CN212870919U

CN212870919U - Missile launching vehicle inflation simulation target

Info

Publication number: CN212870919U
Application number: CN202021224547.7U
Authority: CN
Inventors: 张德昭
Original assignee: Changzhou Dejite Technology Co ltd
Current assignee: Changzhou Dejite Technology Co ltd
Priority date: 2020-06-29
Filing date: 2020-06-29
Publication date: 2021-04-02
Anticipated expiration: 2030-06-29

Abstract

The utility model belongs to the technical field of target manufacturing and processing, in particular to an inflatable simulation target for a missile launching vehicle, which comprises an inflatable simulation target body, wherein front wheels are integrally formed on both sides of the front end of the inflatable simulation target body, rear wheels are integrally formed on both sides of the rear end of the inflatable simulation target body, a plurality of middle wheels are integrally formed at the middle position of the inflatable simulation target body, a first wheel seat plate is fixed on the bottom end surfaces of the front wheels and the rear wheels, a second wheel seat plate is fixed on the bottom end surfaces of the middle wheels, an insert cavity is arranged at the middle position of one side of the first wheel seat plate, an insert rod is inserted in the insert cavity, the bottoms of the front wheels, the rear wheels and the rear wheels are protected by the first wheel seat plate and the second wheel seat plate, the front wheels, the rear wheels and the middle wheels are not easy to be pricked to cause air leakage, and the insert rod positioned in the insert cavity by one side of the first wheel seat plate is inserted in the ground, the front wheels and the rear wheels are fixed to a certain degree, and the wind resistance of the inflatable simulation target body is improved.

Description

Missile launching vehicle inflation simulation target

Technical Field

The utility model belongs to the technical field of the processing is made to the target, concretely relates to emulation target is aerifyd to guided missile launch vehicle.

Background

Military exercises, called military exercises for short, are exercises of operational commands and actions under the induction of imagination conditions, are implemented by armies after theoretical learning and basic training are completed, approximate comprehensive training of actual combat is achieved, the advanced stage of military training is achieved, in the process of military exercises, inflatable simulation targets are required to be used, the simulation degree of the inflatable simulation targets is high, the military exercises are good in effect, the inflatable simulation targets are made into corresponding shapes according to specific requirements, such as tank types, airplane types or building types, and the inflatable simulation targets of missile launching vehicle types are also commonly used.

However, the existing missile launching vehicle inflation simulation target has the following problems in the use process: the missile launching vehicle inflatable simulation target is usually arranged on the ground, and the inflatable tire integrally formed on the periphery of the bottom of the missile launching vehicle inflatable simulation target is in fit contact with the ground, so that the inflatable tire is easily punctured by sharp objects on the ground to cause gas leakage in the use process, and the missile launching vehicle inflatable simulation target is inconvenient to use; although the missile launching vehicle is relatively large in size, the interior of the missile launching vehicle is filled with gas, the overall weight is relatively light, and when the missile launching vehicle is used in a plain area, the missile launching vehicle is poor in wind resistance, easy to stress and move and relatively inconvenient to use.

SUMMERY OF THE UTILITY MODEL

For solving the above-mentioned problem that exists among the prior art, the utility model provides a simulation target is aerifyd to guided missile launch vehicle has simple structure and uses convenient characteristics.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a simulation target is aerifyd to guided missile launch vehicle, is including aerifing the simulation target body, the equal integrated into one piece in front end both sides of aerifing the simulation target body has the front wheel, the equal integrated into one piece in rear end both sides of aerifing the simulation target body has the rear wheel, the intermediate position department integrated into one piece of aerifing the simulation target body has a plurality of middle wheel, the bottom face of front wheel and rear wheel all is fixed with a wheel bedplate, the bottom face of middle wheel is fixed with No. two wheel bedplate, one side intermediate position department of a wheel bedplate has been seted up and has been inserted the chamber, the inside of inserting the chamber is inserted and has been closed the inserted bar.

As the utility model discloses a preferred technical scheme of emulation target is aerifyd to guided missile launch vehicle, the bottom face level of front wheel, rear wheel and well wheel is unanimous, the bottom face level of a wheel bedplate and No. two wheel bedplates is unanimous, a wheel bedplate and No. two wheel bedplates are the rubber material and all are the symmetry setting.

As the utility model discloses a guided missile launch vehicle aerifys preferred technical scheme of emulation target, the upper end of inserted bar is fixed with the rod seat, the outer wall of rod seat is the arc structure all around.

As the utility model discloses a preferred technical scheme of emulation target is aerifyd to guided missile launch vehicle, the up end intermediate position department of rod seat is fixed with the shadoof, the outer wall of shadoof is fixed with the rod cover all around, the shadoof is the arc structure with the rod cover.

As the utility model discloses a preferred technical scheme of emulation target is aerifyd to guided missile launch vehicle, the bottom of inserted bar is the toper structure and mutually perpendicular with a wheel bedplate.

As the utility model discloses a preferred technical scheme of emulation target is aerifyd to guided missile launch vehicle, inserted bar, rod holder and shadoof are metal component.

Compared with the prior art, the beneficial effects of the utility model are that: when the inflatable simulation target body is used, the bottoms of the front wheel, the rear wheel and the rear wheel around the bottom of the inflatable simulation target body are protected through the first wheel seat plate and the second wheel seat plate, the front wheel, the rear wheel and the middle wheel are not easy to be punctured to cause air leakage, and the inflatable simulation target body is simple in structure and convenient and fast to use; the utility model provides a wheel seat board's one side intermediate position department has seted up and has inserted the chamber, and the inside of inserting the chamber is inserted and is closed and be connected with the inserted bar, and the inserted bar that is located to insert the intracavity portion through a wheel seat board one side inlays to be inserted and inserts and insert ground, carries out certain fixed to front wheel and rear wheel, increases the wind resistance of aerifing emulation target body, aerifys the difficult atress activity of emulation target body, simple structure, and it is convenient to use.

Drawings

The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention. In the drawings:

fig. 1 is a schematic structural view of the present invention;

FIG. 2 is a schematic side view of the connection between the front wheel and the first wheel seat plate of the present invention;

FIG. 3 is a schematic side view of the connection between the front wheel and the first wheel seat plate of the present invention;

FIG. 4 is a side view of the connection between the middle wheel and the second wheel seat handle of the present invention;

in the figure: 1. an inflatable simulation target body; 2. a front wheel; 3. a rear wheel; 4. a middle wheel; 5. a first wheel seat plate; 6. a second wheel seat plate; 7. inserting a cavity; 8. inserting a rod; 9. a rod seat; 10. lifting a rod; 11. a rod sleeve.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Examples

Referring to fig. 1-4, the present invention provides the following technical solutions: the missile launching vehicle inflation simulation target comprises an inflation simulation target body 1, front wheels 2 are integrally formed on two sides of the front end of the inflation simulation target body 1, rear wheels 3 are integrally formed on two sides of the rear end of the inflation simulation target body 1, a plurality of middle wheels 4 are integrally formed in the middle position of the inflation simulation target body 1, a first wheel seat plate 5 is fixed on the bottom end surfaces of the front wheels 2 and the rear wheels 3, a second wheel seat plate 6 is fixed on the bottom end surface of the middle wheels 4, an insertion cavity 7 is formed in the middle position of one side of the first wheel seat plate 5, an insertion rod 8 is inserted in the insertion cavity 7, in the embodiment, the inflation simulation target body 1 and the front wheels 2, the rear wheels 3 and the middle wheels 4 around the bottom of the inflation simulation target body 1 can refer to the existing missile launching vehicle inflation simulation target sold in the market, and when the missile launching vehicle inflation simulation target is used, the front wheels 2, the rear wheels and the middle wheels 4 around the bottom of the inflation simulation target body 1 are connected through the first wheel seat plate 5 and the second wheel seat plate 6, The bottoms of the rear wheels 3 and the rear wheels 3 are protected, the front wheels 2, the rear wheels 3 and the middle wheels 4 are not easy to be pricked to cause air leakage, the structure is simple, and the use is convenient; insert through 5 one side of a wheel bedplate and lie in inserting the inside inserted bar 8 of chamber 7 and insert in the ground, carry out certain fixed to front wheel 2 and rear wheel 3, increase the wind resistance of aerifing emulation target body 1, aerify the difficult atress activity of emulation target body 1, simple structure, it is convenient to use.

Specifically, the bottom face level of front wheel 2, rear wheel 3 and well wheel 4 is unanimous, the bottom face level of a wheel seat board 5 and No. two wheel seat boards 6 is unanimous, a wheel seat board 5 and No. two wheel seat boards 6 are the rubber material and all are the symmetry setting, in this embodiment, a wheel seat board 5 is the rubber material, a protection for

front wheel

2 and 3 bottoms of rear wheel, No. two wheel seat boards 6 are the rubber material, a protection for 4 bottoms of well wheel, prevent through a wheel seat board 5 and No. two wheel seat boards 6 that front wheel 2, rear wheel 3 and well wheel 4 are pricked by the sharp object in the ground in the use and take place gas leakage.

Specifically, the upper end of inserted bar 8 is fixed with pole socket 9, and the outer wall of pole socket 9 is arc structure all around, and in this embodiment, pole socket 9 is the metal arc, and the auxiliary of the inserted bar 8 of being convenient for is pressed and is inlayed and insert.

Specifically, the up end intermediate position department of rod seat 9 is fixed with shadoof 10, and the outer wall of shadoof 10 is fixed with rod cover 11 all around, and shadoof 10 is the arc structure with rod cover 11, and in this embodiment, shadoof 10 is the metal arc, and the carrying of rod seat 9 and inserted bar 8 of being convenient for is carried, and rod cover 11 is the rubber arc, and the comfortable of rod seat 9 of being convenient for grips.

Specifically, the bottom of inserted bar 8 is the toper structure and with a wheel seat 5 mutually perpendicular, in this embodiment, inserted cavity 7 is the cylindricality cavity, inserted bar 8 is the metal cylindricality, and the bottom is the toper, can inlay the ground of inserting for front wheel 2 and rear wheel 3 are fixed, thereby increase the wind resistance of aerifing emulation target body 1, make and aerify the difficult atress activity of emulation target body 1.

Specifically, the inserted link 8, the rod seat 9 and the lifting rod 10 are all metal components, and in this embodiment, the metal components are adopted, so that the steel bar is strong, wear-resistant and easy to use.

The utility model discloses a theory of operation and use flow: the utility model discloses when using, will aerify emulation target body 1 and place on the level land, then will aerify emulation target body 1 and inflate the gas strut, simulation target body 1's locating position is aerifyd in proper adjustment, it is just putting and places to make it, and make the bottom face of front wheel 2 and a wheel seat 5 laminate with ground each other, promote pole seat 9 and inserted bar 8 through lifter 10, insert inserted bar 8 in the chamber 7 of inserting that 5 one side intermediate position departments of a wheel seat were seted up, and continue to insert inserted bar 8 in the ground downwards, protect front wheel 2 and rear wheel 3's bottom through a wheel seat 5, protect bottom of taking turns 4 through No. two wheel seats 6, fix front wheel 2 and rear wheel 3 bottoms through a wheel seat 5 and inserted bar 8, then use aerifing emulation target body 1.

Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. The utility model provides a guided missile launching vehicle aerifys emulation target which characterized in that: including aerifing emulation target body (1), the equal integrated into one piece in front end both sides of aerifing emulation target body (1) has front wheel (2), the equal integrated into one piece in rear end both sides of aerifing emulation target body (1) has rear wheel (3), the intermediate position department integrated into one piece of aerifing emulation target body (1) has a plurality of well wheel (4), the bottom face of front wheel (2) and rear wheel (3) all is fixed with a wheel seat board (5), the bottom face of well wheel (4) is fixed with No. two wheel seat boards (6), one side intermediate position department of a wheel seat board (5) has been seted up and has been inserted chamber (7), the inside of inserting chamber (7) is inserted and has been closed inserted bar (8).

2. The missile launcher inflation simulation target of claim 1, wherein: the bottom end face level of front wheel (2), rear wheel (3) and well wheel (4) is unanimous, the bottom end face level of a wheel seat board (5) and No. two wheel bedplate (6) is unanimous, a wheel seat board (5) and No. two wheel bedplate (6) are rubber material and all are the symmetry and set up.

3. The missile launcher inflation simulation target of claim 1, wherein: a rod seat (9) is fixed at the upper end of the inserted rod (8), and the periphery of the outer wall of the rod seat (9) is of an arc-shaped structure.

4. The missile launcher inflation simulation target of claim 3, wherein: a lifting rod (10) is fixed in the middle of the upper end face of the rod seat (9), a rod sleeve (11) is fixed on the periphery of the outer wall of the lifting rod (10), and the lifting rod (10) and the rod sleeve (11) are both arc-shaped structures.

5. The missile launcher inflation simulation target of claim 1, wherein: the bottom end of the inserted bar (8) is of a conical structure and is perpendicular to the first wheel seat plate (5).

6. The missile launcher inflation simulation target of claim 1, wherein: the inserted bar (8), the bar seat (9) and the lifting bar (10) are all metal components.