A box structure of a ground breakage and launch integrated device

Abstract

The utility model discloses a box body structure of ground barrier launching integrated device, including open and close's main box body, mounting seat, net format scale bar, pull and send fuze window and control system, open and close's main box body constitutes the main body structure of launching box, and mounting seat sets up in the main box body, is used for installing launching frame structure, and net format scale bar sets up in the inner wall of main box body, is used for indicating the zoning and filling layer position in main box body, and pull and send fuze window sets up in the lateral wall of main box body through sealing assembly, is used for filling fuze, and control system is integrated and installs in the main box body, and main box body is equipped with the interface for connecting external device and control system. Its structure is reliable, and the use performance is good, and the dynamic sealing of the box body and the box cover, when launching impact or transportation jolt, can effectively maintain the air tightness, improve the overall structural stability, can identify the filling layer height through the grid scale, so that the construction personnel need not rely on experience judgment, improve the convenience.

Description

Technical Field

[0001] This utility model relates to the field of launching device technology, specifically to a box structure for an integrated ground obstacle-clearing and launching device. Background Technology

[0002] Rocket launch systems have important applications in modern military and disaster prevention fields, and their core component, the launch container, must simultaneously fulfill the functions of ammunition storage, transportation, and launch. Traditional launch containers generally suffer from the following shortcomings:

[0003] Functional fragmentation: Storage boxes, transport racks and launch devices are mostly separate structures. Assembly in field environments is time-consuming and prone to misalignment, making it difficult to meet the requirements for rapid response.

[0004] Poor environmental adaptability: The box is not well sealed, especially in humid and dusty environments, which can easily cause the ammunition to get damp or the circuit to fail. Existing sealing structures (such as rubber gaskets) are prone to aging and cracking under extreme temperature differences.

[0005] Low operational efficiency: Projectile loading relies on manual experience for positioning and lacks standardized guidance markings, which can easily lead to loading errors; Fuze installation requires frequent opening and closing of the box cover, increasing the risk of exposure.

[0006] Poor expandability: The external mounting of equipment such as monitoring instruments and electrical control units not only reduces protection, but also makes exposed cables more susceptible to mechanical damage and electromagnetic interference.

[0007] To address the aforementioned issues, a few integrated solutions have attempted to integrate the transmission function into the enclosure, but these solutions generally suffer from structural redundancy and low performance. Utility Model Content

[0008] To solve the above-mentioned technical problems, this utility model provides a box structure for an integrated ground obstacle-clearing and launching device.

[0009] The technical solution of this utility model to solve the above-mentioned technical problems is as follows: A box structure for a ground obstacle-clearing and launching integrated device, comprising:

[0010] The main, closable housing constitutes the main structure of the launch box;

[0011] The mounting base, located inside the main housing, is used to mount the launcher structure;

[0012] A grid-like scale bar is installed on the inner wall of the main container to indicate the internal partitions and filling layers of the main container;

[0013] A pull-out fuse window, sealed by a component, is located on the side wall of the main housing and is used to load the fuse.

[0014] The control system is integrated into the main enclosure, which is equipped with interfaces for connecting external devices and the control system.

[0015] Furthermore, the main enclosure includes a main body and a cover disposed on the upper part of the main body, and the main body and the cover are sealed by a soft gel sealing layer.

[0016] Furthermore, the control system includes an electronic control unit and a power supply unit, which are detachably installed in preset positions within the main housing using quick-lock tool-free screws.

[0017] Furthermore, both the electronic control unit and the power supply unit have sealed housing structures and are equipped with status indicator lights.

[0018] Furthermore, a support is movably installed on the top side of the main body, and a meteorological and terrain detection instrument is installed on the support.

[0019] Furthermore, the top of the main body is equipped with lifting rings for hoisting, and the bottom of the main body is equipped with forks for forklift transport.

[0020] Furthermore, a tail control rope release device is integrated and installed on the side wall of the main body.

[0021] Furthermore, a cable reel is integrated and installed inside the main enclosure.

[0022] Furthermore, a positioning plate is provided at the bottom of the main body. The positioning plate can be folded along the main body, and anchoring nails can be detachably installed on the positioning plate.

[0023] The present invention has the following beneficial effects: The box structure of the ground obstacle breaching and launching integrated device provided by the present invention is reliable and has good performance. The dynamic sealing of the box and the box cover can effectively maintain airtightness during launch impact or transportation bumps, improve sealing performance, and improve overall structural stability. The grid-like scale can mark and divide the internal space of the box into several standardized areas, clearly indicating the filling layer height, so that construction personnel do not need to rely on experience to judge, but can directly and quickly complete the filling arrangement according to the scale indication, thus improving convenience. Attached Figure Description

[0024] Figure 1 This is a schematic diagram of the structure of this utility model;

[0025] Figure 2 This is a schematic diagram of the working structure of this utility model;

[0026] Figure 3 This is a schematic diagram of the grid-style scale bar arrangement structure of this utility model;

[0027] Figure 4 This is the main view of the present invention (positioning plate in open state);

[0028] Figures 1 to 4The reference numerals in the attached drawings are as follows: 1-Main housing, 2-Launching structure, 3-Grid scale bar, 4-Pull-launch fuse window, 5-Control system, 10-Housing body, 11-Cover, 50-Electrical control unit, 51-Power supply unit, 12-Support, 13-Weather and terrain detector, 14-Lifting ring, 15-Forklift, 16-Cable reel, 17-Positioning plate, 18-Anchor nail. Detailed Implementation

[0029] The principles and features of this utility model are described below with reference to the accompanying drawings. The examples given are only for explaining this utility model and are not intended to limit the scope of this utility model.

[0030] like Figures 1 to 3 As shown, a box structure of a ground obstacle breaching and launch integrated device includes an openable and closable main box 1, a mounting base, a grid-scale bar 3, a pull-out fuse window 4, and a control system 5. The mounting base is located inside the main box 1 and is used to install the launcher structure 2.

[0031] The main, closable housing 1 constitutes the main structure of the launch container. In this embodiment, the main housing 1 includes a housing body 10 and a cover 11 located on the upper part of the housing body 10. The housing body 10 and the cover 11 are sealed together by a soft gel sealing layer. The housing body 10 constitutes the main load-bearing structure of the launch container, providing a basic enclosed space for transportation and launch. High-strength materials such as integrally molded metal / composite materials ensure impact resistance and environmental protection. The cover 11 enables the opening and closing of the housing, ensuring ease of operation and environmental sealing. When closed, it forms a sealed space with the housing, blocking external erosion such as rainwater and dust. The soft gel sealing layer covers the joint surface between the housing body 10 and the cover 11, achieving dynamic sealing. During launch impacts or transportation bumps, the gel deforms and fills the micro-gaps in the joints, maintaining airtightness. The rigid structure of the main housing 1, the lockable cover 11, and the dynamic filling of the soft gel sealing layer constitute a three-level protection system, simultaneously solving the sealing failure and structural fragility problems of traditional solutions.

[0032] In this embodiment, a grid-like scale bar 3 is set on the inner wall of the main box 1 to mark the internal partitions and filling layers of the main box 1. By setting grid-like scale markings in the longitudinal height direction of the inner wall of the main box 1, the internal space is divided into several standardized areas such as left / right partitions and front / rear compartments, and the filling layer heights such as bottom, middle, and top layers and horizontal offsets are clearly defined. This allows construction personnel to quickly complete the filling arrangement directly according to the scale indications without relying on experience, while avoiding the risk of projectile collision or launcher interference caused by positioning deviation.

[0033] In this embodiment, the pull-to-fire fuze window 4 is installed on the side wall of the main housing 1 via a sealing assembly and is used for loading the fuze. Before launch, the housing cover does not need to be fully opened; the fuze can be installed or replaced simply through the side wall fuze window, significantly shortening the combat readiness response time. The sealing assembly uses a sealing strip and a non-removable elastic screw. The sealing strip is annularly embedded in the frame of the fuze window, achieving a static seal upon compression. A status indicator light is integrated on the outside of the pull-to-fire fuze window 4, and the fuze ignition signal is fed back through the electronic control system.

[0034] In this embodiment, the control system 5 is integrated into the main housing 1, and the main housing 1 is provided with an interface for connecting external devices and the control system 5. Specifically, the control system 5 includes an electronic control unit 50 and a power supply unit 51, which are detachably installed in preset positions within the main housing 1 using quick-lock tool-free screws. Both the electronic control unit 50 and the power supply unit 51 are sealed housing structures with status indicator lights. The electronic control unit 50 and the power supply unit 51 are highly integrated within the main housing 1, forming a modular and expandable intelligent control hub. The electronic control unit 50 performs rocket launch timing control, ignition, angle correction, and unhooking triggering, while the power supply unit 51 provides a 24V lithium-ion DC power supply.

[0035] A support 12 is movably mounted on the top side of the main housing 1, and a meteorological and terrain detector 13 is mounted on the support 12. The support 12 provides a platform for the detector and supports angle adjustment from 0° to 90° through a hinged design. In the non-use state, the support 12 is folded down and close to the housing; when in use, it quickly unfolds to the working angle. The meteorological and terrain detector 13 collects environmental data in real time and feeds it back to the electronic control unit 50 to assist in launch decisions.

[0036] Furthermore, for ease of transportation, this invention features a lifting ring 14 at the top of the main housing 1 and forks 15 at the bottom for forklift transport. The lifting ring 14 provides an overhead lifting interface, ensuring rapid deployment and transfer of the housing. The forks 15 are compatible with forklift fork insertion and handling, adapting to ground transportation without lifting equipment. The lifting ring 14 and forks 15 enable rapid switching between multiple movement modes.

[0037] The main housing 1 has an integrated tail control rope release device installed on its side wall, and a cable reel 16 is integrated inside the main housing 1. The tail control rope release device, as a mechanical release control, automatically releases the tail control rope after rocket launch via tension comparison, ensuring the missile's flight stability. The release device body is embedded in a pre-cast compartment in the side wall of the housing, reducing the risk of snagging on external protrusions. The cable reel 16 houses shielded twisted-pair optical cables, meeting wired emergency control requirements. Pulling the cable automatically releases it; during retrieval, a crank handle manually winds it back up. The cable reel 16 is fixed to the rear wall interlayer of the housing, without occupying ammunition storage space.

[0038] In addition, such as Figure 4As shown, a positioning plate 17 is provided at the bottom of the main housing 1. The positioning plate 17 can be folded along the main housing 1, and anchoring nails 18 are detachably installed on the positioning plate 17. The positioning plate 17 is hinged at the bottom of the main housing 1. When needed, the positioning plate 17 is opened, and the anchoring nails are passed through the anchoring holes on the positioning plate 17 and inserted into the ground to improve stability. When not in use, the positioning plate 17 can be folded and stored for convenience and speed.

[0039] The above are merely preferred embodiments of the present utility model and are not intended to limit the present utility model. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present utility model shall be included within the protection scope of the present utility model.

Claims

1. A housing structure for a ground-based obstacle-clearing and launching integrated device, characterized in that, include: The main box (1) that can be opened and closed constitutes the main structure of the launch box; Mounting base, located inside the main housing (1), is used to mount the launcher structure (2). A grid-type scale bar (3) is set on the inner wall of the main box (1) to mark the internal partitions and filling layers of the main box (1); A pull-out fuse window (4) is set on the side wall of the main housing (1) through a sealing assembly for filling the fuse; The control system (5) is integrated and installed in the main housing (1), and the main housing (1) is provided with an interface for connecting external devices and the control system (5).

2. The housing structure of the integrated ground obstacle breaching and launching device according to claim 1, characterized in that, The main box (1) includes a box body (10) and a cover (11) disposed on the upper end of the box body (10), and the box body (10) and the cover (11) are sealed by a soft gel sealing layer.

3. The housing structure of the integrated ground obstacle breaching and launching device according to claim 1, characterized in that, The control system (5) includes an electrical control unit (50) and a power supply unit (51), and the electrical control unit (50) and the power supply unit (51) are detachably installed in a preset position inside the main housing (1) by means of quick-lock tool-free screws.

4. The housing structure of the integrated ground obstacle breaching and launching device according to claim 3, characterized in that, Both the electronic control unit (50) and the power supply unit (51) are sealed housing structures and are equipped with status indicator lights.

5. The housing structure of the integrated ground obstacle breaching and launching device according to claim 1, characterized in that, A support (12) is movably installed on the top side of the main body (1), and a meteorological and topographic detector (13) is installed on the support (12).

6. The housing structure of the integrated ground obstacle breaching and launching device according to any one of claims 1 to 5, characterized in that, The top of the main box (1) is provided with a lifting ring (14) for hoisting, and the bottom of the main box (1) is provided with a forklift (15) for forklift transport.

7. The housing structure of the integrated ground obstacle breaching and launching device according to claim 6, characterized in that, The main body (1) has a tail control rope unhooking device integrated on its side wall.

8. The housing structure of the integrated ground obstacle breaching and launching device according to claim 6, characterized in that, The main housing (1) is equipped with a cable reel (16).

9. The housing structure of the integrated ground obstacle breaching and launching device according to claim 6, characterized in that, The bottom of the main box (1) is provided with a positioning plate (17), the positioning plate (17) can be folded along the main box (1), and the positioning plate (17) is detachably provided with anchor nails (18).

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