The technical scheme adopted for solving the technical problems is as follows: an emergency mobile command system for detecting and countering a liftable aircraft comprises
An aircraft detection and reaction system module: the reaction host adopts an industrialized design mode, and an internal integrated ring control system and an automatic alarm system are adopted; erecting an external antenna platform of a host on a lifting platform, and lifting the platform to a high degree;
the equipment cabinets of the whole system are all in a separation design, a power distribution cabin, a counter-control host system cabin, an equipment cabin and a lifting platform control system cabin are mutually and independently separated on a module partition, each module system is independently deployed and tightly combined into a complete control link, and a data acquisition unit and a control unit are arranged in a host; and a sealing structure is additionally arranged above the antenna table, and the whole system adopts a strong and weak electricity separation mode in the aspect of power distribution.
Furthermore, each equipment cabin is internally provided with an independent environmental control system, the environmental variable detection sensor sends the acquired environmental parameter information to the environmental control system, and the environmental control system automatically adjusts environmental conditions such as temperature and humidity in the equipment cabin according to preset parameters; the control console main control panel is reserved with a multifunctional debugging interface, which comprises a serial port, a network port and a USB interface; the control system adopted by the lifting platform unit is a servo control system matched with a servo motor; the whole system is controlled by the control panel of the console, the control buttons of different devices are centralized and operated in a partitioning mode, and a master control person can conveniently master the instant states and the control switching of the states of the different devices at any time.
Compared with the prior art, the utility model has the beneficial effects that:
the system is deployed behind the carriage of the van-type mobile command vehicle, when the requirement of executing the reverse task of the aircraft exists, the lifting of the system can be controlled by the central control panel, and when the vehicle normally runs at ordinary times, the system can be controlled to descend and be completely recovered into the rear of the carriage of the vehicle, so that the requirement of limiting the height of the vehicle in some special operation scenes is avoided. The system is lifted and lowered by controlling the motor to rotate forwards and reversely through the servo driver, the lifting platform is driven to synchronously move on the 4 vertical transmission shafts, the travel value of the motor is preset in the control system, and meanwhile, detection sensors are arranged at the positions of the lifting and lowering critical points, so that the lifting mechanism is ensured not to exceed the specified running stroke. The control software of the system is deployed in a microcomputer in a power distribution cabinet at the rear of the vehicle body, a control picture is output to a control console display screen at the front of the vehicle body through an HDMI extension cable, the control console is integrated into an integrated folding table, and an operator can perform system operation, control and the like on the control console.
Drawings
FIG. 1 is an electrical schematic diagram I of the present utility model;
FIG. 2 is an electrical schematic II of the present utility model;
fig. 3 is an electrical schematic diagram iii of the present utility model.
Detailed Description
In order that the utility model may be more fully understood, several embodiments of the utility model will be described below with reference to the accompanying drawings, but the utility model may be embodied in various forms and is not limited to the embodiments described herein, but rather is provided in order that the disclosure may be more thorough.
1-3, a liftable aerial vehicle detection and reaction emergency mobile command system is provided, which adjusts the deployment mode to vehicle-mounted mobile deployment based on the deployment mode of traditional aerial vehicle detection and reaction equipment, and hardware equipment such as a detection and reaction aerial platform, a lifting mechanism control system, an environment detection sensor and environmental control system, a console control panel, a microcomputer, an HDMI repeater and the like is added.
The system power supply adopts a double-chain power supply mode, a vehicle starting battery is connected to the anode and the cathode of a storage battery in a power distribution cabinet after passing through a double-battery isolator, when the vehicle is started, a vehicle generator can synchronously charge the storage battery in the rear power distribution cabinet, the problem that the vehicle starting battery is fed can be prevented by using the double-battery isolator, two 100AH storage batteries are connected in parallel in the rear power distribution cabinet, the anode and the cathode of the battery are finally connected into an inverter, inversion from 12V direct current to 220V alternating current is realized, and finally 220V stable alternating current is output for the vehicle-mounted system. The whole set of system is in an isolation form in strong and weak current design, and the system is all grounded, so that the interference problem is avoided, and the system stability is improved.
The rear lower part of the vehicle body is provided with a power distribution cabin, a counter-control main system cabin, an equipment cabin and a lifting platform control system cabin, and the equipment in each cabin is arranged in a modularized mode. The power distribution cabin is internally provided with equipment such as an inverter, a storage battery and the like, mainly provides power supply for the system, and is provided with a fire-fighting module so as to cope with emergency. The miniature high-performance computer, the HDMI repeater, the industrial switch, the power amplifier, the networking equipment and the like are mainly deployed in the equipment cabin, the high-performance computer and the networking equipment are connected to the industrial switch through network cables, the power amplifier is connected to the high-performance computer, alarm sound warning is provided for an operator, the HDMI cable output by the high-performance computer is connected to the HDMI repeater, the HDMI cable output by the repeater is connected to the console display screen, and software control interface display is provided for the operator. The anti-system host system is deployed in the anti-system host system cabin, the shock absorbing mechanism is arranged below the anti-system host system cabin, so that the damage or drop of internal equipment elements is prevented when a vehicle runs at a high speed or on a bumpy road section, power supply of the system is provided for the anti-system host system cabin by the power distribution cabin, cables such as external communication, control and detection of the host system are connected to the antenna platform above the anti-system host system through the drag chain, the antenna platform is arranged above the lifting system, and in the lifting process, the cables move along with the drag chain, so that the condition of cable confusion or scraping and collision cannot occur. A sealing structure is arranged above the antenna table, so that the waterproof and dustproof effects can be achieved. The lifting platform realizes synchronous horizontal lifting action by means of four vertical guide rails, detection sensors are arranged at the upper critical point position and the lower critical point position of the lifting platform, the condition that the equipment is damaged by over-travel operation is avoided, the lifting action is realized by means of forward and reverse rotation of a servo motor during operation of the lifting platform, and the precision control of the motion travel is realized during operation. The lifting platform control system cabin serves as a platform motion control core, bears lifting platform automatic motion control tasks, comprises equipment such as a servo controller, a power distribution system, a control system and the like, is connected with a servo motor through a drag chain wiring by using outgoing signals, control cables and the like, and is connected with an industrial switch through a network cable to realize system network interconnection.
All sensor detection signals and control modules of the system are all accessed to the main industrial switch through serial ports or shielding network cables and the like, the micro high-performance computer is also accessed to the main industrial switch through the shielding network cables, and the micro high-performance computer is used for completing analysis of all sensor acquisition signals and issuing control instructions to all modules. Meanwhile, the micro high-performance computer is internally provided with aircraft detection and countercheck control software, radio signals detected by the system can be displayed in real time, analysis of acquired signals can be completed according to a database arranged in the system, warning information is fed back to an operator in real time, a control end operator carries out subsequent processing according to conditions, the whole system can realize unmanned automatic on duty, and manual instructions can be issued according to different scenes. The system power supply and the motion control part are interconnected with the console main control panel through a network protocol, and an operator can realize the functions of system on/off, lifting platform one-key lifting and descending control, system debugging and the like through the main control panel. The folding table is deployed at the control table position, can be unfolded when in use, and can be stored for realizing space maximization after the task is finished. The external control host can be connected with the main control panel interface through a network cable to acquire, debug, control and other contents of the system information, and the external control host can execute the partial operation contents only by holding a security key in view of system security.
Principle of operation: the integrated cabinet is adopted below the system, the system power supply module, the equipment unit module and the like are arranged in a zoned mode, the power supply part and the like are arranged in a power-on-power-off mode, and the influence of an interference source on equipment signal transmission and control can be greatly avoided. A set of lifter is arranged above the integrated cabinet, and the lifting system consists of a transmission screw rod, a motor, a speed reducer, a servo control unit and the like and mainly plays roles in automatic lifting and descending of equipment. The antenna platform is disposed above the lifting platform, the antenna platform is fixedly connected with the lifting platform through the damping mechanism, a communication cable, a control cable and the like in a control box below the antenna platform are connected with a host in a device cabinet below the antenna platform through a drag chain, a rainproof outer cover is arranged above the antenna platform, and after the lifting platform descends, the rainproof outer cover can perfectly fit with the outer edge of a vehicle sky window, so that a rainproof and dustproof effect is achieved. A distance detection sensor is arranged at the edge of the lifting platform, so that the overtravel movement of the mechanical structure can be protected secondarily, and when the sensor triggers or detects that the stroke amount exceeds a set value, the operation of the mechanical mechanism is stopped.
While the utility model has been described in connection with exemplary embodiments, it will be apparent that the practice of the utility model is not limited thereto, but rather, it is intended to cover such insubstantial modifications as may be made by the method concepts and teachings of the utility model, or as may be applied to other applications without modification, without departing from the scope of the utility model.
Claims (6)
1. An emergency mobile command system for detecting and countering a liftable aircraft comprises an aircraft detecting and countering system module: the reaction host adopts an industrialized design mode, and an internal integrated ring control system and an automatic alarm system are adopted; erecting an external antenna platform of a host on a lifting platform, and lifting the platform to a high degree;
the equipment cabinets of the whole system are all in a separation design, the power distribution cabin, the counter-control host system cabin, the equipment cabin and the lifting platform control system cabin are mutually independent and separated on the module partition, the module systems are independently deployed and tightly combined into a complete control link, and a data acquisition unit and a control unit are arranged in the host.
2. The liftable aircraft detection and reaction emergency mobile command system according to claim 1, wherein: and a sealing structure is additionally arranged above the antenna table.
3. The liftable aircraft detection and reaction emergency mobile command system according to claim 1, wherein: the whole system adopts a strong and weak electricity separation mode in the aspect of power distribution.
4. The liftable aircraft detection and reaction emergency mobile command system according to claim 1, wherein: each equipment cabin is internally provided with an independent environmental control system, the environmental variable detection sensor sends acquired environmental parameter information to the environmental control system, and the environmental control system automatically adjusts the temperature and humidity environmental conditions in the equipment cabin according to preset parameters.
5. The liftable aircraft detection and reaction emergency mobile command system according to claim 1, wherein: the control system adopted by the lifting platform unit is a servo control system matched with a servo motor.
6. The liftable aircraft detection and reaction emergency mobile command system according to claim 1, wherein: the whole system is controlled by a console main control panel, the control buttons of different devices are centralized and operated in a partitioning mode, so that a master can conveniently master the instant states and the control switching of the states of the different devices at any time, and a multifunctional debugging interface comprising a serial port, a network port and a USB interface is reserved on the console main control panel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321932509.0U CN220701030U (en) | 2023-07-21 | 2023-07-21 | Liftable aircraft detection and reaction emergency mobile command system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321932509.0U CN220701030U (en) | 2023-07-21 | 2023-07-21 | Liftable aircraft detection and reaction emergency mobile command system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220701030U true CN220701030U (en) | 2024-04-02 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321932509.0U Active CN220701030U (en) | 2023-07-21 | 2023-07-21 | Liftable aircraft detection and reaction emergency mobile command system |
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| Country | Link |
|---|---|
| CN (1) | CN220701030U (en) |
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2023
- 2023-07-21 CN CN202321932509.0U patent/CN220701030U/en active Active
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