Missile adapter

Abstract

The utility model belongs to the technical field of missile adapters, and particularly relates to a missile adapter which comprises a supporting seat, a missile cylinder and an adapter, the supporting seat comprises a base, a screw hole and supporting ribs, the screw hole is formed in the center of the top of the base, and the supporting ribs are circumferentially distributed on the outer side of the screw hole; the missile cylinder is arranged on the base and comprises a cylinder body and a screw rod, the outer wall of the cylinder body is embedded between the supporting ribs, and the screw rod connected with the screw hole is arranged at the bottom of the cylinder body; the adaptive part is arranged in the cylinder body, the supporting ribs are arranged between the base and the cylinder body of the missile cylinder, the circular sleeve type adaptive part is arranged in the cylinder body, the adaptive part is used for supporting between the missile cylinder and a missile shell, the stability of missile placement is guaranteed, the supporting ribs are used for supporting the side edges, the situation that a screw rod inclines and breaks is avoided, and the structural stability is improved.

Description

Technical Field

[0001] The utility model relates to the technical field of missile adapters, in particular to a missile adapter. Background Art

[0002] The adapter is an elastic support system configured between the missile and the launch tube. It plays a role in buffering and reducing vibration during the storage, transportation and loading and unloading of the missile, and plays a role in sealing, supporting and guiding during launch. Missiles launched using launch boxes and launch tubes are basically equipped with adapters.

[0003] When the existing adapter is in use, the missile barrel is connected to the base casting through a threaded connecting shaft. When connected, there is no corresponding support on the side, and the screw is easy to tilt and break, affecting the stability of the structure. Therefore, the present application proposes a missile adapter. Utility Model Content

[0004] The purpose of this section is to summarize some aspects of the embodiments of the utility model and briefly introduce some preferred embodiments. Some simplifications or omissions may be made in this section and the abstract of the specification and the name of the utility model of this application to avoid blurring the purpose of this section, the abstract of the specification and the name of the utility model, and such simplifications or omissions cannot be used to limit the scope of the utility model.

[0005] In view of the above problems and / or the problems existing in the existing missile adapters, the present utility model is proposed.

[0006] Therefore, the purpose of the utility model is to provide a missile adapter, in which a circular sleeve-type adapter is arranged inside the barrel, and the adapter is used to support between the missile barrel and the missile shell to ensure the stability of the missile placement, and the support ribs are used to support the side to avoid the screw from tilting and breaking, thereby improving the structural stability.

[0007] In order to solve the above technical problems, according to one aspect of the present invention, the present invention provides the following technical solutions:

[0008] A missile adapter, comprising:

[0009] The support seat comprises a base, a screw hole and a support rib, wherein the screw hole is arranged at the center of the top of the base, and the support ribs are circumferentially distributed outside the screw hole;

[0010] A missile barrel is arranged on the base, the missile barrel comprises a barrel body and a screw rod, the outer wall of the barrel body is embedded between the supporting ribs, and the bottom of the barrel body is provided with a screw rod connected with a screw hole;

[0011] The adapter is arranged in the cylinder.

[0012] As a preferred solution of the missile adapter described in the utility model, a knob bolt is arranged on the support rib, and the threaded end of the knob bolt faces the barrel.

[0013] As a preferred solution of a missile adapter described in the utility model, wherein: a slide rail is arranged on the inner wall of the cylinder, the adapter comprises a support sleeve and a slide groove, the support sleeve is embedded in the cylinder, and a slide groove connected to the slide rail is arranged on the outer wall of the support sleeve.

[0014] As a preferred solution of the missile adapter described in the utility model, a limiting groove is provided on the outer wall of the cylinder, and when the cylinder is connected to the base, the limiting groove corresponds to the threaded end of the knob bolt.

[0015] As a preferred solution of the missile adapter described in the utility model, the support sleeve is provided with evenly distributed wing grooves.

[0016] As a preferred solution of the missile adapter described in the utility model, the limiting groove is an annular groove, and the inside of the limiting groove is provided with evenly distributed anti-slip convex patterns.

[0017] As a preferred solution of the missile adapter described in the utility model, the support sleeve adopts a multi-layer structure.

[0018] Compared with the prior art: the utility model arranges a circular sleeve-shaped adapter inside the barrel, and uses the adapter to support between the missile barrel and the missile shell to ensure the stability of the missile placement, and arranges support ribs between the base and the barrel of the missile barrel. After the missile barrel is connected to the base, the support ribs are used to support the side to avoid the screw from tilting and breaking, thereby improving the structural stability. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] In order to more clearly illustrate the technical solution of the implementation of the utility model, the utility model will be described in detail below in combination with the drawings and detailed implementation. Obviously, the drawings described below are only some implementations of the utility model. For ordinary technicians in this field, other drawings can be obtained based on these drawings without creative labor. Among them:

[0020] Figure 1 This is a schematic diagram of the shaft side structure of the utility model;

[0021] Figure 2 This is a schematic diagram of the cross-sectional structure of the utility model;

[0022] Figure 3 This is a schematic diagram of the support seat structure of the utility model;

[0023] Figure 4This is a schematic diagram of the internal structure of the missile tube of the utility model;

[0024] Figure 5 It is a schematic diagram of the structure of the adapter of the utility model.

[0025] In the figure: 100 support seat, 110 base, 120 screw hole, 130 support rib, 140 knob bolt, 200 missile barrel, 210 barrel body, 220 screw rod, 230 slide rail, 240 limit groove, 300 adapter, 310 support sleeve, 320 slide groove, 330 wing groove. DETAILED DESCRIPTION

[0026] In order to make the above-mentioned objects, features and advantages of the present invention more obvious and easy to understand, the specific implementation methods of the present invention are described in detail below with reference to the accompanying drawings.

[0027] In the following description, many specific details are set forth to facilitate a full understanding of the present invention, but the present invention may also be implemented in other ways different from those described herein, and those skilled in the art may make similar generalizations without violating the connotation of the present invention. Therefore, the present invention is not limited to the specific implementation methods disclosed below.

[0028] Secondly, the present invention is described in detail with reference to the schematic diagram. When describing the implementation of the present invention, for the sake of convenience, the cross-sectional diagram showing the device structure will not be partially enlarged according to the general proportion, and the schematic diagram is only an example, which should not limit the scope of protection of the present invention. In addition, in actual production, the three-dimensional dimensions of length, width and depth should be included.

[0029] In order to make the purpose, technical solution and advantages of the present invention more clear, the implementation mode of the present invention will be further described in detail below with reference to the accompanying drawings.

[0030] The utility model provides a missile adapter, in which a support rib is arranged between the base and the barrel of the missile barrel. After the missile barrel is connected to the base, the support rib is used to support the side to prevent the screw from tilting and breaking, thereby improving the structural stability. Figure 1-Figure 5 , including: a support seat 100, a missile tube 200 and an adapter 300.

[0031] The support base 100 includes a base 110, a screw hole 120 and a support rib 130. The screw hole 120 is arranged at the center of the top of the base 110, and the support rib 130 is distributed around the outside of the screw hole 120.

[0032] The base 110 is made of rectangular cast iron, and the support ribs 130 are welded structures evenly distributed on the outside of the screw holes 120 .

[0033] The missile barrel 200 is disposed on the base 110. The missile barrel 200 includes a barrel body 210 and a screw rod 220. The outer wall of the barrel body 210 is embedded between the support ribs 130. The screw rod 220 connected to the screw hole 120 is disposed at the bottom of the barrel body 210.

[0034] Among them, the barrel 210 is connected to the screw hole 120 through the screw rod 220. After the connection, the outer wall of the barrel 210 is embedded between the support ribs 130. The support ribs 130 are used to support the barrel 210 to prevent the screw rod 220 from tilting and breaking, thereby improving the structural stability.

[0035] The adapter 300 is disposed in the cylinder 210 , and the adapter 300 is used to support the missile inside the missile cylinder 200 .

[0036] Since threaded connection is adopted, in order to prevent the connection from loosening due to rotation, a knob bolt 140 is provided on the support rib 130 , and the threaded end of the knob bolt 140 faces the cylinder 210 . After connection, the cylinder 210 is fixed by tightening the knob bolt 140 .

[0037] Since the adapter 300 is installed inside the cylinder 210, in order to prevent the adapter 300 from rotating inside the cylinder 210, a slide rail 230 is provided on the inner wall of the cylinder 210. The adapter 300 includes a support sleeve 310 and a slide groove 320. The support sleeve 310 is embedded inside the cylinder 210, and the outer wall of the support sleeve 310 is provided with a slide groove 320 connected to the slide rail 230.

[0038] During installation, the support sleeve 310 is placed from top to bottom. When placed, the slide groove 320 slides on the slide rail 230 to make the support sleeve 310 rise and fall stably and linearly, thereby preventing the support sleeve 310 from rotating in the cylinder 210.

[0039] Since the outer wall of the cylinder 210 is smooth, in order to improve the connection stability, a limiting groove 240 is provided on the outer wall of the cylinder 210. When the cylinder 210 is connected to the base 110, the limiting groove 240 corresponds to the threaded end of the knob bolt 140. The limiting groove 240 is an annular groove, and the inside of the limiting groove 240 is provided with uniformly distributed anti-slip convex patterns.

[0040] After the knob bolt 140 is tightened, the threaded end of the knob bolt 140 is embedded in the limiting groove 240 to prevent the cylinder 210 from rotating and loosening.

[0041] Since the missile is provided with wing panels, in order to accommodate the placement of the missile, evenly distributed wing slots 330 are provided on the support sleeve 310 , and the wing panels of the missile are placed in the wing slots 330 , providing storage space and a launch track.

[0042] The support sleeve 310 adopts a multi-layer structure and adopts an existing adapter structure, and adopts a rubber-plastic plate, a hard polyurethane foam layer, an antistatic cloth and a metal shell in sequence from the inside to the outside.

[0043] During specific use, the missile barrel 200 is connected to the screw hole 120 through the screw rod 220. After the connection, the outer wall of the barrel 210 is embedded between the support ribs 130, and the support ribs 130 are used to support the barrel 210. The barrel 210 is fixed by tightening the knob bolt 140 to prevent the screw rod 220 from tilting and breaking, thereby improving the structural stability. The support sleeve 310 is inserted from top to bottom. When inserted, the slide groove 320 slides on the slide rail 230 to make the support sleeve 310 rise and fall stably and linearly, thereby preventing the support sleeve 310 from rotating on the barrel 210. The wing plate of the missile is placed in the wing groove 330 to provide storage space and launch track, and the missile is placed in the support sleeve 310.

[0044] Although the present invention has been described above with reference to the embodiments, various modifications may be made thereto and parts thereof may be replaced with equivalents without departing from the scope of the present invention. In particular, as long as there is no structural conflict, the various features in the embodiments disclosed in the present invention may be used in combination with each other in any manner, and the fact that these combinations are not exhaustively described in this specification is only for the sake of omitting space and saving resources. Therefore, the present invention is not limited to the specific embodiments disclosed herein, but includes all technical solutions falling within the scope of the claims.

Claims

1. A missile adapter, characterized in that: include: A support base (100) comprises a base (110), a screw hole (120) and support ribs (130), wherein the screw hole (120) is arranged at the center of the top of the base (110), and the support ribs (130) are circumferentially distributed outside the screw hole (120); A missile barrel (200) is arranged on the base (110), the missile barrel (200) comprising a barrel body (210) and a screw rod (220), the outer wall of the barrel body (210) is embedded between the support ribs (130), and the bottom of the barrel body (210) is provided with a screw rod (220) connected to the screw hole (120); The adapter (300) is arranged in the cylinder (210).

2. A missile adapter according to claim 1, characterized in that: The support rib (130) is provided with a knob bolt (140), and the threaded end of the knob bolt (140) faces the cylinder (210).

3. A missile adapter according to claim 1, characterized in that: The inner wall of the cylinder (210) is provided with a slide rail (230), and the adapter (300) comprises a support sleeve (310) and a slide groove (320), wherein the support sleeve (310) is embedded in the cylinder (210), and the outer wall of the support sleeve (310) is provided with a slide groove (320) connected to the slide rail (230).

4. A missile adapter according to claim 2, characterized in that: The outer wall of the cylinder (210) is provided with a limiting groove (240); when the cylinder (210) is in a connected state with the base (110), the limiting groove (240) corresponds to the threaded end of the knob bolt (140).

5. A missile adapter according to claim 3, characterized in that: The support sleeve (310) is provided with evenly distributed wing grooves (330).

6. A missile adapter according to claim 4, characterized in that: The limiting groove (240) is an annular groove, and evenly distributed anti-slip convex patterns are arranged inside the limiting groove (240).

7. A missile adapter according to claim 3, characterized in that: The support sleeve (310) adopts a multi-layer structure.

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