CN219869309U - Inflatable false target - Google Patents
Inflatable false target Download PDFInfo
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- CN219869309U CN219869309U CN202321184084.XU CN202321184084U CN219869309U CN 219869309 U CN219869309 U CN 219869309U CN 202321184084 U CN202321184084 U CN 202321184084U CN 219869309 U CN219869309 U CN 219869309U
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- 230000003137 locomotive effect Effects 0.000 claims 2
- 230000003245 working effect Effects 0.000 abstract description 5
- 230000000087 stabilizing effect Effects 0.000 abstract description 3
- 230000000694 effects Effects 0.000 description 7
- 238000004088 simulation Methods 0.000 description 3
- 238000011835 investigation Methods 0.000 description 2
- 238000009423 ventilation Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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Abstract
The utility model discloses an inflatable false target, and relates to the field of military equipment. The utility model comprises a launching vehicle main body and an inflator, wherein the launching vehicle main body comprises a connecting base, a top plate, a fence, a launching base and a vehicle head, the bottom of the top plate is connected with the connecting base, the fence and the launching base are both connected with the top of the top plate, one side of the connecting base is fixedly provided with an inflation tube, one end of the inflation tube is communicated with the output end of the inflator, one end of the vehicle head is connected with the launching base, the bottom of the vehicle head is connected with the top of the top plate, both sides of the top plate are provided with supporting components, and the supporting components comprise guide rails, screws and sliding blocks; the supporting force between the two sliders and the ground anchors connected with the bottom is uniformly adjusted, so that the working efficiency is improved, the overall stabilizing effect of the launching vehicle body can be improved, the probability that the launching vehicle body shakes to cause task failure when the launching vehicle body is executed is avoided, and the working effect of the launching vehicle body is improved.
Description
Technical Field
The utility model belongs to the field of military equipment, and particularly relates to an inflatable false target.
Background
The military camouflage technology has long history, and during the second battle period, because high-altitude investigation equipment such as airplanes, airships and the like are widely used, huge pressure is brought to the two parties of the battle, therefore, each battle state dispute is in a specific area, various cheap materials are adopted to manufacture a simple military target model, the simple military target model is used for confusing the military investigation of enemies, the enemies are induced to carry out firepower attack, and the aims of protecting own military targets and consuming enemy battle resources are achieved. This is an early decoy.
Chinese patent CN205690988U issued a closed inflatable decoy shelter vehicle comprising a vehicle head; the base is arranged at the rear of the headstock; at least one shelter disposed on the base; the vehicle head, the base and the at least one shelter are inflatable air bags, and the vehicle head, the base and the at least one shelter are detachably connected.
After the inflatable false target in the utility model and the prior art is inflated, as the bottom of the false target is not connected with the ground, when the wind power is large, the whole device is easily blown by the wind, the stability is insufficient, the working effect is further deteriorated, and the false target with the fixing effect is partially provided with the false target, and the fixing effect is further deteriorated due to the fact that the corresponding stable angle cannot be adjusted according to the change of the field.
For the problems in the related art, no effective solution has been proposed at present.
Disclosure of Invention
The present utility model provides an inflatable artificial object to overcome the above-mentioned problems of 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 false target, which comprises a launching vehicle body and an inflator, wherein the launching vehicle body comprises a connecting base, a top plate, a fence, a launching base and a head plate, the bottom of the top plate is connected with the connecting base, the fence and the launching base are both connected with the top of the top plate, one side of the connecting base is fixedly provided with an inflation tube, one end of the inflation tube is communicated with the output end of the inflator, one end of the head plate is connected with the launching base, the bottom of the head plate is connected with the top of the top plate, both sides of the top plate are provided with supporting components, each supporting component comprises a guide rail, a screw rod and a sliding block, the guide rail is connected with one side of the top plate, the screw rod is rotationally connected with the guide rail, the two sliding blocks are sleeved on the screw rod, one end of the sliding block is connected with a ground anchor, and the other end of the ground anchor is connected with the ground.
Preferably, the launching vehicle main body further comprises rollers, and a plurality of rollers are respectively connected with two ends of the connecting base.
Preferably, the support assembly further comprises a handle fixedly connected with the other end of the screw rod.
Preferably, windows are arranged on two sides of the headstock, and a skylight is arranged at the top of the headstock.
Preferably, the top of the transmitting base is provided with a plurality of transmitters.
Preferably, a plurality of missiles are arranged between the fence and the launching base.
Preferably, a controller is fixedly mounted at one end of the inflator.
Preferably, the connection base, the top plate, the fence, the launching base, the headstock, the roller, the launcher and the missile are all of an inflatable structure, and the top plate, the fence, the launching base, the headstock and the launcher ventilation cavity are mutually communicated.
The utility model has the following beneficial effects:
when a task needs to be executed, a worker starts the inflator through the controller, the output end of the inflator inflates the launching vehicle body through the inflation pipe, after the launching vehicle body is inflated, the worker installs the guide rails on two sides of the connecting base, then rotates the corresponding handle, the handle can drive the screw to rotate after rotating, the two sliding blocks can be driven to move oppositely or reversely under the action of the guide rails after rotating, the two sliding blocks can be enabled to horizontally adjust the positions at the same time, the supporting force between the two sliding blocks and the ground anchor connected with the bottom is evenly adjusted, the working efficiency is improved, the overall stabilizing effect of the launching vehicle body is improved, the probability of task failure caused by shaking of the launching vehicle body when the task is executed is avoided, and the working effect of the launching vehicle body is improved;
after finishing the task, the staff breaks off the connection between the ground anchor and the sliding block firstly, then the guide rails on two sides of the connecting base are detached, namely the screw rod, the sliding block and the handle are detached, then the gas in the launching vehicle main body is pumped out through the inflator, namely the launching vehicle main body is changed into a soft couch form, and the launching vehicle is easier to carry and improves the practicability.
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 a main body of a launch vehicle;
FIG. 2 is a schematic perspective view of the present utility model;
FIG. 3 is a schematic perspective view of the present utility model
Fig. 4 is an enlarged schematic view of a portion a in fig. 3.
In the drawings, the list of components represented by the various numbers is as follows:
1. a launch vehicle body; 101. the base is connected; 102. a top plate; 103. a fence; 104. a transmitting base; 1041. a transmitter; 1042. a missile; 105. a headstock; 1051. a vehicle window; 1052. a skylight; 106. a roller; 2. an inflator; 21. a controller; 3. an inflation tube; 4. a support assembly; 41. a guide rail; 42. a screw; 43. a slide block; 44. a handle; 5. and (5) an earth anchor.
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 present utility model is an inflatable dummy object, comprising a launching vehicle body 1 and an inflator 2, wherein the launching vehicle body 1 comprises a connecting base 101, a top plate 102, a fence 103, a launching base 104 and a head 105, the bottom of the top plate 102 is connected with the connecting base 101, the fence 103 and the launching base 104 are both connected with the top of the top plate 102, one side of the connecting base 101 is fixedly provided with an inflation tube 3, one end of the inflation tube 3 is communicated with the output end of the inflator 2, one end of the head 105 is connected with the launching base 104, the bottom is connected with the top of the top plate 102, both sides of the top plate 101 are provided with supporting components 4, the supporting components 4 comprise a guide rail 41, a screw rod 42 and a sliding block 43, the guide rail 41 is connected with one side of the top plate 102, the screw rod 42 is rotatably connected with the guide rail 41, both sliding blocks 43 are sleeved on the screw rod 42, one end of the sliding block 43 is connected with a ground anchor 5, and the other end of the ground anchor 5 is connected with the ground.
When a task needs to be executed, a worker starts the inflator 2, the output end of the inflator 2 inflates the connecting base 101 through the inflation tube 3, so that the launching vehicle main body 1 inflates, after the launching vehicle main body 1 inflates, the output end of the launching base 104 can incline to the sky, the device is more vivid, the worker installs the guide rail 41 on two sides of the connecting base 101, then rotates the corresponding screw rods 42, and can drive the two sliding blocks 43 to move towards or away from each other under the action of the guide rail 41 after the screw rods 42 rotate, so that the two sliding blocks 43 can be horizontally adjusted at the same time, the supporting force between the two sliding blocks 43 and the ground anchor 5 connected with the bottom is uniformly adjusted, the working efficiency is improved, the integral stabilizing effect of the launching vehicle main body 1 is improved, the probability of task failure caused by shaking of the launching vehicle main body 1 when the task is executed is avoided, and the working effect of the launching vehicle main body 1 is improved;
after the task is finished, the worker disconnects the connection between the ground anchor 5 and the sliding block 43 firstly, then the guide rail 41 connected with the two sides of the base 101 is detached, namely the screw rod 42, the sliding block 43 and the handle 44 can be detached, then the gas in the launching vehicle body 1 is pumped out through the inflator 2, namely the launching vehicle body 1 can be changed into a soft couch shape, the carrying is easier, and the practicability is improved.
In one embodiment, the launch vehicle body 1 further comprises rollers 106, and the rollers 106 are respectively connected to two ends of the connection base 101.
After the launching vehicle main body 1 is inflated, the plurality of rollers 106 can support the connecting base 101 to a certain height, so that the launching vehicle main body 1 can be of a similar size to a practical combat vehicle, and the simulation effect is further improved.
In one embodiment, the support assembly 4 further includes a handle 44, the handle 44 being fixedly connected to the other end of the screw 42.
The handhold 44 is arranged to facilitate the rotation of the screw 42 by the staff, thereby improving the practicability.
In one embodiment, the vehicle head 105 is provided with windows 1051 on both sides and a sunroof 1052 on top.
The arrangement of the vehicle window 1051 and the sunroof 1052 can further improve the simulation effect of the vehicle head 105, and further improve the working effect of the launching vehicle body 1.
In one embodiment, the top of the transmitting base 104 is provided with a number of transmitters 1041.
A plurality of transmitters 1041 set up at the top of launch base 104, can improve the vertical height of transmitter 1041 for enemy reconnaissance machine sees more easily, improves the frightening effect.
In one embodiment, a number of missiles 1042 are provided between the rail 103 and the launch base 104.
The number of missiles 1042 of the device can be clearly observed by an enemy by placing a plurality of missiles 1042 beside the launching base 104, so that deterrence and simulation effect are further improved.
In one embodiment, one end of the inflator 2 is fixedly mounted with a controller 21.
The controller 21 can start the inflator 2 to inflate or deflate, and the dual-purpose type improves the practicability.
In one embodiment, the connection base 101, the top plate 102, the rail 103, the launch base 104, the headstock 105, the rollers 106, the launcher 1041, and the missile 1042 are all inflatable structures, and the top plate 102, the rail 103, the launch base 104, the headstock 105, and the launcher 1041 vent chambers are in communication with one another.
When the launching vehicle main body 1 is required to be used, the whole launching vehicle main body 1 can be inflated by directly inflating the connecting base 101 through the inflation tube 3, so that the launching vehicle main body 1 is convenient to inflate and exhaust, multiple positions do not need to be inflated repeatedly, and the working efficiency is improved.
Working principle:
when a task needs to be executed, a worker starts the inflator 2 through the controller 21, the output end of the inflator 2 inflates the connecting base 101 through the inflation tube 3, at the moment, as the connecting base 101 is the same as the top plate 102, the rail 103, the transmitting base 104, the transmitter 1041 and the ventilation cavity of the headstock 105, the transmitting vehicle main body 1 is inflated, after the transmitting vehicle main body 1 is inflated, the output end of the transmitting base 104 can incline to the sky, so that the device is more vivid, meanwhile, the missile 1042 is put into the rail 103, the enemy can clearly observe the number of the missiles 1042, the deterrent force is increased, the worker installs the guide rails 41 on two sides of the connecting base 101, then rotates the corresponding handles 44, the handles 44 can drive the screw rods 42 to rotate after rotating, and the two sliding blocks 43 can be driven to move towards each other or away from each other under the action of the guide rails 41, the two sliding blocks 43 can be horizontally adjusted at the same time, the supporting force between the two sliding blocks 43 and the ground anchors 5 connected with the bottom can be uniformly adjusted, the working efficiency is improved, the whole transmitting vehicle main body 1 can be improved, the stable effect of the transmitting vehicle main body 1 is prevented from shaking the task is prevented from being caused when the task is executed, and the main body 1 fails to execute the task is executed;
after the task is finished, the worker disconnects the connection between the ground anchor 5 and the sliding block 43 firstly, then the guide rail 41 connected with the two sides of the base 101 is detached, namely the screw rod 42, the sliding block 43 and the handle 44 can be detached, then the gas in the launching vehicle body 1 is pumped out through the inflator 2, namely the launching vehicle body 1 can be changed into a soft couch shape, the carrying is easier, and the practicability is improved.
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. An inflatable decoy comprising a launch vehicle body (1) and an inflator (2), characterized in that: the utility model provides a launch vehicle main part (1) is including connecting base (101), roof (102), rail (103), launch base (104) and locomotive (105), the bottom of roof (102) with connect base (101) and be connected, rail (103) with launch base (104) all with the top of roof (102) is connected, one side fixed mounting of connecting base (101) has gas tube (3), the one end of gas tube (3) with the output intercommunication of inflator (2), the one end of locomotive (105) with launch base (104) are connected, and the bottom with the top of roof (102) is connected, the both sides of roof (101) all are provided with supporting component (4), supporting component (4) include guide rail (41), screw rod (42) and slider (43), guide rail (41) with one side of roof (102) is connected, screw rod (42) with guide rail (41) rotate and are connected, two slider (43) all set up on slider (42), the one end that is connected with ground anchor (5) of slider (5).
2. An inflatable decoy according to claim 1, characterized in that: the launching vehicle main body (1) further comprises rollers (106), and the rollers (106) are respectively connected with two ends of the connecting base (101).
3. An inflatable decoy according to claim 1, characterized in that: the support assembly (4) further comprises a handle (44), and the handle (44) is fixedly connected with the other end of the screw rod (42).
4. An inflatable decoy according to claim 1, characterized in that: one end of the inflator (2) is fixedly provided with a controller (21).
5. An inflatable decoy according to claim 2, characterized in that: both sides of the headstock (105) are provided with windows (1051), and the top is provided with a skylight (1052).
6. An inflatable decoy according to claim 4, wherein: the top of the emission base (104) is provided with a plurality of emitters (1041).
7. An inflatable decoy according to claim 5, wherein: a plurality of missiles (1042) are arranged between the fence (103) and the launching base (104).
8. An inflatable decoy according to claim 6, wherein: the connecting base (101), the top plate (102), the fence (103), the launching base (104), the headstock (105), the roller (106), the launcher (1041) and the missile (1042) are all inflatable structures.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321184084.XU CN219869309U (en) | 2023-05-16 | 2023-05-16 | Inflatable false target |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321184084.XU CN219869309U (en) | 2023-05-16 | 2023-05-16 | Inflatable false target |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219869309U true CN219869309U (en) | 2023-10-20 |
Family
ID=88369011
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321184084.XU Active CN219869309U (en) | 2023-05-16 | 2023-05-16 | Inflatable false target |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219869309U (en) |
-
2023
- 2023-05-16 CN CN202321184084.XU patent/CN219869309U/en active Active
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