An aircraft standard parts soaking and storage device
By designing a storage device for standard aircraft parts with a lid and a flow channel, the problems of parts scattering and cumbersome primer treatment were solved, achieving safe storage of parts and efficient primer treatment.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- AVIC CHENGFEI COMML AIRCRAFT COMPANY
- Filing Date
- 2025-06-03
- Publication Date
- 2026-05-26
AI Technical Summary
Traditional aircraft standard parts storage devices are prone to tipping over, causing parts to scatter. Primer treatment is cumbersome and can easily damage parts, increasing time and labor costs.
Design a storage box with a lid, a flow channel, and a baffle plate. The lid prevents parts from falling out, and the flow channel drains the primer liquid, simplifying the primer treatment process.
It effectively prevents parts from scattering, simplifies the primer treatment process, reduces part damage, and improves ease of use and safety.
Smart Images
Figure CN224278230U_ABST
Abstract
Description
Technical Field
[0001] This application relates to the field of parts storage technology, specifically to a device for soaking and storing standard aircraft parts. Background Technology
[0002] In aerospace parts manufacturing and assembly sites, traditional standard parts storage boxes have an open design, which makes them prone to tipping over, scattering, and being difficult to recycle. Once a standard part is lost, it may become redundant equipment on the aircraft, threatening flight safety. In addition, some standard parts require a primer treatment, and the current process relies on manual soaking and drying, which is cumbersome, easily damages the standard parts, and increases time and labor costs. Utility Model Content
[0003] The main purpose of this application is to provide an aircraft standard parts soaking and storage device, which aims to solve the technical problems of existing standard parts storage devices having openings that easily cause parts to scatter and make it inconvenient to apply a base coat to the standard parts.
[0004] The technical solution adopted in this application is as follows:
[0005] An aircraft standard parts soaking and storage device includes a storage box, a box cover on the top of the storage box, a flow guide channel on one side of the storage box, a slot on the side of the storage box located in the flow guide channel, a liquid baffle plate in the slot, and a perforated plate integrally formed with the storage box on the side of the liquid baffle plate away from the flow guide channel.
[0006] Optionally, the top of the storage box is provided with an integrally formed horizontal top plate and a sloping top plate. The horizontal top plate is provided with a first box opening and a first box cover. The sloping top plate is provided with a second box opening and a second box cover.
[0007] Optionally, one side of the first lid is connected to the storage box via a hinge with a torsion spring, and the other side of the first lid is connected to the storage box via a fastener.
[0008] Optionally, the fastener includes a latch on the storage box and a hook on the first box lid, the hook engaging with the latch.
[0009] Optionally, the second lid is located inside the storage box and opens by pushing inward.
[0010] Optionally, the second lid is connected to the storage box via a magnetic connector.
[0011] Optionally, the outer periphery of the baffle plate is covered with a sealing rubber sleeve.
[0012] Optionally, a 45° inclined ramp is provided inside the storage box on one side of the perforated plate.
[0013] Optionally, the baffle plate is provided with a lifting plate hole.
[0014] Optionally, the outer wall of the storage box is provided with a label slot.
[0015] Compared with the prior art, the beneficial effects of this application are:
[0016] This application proposes an aircraft standard parts soaking and storage device. By setting a lid on a traditional open storage box, the parts inside the box can be prevented from scattering when the box is tilted. At the same time, a guide channel is set up so that after the primer is applied inside the box, the liquid baffle can be lifted to drain the primer liquid, simplifying the primer treatment process for standard parts and reducing damage to the standard parts. Attached Figure Description
[0017] Figure 1 A schematic diagram of the aircraft standard parts soaking and storage device provided in the embodiments of this application from one perspective;
[0018] Figure 2 A schematic diagram of the aircraft standard parts soaking and storage device provided in an embodiment of this application from another perspective;
[0019] Figure 3 A cross-sectional structural diagram of the aircraft standard parts soaking and storage device provided in the embodiments of this application from one perspective.
[0020] Explanation of the labels in the attached drawings:
[0021] 1-Storage box, 2-First box lid, 3-Second box lid, 4-Drainage channel, 5-Mesh plate, 6-Liquid baffle, 7-Sloping platform, 8-Label slot. Detailed Implementation
[0022] The technical solutions of the embodiments of this application will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only a part of the embodiments of this application, and not all of the embodiments. Based on the embodiments of this application, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the scope of protection of this application.
[0023] It should be noted that all directional indicators (such as up, down, left, right, front, back, etc.) in the embodiments of this application are only used to explain the relative positional relationship and movement of each component in a certain specific posture (as shown in the figure). If the specific posture changes, the directional indicator will also change accordingly.
[0024] In this application, unless otherwise expressly specified and limited, the terms "connection," "fixed," etc., should be interpreted broadly. For example, "fixed" can mean a fixed connection, a detachable connection, or an integral part; it can mean a mechanical connection or an electrical connection; it can mean a direct connection or an indirect connection through an intermediate medium; it can mean the internal communication of two components or the interaction between two components, unless otherwise expressly limited. Those skilled in the art can understand the specific meaning of the above terms in this application according to the specific circumstances.
[0025] Furthermore, if the embodiments of this application involve descriptions such as "first" or "second," these descriptions are for descriptive purposes only and should not be construed as indicating or implying their relative importance or implicitly specifying the number of technical features indicated. Therefore, a feature defined with "first" or "second" may explicitly or implicitly include at least one of those features. Additionally, the meaning of "and / or" throughout the text includes three parallel solutions; for example, "A and / or B" includes solution A, solution B, or a solution where both A and B are satisfied simultaneously. Furthermore, the technical solutions of the various embodiments can be combined with each other, but this must be based on the ability of those skilled in the art to implement them. When the combination of technical solutions is contradictory or impossible to implement, it should be considered that such a combination of technical solutions does not exist and is not within the scope of protection claimed in this application.
[0026] See attached document Figures 1 to 3 As shown, this application embodiment provides an aircraft standard parts soaking and storage device, including a storage box 1, a box cover is provided on the top of the storage box 1, a guide channel 4 is provided on one side of the storage box 1, a slot is provided on the side of the storage box 1 located in the guide channel 4, a liquid baffle 6 is provided in the slot, and a mesh plate 5 integrally formed with the storage box 1 is provided on the side of the liquid baffle 6 away from the guide channel 4.
[0027] In the above embodiment, by providing a lid on the top of the storage box 1, the lid can prevent the standard items from scattering if the storage box 1 is tipped over after being filled with them. At the same time, by providing a baffle plate 6, the primer liquid can be introduced into the storage box 1, preventing the primer liquid from flowing out of the guide channel 4. Thus, the standard items in the box can be primed. After the primer is applied, the baffle plate 6 can be lifted to allow the liquid to be discharged from the guide channel 4 through the mesh plate 5, avoiding the need to repeatedly handle the standard items for primer treatment and reducing damage to the standard items.
[0028] In one embodiment, the top of the storage box 1 is provided with an integrally formed horizontal top plate and a sloping top plate. The horizontal top plate has a first opening, and the first opening has a first lid 2. One side of the first lid 2 is connected to the storage box 1 via a hinge with a torsion spring, and the other side of the first lid 2 is connected to the storage box 1 via a fastener. The fasteners conventionally include latches and hooks. The latches are integrally formed on the side of the storage box 1, and the hooks are integrally formed on the first lid 2, with the hooks overlapping the latches.
[0029] In the above embodiment, the design of the first lid 2 allows users to quickly and easily open and close the lid, thus facilitating the placement and removal of the labels. The first lid 2, with its hinge structure featuring a torsion spring, ensures a tight fit when closed, thereby guaranteeing the airtightness of the storage device and preventing the internal labels from being exposed. Simultaneously, the fastener design makes opening the lid more convenient, enhancing usability.
[0030] In one embodiment, the sloping top plate is provided with a second opening, and the second opening is provided with a second cover 3. The second cover 3 is located inside the storage box 1, and the second cover 3 is connected to the storage box 1 by a magnetic connector. The second opening is opened by pushing inward. The magnetic connector can be two magnets that attract each other and are respectively embedded in the inner top surface of the storage box 1 and the surface of the second cover 3, forming opposite magnets attracting each other to tightly close the second opening.
[0031] In the above embodiment, to further enhance ease of use and safety, a second opening is designed on the side of the storage box 1. Users can quickly remove the items by pushing the second lid 3 inward without fully opening the lid. After the items are removed, the magnetic opening automatically closes, effectively preventing items from spilling when the storage box 1 is tilted, thereby improving safety. The magnetic design is not only easy to operate, but also ensures that the opening remains closed when not in use, preventing impurities from entering the storage box 1.
[0032] In one embodiment, a 45° inclined ramp 7 is provided inside the storage box 1 on one side of the perforated plate.
[0033] In the above embodiment, considering that the liquid needs to be completely drained after the base coating material is soaked, the storage box 1 is designed with a flow guide 4. When the storage box 1 is tilted at 45°, the base coating material can flow out completely through the mesh plate 5 and the flow guide 4, ensuring that no residue remains in the device. This design not only facilitates cleaning and maintenance, but also avoids material damage or contamination caused by liquid residue.
[0034] In one embodiment, the outer periphery of the baffle plate 6 is covered with a sealing rubber sleeve, and the top of the baffle plate 6 is provided with a lifting plate hole.
[0035] In the above embodiment, to address potential liquid splashing or overflow during the pouring of the primer and soaking process, the storage box is designed with slots and a baffle plate 6 on its side. The baffle plate 6 effectively blocks the internal primer liquid, preventing it from overflowing outside the storage box 1, thus maintaining a clean working environment. The side of the baffle plate 6 that contacts the slot is made of rubber to further enhance sealing performance and prevent liquid leakage. This design not only improves the functionality of the storage box but also optimizes the user experience, ensuring the safety and efficiency of the liquid handling process. Simultaneously, the baffle plate 6's lifting hole design facilitates easy replacement or cleaning by the user when needed, ensuring the long-term effectiveness of the storage box.
[0036] In one embodiment, the outer wall of the storage box 1 is provided with a label slot 8.
[0037] In the above embodiment, a label slot 8 is designed on the front of the storage box. The label content makes it easy for users to quickly identify the type of standard items in the storage box, which helps to classify and manage the standard items and improve work efficiency.
[0038] Based on the above, the present application provides an aircraft standard parts soaking and storage device, the method of which is as follows:
[0039] First, carefully stack the standard items that need to be processed inside the storage box 1, ensuring that the standard items are placed stably;
[0040] Then, insert a baffle plate 6 into the side of the storage box 1 to ensure that the space of the storage box 1 is sealed and to prevent liquid from flowing out from the mesh plate 5 on the side and the flow guide groove on the lower side.
[0041] Next, pour the primer material through the opening at the top of storage box 1, ensuring that the material evenly covers the standard parts;
[0042] Then, close the top lid to ensure that storage box 1 is completely sealed, and begin the soaking process;
[0043] Next, after soaking is complete, according to the requirements of the primer material, wait for the standard to be fully soaked, tilt the storage box 1 at 45°, remove the side baffle 6, and let the primer material flow out through the mesh plate 5 and the guide channel 4.
[0044] Finally, ensure the standard is completely dry to avoid any residual primer affecting its use. Replace the top lid to ensure safe storage of the standard.
[0045] In summary, the aircraft standard parts soaking and storage device provided in this application solves the problem of standard parts easily spilling due to the design of the box lid to prevent the standard parts from spilling, the automatic closing function, and the integrated primer treatment, while simplifying the standard parts primer treatment process.
[0046] The above description is only a preferred embodiment of this application and is not intended to limit this application. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of this application should be included within the protection scope of this application.
Claims
1. An aircraft standard part soaking and storage device, characterized by, The device includes a storage box, a lid on the top of the storage box, a flow channel on one side of the storage box, a slot on the side of the storage box located in the flow channel, a baffle plate in the slot, and a perforated plate integrally formed with the storage box on the side of the baffle plate away from the flow channel.
2. The aircraft standard part soaking and storage device of claim 1, wherein, The top of the storage box is provided with an integrally formed horizontal top plate and a sloping top plate. The horizontal top plate is provided with a first box opening and a first box cover. The sloping top plate is provided with a second box opening and a second box cover.
3. The aircraft standard part soaking and storage device of claim 2, wherein, One side of the first box lid is connected to the storage box via a hinge with a torsion spring, and the other side of the first box lid is connected to the storage box via a fastener.
4. The aircraft standard part soaking and storage device of claim 3, wherein, The fastener includes a latch on the storage box and a hook on the first box lid, the hook being attached to the latch.
5. The aircraft standard parts soaking and storage device according to claim 2, characterized in that, The second lid is located inside the storage box and opens by pushing it inward.
6. The aircraft standard parts soaking and storage device according to claim 5, characterized in that, The second lid is connected to the storage box via a magnetic connector.
7. The aircraft standard parts soaking and storage device according to claim 1, characterized in that, The outer periphery of the baffle plate is covered with a sealing rubber sleeve.
8. The aircraft standard parts soaking and storage device according to claim 1, characterized in that, The storage box has a 45-degree inclined ramp located on one side of the perforated plate.
9. The aircraft standard parts soaking and storage device according to claim 1, characterized in that, The baffle plate is provided with a lifting hole.
10. The aircraft standard parts soaking and storage device according to claim 1, characterized in that, The outer wall of the storage box is provided with a label slot.