CN220689925U

CN220689925U - Missile carrier

Info

Publication number: CN220689925U
Application number: CN202321775906.1U
Authority: CN
Inventors: 朱荣生; 熊瑶
Original assignee: Jiangxi Jingqin Technology Co ltd
Current assignee: Jiangxi Jingqin Technology Co ltd
Priority date: 2023-07-07
Filing date: 2023-07-07
Publication date: 2024-03-29
Anticipated expiration: 2033-07-07

Abstract

The utility model discloses a missile carrier. The utility model comprises two bases and two placing seats, wherein the upper surfaces of the placing seats are provided with placing grooves, the upper surfaces of the placing seats are provided with rotating rods, the upper ends of the rotating rods are fixedly connected with adjusting rods, one ends of the adjusting rods are fixedly connected with moving rods, the bottom ends of the moving rods are fixedly connected with sliding rods, the Zhou Cemian of the sliding rods are provided with nuts, a connecting shaft is connected between the two adjusting rods, and the upper surfaces of the two placing seats are provided with sliding grooves. According to the missile placing device, the sliding rod, the screw cap and the adjusting rod are arranged, the sliding rod is pulled, the adjusting rod is driven by the sliding rod to move, and the included angle between the two adjusting rods changes in the moving process of the adjusting rod, so that the distance between the two placing seats is adjusted, the missile placing device can be used for adjusting and placing according to the types of missiles, and the missile placing device is suitable for placing missiles with different lengths and high in practicability.

Description

Missile carrier

Technical Field

The utility model belongs to the technical field of missile carrier, and particularly relates to a missile carrier.

Background

Missiles (which are an aircraft that carries a warhead, relies on its own power means to propel, is guided by a guidance system to control the flight path, guides and destroys the target, are typically composed of a warhead, control system, engine means, and projectile, etc. the payload of the target is the warhead (or warhead).

Before the missile is used, the missile carrier is usually required to be used for storing the missile, and the existing missile carrier cannot be used for adjusting and storing according to different types of missiles due to different shapes of the missiles, so that the practicability is lower.

Disclosure of Invention

The utility model aims to provide a missile carrier, which solves the problems that before a missile is used, the missile carrier is usually required to be used for storing the missile, and the existing missile carrier cannot be used for adjusting and storing according to different types of missiles due to different shapes of the missiles with different types, so that the practicability is lower.

In order to solve the technical problems, the utility model is realized by the following technical scheme:

the utility model relates to a missile supporting frame which comprises two bases and two placing seats, wherein the upper surfaces of the placing seats are provided with placing grooves, the upper surfaces of the placing seats are provided with rotating rods, the upper ends of the rotating rods are fixedly connected with adjusting rods, one ends of the adjusting rods are fixedly connected with moving rods, the bottom ends of the moving rods are fixedly connected with sliding rods, the peripheral side surfaces of the sliding rods are provided with nuts, a connecting shaft is connected between the two adjusting rods, and the upper surfaces of the two placing seats are provided with sliding grooves.

The lifting device comprises a base, a lifting rod is arranged in the mounting column, the upper end of the lifting rod is fixedly connected with a placement seat, a plurality of slots are formed in the surface of the lifting rod, a fixing seat is arranged in the mounting column in a surface-fixed mode, a spring is fixedly arranged in the fixing seat, one end of the spring is fixedly connected with a sliding block, an inserting rod is fixedly connected with the surface of the sliding block, a connecting groove is formed in the bottom surface of the fixing seat, a pull rod is arranged in the connecting groove, and one end of the pull rod is fixedly connected with the sliding block.

Wherein, two the bottom surface of base all installs a plurality of universal wheels.

One end of the sliding rod is installed in the sliding groove, the sliding rod is in sliding fit with the sliding groove, and the sliding rod is in threaded fit with the nut.

Wherein, two adjust the pole all with connecting axle normal running fit, adjust pole and bull stick normal running fit.

Wherein, the one end of inserted bar is installed in the slot, and inserted bar and slot sliding fit.

The pull rod is in sliding fit with the connecting groove, the sliding block is in sliding fit with the fixing seat, and the lifting rod is in sliding fit with the mounting column.

The utility model has the following beneficial effects:

1. according to the missile placing device, the sliding rod, the screw cap and the adjusting rod are arranged, the sliding rod is pulled, the adjusting rod is driven by the sliding rod to move, and the included angle between the two adjusting rods changes in the moving process of the adjusting rod, so that the distance between the two placing seats is adjusted, the missile placing device can be used for adjusting and placing according to the types of missiles, and the missile placing device is suitable for placing missiles with different lengths and high in practicability.

2. The lifting rod, the spring and the inserted link are arranged, the lifting rod is pulled, the height of the placing seat can be adjusted, the lifting rod is suitable for users with different heights to operate, and after the height adjustment is finished, the spring pushes the sliding block to further push the inserted link to be inserted into the slot to fix the height of the lifting rod.

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 present utility model, the drawings that are needed for the description of the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present utility model, and that other drawings may 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 a schematic view of a front left side perspective of the present utility model;

FIG. 3 is a schematic diagram of the front view of the present utility model;

FIG. 4 is a right side view of the present utility model;

fig. 5 is a schematic view of the cross-sectional structure A-A of fig. 4.

In the drawings, the list of components represented by the various numbers is as follows: 1. a base; 2. a placement seat; 3. a placement groove; 4. a rotating rod; 5. an adjusting rod; 6. a moving rod; 7. a connecting shaft; 8. a chute; 9. a mounting column; 10. a lifting rod; 11. a fixing seat; 12. a slot; 13. a universal wheel; 14. a pull rod; 15. a slide bar; 16. a screw cap; 17. a spring; 18. a slide block; 19. a rod; 20. and a connecting groove.

Detailed Description

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

In the description of the present utility model, it should be understood that the terms "upper," "middle," "outer," "inner," and the like indicate an orientation or a positional relationship, and are merely for convenience of describing the present utility model and simplifying the description, but do not indicate or imply that the components or elements referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus should not be construed as limiting the present utility model.

Referring to fig. 1-5, the missile supporting frame disclosed by the utility model comprises two bases 1 and two placing seats 2, wherein a placing groove 3 is formed in the upper surface of each placing seat 2, a rotating rod 4 is installed on the upper surface of each placing seat 2, an adjusting rod 5 is fixedly connected to the upper end of each rotating rod 4, one end of each adjusting rod 5 is fixedly connected with a moving rod 6, the bottom end of each moving rod 6 is fixedly connected with a sliding rod 15, a nut 16 is installed on the peripheral side surface of each sliding rod 15, a connecting shaft 7 is connected between each two adjusting rods 5, sliding grooves 8 are formed in the upper surfaces of the two placing seats 2, the sliding rods 15, the nuts 16 and the adjusting rods 5 are arranged, the sliding rods 15 are pulled to drive the adjusting rods 5 to move through the moving rods 6, and therefore the distance between the two placing seats 2 is adjusted, the missile supporting frame can be adjusted and placed according to the types of missiles, and the missile supporting frame is high in practicability.

The upper surface of the base 1 is fixedly provided with a mounting column 9, a lifting rod 10 is arranged in the mounting column 9, the upper end of the lifting rod 10 is fixedly connected with the placing seat 2, a plurality of slots 12 are formed in the surface of the lifting rod 10, a fixed seat 11 is fixedly arranged in the surface of the mounting column 9, a spring 17 is fixedly arranged in the fixed seat 11, one end of the spring 17 is fixedly connected with a sliding block 18, the surface of the sliding block 18 is fixedly connected with an inserting rod 19, a connecting groove 20 is formed in the bottom surface of the fixed seat 11, a pull rod 14 is arranged in the connecting groove 20, one end of the pull rod 14 is fixedly connected with the sliding block 18, the lifting rod 10, the spring 17 and the inserting rod 19 are arranged, the lifting rod 10 is pulled, the height of the placing seat 2 can be adjusted, the lifting rod is suitable for users with different heights to operate, after the height adjustment is completed, the spring 17 pushes the sliding block 18, and the inserting rod 19 is further pushed into the slots 12 to be inserted into the slots 12 to fix the height of the lifting rod 10.

Wherein, a plurality of universal wheels 13 are all installed to the bottom surface of two bases 1, set up a plurality of universal wheels 13, make things convenient for the removal of equipment.

Wherein, the one end of slide bar 15 is installed in spout 8, and slide bar 15 and spout 8 sliding fit, slide bar 15 and nut 16 screw thread fit set up slide bar 15 and nut 16 screw thread fit, after the size of placing seat 2 is adjusted, screw up the nut 16 and can fix the size of placing seat 2.

Wherein, two regulation poles 5 all with connecting axle 7 normal running fit, adjust pole 5 and bull stick 4 normal running fit, set up regulation pole 5 and bull stick 4 for two regulation poles 5 can rotate, thereby adjust the size of placing seat 2 through adjusting the interval between two regulation poles 5.

Wherein, the one end of inserted bar 19 is installed in slot 12, and inserted bar 19 and slot 12 sliding fit set up inserted bar 19 and slot 12, can fix the height of lifter 10.

Wherein, pull rod 14 and spread groove 20 sliding fit, slider 18 and fixing base 11 sliding fit, lifter 10 and erection column 9 sliding fit set up pull rod 14, and pull rod 14 pulls slider 18, and then drives inserted bar 19 and remove, conveniently controls the height of lifter 10.

Examples

As shown in fig. 1 to 5, the missile carrier of the present utility model is used as follows: when the missile placing device is used, equipment is moved to a corresponding position, the height of the placing seat 2 is adjusted according to the height of a worker, the pull rod 14 is pulled in a direction away from the slot 12, the pull rod 14 drives the inserting rod 19 to move through the sliding block 18, after the height adjustment is finished, the pull rod 14 is loosened, the sliding block 18 pushes the inserting rod 19 to be inserted into the slot 12 under the action of the spring 17, the height adjustment of the placing seat 2 is finished, then the distance between the two placing seats 2 is adjusted according to the length of a missile, the sliding rod 15 is pulled, the adjusting rod 5 is driven to move by the sliding rod 15 through the moving rod 6, the included angle between the two adjusting rods 5 is changed in the moving process of the adjusting rod 5, so that the distance between the two placing seats 2 is adjusted, then the nut 16 is screwed down to fix the size of the placing seat 2, and then the missile is placed.

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 present 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 preferred embodiments of the utility model disclosed above are intended only to assist in the explanation of 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. The utility model is limited only by the claims and the full scope and equivalents thereof.

Claims

1. The utility model provides a guided missile carrier, includes two bases (1) and two places seat (2), its characterized in that: place the upper surface of seat (2) and seted up standing groove (3), the upper surface of placing seat (2) installs bull stick (4), the upper end fixedly connected with of bull stick (4) adjusts pole (5), the one end fixedly connected with movable rod (6) of regulation pole (5), the bottom fixedly connected with slide bar (15) of movable rod (6), nut (16) are installed to the week side of slide bar (15), two be connected with connecting axle (7) between regulation pole (5), two spout (8) have all been seted up to the upper surface of placing seat (2).

2. The missile carrier according to claim 1, wherein the mounting column (9) is fixedly mounted on the upper surface of the base (1), the lifting rod (10) is mounted in the mounting column (9), the upper end of the lifting rod (10) is fixedly connected with the placement seat (2), a plurality of slots (12) are formed in the surface of the lifting rod (10), the fixing seat (11) is fixedly mounted on the surface of the mounting column (9), the spring (17) is fixedly mounted in the fixing seat (11), one end of the spring (17) is fixedly connected with the sliding block (18), the inserting rod (19) is fixedly connected with the surface of the sliding block (18), the connecting groove (20) is formed in the bottom surface of the fixing seat (11), the pull rod (14) is mounted in the connecting groove (20), and one end of the pull rod (14) is fixedly connected with the sliding block (18).

3. A missile launcher according to claim 1, characterized in that the bottom surfaces of both bases (1) are provided with universal wheels (13).

4. A missile carrier according to claim 1, characterized in that one end of the slide bar (15) is mounted in the chute (8), and that the slide bar (15) is in sliding engagement with the chute (8), and that the slide bar (15) is in threaded engagement with the nut (16).

5. A missile carrier according to claim 1, characterized in that both of the adjustment rods (5) are in a rotational fit with the connecting shaft (7), the adjustment rods (5) being in a rotational fit with the swivel rods (4).

6. A missile launcher according to claim 2, characterized in that one end of the spigot (19) is mounted in the socket (12) and the spigot (19) is in sliding engagement with the socket (12).

7. A missile carrier according to claim 2, characterized in that the pull rod (14) is in sliding fit with the connecting slot (20), the slider (18) is in sliding fit with the fixed seat (11), and the lifting rod (10) is in sliding fit with the mounting post (9).