Missile fuze transfer packaging device
Patent Information
- Application Number
- CN202522205068.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-10-17
- Publication Date
- 2026-09-04
- Estimated Expiration
- 2035-10-17
AI Technical Summary
[0005]本实用新型的目的在于提供一种导弹引信转运包装装置,以解决上述背景技术中提出“无法适应其他规格的导弹引信”的问题
[0013] The protective components of this invention feature a tapered guide plate that quickly guides the fuze into the placement cavity, improving loading efficiency. A helical spring, in conjunction with a limiting slider and positioning baffle, adaptively adjusts the clamping force according to the fuze size, ensuring stability during fuze transport and increasing applicability to fuzes of different specifications, thus effectively improving the device's practicality and convenience. A support pad provides cushioning protection to the bottom of the fuze, further reducing the impact of vibration and shock, and overall enhancing the device's protective performance against missile fuzes.
Smart Images

Figure CN224715483U_ABST
Abstract
Description
Technical Field
[0001] This utility model belongs to the field of ammunition packaging technology, specifically relating to a missile fuse transfer and packaging device. Background Technology
[0002] As a core and sensitive component responsible for the precise detonation of a missile warhead, the missile fuse not only integrates vulnerable structures such as microelectronic detection elements and precision mechanical triggering mechanisms, but also has potential safety risks due to the characteristics of its energetic components. Its condition during transportation directly determines the reliability of its subsequent combat use, so it must rely on a dedicated packaging device to achieve comprehensive protection.
[0003] Existing specialized packaging devices for missile fuse protection often use holes and slots to position the fuses. While this provides some degree of positioning and restraint, in practice, relying solely on simple holes and slots for fuse positioning often results in limited applicability to different fuse sizes. This necessitates increasing the number of devices required when dealing with fuses of varying sizes, thereby raising operating costs.
[0004] Therefore, this utility model provides a missile fuse transfer and packaging device. Utility Model Content
[0005] The purpose of this invention is to provide a missile fuze transfer and packaging device to solve the problem mentioned in the background art of "inability to adapt to other specifications of missile fuzes".
[0006] To achieve the above objectives, this utility model provides the following technical solution: a missile fuse transfer and packaging device, comprising a packaging box, a packaging box lid hinged to the top of the packaging box, a partition frame installed inside the packaging box, the partition frame dividing the interior of the packaging box into several storage cavities, a protective component provided inside each storage cavity, the protective component including a packaging block placed inside the storage cavity, the packaging block having a placement cavity inside, the inner wall of the placement cavity having symmetrically distributed limiting grooves, a linearly arrayed helical spring fixedly connected inside the limiting grooves, a limiting slider fixedly connected to the other end of the helical spring, and a positioning baffle fixedly connected to the side of the limiting slider.
[0007] In a preferred embodiment, a guide plate is fixedly connected to the top of the positioning baffle, a support pad is fixedly connected between the positioning baffles and at the bottom of the storage cavity, and the limiting slider is slidably connected inside the limiting groove.
[0008] In one preferred embodiment, the packaging box has a limiting slot inside, and the divider includes a support rod fixedly connected to the inside of the packaging box, with horizontal plates slidably engaged on the left and right sides of the support rod.
[0009] In a preferred embodiment, the support rod is slidably engaged with longitudinal plates on its front and rear sides, and the longitudinal plates and transverse plates are slidably connected to the limiting slots.
[0010] In a preferred embodiment, a sealing ring is fixedly connected to the top of the packaging box, and a sealing groove is provided at the bottom of the packaging box lid.
[0011] In a preferred embodiment, a connecting block is fixedly connected to the outside of the packaging box, and a handle is rotatably connected to the connecting block via a rotating shaft. A support leg is fixedly connected to the bottom of the second section of the packaging box, and a positioning hole is provided on the top of the packaging box lid.
[0012] Compared with the prior art, the beneficial effects of this utility model are:
[0013] The protective components of this invention feature a tapered guide plate that quickly guides the fuze into the placement cavity, improving loading efficiency. A helical spring, in conjunction with a limiting slider and positioning baffle, adaptively adjusts the clamping force according to the fuze size, ensuring stability during fuze transport and increasing applicability to fuzes of different specifications, thus effectively improving the device's practicality and convenience. A support pad provides cushioning protection to the bottom of the fuze, further reducing the impact of vibration and shock, and overall enhancing the device's protective performance against missile fuzes.
[0014] This utility model utilizes a sliding design of longitudinal and transverse plates along support rods and limiting slots, allowing for flexible adjustment of the size and number of storage cavities. This adapts to the storage needs of missile fuses of different specifications, eliminating the need for separate packaging devices for different fuses and reducing packaging costs. The positioning function of the limiting slots on the longitudinal and transverse plates ensures the stability of the partition structure after adjustment, preventing fuse collisions caused by partition displacement during transportation. Furthermore, it allows for the rational allocation of internal space within the packaging box according to actual storage requirements, improving space utilization. Attached Figure Description
[0015] Figure 1 This is a schematic diagram of the overall three-dimensional structure of this utility model;
[0016] Figure 2 This is a three-dimensional cross-sectional structural diagram of the packaging block component of this utility model;
[0017] Figure 3 This is a schematic diagram of the overall three-dimensional structure of this utility model;
[0018] Figure 4This is a three-dimensional structural diagram of the packaging box and divider components of this utility model.
[0019] In the diagram: 1. Packaging box body; 2. Packaging box lid; 3. Divider; 4. Storage cavity; 5. Limiting slot; 6. Sealing ring; 7. Sealing groove; 8. Connecting block; 9. Handle; 10. Support leg; 11. Positioning hole; 301. Support rod; 302. Vertical plate; 303. Horizontal plate; 401. Packaging block; 402. Placement cavity; 403. Support pad; 404. Limiting slide groove; 405. Helical spring; 406. Limiting slider; 407. Positioning baffle; 408. Guide plate. Detailed Implementation
[0020] The present invention will be further described below with reference to the embodiments.
[0021] The following embodiments are used to illustrate the present invention, but should not be used to limit the scope of protection of the present invention. The conditions in the embodiments can be further adjusted according to specific conditions, and simple improvements to the method of the present invention under the premise of the concept of the present invention are all within the scope of protection claimed by the present invention.
[0022] Please see Figure 1-4 This utility model provides a missile fuse transfer and packaging device, including a packaging box 1, a packaging box cover 2 hinged to the top of the packaging box 1, a partition frame 3 installed inside the packaging box 1, the partition frame 3 dividing the interior of the packaging box 1 into several storage cavities 4, a protective component provided inside the storage cavities 4, the protective component including a packaging block 401 placed inside the storage cavity 4, a placement cavity 402 opened inside the packaging block 401, and a symmetrically distributed limiting groove 404 opened on the inner wall of the placement cavity 402. A helical spring 405 arranged in a linear array is fixedly connected to the part. A limit slider 406 is fixedly connected to the other end of the helical spring 405. A positioning baffle 407 is fixedly connected to the side of the limit slider 406. The side of the positioning baffle 407 away from the limit slider 406 is arc-shaped. A guide plate 408 is fixedly connected to the top of the positioning baffle 407. The guide plate 408 is conical. A support pad 403 is fixedly connected between the positioning baffles 407 and at the bottom of the storage cavity 4. The limit slider 406 is slidably connected inside the limit groove 404.
[0023] When using this missile fuze transfer and packaging device, first open the packaging box cover 2, align the missile fuze with the storage cavity 4 separated by the internal partition 3 of the packaging box 1. The fuze will first contact the conical guide plate 408 on the top of the packaging block 401, and smoothly enter the placement cavity 402 inside the packaging block 401 under the guidance of the guide plate 408. When the fuze is placed downwards, it will press the positioning baffles 407 on both sides. The positioning baffles 407 drive the side limiting sliders 406 to slide outwards along the limiting grooves 404, while compressing the helical springs 405 inside the limiting grooves 404. The helical springs 405 generate a reverse elastic force due to elastic deformation, which is transmitted to the positioning baffles 407 through the limiting sliders 406, so that the positioning baffles 407 tightly fit against the outer wall of the fuze to achieve limiting; finally, the fuze... The fuse bottom rests on the support pad 403 located at the bottom of the placement cavity 402 and between the positioning baffles 407. The support pad 403 provides support for the bottom of the fuse, completing the storage and positioning of the fuse. The protective components of this utility model can quickly guide the fuse into the placement cavity 402 through the conical guide plate 408, improving loading efficiency. The helical spring 405, together with the limiting slider 406 and the positioning baffles 407, can adaptively adjust the clamping force according to the fuse size, ensuring the stability of the fuse during transportation and increasing the applicability to fuses of different specifications, thereby effectively improving the practicality and convenience of the device. The support pad 403 can provide buffer protection for the bottom of the fuse, further reducing the impact of vibration and impact on the fuse, and improving the overall protective performance of the device for missile fuses.
[0024] Specifically, such as Figure 1 and Figure 4 As shown, a limiting slot 5 is provided inside the packaging box 1. The divider 3 includes a support rod 301 fixedly connected inside the packaging box 1. A horizontal plate 303 is slidably engaged on the left and right sides of the support rod 301. A vertical plate 302 is slidably engaged on the front and rear sides of the support rod 301. The vertical plate 302, the horizontal plate 303 and the limiting slot 5 are slidably connected.
[0025] When the number or size of the storage cavities 4 needs to be adjusted according to the size of the missile fuze, the number or size of the storage cavities 4 can be adjusted by taking out and placing the longitudinal plates 302 and 303 in the partition frame 3. This utility model, through the sliding design of the longitudinal plates 302 and 303 along the support rod 301 and the limiting slot 5, allows the number and size of the storage cavities 4 to be flexibly adjusted, which can adapt to the storage needs of missile fuzes of different specifications. There is no need to design special packaging devices for different fuzes, thus reducing packaging costs. The positioning function of the limiting slot 5 on the longitudinal plates 302 and 303 can ensure the stability of the partition frame 3 structure after adjustment and avoid fuze collisions caused by the displacement of the partition frame 3 during transportation. At the same time, it can reasonably allocate the internal space of the packaging box 1 according to the actual storage needs, thereby improving space utilization.
[0026] Specifically, such as Figure 1 and Figure 4 As shown, a sealing ring 6 is fixedly connected to the top of the packaging box 1, and a sealing groove 7 is opened at the bottom of the packaging box cover 2. The cooperation structure of the sealing ring 6 and the sealing groove 7 can effectively prevent external dust and moisture from entering the interior of the packaging box 1, protect the missile fuse from environmental factors, and ensure the stability of the fuse performance. A connecting block 8 is fixedly connected to the outside of the packaging box 1, and a handle 9 is rotatably connected to the connecting block 8 through a rotating shaft. The combination design of the connecting block 8 and the handle 9 provides a convenient force application point for the device handling, reduces the difficulty of handling, and the rotatable characteristic of the handle 9 improves the flexibility of use. A support leg 10 is fixedly connected to the bottom of the second section of the packaging box 1, and a positioning hole 11 is opened at the top of the packaging box cover 2. The support leg 10 can reduce the wear of the bottom of the packaging box 1 and extend the service life of the device. The positioning hole 11 can ensure the accurate position when multiple devices are stacked, avoid the device tipping over during the stacking process, save storage space, and improve storage safety.
[0027] Working principle and usage process of this utility model:
[0028] When using the missile fuse transfer and packaging device, the staff first open the packaging box cover 2 hinged at the top of the packaging box 1. If it is necessary to adapt to different specifications of missile fuses, the staff can push the longitudinal plates 302 on the front and rear sides and the transverse plates 303 on the left and right sides of the support rod 301 fixed inside the packaging box 1 in the partition frame 3, so that the longitudinal plates 302 and transverse plates 303 slide along the limiting slots 5 to adjust the number and size of the storage chambers 4.
[0029] The missile fuse is then aligned with the packaging block 401 inside the storage cavity 4. The fuse is guided into the placement cavity 402 by the conical guide plate 408. During the process, the fuse presses against the positioning baffle 407, which drives the limiting slider 406 to slide along the limiting groove 404 and compress the helical spring 405. The elastic force of the helical spring 405 causes the positioning baffle 407 to fit against the outer wall of the fuse and limit its position. The bottom of the fuse finally falls on the support pad 403.
[0030] Next, close the packaging box lid 2, so that the sealing ring 6 on the top of the packaging box 1 is embedded in the sealing groove 7 to achieve a seal; during subsequent handling, you can hold the handle 9 on the connecting block 8 to apply force, and when stacking in storage, place the upper device in the corresponding positioning hole 11 on the top of the lower packaging box lid 2, and the support legs 10 at the bottom of the packaging box 1 at the same time prevent the bottom of the box from being directly worn.
[0031] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.
Claims
1. A missile fuse transfer and packaging device, comprising a packaging box (1), characterized in that: The top of the packaging box (1) is hinged with a packaging box cover (2). A partition frame (3) is installed inside the packaging box (1). The partition frame (3) divides the interior of the packaging box (1) into several storage cavities (4). A protective component is provided inside the storage cavity (4). The protective component includes a packaging block (401) placed inside the storage cavity (4). A placement cavity (402) is opened inside the packaging block (401). A symmetrically distributed limiting groove (404) is opened on the inner wall of the placement cavity (402). A linearly arrayed helical spring (405) is fixedly connected inside the limiting groove (404). A limiting slider (406) is fixedly connected to the other end of the helical spring (405). A positioning baffle (407) is fixedly connected to the side of the limiting slider (406).
2. The missile fuse transfer and packaging device according to claim 1, characterized in that: A guide plate (408) is fixedly connected to the top of the positioning baffle (407), a support pad (403) is fixedly connected between the positioning baffles (407) and at the bottom of the storage cavity (4), and the limiting slider (406) is slidably connected inside the limiting groove (404).
3. The missile fuse transfer and packaging device according to claim 1, characterized in that: The packaging box (1) has a limiting slot (5) inside. The divider (3) includes a support rod (301) fixedly connected inside the packaging box (1). The support rod (301) has a horizontal plate (303) slidably engaged on the left and right sides.
4. A missile fuse transfer and packaging device according to claim 3, characterized in that: The support rod (301) is slidably engaged with the longitudinal plate (302) on both the front and rear sides, and the longitudinal plate (302), the transverse plate (303) and the limiting groove (5) are slidably connected.
5. A missile fuse transfer and packaging device according to claim 1, characterized in that: A sealing ring (6) is fixedly connected to the top of the packaging box (1), and a sealing groove (7) is opened at the bottom of the packaging box cover (2).
6. A missile fuse transfer and packaging device according to claim 5, characterized in that: A connecting block (8) is fixedly connected to the outside of the packaging box (1), and a handle (9) is rotatably connected to the connecting block (8) via a rotating shaft. A support leg (10) is fixedly connected to the bottom of the second section of the packaging box (1), and a positioning hole (11) is opened on the top of the packaging box cover (2).