CN221037091U - Inflatable launching vehicle false target - Google Patents
Inflatable launching vehicle false target Download PDFInfo
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- CN221037091U CN221037091U CN202322583319.9U CN202322583319U CN221037091U CN 221037091 U CN221037091 U CN 221037091U CN 202322583319 U CN202322583319 U CN 202322583319U CN 221037091 U CN221037091 U CN 221037091U
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- 238000004088 simulation Methods 0.000 claims abstract description 103
- 230000006698 induction Effects 0.000 claims description 4
- 230000003137 locomotive effect Effects 0.000 claims 2
- 230000000694 effects Effects 0.000 abstract description 22
- 230000005540 biological transmission Effects 0.000 abstract 1
- 238000000034 method Methods 0.000 description 11
- 230000005484 gravity Effects 0.000 description 3
- 239000002131 composite material Substances 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000004033 plastic Substances 0.000 description 2
- 229920003023 plastic Polymers 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
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- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The utility model discloses an inflatable launching vehicle false target, and relates to the field of false targets. The simulation vehicle comprises a simulation vehicle frame, wherein a movable assembly is arranged at the bottom of the simulation vehicle frame, a plurality of simulation radar boxes and simulation storage boxes are respectively connected to two sides of the movable assembly, the movable assembly comprises a simulation roller shaft and simulation wheels, a plurality of connecting blocks and a cushion are connected to the top of the simulation vehicle frame, a transmitting base is connected between the two connecting blocks, the top of the transmitting base is provided with the transmitting assembly, the transmitting assembly comprises a connecting air bag, a mounting seat, a fixing frame and a simulation missile, a plurality of elastic tubes are connected to the bottom of the connecting air bag, and a second inflation tube is arranged at the side end of the transmitting assembly; the connection gasbag can drive a plurality of emulation guided missiles and swing by a small margin when the swing, can be for adjusting the guided missile transmission orbit when enemy reconnaissance, can let enemy more produce wrong judgement more easily, further improves the simulation effect of this equipment.
Description
Technical Field
The utility model belongs to the field of decoys, and particularly relates to an inflatable launching vehicle decoy.
Background
Military decoys have been developed for decades, and are of various kinds and are divided into structural forms: inflatable decoys, skeletal skinned decoys, assembled composite decoys, compression-expansion decoys, foam-molded decoys, and the like. The inflatable false target is composed of inflatable components of plastic, rubber film or fabric, and has the characteristics of high fidelity of appearance, light weight, small storage volume, high setting speed, low relative price and the like.
Chinese patent CN217005523U discloses an inflatable launching vehicle false target, relates to military target camouflage technical field, including inflatable launching vehicle body and wind-proof device, launching vehicle body rear portion is equipped with the launching frame, is equipped with the guided missile in the launching frame, and launching frame and guided missile are inflatable structure to make together, launching frame and guided missile communicate each other.
The inflatable launching vehicle false target in the prior art can not automatically change the corresponding state according to the current environment after inflation is completed, and an operator is required to manually adjust the inflatable launching vehicle false target, so that in the simulation process, the simulation effect and the practicability are not obvious, meanwhile, the whole equipment can not detect the current wind speed, the simulation means used by the operator in different scenes are the same, so that an adversary can easily make a target through the simulation means in the investigation, and the use limitation is larger.
For the problems in the related art, no effective solution has been proposed at present.
Disclosure of utility model
Aiming at the problems in the related art, the utility model provides an inflatable launching vehicle false target to overcome the technical problems in the prior art.
In order to solve the technical problems, the utility model is realized by the following technical scheme:
The utility model relates to an inflatable launching vehicle false target which comprises a simulation frame, wherein a movable assembly is arranged at the bottom of the simulation frame, a plurality of simulation radar boxes and simulation storage boxes are respectively connected to two sides of the simulation frame, the movable assembly comprises a simulation roller shaft and simulation wheels, a plurality of connecting blocks and a cushion are connected to the top of the simulation frame, a launching base is connected between the two connecting blocks, the top of the launching base is provided with the launching assembly, the launching assembly comprises a connecting air bag, a mounting seat, a fixing frame and a simulation missile, a plurality of elastic tubes are connected to the bottom of the connecting air bag, a second inflation tube is arranged at the side end of the connecting air bag, the other end of the elastic tube is connected with the top of the cushion, and a first inflation tube is connected to the side end of the simulation frame.
Preferably, the method comprises the steps of. The connection air bag is connected with the emission base, the mounting seat is connected with the top of the connection air bag, the fixing frame is connected with the top of the mounting seat, and the simulation missile is connected with one end of the fixing frame.
Preferably, the method comprises the steps of. The launching assembly further comprises a supporting frame, wherein the supporting frame is connected with the top of the connecting air bag and connected with the simulation missile.
Preferably, the method comprises the steps of. The top of the simulation frame is connected with a simulation head, and the top of the simulation head is connected with a plurality of searchlights.
Preferably, the method comprises the steps of. The side ends of the simulation radar box and the simulation storage box are provided with infrared induction lamps.
Preferably, the method comprises the steps of. The tail baffle is installed to the one end of emulation frame, the outward appearance of tail baffle is parallelogram.
Preferably, the method comprises the steps of. The connecting air bag, the mounting seat, the fixing frame, the simulation missile and the supporting frame are hollow cavities and are mutually communicated.
Preferably, the method comprises the steps of. The simulation frame, the moving assembly, the simulation radar box, the simulation storage box, the connecting block, the back cushion, the simulation head, the searchlight and the tail baffle are hollow cavities and are mutually communicated
The utility model has the following beneficial effects:
In the process of inflating the connecting air bags, the connecting air bags can rotate in a small amplitude under the limit of self gravity, wind power and two connecting blocks, and staff can make corresponding position placement on the current wind direction and wind speed according to the swing amplitude of the connecting air bags, so that the simulation effect of the device can be adjusted according to different scenes, and the practicability and the vivid effect are improved;
After the equipment is fixed in position, under the effect of sufficient wind force, the connection air bag still can appear shaking, and because the elastic tube can limit the connection air bag, a plurality of simulation missiles can be driven to swing in a small amplitude when the connection air bag swings, the missile launching track can be wrongly regulated when enemy reconnaissance is performed, the enemy can be more easily judged in error, and the simulation effect of the equipment is further improved.
Of course, it is not necessary for any one product to practice the utility model to achieve all of the advantages set forth above at the same time.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the utility model, the drawings that are needed for the description of the embodiments will be briefly introduced below, it being obvious that the drawings in the following description are only some embodiments of the utility model, and that other drawings can be obtained according to these drawings without inventive effort for a person skilled in the art.
FIG. 1 is a schematic perspective view of the present utility model;
FIG. 2 is an enlarged schematic view of portion A of FIG. 1;
FIG. 3 is a schematic perspective view of the present utility model;
Fig. 4 is an enlarged schematic view of section B of the present utility model.
In the drawings, the list of components represented by the various numbers is as follows:
1. A simulated frame; 2. a moving assembly; 201. a simulation roll shaft; 202. simulating a wheel; 3. a simulation radar box; 4. a simulated storage box; 5. a connecting block; 6. a transmitting base; 7. a transmitting assembly; 701. connecting an air bag; 702. a mounting base; 703. a fixing frame; 704. simulating a missile; 705. a second inflation tube; 706. a support frame; 8. an elastic tube; 9. a back cushion; 10. a first inflation tube; 11. simulating a headstock; 12. a searchlight; 13. a tail baffle.
Detailed Description
The following description of the technical solutions in the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings in the embodiments of the present utility model, and it is apparent that the described embodiments are only some embodiments of the present utility model, not all embodiments. All other embodiments, based on the embodiments of the utility model, which would be apparent to one of ordinary skill in the art without inventive effort are within the scope of the utility model.
In the description of the present utility model, it should be understood that the terms "open," "upper," "lower," "top," "middle," "inner," and the like indicate an orientation or positional relationship, merely for convenience of description and to simplify the description, and do not indicate or imply that the components or elements referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus should not be construed as limiting the utility model.
Referring to fig. 1-4, the utility model discloses an inflatable launching vehicle false target, which comprises a simulation frame 1, wherein a moving component 2 is arranged at the bottom of the simulation frame 1, a plurality of simulation radar boxes 3 and simulation storage boxes 4 are respectively connected to two sides of the simulation frame, the moving component 2 comprises a simulation roller shaft 201 and simulation wheels 202, a plurality of connecting blocks 5 and a cushion 9 are connected to the top of the simulation frame 1, a launching base 6 is connected between the two connecting blocks 5, a launching component 7 is arranged at the top of the launching base 6, the launching component 7 comprises a connecting air bag 701, a mounting seat 702, a fixing frame 703 and a simulation missile 704, a plurality of elastic tubes 8 are connected to the bottom of the connecting air bag 701, a second air tube 705 is arranged at the side end of the connecting air bag, the other end of the elastic tube 8 is connected with the top of the cushion 9, and a first air tube 10 is connected to the side end of the simulation frame 1.
When an operator needs to use the device, the operator is connected with the first inflation tube 10 through the output end of the inflation device, then the inflation device is started, so that the first inflation tube 10 can infuse the transmitted gas into the simulation frame 1, at the moment, the gas in the simulation frame 1 can enter the simulation roll shaft 201, the simulation wheel 202, the simulation radar box 3, the simulation storage box 4, the connecting block 5 and the cushion 9 through the communicated hollow cavity, at the moment, the parts connected with the simulation frame 1 can be gradually expanded in the gas increasing state, when the gas in the simulation frame 1 reaches the specified capacity, the inflation device is closed, the connecting end of the first inflation tube 10 is closed, at the moment, part of the structure of the device is in the expansion state, so that the appearance is more like a real military vehicle, then, the output end of the air charging equipment is connected with a second air charging pipe 705, the air charging equipment is started, the second air charging pipe 705 can transmit the infused gas into the connecting air bag 701, the gas in the connecting air bag 701 can flow into the transmitting base 6, the mounting seat 702, the fixing frame 703, the simulation missile 704 and the supporting frame 706, in the process of inflating the connecting air bag 701, the connecting air bag 701 can rotate in a small amplitude due to self gravity, wind force and the limit of two connecting blocks 5, and staff can make corresponding position placement for the current wind direction and wind speed according to the swing amplitude of the connecting air bag 701, so that the simulation effect of the equipment can adjust corresponding simulation effect according to different scenes, and the practicability and the vivid effect are improved;
After the equipment is fixed in position, under the effect of sufficient wind force, the condition that the connecting air bag 701 still can appear rocking, because the elastic tube 8 can be spacing to the connecting air bag 701, and then can drive a plurality of simulation missiles 704 to swing by a small margin when making the connecting air bag 701 swing, can be in order to adjust the missile launching track when enemy reconnaissance, can let enemy more produce wrong judgement easily, further improve the simulation effect of this equipment.
In one embodiment, the connection airbag 701 is connected to the launch base 6, the mount 702 is connected to the top of the connection airbag 701, the mount 703 is connected to the top of the mount 702, and the simulated missile 704 is connected to one end of the mount 703.
Through connecting gasbag 701, mount pad 702, mount 703 and mount pad 702 each other, can make overall structure more integrate, improve the simulation effect.
In one embodiment, the launch assembly 7 further comprises a support bracket 706, the support bracket 706 being connected to the top of the connection airbag 701 and to the simulated missile 704.
The support frame 706 can symbolically improve the authenticity of the simulated missile 704 and the visual simulation effect.
In one embodiment, the top of the simulated frame 1 is connected with a simulated head 11, and the top of the simulated head 11 is connected with a plurality of searchlights 12.
The appearance of the equipment is more like that of a military launching vehicle, and the simulation effect is further improved.
In one embodiment, the side ends of the simulated radar box 3 and the simulated storage box 4 are both provided with infrared induction lamps.
Through starting the infrared induction lamp, can make the outer wall of emulation radar box 3 and emulation storage tank 4 give off light, can reach the effect of attracting enemy's army when night.
In one embodiment, a tail baffle 13 is mounted at one end of the simulated frame 1, and the tail baffle 13 has a parallelogram shape in appearance.
The device is arranged in a parallelogram, so that one end of the tail baffle 13 can generate obvious structural modeling when being positioned behind enemy, and the simulation effect of the structure is improved.
In one embodiment, the connection airbag 701, the mounting block 702, the mount 703, the simulated missile 704, and the support frame 706 are hollow cavities and are in communication with one another.
The effect of simultaneously inflating the transmitting base 6, the mounting seat 702, the fixing frame 703, the simulation missile 704 and the supporting frame 706 can be achieved only by inflating the inside of the connecting airbag 701, the inflating equipment is not required to be connected for multiple times, the mounting time is saved, and the working efficiency is improved.
In one embodiment, the simulated frame 1, the moving assembly 2, the simulated radar box 3, the simulated storage box 4, the connecting block 5, the cushion 9, the simulated head 11, the searchlight 12 and the tail baffle 13 are hollow cavities and are mutually communicated, and the equipment is made of TPU composite materials through welding and heat sealing.
The TPU not only has most of the characteristics of rubber and common plastics, but also has excellent comprehensive physical and chemical properties, so that the equipment can be inflated once for 6 hours without air supplement, and the intermittent inflation effect is achieved.
Working principle:
When an operator needs to use the device, the operator is connected with the first inflation tube 10 through the output end of the inflation device, then the inflation device is started, so that the first inflation tube 10 can infuse the transmitted gas into the simulation frame 1, at the moment, the gas in the simulation frame 1 can enter the simulation roll shaft 201, the simulation wheel 202, the simulation radar box 3, the simulation storage box 4, the connecting block 5, the cushion 9, the simulation head 11, the searchlight 12 and the tail baffle 13 through the communicated hollow cavity, at the moment, the parts connected with the simulation frame 1 can be gradually inflated in the increased state of the gas, when the gas in the simulation frame 1 reaches the specified capacity, the inflation device is closed, the connecting end of the first inflation tube 10 is closed, at the moment, part of the structure of the device is in the inflated state, the shape of the device is more like a real military vehicle, then the output end of the inflation device is connected with the second inflation tube 705, the inflation device is started, the second inflation tube 705 can transmit the infused gas into the connection air bag 701, the gas in the connection air bag 701 can flow to the inside of the emission base 6, the mounting seat 702, the fixing frame 703, the simulation missile 704 and the supporting frame 706, in the process of inflating the connection air bag 701, the connection air bag 701 can generate small-amplitude rotation under the limit of self gravity, wind power and two connecting blocks 5, and staff can make corresponding position placement for the current wind direction and wind speed according to the swing amplitude of the connection air bag 701, so that the simulation effect of the device can be adjusted according to different scenes, and the practicability and vivid effect are improved;
After the equipment is fixed in position, under the effect of sufficient wind force, the condition that the connecting air bag 701 still can appear rocking, because the elastic tube 8 can be spacing to the connecting air bag 701, and then can drive a plurality of simulation missiles 704 to swing by a small margin when making the connecting air bag 701 swing, can be in order to adjust the missile launching track when enemy reconnaissance, can let enemy more produce wrong judgement easily, further improve the simulation effect of this equipment.
In the description of the present specification, the descriptions of the terms "one embodiment," "example," "specific example," and the like, mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the utility model. In this specification, schematic representations of the above terms do not necessarily refer to the same embodiments or examples. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
The above disclosed preferred embodiments of the utility model are merely intended to help illustrate the utility model. The preferred embodiments are not exhaustive or to limit the utility model to the precise form disclosed. Obviously, many modifications and variations are possible in light of the above teaching. The embodiments were chosen and described in order to best explain the principles of the utility model and the practical application, to thereby enable others skilled in the art to best understand and utilize the utility model.
Claims (8)
1. The utility model provides an inflatable launching vehicle false target, includes emulation frame (1), its characterized in that: the simulation frame comprises a simulation frame body (1), wherein a moving assembly (2) is arranged at the bottom of the simulation frame body (1), a plurality of simulation radar boxes (3) and simulation storage boxes (4) are respectively connected to two sides of the moving assembly, the moving assembly (2) comprises a simulation roll shaft (201) and simulation wheels (202), a plurality of connecting blocks (5) and a back cushion (9) are connected to the top of the simulation frame body (1), a transmitting base (6) is connected between the connecting blocks (5), a transmitting assembly (7) is arranged at the top of the transmitting base (6), the transmitting assembly (7) comprises a connecting air bag (701), a mounting seat (702), a fixing frame (703) and a simulation missile (704), a plurality of elastic tubes (8) are connected to the bottom of the connecting air bag (701), a second air tube (705) is arranged at the side end of the connecting air bag, the other end of each elastic tube (8) is connected to the top of the corresponding back cushion (9), and a first air tube (10) is connected to the side end of the simulation frame body (1).
2. An inflatable launch vehicle decoy as defined in claim 1, wherein: the connection airbag (701) is connected with the emission base (6), the mounting seat (702) is connected with the top of the connection airbag (701), the fixing frame (703) is connected with the top of the mounting seat (702), and the simulation missile (704) is connected with one end of the fixing frame (703).
3. An inflatable launch vehicle decoy as defined in claim 2, wherein: the launching assembly (7) further comprises a supporting frame (706), and the supporting frame (706) is connected with the top of the connecting air bag (701) and connected with the simulation missile (704).
4. An inflatable launch vehicle decoy as defined in claim 1, wherein: the top of emulation frame (1) is connected with emulation locomotive (11), the top of emulation locomotive (11) is connected with a plurality of searchlight (12).
5. An inflatable launch vehicle decoy as defined in claim 1, wherein: the side ends of the simulation radar box (3) and the simulation storage box (4) are provided with infrared induction lamps.
6. An inflatable launch vehicle decoy as defined in claim 4, wherein: the simulation vehicle frame is characterized in that a tail baffle (13) is arranged at one end of the simulation vehicle frame (1), and the appearance of the tail baffle (13) is parallelogram.
7. An inflatable launch vehicle decoy as defined in claim 1, wherein: the launching base (6), the connecting air bag (701), the mounting seat (702), the fixing frame (703), the simulation missile (704) and the supporting frame (706) are hollow cavities and are mutually communicated.
8. An inflatable launch vehicle decoy as defined in claim 6, wherein: the simulation frame (1), the moving assembly (2), the simulation radar box (3), the simulation storage box (4), the connecting block (5), the back cushion (9), the simulation vehicle head (11), the searchlight (12) and the tail baffle (13) are hollow cavities and are mutually communicated.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322583319.9U CN221037091U (en) | 2023-09-22 | 2023-09-22 | Inflatable launching vehicle false target |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322583319.9U CN221037091U (en) | 2023-09-22 | 2023-09-22 | Inflatable launching vehicle false target |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221037091U true CN221037091U (en) | 2024-05-28 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322583319.9U Active CN221037091U (en) | 2023-09-22 | 2023-09-22 | Inflatable launching vehicle false target |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN221037091U (en) |
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2023
- 2023-09-22 CN CN202322583319.9U patent/CN221037091U/en active Active
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