CN214148996U - Inflatable air-defense missile launching vehicle simulation system - Google Patents
Inflatable air-defense missile launching vehicle simulation system Download PDFInfo
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- CN214148996U CN214148996U CN202120005908.7U CN202120005908U CN214148996U CN 214148996 U CN214148996 U CN 214148996U CN 202120005908 U CN202120005908 U CN 202120005908U CN 214148996 U CN214148996 U CN 214148996U
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Abstract
The utility model discloses an inflatable air-defense missile launching vehicle simulation system belongs to the shooting training device field. The inflatable air-defense missile launching vehicle simulation system comprises a simulation target, a sensing assembly and an inflating device, wherein at least one air chamber is arranged in an inner cavity of the simulation target, the sensing assembly is arranged in the at least one air chamber, each air chamber in the at least one air chamber and the sensing assembly are connected with the inflating device, and the inflating device is in signal connection with an upper computer of a command center. The utility model provides an inflatable air-defense missile launching vehicle simulation system which adopts an inflatable air bag structure and has the characteristics of visible light, infrared radiation and radar scattering similar to those of a physical air-defense missile launching vehicle, and the framework of the simulation system is light high-strength airtight rubberized fabric so as to ensure the integral air tightness; and the airtight rubber coating cloth of the inflatable air-defense missile launching vehicle simulation system is coated with PVC on two sides, and has the performances of high airtightness, wear resistance, high and low temperature resistance, sunlight resistance, small permanent deformation, easiness in shaping and processing and the like.
Description
Technical Field
The utility model relates to a shooting training technical field, in particular to inflatable air defense missile launching vehicle analog system.
Background
The military camouflage technology has a long history, and as the high-altitude detection equipment is widely used, huge pressure is brought to both parties of the battle, so that the military target marking model is manufactured by adopting various cheap materials and is used for puzzling the military detection of the enemy and inducing the enemy to carry out firepower attack, and the purposes of protecting the military target safety of the enemy and consuming the battle resources of the enemy are achieved.
In modern war, the rapid development and application of high-technology reconnaissance system provides a wider application stage for the simulation technology. The method is an efficient and cost-effective measure by setting a false target measure to simulate various exposure signs of a real target, manufacturing and displaying false information, and causing misjudgment and mishit of an enemy.
Therefore, it is necessary to provide an inflatable air-defense missile launching vehicle simulation system which is simple in design and manufacture, low in cost, excellent in technical and tactical performance and capable of realizing a rapid deployment technology, a remote control technology and a state monitoring technology.
SUMMERY OF THE UTILITY MODEL
In order to solve at least one aspect of the above-mentioned problem and defect that exist among the prior art, the utility model provides an inflatable air-defense missile launching vehicle simulation system. The technical scheme is as follows:
an object of the utility model is to provide an inflatable air defense missile launching vehicle analog system.
According to the utility model discloses an aspect provides an inflatable air defense missile launching vehicle analog system, wherein, inflatable air defense missile launching vehicle analog system includes simulation target, sensing component and aerating device, at least one air chamber has in the inner chamber of simulation target, sensing component sets up in the at least one air chamber, just each air chamber in the at least one air chamber with sensing component all with aerating device connects, aerating device and command center's host computer signal connection.
Specifically, the sensing assembly comprises a position sensor, a pressure sensor and a temperature sensor for deployment positioning, and the position sensor, the pressure sensor and the temperature sensor are all in signal connection with a controller in the inflating device.
Further, each air chamber of the at least one air chamber is provided with an inflation inlet for inflation deployment and a deflation port for deflation recovery, the inflation device comprises an air compressor and an air pump which are connected with the controller, the air compressor is connected with the inflation inlet, and the air pump is connected with the deflation port.
Specifically, the simulation target comprises a frame and a skin layer which are connected together, wherein the frame is airtight rubber-coated cloth, and the skin layer is light waterproof cloth.
Preferably, the airtight rubberized fabric is high-strength polyester rubberized fabric, and the two sides of high-strength polyester rubberized fabric are both provided with polyvinyl chloride coatings, be provided with the camouflage coating layer of simulation visible light characteristic on the light-weight waterproof fabric.
Specifically, the simulation target further comprises a radar reflector for ensuring radar reflection characteristics of the simulation target and an infrared radiation device for simulating infrared characteristics, and the radar reflector and the infrared radiation device are arranged in the at least one air chamber.
Preferably, the radar reflector is a metallized film or a metal wire fabric, and the infrared radiation device is a heater.
Further, the simulation target also comprises a windproof fixing device which is arranged on at least one side of the frame and is fixedly connected with the ground.
Specifically, the simulation target comprises an inflatable chassis vehicle, inflatable tires, an inflatable support frame, an inflatable traction table, an inflatable launcher, at least one inflatable missile launching box and an inflatable control box.
Specifically, each of the inflatable chassis, the inflatable tire, the inflatable support frame, the inflatable traction table, the inflatable launcher, the at least one inflatable missile launching box and the inflatable control box is provided with the at least one air chamber, and the at least one air chamber is communicated with each other or is arranged independently of each other.
According to the utility model discloses an inflatable air-defense missile launching vehicle analog system has at least one in following advantage:
(1) the simulation target in the simulation system of the inflatable air-defense missile launching vehicle provided by the utility model adopts an inflatable air bag structure and has the characteristics of visible light, infrared radiation and radar scattering similar to those of a physical air-defense missile launching vehicle;
(2) the material used by the simulation target frame of the inflatable air-defense missile launching vehicle simulation system provided by the utility model is light high-strength airtight rubberized fabric, so that the whole air tightness can be ensured;
(3) the utility model provides an airtight rubber coating cloth of a simulation target in the inflatable air-defense missile launching vehicle simulation system, both sides of which are coated PVC, and the simulation target has the performances of high airtightness, wear resistance, high and low temperature resistance, sunlight resistance, small permanent deformation, easy shaping and processing and the like;
(4) the utility model provides a simulation target among inflatable air-defense missile launching vehicle analog system no longer needs the air-blower for it lasts the air feed after wholly aerifing the completion.
Drawings
These and/or other aspects and advantages of the present invention will become apparent and readily appreciated from the following description of the preferred embodiments, taken in conjunction with the accompanying drawings of which:
fig. 1 is a schematic structural diagram of an inflatable air defense missile launching vehicle simulation system according to an embodiment of the invention;
FIG. 2 is a schematic diagram of the structure of the mock target shown in FIG. 1.
Detailed Description
The technical solution of the present invention is further specifically described below by way of examples and with reference to the accompanying drawings. In the specification, the same or similar reference numerals denote the same or similar components. The following description of the embodiments of the present invention with reference to the drawings is intended to explain the general inventive concept and should not be construed as limiting the invention.
Referring to fig. 1, an inflatable air defense missile launch vehicle simulation system 100 is shown according to one embodiment of the present invention. The simulation system 100 of the inflatable air-defense missile launching vehicle comprises a simulation target 10, a sensing assembly 20 and an inflating device 30. The simulation target 10 adopts an inflatable air bag structure, and a simulation system which is consistent with the appearance of an air-defense missile launching vehicle (not shown) is constructed to be used as a target hitting target of a target projectile. In use, the simulation target 10 is inflated to a relatively stable state with certain internal air pressure and is arranged in the search range of the radar of the terminal-guided missile (not shown), then the infrared heat source 12 (namely, an infrared radiation device, which is described in detail below) is locally deployed to enable the part of the simulation target to have infrared characteristics, and then the radar reflector 11 (which is described in detail below) is erected to enable the radar cross-sectional area of the simulation target 10 to be larger than the capture threshold of the terminal-guided radar of the radar-guided missile (not shown), so that the function of quickly arranging the false target in an emergency situation is achieved.
Referring to fig. 1 and 2, the simulation target 10 includes an inflatable chassis 13, an inflatable tire 14, an inflatable support frame 15, an inflatable traction table 16, an inflatable launcher 17, four inflatable missile launching boxes 18, and an inflatable control box 19. In one example, the inflatable missile launching box can be designed in two, three or more. In one example, the inflatable chassis 13, the inflatable tires 14, the inflatable support frames 15, the inflatable traction table 16, the inflatable launcher 17, the four inflatable missile launching boxes 18 and the inflatable control box 19 are all designed as airbag structures, and the air passages between the adjacent parts can be communicated with each other or not, of course. For example, the air paths of the inflatable chassis 13, the inflatable tires 14, the inflatable support frames 15, the inflatable traction table 16, the driving device 161, the inflatable launcher 17, the four inflatable missile launching boxes 18, the antenna 181 and the inflatable control box 19 are all communicated with each other, so that the inner cavity of the simulation target 10 forms an integral air chamber. Of course, those skilled in the art will also appreciate that the gas paths between adjacent sections may not be connected, forming separate sections, such that the internal cavity of the mock target 10 is divided into a plurality of separate gas chambers. The skilled person can make corresponding selections as required, and this example is only an illustrative example, and the skilled person should not be construed as a limitation of the present invention.
In one example, the inflator 30 includes an air compressor 31 and an air extractor 32. Each plenum is designed with an inflation port (not shown) for inflation deployment and a deflation port (not shown) for deflation recovery. The inflation port is connected to the air compressor 31 via an inflation gas path (not shown), and the deflation port is connected to the air pump via a deflation gas path (not shown). Of course, those skilled in the art will understand that the inflation port and the deflation port can be designed as the same air port, the air port is connected to the air compressor 31 and the air pump 32 through an air path, one end of the air path is connected to the air port, the other end is divided into a first air path branch and a second air path branch, the first air path branch is connected to the air compressor 31, and the second air path branch is connected to the air pump 32. The skilled person can make corresponding selections as required, and this example is only an illustrative example, and the skilled person should not be construed as a limitation of the present invention. In one example, the number of inflation ports and deflation ports may be designed accordingly according to the number of air chambers, for example, one inflation port and one deflation port may be designed for each independent air chamber, or one common air port may be designed.
In one example, the inner cavity of the simulation target 10 is an integral air chamber, the inflation inlet and the deflation inlet are respectively arranged at the left side and the right side of the front end of the simulation target 10, when in inflation, the inflation device 30 delivers air to the inflation inlet through the air path, and after inflation, the inflation inlet is closed, and continuous air supply for the inflation inlet by a blower is not needed.
In one example, the simulated target 10 includes a frame (not shown) and a skin layer (not shown). The inner cavity of the frame is the air chamber. In one example, the skin layer and the frame are bonded to each other. Of course, other fixing means, such as sewing, may be used by those skilled in the art instead of the adhesive connection, as long as the skin layer and the frame are fixedly connected to each other. In one example, the dummy target 10 uses an airtight rubberized fabric with light weight and high strength as a frame material of the inflatable target, thereby ensuring the overall airtightness of the dummy target. Preferably, the airtight rubber coated fabric base fabric is a high-strength polyester plain fabric, and the two surfaces of the airtight rubber coated fabric base fabric are also provided with coatings of PVC (polyvinyl chloride), so that the simulation target 10 has the performances of high airtightness, wear resistance, high and low temperature resistance, sunlight resistance, small permanent deformation, easiness in shaping and processing and the like.
In one example, a skin layer is provided on the outside of the frame, and a lightweight waterproof cloth is used as the skin layer and the exterior of the missile launcher is painted. Preferably, the light-weight waterproof cloth is coated with a waterproof coating on the basis of the high-strength polyester cloth, so that the simulation target 10 has the performances of light weight, water resistance, spraying, painting and printing and the like, and the appearance of the false target is ensured to be similar to a real object as much as possible. In one example, the outer layer of the lightweight tarp is coated with the camouflage paint to form a camouflage appearance similar to a real object and has visible light characteristics consistent with the real object.
In one example, a radar reflector 11 and an infrared radiation device 12 are also provided in at least one gas chamber of the simulated target 10. In one example, metallized film or metal wire fabric is used to simulate the radar reflection characteristics of a physical metal housing. Preferably, the material of the radar reflector 11 is an aluminized plastic film. In one example, the infrared radiation device 12 is a heater, thereby creating an infrared signature that is consistent with the physical object.
In one example, in order to secure the stability of the dummy target 10, wind-proof fixing devices (not shown) are provided at the upper left and right sides of the dummy target 10. Preferably, the windproof fixing device is a pull buckle and a pull rope, the pull buckle is fixed on the simulation target 10, one end of the pull rope is fixedly connected with the pull buckle, and the other end of the pull rope is fixedly connected with the ground, for example, through a ground nail. One skilled in the art can replace the wind-proof fixture with any one of the prior art, as long as the simulation target 10 can be fixedly connected to the ground.
In one example, a sensing assembly 20 is provided in the inner cavity (i.e., air chamber) of the mock target 10, connected to the inflation device 30 by wire or wirelessly. The sensing assembly 20 includes a position sensor 21 for positioning the mock target 10 for deployment, a pressure sensor 22 for detecting the pressure within the mock target 10 for corresponding inflation or deflation based on the pressure value, and a temperature sensor 23 for detecting the temperature at which the infrared radiation device 12 heats the mock target 10. When the device is used, the position sensor 21 sends the position information of the simulation target 10, the pressure sensor 22 sends the pressure information of the simulation target 10 and the temperature sensor 23 sends the temperature information of the simulation target 10 to the inflation device 30 in a signal mode (namely, signal connection is realized), the inflation device 30 transmits the received signals to the upper computer 40 of the command center in a wired or wireless connection mode, the upper computer 40 gives an instruction of the arrangement position of the simulation target 10 to the arrangement position according to the received corresponding signals, transmits inflation or deflation signals to the inflation device 30 (namely, signal connection between the inflation device and the upper computer of the command center is realized), and transmits signals whether heating continues or not to the infrared radiation device 12 in the simulation target 10 through the inflation device.
In one example, the position sensor 21, the pressure sensor 22 and the temperature sensor 23 are connected with the controller 33 in the inflator 30 in a wired or wireless mode, the position sensor 21, the pressure sensor 22 and the temperature sensor 23 transmit signals to the controller 33 in the inflator 30, and the controller 33 is connected with the upper computer 40 of the command center in a wired or wireless mode.
According to the utility model discloses an inflatable air-defense missile launching vehicle analog system has at least one in following advantage:
(1) the utility model provides an inflatable air-defense missile launching vehicle simulation system which adopts an inflatable air bag structure and has the visible light, infrared radiation and radar scattering characteristics similar to those of a physical air-defense missile launching vehicle;
(2) the framework of the inflatable air-defense missile launching vehicle simulation system provided by the utility model is made of light high-strength airtight rubberized fabric, so that the whole air tightness can be ensured;
(3) the utility model provides an airtight rubber coating cloth of the inflatable air-defense missile launching vehicle simulation system, the two sides of which are coated PVC, and the inflatable air-defense missile launching vehicle simulation system has the performances of high airtightness, wear resistance, high and low temperature resistance, sunlight resistance, small permanent deformation, easy shaping and processing and the like;
(4) the utility model provides an inflatable air-defense missile launching vehicle analog system no longer needs the air-blower to last the air feed for it after wholly aerifing the completion.
Although a few embodiments of the present general inventive concept have been shown and described, it would be appreciated by those skilled in the art that changes may be made in these embodiments without departing from the principles and spirit of the general inventive concept, the scope of which is defined in the claims and their equivalents.
Claims (10)
1. An inflatable air defense missile launching vehicle simulation system is characterized in that,
the inflatable air-defense missile launching vehicle simulation system comprises a simulation target, a sensing assembly and an inflating device, wherein at least one air chamber is arranged in an inner cavity of the simulation target, the sensing assembly is arranged in the at least one air chamber, each air chamber in the at least one air chamber and the sensing assembly are connected with the inflating device, and the inflating device is in signal connection with an upper computer of a command center.
2. The inflatable air defense missile launch vehicle simulation system of claim 1,
the sensing assembly comprises a position sensor, a pressure sensor and a temperature sensor which are used for deployment and positioning, and the position sensor, the pressure sensor and the temperature sensor are in signal connection with a controller in the inflating device.
3. The inflatable air defense missile launch vehicle simulation system of claim 2,
each air chamber in at least one air chamber all is provided with the inflation inlet that is used for aerifing the deployment and is used for the relief of gas recovery to retrieve, aerating device include with air compressor and the air extractor that the controller is connected, air compressor with the inflation inlet is connected, the air extractor with the relief of gas is connected.
4. The inflatable air defense missile launch vehicle simulation system of claim 3,
the simulation target comprises a frame and a skin layer which are connected together, the frame is made of airtight rubber-coated cloth, and the skin layer is made of light waterproof cloth.
5. The inflatable air defense missile launching vehicle simulation system of claim 4,
the airtight rubberized fabric is high-strength polyester rubberized fabric, two sides of the high-strength polyester rubberized fabric are both provided with polyvinyl chloride coatings, and the light-weight waterproof fabric is provided with a camouflage paint layer simulating visible light characteristics.
6. The inflatable air defense missile launch vehicle simulation system of claim 5,
the simulation target further comprises a radar reflector for ensuring radar reflection characteristics of the simulation target and an infrared radiation device for simulating infrared characteristics, and the radar reflector and the infrared radiation device are arranged in the at least one air chamber.
7. The inflatable air defense missile launching vehicle simulation system of claim 6,
the radar reflector is a metal-plated film or a metal wire fabric, and the infrared radiation device is a heater.
8. The inflatable air defense missile launch vehicle simulation system of claim 7,
the simulation target further comprises a windproof fixing device which is arranged on at least one side of the frame and is fixedly connected with the ground.
9. The inflatable air defense missile launch vehicle simulation system of any one of claims 1 to 8,
the simulation target comprises an inflatable chassis vehicle, inflatable tires, an inflatable support frame, an inflatable traction table, a driving device, an inflatable launcher, at least one inflatable missile launching box, an antenna and an inflatable control box.
10. The inflatable air defense missile launch vehicle simulation system of claim 9,
the inflatable chassis vehicle, the inflatable tire, the inflatable support frame, the inflatable traction table, the inflatable launcher, the at least one inflatable missile launching box and the inflatable control box are respectively provided with the at least one air chamber, and the at least one air chamber is communicated with each other or is arranged independently.
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| Application Number | Priority Date | Filing Date | Title |
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| CN202120005908.7U CN214148996U (en) | 2021-01-04 | 2021-01-04 | Inflatable air-defense missile launching vehicle simulation system |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202120005908.7U CN214148996U (en) | 2021-01-04 | 2021-01-04 | Inflatable air-defense missile launching vehicle simulation system |
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| CN214148996U true CN214148996U (en) | 2021-09-07 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113865438A (en) * | 2021-09-09 | 2021-12-31 | 河北汉光重工有限责任公司 | Patriot-2 air defense missile launching vehicle target with modular design |
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- 2021-01-04 CN CN202120005908.7U patent/CN214148996U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113865438A (en) * | 2021-09-09 | 2021-12-31 | 河北汉光重工有限责任公司 | Patriot-2 air defense missile launching vehicle target with modular design |
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