CN211317086U

CN211317086U - Missile box convenient for missile release

Info

Publication number: CN211317086U
Application number: CN201921948924.9U
Authority: CN
Inventors: 李荣璋
Original assignee: Sichuan Weiqier Trading Co ltd
Current assignee: Sichuan Xinlida Technology Development Co.,Ltd.
Priority date: 2019-11-12
Filing date: 2019-11-12
Publication date: 2020-08-21
Anticipated expiration: 2029-11-12

Abstract

The utility model relates to a field of guided missile storage discloses a conveniently put guided missile case of bullet, including box and case lid. The box body is located to the case lid, and box and case lid pass through the connector link and connect. The method is characterized in that: the box body and the box cover are both internally provided with a plurality of supports. The support is provided with a placing groove for accommodating the guided missile. The box body is provided with a plurality of limiting blocks at two opposite sides of the opening in a protruding mode. The two sides of the opening of the box cover are provided with limit grooves in cooperation with the limit blocks, so that the limit blocks are respectively accommodated in one limit groove when the box cover is arranged on the box body. After the guided missile box places the guided missile inside, the guided missile can be clamped by matching the support of the box body with the support of the box cover, the condition that the guided missile is fixed in the guided missile box by a special fastener is avoided, the guided missile placing process is simplified, the efficiency is improved, and the requirement of rapid response is met. And finally, the box cover cannot rock relative to the box body due to the matching of the limiting blocks and the limiting grooves, so that the stability of the missile box is ensured.

Description

Missile box convenient for missile release

Technical Field

The utility model relates to a field of guided missile storage particularly, relates to a conveniently put guided missile case of bullet.

Background

Missiles are important military weapons and are typically stored in missile boxes. The missile box plays a role in protecting the missile, and the quality of the missile in use is ensured. When the guided missile is placed in the guided missile box, the stability of the guided missile needs to be ensured, and the guided missile is prevented from being damaged due to shaking in the transportation process.

The chinese utility model patent of publication No. CN206944842U entitled "a guided missile container" discloses a guided missile storage box, and the inside downside of its box is fixed with the supporting seat, and length direction in the middle of the supporting seat opens has the cross-section to be semicircular projectile body fixed slot, and the top of supporting seat middle part and right part is equipped with two sets of semi-annular projectile body glands respectively, and the one end of projectile body gland forms normal running fit with the box is articulated, and the other end of projectile body gland passes through hasp and box fixed connection. When the missile fixing device is used, a missile is placed on the supporting seat, and then the missile is fastened and fixed in the missile guiding box through the missile body pressing cover. The missile box has troublesome fixed operation on the missile and can not meet the requirement of rapid response.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a conveniently put guided missile case of bullet, it can be quick be fixed in the guided missile incasement with the guided missile.

The embodiment of the utility model is realized like this:

a missile box convenient for missile release comprises a box body and a box cover; the box cover is arranged on the box body, and the box body is connected with the box cover through a connecting buckle; the method is characterized in that: a plurality of supports are arranged inside the box body and the box cover; the support is provided with a placing groove for accommodating the missile; a plurality of limiting blocks are arranged on two opposite sides of the opening of the box body in a protruding mode; the two sides of the opening of the box cover are provided with limiting grooves in cooperation with the limiting blocks, so that the limiting blocks are respectively accommodated in one limiting groove when the box cover is arranged on the box body.

Further, the rubber mat also comprises a plurality of rubber mats; the wall of the support on the placing groove is provided with a clamping groove; the rubber pad is provided with can the joint in the joint piece in joint groove to make the rubber pad can install in the support.

Furthermore, a bottom plate of the box body is provided with a plurality of accommodating grooves for accommodating the rubber pads.

Further, the support is provided with a spongy cushion on the wall of the placing groove.

Furthermore, the limiting blocks are arranged in pairs; the two limiting blocks in each pair are oppositely arranged on two sides of the box body; the top ends of each pair of limiting blocks are obliquely arranged close to each other.

Further, the support of the box body and the support of the box cover are arranged in pairs, so that the support of the box body and the support of the box cover enclose a closed placing groove after the box cover is arranged on the box body.

Further, the connecting buckle is a hasp.

The utility model has the advantages that:

when in use, the missile is placed in the box body. At the moment, the missile is accommodated in the placing grooves of the plurality of supports of the box body. Then, the box cover is covered on the box body, and the box body and the box cover are fixedly connected through the connecting buckle. After the box cover is arranged on the box body, the guided missiles are accommodated in the placing grooves of the plurality of supports of the box body and the placing grooves of the plurality of supports of the box cover; meanwhile, the limiting blocks are respectively accommodated in one limiting groove.

After the guided missile box places the guided missile inside, the guided missile can be clamped by matching the support of the box body with the support of the box cover, the condition that the guided missile is fixed in the guided missile box by a special fastener is avoided, the guided missile placing process is simplified, the efficiency is improved, and the requirement of rapid response is met. The missile can be clamped tightly by matching the support of the box body with the support of the box cover, so that the structure of the missile box is simplified. Finally, after the box body is covered by the box cover through the cooperation of the limiting blocks and the limiting grooves, the box cover cannot rock relative to the box body, the stability of the missile box is guaranteed, and the missile can be well protected by the missile box.

Drawings

In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings that are required to be used in the embodiments will be briefly described below, it should be understood that the following drawings only illustrate some embodiments of the present invention, and therefore should not be considered as limiting the scope, and for those skilled in the art, other related drawings can be obtained according to the drawings without inventive efforts.

Fig. 1 is a schematic view of a box body of the present invention;

fig. 2 is a schematic view of the case cover of the present invention;

FIG. 3 is an enlarged view taken at a in FIG. 2;

fig. 4 is a schematic view of the rubber pad of the present invention.

Icon: 1-box body, 11-limiting block, 12-bottom plate, 121-containing groove, 2-box cover, 21-limiting groove, 3-connecting buckle, 4-support, 41-placing groove, 42-clamping groove, 5-rubber pad and 51-clamping block.

Detailed Description

In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all, embodiments of the present invention. The components of embodiments of the present invention, as generally described and illustrated in the figures herein, may be arranged and designed in a wide variety of different configurations.

Thus, the following detailed description of the embodiments of the present invention, presented in the accompanying drawings, is not intended to limit the scope of the invention, as claimed, but is merely representative of selected embodiments of the invention. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.

It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, it need not be further defined and explained in subsequent figures.

In the description of the present invention, it should also be noted that, unless otherwise explicitly specified or limited, the terms "disposed," "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.

Example (b):

referring to fig. 1 to 4, the present embodiment provides a missile box convenient for missile discharging, which includes a box body 1 and a box cover 2. The case lid 2 lid is located box 1, and box 1 and case lid 2 are connected through connector link 3. In this embodiment, the connection buckle 3 is a buckle. One part of the hasp is arranged on the box body 1, and the other part of the hasp is arranged on the box cover 2. When the hasps are separated, the box body 1 and the box cover 2 can be completely separated, and the guided missile is greatly convenient to take and place. The box body 1 and the box cover 2 are both internally provided with a plurality of supports 4. The support 4 is provided with a housing groove 41 for housing the missile. The placing groove 41 is semicircular, and the shape of the placing groove is matched with the shape of the guided missile, so that the outer surface of the guided missile is well attached to the groove wall of the placing groove 41 after the guided missile is placed in the missile box. The supports 4 in the box body 1 and the box cover 2 are uniformly distributed, so that the guided missiles are stressed in the guided missile box uniformly. Two opposite sides of the opening of the box body 1 are respectively provided with a plurality of limiting blocks 11 in a protruding mode. The two sides of the opening of the case cover 2 are provided with limiting grooves 21 in cooperation with the limiting blocks 11, so that the limiting blocks 11 are respectively accommodated in one limiting groove 21 when the case cover 2 is covered on the case body 1.

When in use, the missile is placed in the box body 1. The missile is accommodated in the placing groove 41 of the plurality of supports 4 of the box body 1 and supported by the plurality of supports 4. Then, the case cover 2 is covered on the case body 1, and the case body 1 and the case cover 2 are fixedly connected through the connecting buckle 3. After the box cover 2 is covered on the box body 1, the missile is accommodated in the placing grooves 41 of the plurality of supports 4 of the box body 1 and the placing grooves 41 of the plurality of supports 4 of the box cover 2. Meanwhile, the limiting blocks 11 are respectively accommodated in one limiting groove 21.

After the guided missile box is placed inside, the guided missile can be clamped by matching the support 4 of the box body 1 and the support 4 of the box cover 2, the guided missile is not required to be fixed in the guided missile box by using a special fastener, the guided missile placing process is simplified, the efficiency is improved, and the requirement of rapid response is better met. The missile can be clamped by matching the support 4 of the box body 1 with the support 4 of the box cover 2, and the structure of the missile box is simplified. Finally, after the box cover 2 is arranged on the box body 1 through the cooperation of the limiting blocks 11 and the limiting grooves 21, the box cover 2 cannot rock relative to the box body 1, the stability of the missile box is guaranteed, and the missile box can well protect a missile.

The practical missile box convenient for missile release further comprises a plurality of rubber pads 5. The support 4 is provided with a clamping groove 42 on the groove wall of the placing groove 41. The rubber pad 5 is provided with a clamping block 51 which can be clamped in the clamping groove 42, so that the rubber pad 5 can be installed on the support 4. In practice, there are a plurality of missile types, and each missile type has different overall dimensions; each missile is not cylindrical, and the outer diameters of two ends of each missile can be different; these may result in different sizes of the placement slots 41, which in turn results in a missile box that is only suitable for one missile type. After the rubber pad 5 is mounted on the support 4, the size of the placing groove 41 is reduced; after the rubber pad 5 is taken down from the support 4, the size of the placing groove 41 is increased; the rubber pads 5 enable the size of the placing groove 41 to be adjusted, and therefore one missile box can be suitable for missiles of multiple models. In practice, a plurality of rubber pads 5 with different thicknesses can be configured, so that the accommodating groove 41 can be adjusted to have more sizes and can be adapted to more missile models.

In this embodiment, the bottom plate 12 of the box 1 is provided with a plurality of receiving grooves 121 for receiving the rubber pads 5. When the rubber pad 5 is not used, the rubber pad 5 can be placed in the accommodating groove 121, so that the rubber pad 5 can be conveniently accommodated.

In this embodiment, the sponge pad is disposed on the wall of the placing groove 41 of the support 4. When the rubber pad 5 is not arranged on the support 4, a sponge pad is arranged between the support 4 and the missile, so that the missile can be prevented from being damaged by friction with the support 4; meanwhile, the spongy cushion can absorb shock, and the missile is protected as far as possible.

In this embodiment, the stoppers 11 are provided in pairs. The two limit blocks 11 of each pair are oppositely arranged at two sides of the box body 1. The top ends of each pair of limiting blocks 11 are obliquely arranged close to each other. After the guided missile is placed in the placing groove 41, the guided missile is clamped by the pair of limiting blocks 11, and the guided missile can be well positioned.

In this embodiment, the support 4 of the box 1 and the support 4 of the box cover 2 are arranged in pair, so that the support 4 of the box 1 and the support 4 of the box cover 2 enclose a closed placing groove 41 after the box cover 2 is covered on the box 1. After the guided missile is placed in the guided missile box, the guided missile is firmly embraced by the support 4 of the box body 1 and the support 4 of the box cover 2, and the guided missile can be well positioned. The missile is stably placed in the missile box.

The above is only a preferred embodiment of the present invention, and is not intended to limit the present invention, and various modifications and changes will occur to those skilled in the art. 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. A missile box convenient for missile release comprises a box body (1) and a box cover (2); the box cover (2) is arranged on the box body (1) in a covering mode, and the box body (1) is connected with the box cover (2) through a connecting buckle (3); the method is characterized in that: a plurality of supports (4) are arranged inside the box body (1) and the box cover (2); the support (4) is provided with a placing groove (41) for containing a guided missile; a plurality of limiting blocks (11) are respectively arranged on two opposite sides of the opening of the box body (1) in a protruding mode; the two sides of the opening of the box cover (2) are provided with limiting grooves (21) in cooperation with the limiting blocks (11), so that the limiting blocks (11) are respectively accommodated in one limiting groove (21) when the box cover (2) is arranged on the box body (1).

2. The missile box convenient for missile release according to claim 1 is characterized in that: also comprises a plurality of rubber pads (5); the wall of the support (4) on the placing groove (41) is provided with a clamping groove (42); the rubber pad (5) is provided with a clamping block (51) which can be clamped in the clamping groove (42), so that the rubber pad (5) can be arranged on the support (4).

3. The missile box convenient for missile release according to claim 2 is characterized in that: the bottom plate (12) of the box body (1) is provided with a plurality of accommodating grooves (121) for accommodating the rubber pads (5).

4. The missile box convenient for missile release according to claim 1 is characterized in that: the sponge pads are arranged on the wall of the placing groove (41) of the support (4).

5. The missile box convenient for missile release according to claim 1 is characterized in that: the limiting blocks (11) are arranged in pairs; the two limiting blocks (11) in each pair are oppositely arranged on two sides of the box body (1); the top ends of each pair of the limiting blocks (11) are obliquely arranged close to each other.

6. The missile box convenient for missile release according to claim 1 is characterized in that: the support (4) of the box body (1) and the support (4) of the box cover (2) are arranged in pairs, so that the box cover (2) is arranged on the box body (1) in a covering mode, and the support (4) of the box body (1) and the support (4) of the box cover (2) enclose to form a closed placing groove (41).

7. The missile box convenient for missile release according to claim 1 is characterized in that: the connecting buckle (3) is a hasp.