Rocket projectile body boxing auxiliary guiding device

By using guide plates, buffer pads, and pneumatic springs in the guiding device, the problem of shaking during rocket loading was solved, enabling the rocket to be loaded smoothly and accurately into the container, reducing the risk of collision and damage.

CN223891647UActive Publication Date: 2026-02-10WUHAN LONGZHIYU DESIGN RES CO LTD
View PDF 0 Cites 0 Cited by

Patent Information

Application Number
CN202520612781.3
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-04-02
Publication Date
2026-02-10
Estimated Expiration
2035-04-02

AI Technical Summary

Technical Problem

In the current rocket packing process, the rocket is prone to shaking and not being able to align with the bottom of the packaging box, which can lead to collisions, affecting packing accuracy and rocket performance.

Method used

The system employs a guiding device, including a guide plate, a buffer pad, and a pneumatic spring. Through the guide groove and the lifting point adapter bracket, the rocket achieves a smooth descent and accurate positioning. The buffer pad reduces collisions, and the pneumatic spring mitigates impact forces.

Benefits of technology

This improved the accuracy and safety of rocket loading, reduced the risk of rocket damage, and ensured the rocket was loaded smoothly into the container.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN223891647U_ABST
    Figure CN223891647U_ABST
Patent Text Reader

Abstract

The utility model relates to the technical field of spaceflight rockets, and discloses a rocket projectile body encasement auxiliary guiding device which comprises a packaging box, a plurality of guiding mechanisms are arranged in the packaging box, the guiding mechanisms comprise a plurality of installation bases, and guiding supports are arranged in the installation bases in a sliding mode. Guide plates are fixedly arranged on the two opposite sides of the multiple guide supports correspondingly, guide grooves are formed in the two opposite sides of the multiple guide plates correspondingly, a rocket product is arranged in the packaging box, and a plurality of lifting installation connectors are fixedly arranged on the two sides of the rocket product correspondingly. And the opposite sides of every two hoisting mounting interfaces are in threaded connection with hoisting point adapter brackets. According to the utility model, the crash pad can reduce the collision between the rocket product and the guide plate, so that the damage to the surface of the rocket product is reduced, the descending of the guide plate and the guide bracket can guide the rocket product to fall into a preset position in a packaging box, and the boxing accuracy is improved.
Need to check novelty before this filing date? Find Prior Art

Description

Technical Field

[0001] This utility model relates to the field of aerospace rocket technology, and in particular to a rocket body packing auxiliary guidance device. Background Technology

[0002] Existing rockets or other aircraft have large diameters, long lengths, and weigh between 20 and 100 tons. Therefore, in order to consider transportation or transshipment, special packaging boxes for rockets need to be designed. Currently, most rocket packaging boxes on the market have an open top design, which means that when the rocket is packed, the rocket body needs to be lifted to the top of the packaging box using a special lifting device, and then slowly lowered into the box.

[0003] Currently, during the rocket body packing process, after the rocket is hoisted, it is easily affected by environmental or human factors, causing the rocket to sway in mid-air. When the rocket is falling, due to the swaying, it will be difficult for the rocket to align with the mounting position at the bottom of the packaging box, which may lead to an accidental collision between the rocket and the inner wall of the packaging box during the descent, potentially affecting the overall performance of the rocket.

[0004] Therefore, those skilled in the art have provided a rocket body packing auxiliary guidance device to solve the problems mentioned in the background art. Utility Model Content

[0005] The purpose of this utility model is to address the shortcomings of existing technologies by proposing a rocket body packing auxiliary guiding device. Through the guiding device, the rocket product is slowly lowered into the packaging box, improving the accuracy and efficiency of packing and reducing the risk of rocket product damage due to positioning deviation.

[0006] To achieve the above objectives, the present invention provides the following technical solution:

[0007] A rocket body packing auxiliary guiding device includes a packaging box, the packaging box is provided with multiple guiding mechanisms, the multiple guiding mechanisms include multiple mounting bases, each of the multiple mounting bases is slidably provided with a guide bracket, each of the multiple guide brackets is fixedly provided with a guide plate on each opposite side, and each of the multiple guide plates is provided with a guide groove on each opposite side.

[0008] The packaging box contains rocket products. Multiple hoisting and installation interfaces are fixedly installed on both sides of the rocket products. Each pair of opposite sides of the multiple hoisting and installation interfaces is threadedly connected to a hoisting point adapter bracket.

[0009] Furthermore, the multiple lifting point adapter brackets are externally slidably disposed inside the multiple guide grooves, and the multiple lifting point adapter brackets are respectively disposed on opposite sides of the multiple guide plates.

[0010] Furthermore, each of the multiple guide plates is fixedly provided with a buffer pad on one of its opposite sides, and the multiple buffer pads are all made of aerogel material.

[0011] Furthermore, each of the multiple mounting bases is fixedly provided with a box wall mounting bracket on opposite sides, and each of the multiple box wall mounting brackets is fixedly provided on opposite sides inside the packaging box.

[0012] Furthermore, pneumatic springs are fixedly installed on opposite sides of each of the multiple mounting bases, and the output ends of the multiple pneumatic springs are respectively fixedly installed on opposite sides of each of the multiple guide brackets.

[0013] Furthermore, the lower ends of the plurality of mounting bases are fixedly disposed inside the lower end of the packaging box, and the plurality of guide plates are slidably disposed on opposite sides of the plurality of mounting bases.

[0014] Furthermore, the multiple guide plates are respectively arranged on opposite sides of the rocket product, and the multiple guide plates are respectively arranged on opposite sides of the multiple guide supports.

[0015] This utility model has the following beneficial effects:

[0016] This utility model proposes a rocket body packing auxiliary guiding device. When loading the rocket product into the packaging box, it is aligned with the top of the packaging box and lowered. The buffer pad reduces the collision between the rocket product and the guide plate, thereby reducing damage to the surface of the rocket product. When the lifting point adapter bracket slides into the guide groove, the rocket product continues to descend, causing the guide bracket to move downward inside the mounting base. The guide plate slides in the mounting base, thereby guiding the rocket product to fall into the predetermined position inside the packaging box, improving the accuracy of packing. Furthermore, during the descent of the guide bracket, the output end of the pneumatic spring will contract, thereby reducing the impact force during descent, ensuring that the rocket product can safely and accurately fall into the predetermined position inside the packaging box. Attached Figure Description

[0017] Figure 1 This is an exploded isometric view of the guide mechanism of this utility model;

[0018] Figure 2 This utility model Figure 1 Enlarged diagram of point A in the diagram;

[0019] Figure 3 This is a cross-sectional isometric view of the present invention in its lifting state;

[0020] Figure 4 This utility model Figure 3 Enlarged diagram of point B in the diagram;

[0021] Figure 5 This is a cross-sectional isometric view of the present invention in its landing state.

[0022] Legend:

[0023] 1. Packaging box; 2. Lifting and installation interface; 3. Rocket product; 4. Guiding mechanism; 401. Guide bracket; 402. Box wall mounting bracket; 403. Mounting base; 404. Pneumatic spring; 405. Buffer pad; 406. Guide plate; 407. Lifting point adapter bracket; 408. Guide groove. Detailed Implementation

[0024] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0025] Reference Figures 1-5 One embodiment provided by this utility model:

[0026] A rocket body packing auxiliary guiding device includes a packaging box 1. The packaging box 1 is provided with multiple guiding mechanisms 4. The multiple guiding mechanisms 4 include multiple mounting bases 403. Each of the multiple mounting bases 403 has a guide bracket 401 slidably arranged inside. Each of the multiple guide brackets 401 has a guide plate 406 fixedly arranged on each pair of opposite sides. Each of the multiple guide plates 406 has a guide groove 408 opened on each pair of opposite sides.

[0027] The packaging box 1 contains rocket product 3. Multiple hoisting and installation interfaces 2 are fixedly installed on both sides of rocket product 3. Each pair of opposite sides of the multiple hoisting and installation interfaces 2 is threadedly connected to a hoisting point adapter bracket 407.

[0028] Multiple lifting point adapter brackets 407 are externally slidably disposed inside multiple guide grooves 408. The multiple lifting point adapter brackets 407 are respectively disposed on opposite sides of multiple guide plates 406. Each opposite side of multiple guide plates 406 is fixedly provided with a buffer pad 405, all made of aerogel. Each opposite side of multiple mounting bases 403 is fixedly provided with a box wall mounting bracket 402. The opposite sides of multiple box wall mounting brackets 402 are respectively fixedly disposed on both sides inside the packaging box 1. Multiple mounting bases 403... 03 Pneumatic springs 404 are fixedly installed on opposite sides of each pair of 03. The output ends of multiple pneumatic springs 404 are fixedly installed on opposite sides of multiple guide brackets 401. The lower ends of multiple mounting bases 403 are fixedly installed inside the lower end of the packaging box 1. Multiple guide plates 406 are slidably installed on opposite sides of multiple mounting bases 403. The opposite sides of multiple guide plates 406 are respectively installed on both sides of rocket product 3. The opposite sides of multiple guide plates 406 are respectively installed on opposite sides of multiple guide brackets 401.

[0029] Specifically, when loading rocket product 3 into packaging box 1, the lifting installation interface 2 is fixed to both sides of rocket product 3. Then, the lifting point adapter bracket 407 is connected to the lifting installation interface 2. After completing the above operations, the lifting equipment is started, the rocket product 3 is lifted smoothly and moved to the top of packaging box 1.

[0030] As the rocket product 3 descends, the lifting point adapter bracket 407 will slowly slide into the opposite side of the guide plate 406, and then slide into the guide groove 408. The guide groove 408 can adaptively correct itself to ensure accurate packing position. As the rocket product 3 continues to descend, the guide plate 406 will be affected by gravity, which will drive the guide bracket 401 to move downward inside the mounting base 403. The downward movement of the guide bracket 401 in the mounting base 403 can play a preliminary guiding role for the rocket product 3. At the same time, the guide plate 406 slides synchronously in the mounting base 403 to further enhance the guiding effect. Moreover, the downward movement of the guide bracket 401 will cause the output end of the pneumatic spring 404 to contract, thereby reducing the impact force generated when the rocket product 3 descends, allowing the guiding device to smoothly follow the descent of the rocket product 3, thereby ensuring that the rocket product 3 falls into the predetermined position inside the packaging box 1.

[0031] When rocket product 3 comes into contact with guide plate 406, the buffer pad 405 made of aerogel material fully exerts its buffering effect, effectively reducing the collision force between rocket product 3 and guide plate 406. At the same time, it can effectively reduce damage to the surface of rocket product 3, effectively protect the integrity of rocket product 3, and achieve comprehensive protection of the stability and accuracy of the packing process. The whole process is simple and convenient to operate. Moreover, each component adopts a modular design, which is easy to install and disassemble, providing convenience for later maintenance and replacement. The box wall mounting bracket 402 fixes the mounting base 403 to both sides inside the packaging box 1, and the lower end of the mounting base 403 is fixedly connected to the lower end inside the packaging box 1, thereby ensuring the stability of the entire guiding mechanism 4 inside the packaging box 1. It can withstand various forces during the packing process of rocket product 3 and ensure the normal operation of the device.

[0032] Working principle: When the rocket product 3 needs to be loaded into the packaging box 1, first fix the lifting installation interface 2 to both sides of the rocket product 3. Then, connect the lifting installation interface 2 to the lifting point adapter bracket 407. Subsequently, connect the lifting equipment to the lifting point adapter bracket 407. Next, lift the rocket product 3 and move it directly above the packaging box 1. During the descent, the lifting point adapter bracket 407 slides into the guide groove 408 on the guide plate 406. As the rocket product 3 continues to descend, the guide plate 406 will descend synchronously under the action of gravity, driving the guide bracket 401 to move downward inside the mounting base 403. The guide bracket 401 is installed... When the base 403 moves downward, it guides the rocket product 3. At the same time, the guide plate 406 slides in the mounting base 403, further guiding the rocket. The downward movement of the guide bracket 401 causes the output end of the pneumatic spring 404 to contract, reducing the impact of the descent. This allows the guiding device to gradually follow the rocket product 3 downward, ensuring that the rocket product 3 can accurately fall into the predetermined position inside the packaging box 1. When the rocket product 3 contacts the guide plate 406, the buffer pad 405 acts as a buffer, reducing the collision force between the rocket product 3 and the guide plate 406, further ensuring the smoothness and accuracy of the packing process.

[0033] Finally, it should be noted that the above description is only a preferred embodiment of the present utility model and is not intended to limit the present utility model. Although the present utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present utility model should be included within the protection scope of the present utility model.

Claims

1. A rocket body packing auxiliary guiding device, comprising a packaging box (1), characterized in that: The packaging box (1) is provided with multiple guiding mechanisms (4) inside. The multiple guiding mechanisms (4) include multiple mounting bases (403). Each of the multiple mounting bases (403) is slidably provided with a guide bracket (401). Each of the multiple guide brackets (401) is fixedly provided with a guide plate (406) on each opposite side. Each of the multiple guide plates (406) is provided with a guide groove (408) on each opposite side. The packaging box (1) contains a rocket product (3). Multiple hoisting and installation interfaces (2) are fixedly installed on both sides of the rocket product (3). Each pair of hoisting and installation interfaces (2) is threaded with a hoisting point adapter bracket (407) on opposite sides.

2. The rocket body packing auxiliary guidance device according to claim 1, characterized in that: Multiple lifting point adapter brackets (407) are externally slidably disposed inside multiple guide grooves (408), and the multiple lifting point adapter brackets (407) are respectively disposed on opposite sides of multiple guide plates (406).

3. The rocket body packing auxiliary guidance device according to claim 1, characterized in that: Each of the multiple guide plates (406) has a buffer pad (405) fixedly installed on one side of each pair of opposite sides, and the multiple buffer pads (405) are all made of aerogel material.

4. The rocket body packing auxiliary guidance device according to claim 1, characterized in that: Each of the multiple mounting bases (403) is fixedly provided with a box wall mounting bracket (402) on opposite sides, and the multiple box wall mounting brackets (402) are fixedly provided on opposite sides inside the packaging box (1) on both sides.

5. The rocket body packing auxiliary guidance device according to claim 1, characterized in that: Each of the mounting bases (403) is fixedly provided with a pneumatic spring (404) on opposite sides of each pair, and the output ends of the pneumatic springs (404) are respectively fixedly provided on opposite sides of each pair of guide brackets (401).

6. The rocket body packing auxiliary guidance device according to claim 1, characterized in that: The lower ends of the multiple mounting bases (403) are fixedly installed inside the lower end of the packaging box (1), and the multiple guide plates (406) are slidably installed on opposite sides of the multiple mounting bases (403).

7. The rocket body packing auxiliary guidance device according to claim 1, characterized in that: Multiple guide plates (406) are respectively arranged on opposite sides of the rocket product (3), and multiple guide plates (406) are respectively arranged on opposite sides of multiple guide brackets (401).