A special packaging box for aircraft parts

Abstract

This utility model provides a special packaging box for aircraft parts, belonging to the field of aircraft parts packaging. It includes a box body, a movable component at the bottom for easy movement, and a sealing component at the top to prevent external contaminants from entering the box. Through the movable component, in use, the user first pulls the lever out of the limiting groove in the base. After adjusting the lever, the user grasps it and applies pulling force. At this time, two sets of symmetrical pulleys bolted to one end of the base contact the ground. Under the action of pulling force, the pulleys roll along the ground. When not in use, the lever can be pushed back into the limiting groove, reducing the extension length of the lever and saving space.

Description

Technical Field

[0001] This utility model relates to the field of aircraft parts packaging, and more specifically, to a special packaging box for aircraft parts. Background Technology

[0002] Aircraft parts generally possess extremely high manufacturing precision and significant value, and their performance directly impacts flight safety. During transportation and storage, appropriate packaging can effectively protect against various potential damages such as collisions, compression, moisture, and dust, preventing damage to the parts and thus affecting their performance. Therefore, aircraft parts packaging boxes occupy a crucial position in the aviation manufacturing and maintenance field, and their design must meet multiple requirements, including high protection, mobility, and environmental adaptability.

[0003] The existing technology still has the following drawbacks:

[0004] (1) The packaging box has poor mobility. In the actual transportation and handling of aircraft parts, a lot of manpower is often required, and the operation process is also cumbersome and inconvenient.

[0005] (2) The sealing performance has not reached the ideal state, and there is still a risk that external pollutants will enter the interior of the box, thereby damaging the aircraft parts.

[0006] Therefore, we made improvements and proposed a special packaging box for aircraft parts. Utility Model Content

[0007] The purpose of this utility model is to address the problems of poor mobility and inadequate sealing of existing packaging boxes.

[0008] To achieve the above-mentioned objectives, this utility model provides the following technical solution:

[0009] Specialized packaging boxes for aircraft parts were developed to address the aforementioned issues.

[0010] The specific details of this utility model are as follows:

[0011] The package includes a box body, the bottom of which is provided with a movable component to facilitate moving the packaging box, and the top of which is provided with a sealing component to prevent external contaminants from entering the interior of the box body and to protect aircraft parts from damage. The interior of the box body is provided with a placement component for placing aircraft parts.

[0012] The movable component includes a base that is fixedly connected to the bottom of the housing by bolts. Two sets of pulleys are bolted to one end of the base, and the two sets of pulleys are symmetrically arranged. A limit groove is formed at the other end of the base, and a pull rod is slidably connected to the limit groove.

[0013] As a preferred technical solution of this utility model, the sealing assembly includes a cover plate hinged to the top of the box, and the outer wall of the cover plate is hinged with a latch, the number of latches being four sets, and a lock seat is bolted to the outer wall of the box at the position corresponding to the latch.

[0014] As a preferred embodiment of this utility model, the placement component includes a honeycomb aluminum plate fixedly connected to the inner wall of the box body. The honeycomb aluminum plate is disposed on the inner side wall and the inner bottom wall of the box body. Six sets of sliding strips are bolted to the inner side wall of the box body. The six sets of sliding strips are symmetrically arranged in pairs. A partition is slidably connected inside the sliding strip.

[0015] As a preferred technical solution of this utility model, an induction light strip is bolted to the inner wall of the cover plate, and the induction light strip is rectangular in shape.

[0016] As a preferred technical solution of this utility model, the bottom of the base is fixedly connected with two sets of anti-slip pads, and the two sets of anti-slip pads are arranged symmetrically.

[0017] As a preferred technical solution of this utility model, the side wall of the box is rotatably connected with a handle, and the number of handles is three sets, which are located at the bottom of the lock seat.

[0018] As a preferred technical solution of this utility model, the outer wall of the cover plate is fixedly provided with longitudinal reinforcing ribs, and the number of longitudinal reinforcing ribs is four sets.

[0019] Compared with the prior art, the beneficial effects of this utility model are as follows:

[0020] In the solution of this utility model:

[0021] 1. With the set movable component, when in use, the user first pulls the pull rod out of the limiting groove of the base. After adjusting the pull rod, the user holds the pull rod and applies pulling force. At this time, the two sets of symmetrical pulleys bolted to one end of the base contact the ground. Under the action of pulling force, the pulleys will roll along the ground. When the pull rod is not in use, the pull rod can be pushed back into the limiting groove to reduce the extension length of the pull rod and save space.

[0022] 2. With the sealing components in place, when in use, lift the latch and rotate to open the cover, where aircraft parts can be placed inside the case. After placement, the cover can be closed, and the latch and lock seat will engage to secure the cover tightly to the top of the case, achieving a seal and effectively preventing external dust, moisture, impurities, etc., from entering the case, thus providing excellent protection for the aircraft parts inside. Attached Figure Description

[0023] Figure 1 A schematic diagram of the structure of the special packaging box for aircraft parts provided by this utility model;

[0024] Figure 2 A schematic diagram of the bottom structure of the special packaging box for aircraft parts provided by this utility model;

[0025] Figure 3 A side view of the special packaging box for aircraft parts provided by this utility model;

[0026] Figure 4 A cross-sectional structural diagram of the special packaging box for aircraft parts provided by this utility model;

[0027] Figure 5 A cross-sectional structural diagram of the special packaging box for aircraft parts provided by this utility model.

[0028] The image shows:

[0029] 1. Cabinet; 2. Moving assembly; 201. Base; 202. Casters; 203. Pull rod; 3. Sealing assembly; 301. Cover plate; 302. Lock; 303. Lock seat; 4. Placement assembly; 401. Honeycomb aluminum plate; 402. Sliding strip; 403. Partition; 5. Sensor light strip; 6. Anti-slip mat; 7. Handle; 8. Reinforcing rib. Detailed Implementation

[0030] To make the objectives, technical solutions, and advantages of the embodiments of this utility model clearer, the technical solutions of the embodiments of this utility model will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some, not all, of the embodiments of this utility model.

[0031] Therefore, the following detailed description of the embodiments of this utility model is not intended to limit the scope of the claimed utility model, but merely to illustrate some embodiments of the utility model. All other embodiments obtained by those skilled in the art based on the embodiments of this utility model without inventive effort are within the scope of protection of this utility model.

[0032] It should be noted that, unless otherwise specified, the embodiments and features and technical solutions in the present invention can be combined with each other.

[0033] It should be noted that similar labels and letters in the following figures indicate similar items. Therefore, once an item is defined in one figure, it does not need to be further defined and explained in subsequent figures.

[0034] like Figure 1 and Figure 4As shown, this embodiment proposes a special packaging box for aircraft parts, including a box body 1. The bottom of the box body 1 is provided with a moving component 2 for easy movement of the packaging box, and the top of the box body 1 is provided with a sealing component 3. The sealing component 3 is used to prevent external contaminants from entering the interior of the box body 1 and to protect the aircraft parts from damage. The interior of the box body 1 is provided with a placement component 4 for placing the aircraft parts.

[0035] like Figure 2 As shown, the movable component 2 includes a base 201 that is bolted to the bottom of the housing 1. Two sets of pulleys 202 are bolted to one end of the base 201, and the two sets of pulleys 202 are symmetrically arranged. A limit groove is formed at the other end of the base 201, and a pull rod 203 is slidably connected to the limit groove. The user can flexibly adjust the length of the pull rod 203 as needed for easy use. In use, the user first pulls the pull rod 203 out of the limit groove of the base 201. After adjusting the pull rod 203, the user holds the pull rod 203 and applies a pulling force. At this time, the two sets of symmetrical pulleys 202 bolted to one end of the base 201 contact the ground. Under the action of the pulling force, the pulleys 202 will roll along the ground. When the pull rod 203 is not in use, it can be pushed back into the limit groove to reduce the extension length of the pull rod 203 and save space.

[0036] like Figure 2 As shown, the sealing assembly 3 includes a cover plate 301 hinged to the top of the housing 1. The outer wall of the cover plate 301 is hinged with four sets of latches 302. A locking seat 303 is bolted to the outer wall of the housing 1 at the position corresponding to the latches 302. In use, the latches 302 are lifted, and the cover plate 301 is rotated to open, allowing aircraft parts to be placed inside the housing 1. After placement, the cover plate 301 can be closed. The latches 302 and locking seats 303 will engage with each other, tightly fixing the cover plate 301 to the top of the housing 1, thus sealing the housing 1 and effectively preventing external dust, moisture, impurities, etc., from entering the housing 1, providing excellent protection for the aircraft parts inside.

[0037] like Figure 4 As shown, the placement component 4 includes a honeycomb aluminum plate 401 fixedly connected to the inner wall of the box 1. The honeycomb aluminum plate 401 is disposed on the inner side wall and the inner bottom wall of the box 1. Six sets of sliding strips 402 are bolted to the inner side wall of the box 1. The six sets of sliding strips 402 are arranged symmetrically in pairs. A partition 403 is slidably connected inside the sliding strips 402. The honeycomb structure of the honeycomb aluminum plate 401 gives it excellent cushioning performance, which can significantly reduce the impact and vibration of the items inside the box during transportation and handling, and reduce the risk of damage to the items. The setting of the sliding strips 402 and the partitions 403 allows the internal space of the box 1 to be flexibly divided according to actual needs. Users can personalize the layout according to the characteristics of different items, improve space utilization, and avoid items being squeezed and collided with each other inside the box.

[0038] like Figure 5 As shown, a sensor light strip 5 is bolted to the inner wall of the cover plate 301. The sensor light strip 5 is rectangular in shape. When the cover plate 301 is opened, the sensor light strip 5 will light up automatically, making it convenient for staff to place and take out aircraft parts without the need for manual operation of the switch, providing users with a more convenient user experience, especially in low-light environments.

[0039] like Figure 2 As shown, two sets of anti-slip pads 6 are fixedly connected to the bottom of the base 201. The two sets of anti-slip pads 6 are symmetrically arranged. When the packaging box is laid flat to place the aircraft parts, the two sets of anti-slip pads 6 will contact the ground, which can effectively reduce the wear of the base 201. The elastic deformation of the anti-slip pads 6 can also absorb the impact force generated when the packaging box is placed to a certain extent, reducing the noise caused by the collision between the packaging box and the ground.

[0040] like Figure 1 As shown, the side wall of the box 1 is rotatably connected to a handle 7. There are three sets of handles 7, which are located at the bottom of the lock seat 303. This allows the handles 7 to rotate freely around the connection point within a certain angle range. When there is no need to move the box, the handles 7 can rotate back to the position that fits against the side wall of the box 1, reducing the space occupied and maintaining the neatness of the appearance of the box 1.

[0041] like Figure 3 As shown, the outer wall of the cover plate 301 is fixedly provided with longitudinal reinforcing ribs 8. There are four sets of longitudinal reinforcing ribs 8. The four sets of longitudinal reinforcing ribs 8 are evenly distributed on the outer wall of the cover plate 301, forming a support structure similar to a frame, which enhances the overall structural strength of the cover plate 301 and makes it less prone to deformation or damage when subjected to force.

[0042] Specifically, when using the special packaging box for aircraft parts: (e.g.) Figure 2 As shown, lifting the latch 302 and rotating the cover 301 opens the box 1, allowing aircraft parts to be placed inside. After placement, the cover 301 can be closed. The latch 302 and the lock seat 303 will engage, firmly securing the cover 301 to the top of the box 1, achieving a seal and effectively preventing external dust, moisture, and impurities from entering the box 1. This provides excellent protection for the aircraft parts inside. Figure 4As shown, the honeycomb structure of the honeycomb aluminum plate 401 on the inner wall of the box 1 gives it excellent cushioning performance, which can significantly reduce the impact and vibration of the items inside the box during transportation and handling, and reduce the risk of damage to the items. The sliding strip 402 and the partition 403 allow the internal space of the box 1 to be flexibly divided according to actual needs. Users can personalize the layout according to the characteristics of different items, improve space utilization, and avoid items being squeezed or collided with each other inside the box. When the cover 301 is opened, the sensor light strip 5 automatically lights up, which makes it easy for staff to place and take out aircraft parts without the need for manual operation of the switch, providing users with a more convenient user experience, especially in low-light environments.

[0043] All technical features in this embodiment can be freely combined according to actual needs.

[0044] The above embodiments are preferred implementations of this utility model. In addition, this utility model can also be implemented in other ways. Any obvious substitutions without departing from the concept of this technical solution are within the protection scope of this utility model.

Claims

1. A packaging box for aircraft parts, comprising a box body (1), characterized in that, The bottom of the box (1) is provided with a moving component (2) for easy movement of the packaging box, and the top of the box (1) is provided with a sealing component (3). The sealing component (3) is used to prevent external contaminants from entering the interior of the box (1) and to protect the aircraft parts from damage. The interior of the box (1) is provided with a placement component (4) for placing the aircraft parts. The moving component (2) includes a base (201) that is fixedly connected to the bottom of the housing (1) by bolts. Two sets of pulleys (202) are bolted to one end of the base (201). The two sets of pulleys (202) are symmetrically arranged. A limit groove is opened at the other end of the base (201). A pull rod (203) is slidably connected to the limit groove.

2. The packaging box for aircraft parts according to claim 1, characterized in that, The sealing assembly (3) includes a cover plate (301) hinged to the top of the housing (1), and a latch (302) is hinged to the outer wall of the cover plate (301). There are four sets of latches (302), and a lock seat (303) is bolted to the outer wall of the housing (1) at the position corresponding to the latch (302).

3. The aircraft parts specific packaging box of claim 1, wherein, The placement component (4) includes a honeycomb aluminum plate (401) fixedly connected to the inner wall of the box (1). The honeycomb aluminum plate (401) is disposed on the inner side wall and the inner bottom wall of the box (1). Six sets of sliding strips (402) are bolted to the inner side wall of the box (1). The six sets of sliding strips (402) are symmetrically arranged in pairs. A partition (403) is slidably connected inside the sliding strip (402).

4. The aircraft parts specific packaging box of claim 2, wherein, The inner wall of the cover plate (301) is bolted with an induction light strip (5), which is rectangular in shape.

5. The aircraft parts specific packaging box of claim 1, wherein, The bottom of the base (201) is fixedly connected to two sets of anti-slip pads (6), and the two sets of anti-slip pads (6) are arranged symmetrically.

6. The aircraft parts specific packaging box of claim 1, wherein, The side wall of the box (1) is rotatably connected to a handle (7), and there are three sets of handles (7), which are located at the bottom of the lock seat (303).

7. The aircraft parts specific packaging box of claim 2, wherein, The outer wall of the cover plate (301) is fixedly provided with longitudinal reinforcing ribs (8), and the number of longitudinal reinforcing ribs (8) is four sets.

Images