Universal missile carrier structure

Abstract

This utility model discloses a universal missile bracket structure, including a movable tray and multiple sets of transverse sliding seats that are slidably sleeved with the movable tray. An arc-shaped bracket is also engaged at the top of each transverse sliding seat, and a strap is provided between the two ends of the arc-shaped bracket. A stop component for controlling the movement state of the transverse sliding seat is also connected to the movable tray on the transverse sliding seat. The advantages of this utility model compared to the prior art are: it provides a universal missile bracket structure that is easy to operate and use, allows for modular installation, and is easy to install, remove, and adjust.

Description

Technical Field

[0001] This utility model relates to the field of mechanical engineering technology, specifically to a general missile bracket structure. Background Technology

[0002] When transferring and using missiles, missile carriers are generally required. Currently, there are fixed missile carriers, but they have poor adaptability in practical applications. The number of carriers is difficult to control and adjust, and modular installation cannot be achieved. At the same time, it is not easy to lock and use them for missiles of different diameters. As for the carrier body, special vehicles are generally required for transportation. However, when the carrier body is transported by vehicle, the fixing effect of the carrier body is poor, making it difficult to use. Utility Model Content

[0003] (I) Problems to be solved

[0004] The technical problem to be solved by this utility model is to overcome the above-mentioned technical defects and provide a universal missile bracket structure that is easy to operate and use, can be modularly installed, and is easy to install, remove, and adjust.

[0005] (II) Technical Solution

[0006] To solve the above-mentioned technical problems, the technical solution provided by this utility model is as follows: a universal missile bracket structure, including a movable tray and multiple sets of transverse sliding seats that are slidably connected to the movable tray, wherein an arc-shaped bracket is also engaged at the top of the transverse sliding seat, and a strap is provided between the two ends of the arc-shaped bracket;

[0007] The transverse sliding seat is also equipped with a stop component connected to the movable tray for controlling the movement state of the transverse sliding seat.

[0008] As an improvement, the top of the movable tray is connected to a T-shaped crossbeam, and the lower end of the transverse sliding seat is recessed along its length to provide a T-shaped groove that matches the T-shaped crossbeam.

[0009] The stop assembly includes a pin groove through a T-shaped slide on the transverse sliding seat, a shaft hole on the T-shaped crossbeam that matches the pin groove, and a pin is fitted inside the pin groove.

[0010] As an improvement, a positioning bolt is also connected to one end of the mobile tray.

[0011] As an improvement, the inner side walls of the T-shaped groove are also recessed with rotating shaft grooves, and rollers are rotatably connected in the rotating shaft grooves, with the rollers abutting against the T-shaped crossbeam.

[0012] As an improvement, the top of the transverse sliding seat is recessed and has a groove that matches the bottom of the arc-shaped bracket. A second pin is also provided between the arc-shaped bracket and the transverse sliding seat.

[0013] (III) Beneficial Effects

[0014] The advantages of this utility model compared with the prior art are as follows: In this application, the modular assembly of the movable tray, the transverse sliding seat and the arc-shaped bracket can be combined according to different transportation and usage needs to meet different requirements. The additional stop components, positioning bolts and other structures added in this application can easily realize the installation and fixation of each component. In specific applications, the missile body is locked by using straps in conjunction with the arc-shaped bracket. Attached Figure Description

[0015] Figure 1 This is a schematic diagram of a general-purpose missile bracket structure.

[0016] Figure 2 This is a second-view structural diagram of a general-purpose missile bracket structure.

[0017] As shown in the figure: 1. Moving pallet; 2. Horizontal sliding seat; 3. Arc-shaped bracket; 4. Strap; 5. T-shaped crossbeam; 6. T-shaped slide; 7. Pin groove one; 8. Shaft hole; 9. Pin one; 10. Positioning bolt; 11. Rotary shaft groove; 12. Roller; 13. Slot; 14. Pin two. Detailed Implementation

[0018] The specific embodiments of this utility model will be further described below with reference to the accompanying drawings. Identical components are indicated by the same reference numerals.

[0019] It should be noted that the terms “front,” “back,” “left,” “right,” “up,” and “down” used in the following description refer to the directions shown in the attached diagram, while the terms “inside” and “outside” refer to the directions toward or away from the geometric center of a specific component, respectively.

[0020] It should be noted that when an element is referred to as being "fixed to" another element, it can be directly on the other element or there may be an intervening element. When an element is referred to as being "connected to" another element, it can be directly connected to the other element or there may be an intervening element. The terms "vertical," "horizontal," "left," "right," and similar expressions used in this document are for illustrative purposes only.

[0021] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly associated with those skilled in the art to which this invention pertains. The terminology used herein is for the purpose of describing particular embodiments and is not intended to limit the invention. The term "and / or" as used herein includes any and all combinations of one or more of the associated listed items.

[0022] To make the content of this utility model easier to understand, the technical solutions in the embodiments of this utility model will be clearly and completely described below with reference to the accompanying drawings.

[0023] Please refer to the appendix carefully. Figure 1-2 A general missile bracket structure includes a movable tray 1 and multiple sets of transverse sliding seats 2 that are slidably connected to the movable tray 1. The top of the transverse sliding seat 2 is also engaged with an arc-shaped bracket 3. One end of the movable tray 1 is also connected with a positioning bolt 10, which can be used to install the movable tray 1 to the carriage.

[0024] In use, a strap 4 is provided between the two ends of the arc-shaped bracket 3. The strap can be used in a conventional binding method, such as an adjustable strap, fixing one end to the other end and wrapping it around one end of the arc-shaped bracket 3, or locking it with a ratchet.

[0025] During installation, to ensure stability, the transverse sliding seat 2 is also equipped with a stop component connected to the moving tray 1 to control the movement state of the transverse sliding seat 2.

[0026] In one embodiment:

[0027] The top of the movable tray 1 is connected to a T-shaped crossbeam 5. The lower end of the transverse sliding seat 2 is recessed along its length and has a T-shaped groove 6 that matches the T-shaped crossbeam 5. At the same time, the stop assembly includes a pin groove 7 that passes through the T-shaped groove 6 on the transverse sliding seat 2. The T-shaped crossbeam 5 has a shaft hole 8 that matches the pin groove 7. A pin 9 is fitted inside the pin groove 7. The setting of the pin groove 7 and the shaft hole 8 completes the locking of multiple sets of transverse sliding seats 2 after sliding installation.

[0028] When using swipe:

[0029] The inner side walls of the T-shaped slide 6 are also recessed with rotating shaft grooves 11. Rollers 12 are rotatably connected in the rotating shaft grooves 11. The rollers 12 abut against the T-shaped crossbeam 5. The rollers 12 increase the sliding stability and ease of use.

[0030] The top of the transverse sliding seat 2 is recessed and has a groove 13 that matches the bottom of the arc-shaped bracket 3. A second pin 14 is also connected between the arc-shaped bracket 3 and the transverse sliding seat 2. The installation and use of the arc-shaped bracket 3 and the transverse sliding seat 2 can be completed through the cooperation of the groove 13 and the second pin 14.

[0031] Used for mounting, dismounting, and transporting different types of missiles, it is compatible with the corresponding missile models and can be replaced with the corresponding missile brackets to achieve universality. The mobile pallet can be installed on the corresponding vehicle body. The crossbeam sliding assembly is designed with rollers to move and disassemble on the mobile pallet. The straps are used to fix the missile.

[0032] The contents not described in detail in this specification are existing technologies known to those skilled in the art.

[0033] All standard parts used in this utility model can be purchased from the market, and irregular parts can be customized according to the description and drawings. The specific connection methods of each part adopt conventional methods such as bolts, rivets, and welding that are mature in the prior art. The machinery, parts and equipment adopt conventional models in the prior art. In addition, the circuit connection adopts conventional connection methods in the prior art, which will not be described in detail here. The contents not described in detail in this specification belong to the prior art known to those skilled in the art.

[0034] The present invention and its embodiments have been described above. This description is not restrictive, and the accompanying drawings are only one embodiment of the present invention; the actual structure is not limited thereto. In conclusion, if those skilled in the art are inspired by this description and design similar structures and embodiments without departing from the inventive spirit of the present invention, such designs should fall within the protection scope of the present invention.

Claims

1. A universal missile cradle structure, characterized by: It includes a movable tray (1) and multiple sets of transverse sliding seats (2) that are slidably connected to the movable tray (1). The top of the transverse sliding seat (2) is also connected to an arc-shaped bracket (3), and a strap (4) is provided between the two ends of the arc-shaped bracket (3). The transverse sliding seat (2) is also connected to the movable tray (1) and is equipped with a stop component for controlling the movement state of the transverse sliding seat (2).

2. A universal missile cradle structure according to claim 1, characterized in that: The top of the movable tray (1) is connected to a T-shaped crossbeam (5), and the lower end of the transverse sliding seat (2) is recessed along its length direction to provide a T-shaped groove (6) that matches the T-shaped crossbeam (5). The stop assembly includes a pin groove (7) through the T-shaped groove (6) on the transverse sliding seat (2), a shaft hole (8) is provided on the T-shaped crossbeam (5) to match the pin groove (7), and a pin (9) is fitted inside the pin groove (7).

3. A universal missile carrier structure according to claim 1 or 2, characterised in that: One end of the movable tray (1) is also connected to a positioning bolt (10).

4. A universal missile carrier structure according to claim 2, characterized in that: The inner side walls of the T-shaped chute (6) are also recessed with a rotating shaft groove (11), and a roller (12) is rotatably connected in the rotating shaft groove (11), and the roller (12) abuts against the T-shaped crossbeam (5).

5. A universal missile carrier structure according to claim 1, characterized in that: The top of the transverse sliding seat (2) is recessed and has a slot (13) that matches the bottom of the arc-shaped bracket (3). A second pin (14) is also connected between the arc-shaped bracket (3) and the transverse sliding seat (2).

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