Internal buffer function aviation case with multi-angle buffer module
By introducing vertical, horizontal, and top cushioning components into the flight case, the problem of incomplete cushioning in existing flight cases is solved, achieving all-round cushioning protection.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-03-18
- Publication Date
- 2026-03-13
AI Technical Summary
Existing flight cases exhibit obstruction during lateral and vertical cushioning, making it difficult to achieve effective all-around cushioning protection.
The design incorporates vertical, horizontal, and top positioning components for flight cases, including vertical buffer slides, horizontal buffer plates, side buffers, and a top resilient rubber shell, providing vertical, horizontal, and top cushioning protection, respectively.
It provides all-around protection for the inner liner, including vertical, horizontal, and top cushioning, enhancing the stability of objects inside the inner liner.
Smart Images

Figure CN223990362U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of aviation case technology, and in particular to an aviation case with an internal buffer function and a multi-angle buffer module. Background Technology
[0002] Traditional simple wooden crates cannot effectively protect these high-tech products during long-distance transportation, and their poor maneuverability is a major drawback. Therefore, a new alternative packaging product—the flight case—has emerged to address these shortcomings. Increasingly frequent international trade has propelled the use and development of flight cases into a golden age, particularly in high-tech fields such as stage lighting equipment, medical instruments, audiovisual multimedia systems, optoelectronics, and military transport packaging and equipment transportation. Currently, flight cases are a crucial piece of transportation equipment.
[0003] For example, Chinese patent CN212173172U discloses a shockproof flight case, including a case body, a shock-absorbing spring sleeved on the positioning rod, one end of the shock-absorbing spring being fixedly welded to the inner wall of the case body, multiple slots being opened on both sides of the inner wall of the inner case, partitions being movably engaged in the slots by locking blocks, a third buffer layer being adhered to both sides of the partition, a first buffer layer being adhered to the inner wall of the inner case, a second buffer layer being adhered to the bottom of the case lid, and a connecting pipe being welded to the side of the case body.
[0004] Although the above technical solutions have solved the corresponding technical problems, they still have the following drawbacks:
[0005] The above technical solution uses multiple sliding grooves, positioning rods, and shock-absorbing springs to achieve buffering of the inner box. However, when the inner box is buffered laterally, the vertical positioning rods and sliding grooves will block the horizontal positioning rods. At the same time, when the inner box is buffered vertically, the horizontal positioning rods and sliding grooves will form an obstruction. Therefore, it is difficult to achieve effective buffering of the inner box. Utility Model Content
[0006] The purpose of this utility model is to provide an internal buffer function flight case with a multi-angle buffer module. It can not only provide vertical buffering for the buffer liner when it is subjected to vertical force by setting a vertical buffer component, but also provide lateral buffering protection for objects placed inside the buffer liner by setting a horizontal buffer component, and provide effective buffering protection for objects placed inside the buffer liner from the top by setting a top positioning component, thereby achieving all-round protection for objects placed inside the buffer liner.
[0007] To achieve the above objectives, the main technical solutions adopted by this utility model include:
[0008] An internally cushioned flight case with a multi-angle buffer module includes:
[0009] The box has a lid on top that works in conjunction with the box. Inside the box is a buffer liner that provides multi-directional cushioning and protection. Vertical buffer components are provided on both sides of the buffer liner, and horizontal buffer components are provided on both sides of the inner wall of the buffer liner.
[0010] The aforementioned flight case with an internal buffer function and a multi-angle buffer module includes a vertical buffer assembly comprising two mounting blocks fixedly connected to the side of the inner wall of the case. The two mounting blocks are fixedly connected by a buffer slide rod. Two symmetrically arranged buffer sliders are slidably connected to the buffer slide rod. A buffer spring is sleeved on the buffer slide rod located between the buffer sliders and the mounting blocks.
[0011] The aforementioned internal buffer function flight case with multi-angle buffer module includes a side buffer plate, wherein the lateral buffer component includes a side buffer plate, and the side of the side buffer plate is provided with a plurality of side buffers arranged at equal intervals.
[0012] The aforementioned flight case with an internal buffer function and multi-angle buffer module includes a side buffer comprising a buffer shell fixedly connected to the side of the inner wall of the case, a side buffer spring fixedly connected to the inner wall of the buffer shell, a buffer rod fixedly connected to the side of the side buffer spring, and the other end of the buffer rod fixedly connected to the side of the side buffer plate.
[0013] The aforementioned flight case with an internal buffer function and a multi-angle buffer module has a top positioning component at the bottom of the case cover.
[0014] The aforementioned flight case with an internal cushioning function and a multi-angle buffer module includes a top positioning component comprising an elastic rubber shell fixedly connected to the bottom of the case cover, wherein a plurality of vertical buffer springs are arranged at equal intervals inside the elastic rubber shell.
[0015] The aforementioned flight case with an internal buffer function and multi-angle buffer module has a vertical buffer pad fixedly connected to the bottom of the elastic rubber shell.
[0016] The aforementioned internal buffer function flight case with multi-angle buffer module has a side buffer pad provided on the side of the side buffer plate away from the side buffer.
[0017] This utility model has at least the following beneficial effects:
[0018] The internal buffer function flight case with multi-angle buffer module provided by this utility model not only achieves vertical buffering of the buffer liner when it is subjected to vertical force by setting the vertical buffer component, but also provides lateral buffering protection for objects placed inside the buffer liner by setting the horizontal buffer component, and provides effective buffering protection for objects placed inside the buffer liner from the top by setting the top positioning component, thereby achieving all-round protection for objects placed inside the buffer liner. Attached Figure Description
[0019] The accompanying drawings, which are included to provide a further understanding of this application and form part of this application, illustrate exemplary embodiments and are used to explain this application, but do not constitute an undue limitation of this application. In the drawings:
[0020] Figure 1 This is a structural schematic diagram of the internal buffer function of the flight case with multi-angle buffer module according to this utility model;
[0021] Figure 2 This is a cross-sectional structural diagram of the flight case with internal buffer function and multi-angle buffer module according to this utility model;
[0022] Figure 3 This is a schematic diagram of the vertical buffer component in the flight case with the internal buffer function of the multi-angle buffer module of this utility model;
[0023] Figure 4 This is a schematic diagram of the lateral buffer assembly in the flight case with the internal buffer function of the multi-angle buffer module according to this utility model;
[0024] Figure 5 This is a schematic diagram of the side buffer in the flight case with the internal buffer function of the multi-angle buffer module of this utility model;
[0025] Figure 6 This is a schematic diagram of the top positioning component in the internal buffer function flight case with multi-angle buffer module of this utility model.
[0026] Explanation of icon numbers:
[0027] 1. Box body; 2. Box lid; 3. Cushioning liner;
[0028] 301. Vertical buffer assembly; 302. Horizontal buffer assembly; 303. Top positioning assembly;
[0029] 3011, Mounting block; 3012, Buffer slide bar; 3013, Buffer slider; 3014, Buffer spring;
[0030] 3021. Side buffer plate; 3022. Side buffer pad; 3023. Side buffer;
[0031] 30231, Buffer housing; 30232, Side buffer spring; 30233, Buffer rod;
[0032] 3031, Elastic rubber shell; 3032, Vertical buffer spring; 3033, Vertical buffer pad. Detailed Implementation
[0033] The following will describe in detail the implementation of this application with reference to the accompanying drawings and embodiments, so that the implementation process of how this application uses technical means to solve technical problems and achieve technical effects can be fully understood and implemented accordingly.
[0034] Please refer to Figures 1 to 6 As shown, an embodiment of the present invention provides an internal buffer function flight case with a multi-angle buffer module, comprising: a case body 1, a case cover 2 that cooperates with the case body 1 on the top of the case body 1, a buffer liner 3 that can provide multi-directional buffer protection inside the case body 1, vertical buffer components 301 on both sides of the buffer liner 3, and horizontal buffer components 302 on both sides of the inner wall of the buffer liner 3.
[0035] In order to increase the stability of the upper and lower buffering of the inner liner 3, two sets of vertical buffer components 301 can be set on both sides of the inner liner 3.
[0036] By adopting the above technical solution, not only can the vertical buffer component 301 provide vertical buffering for the buffer liner 3 when it is subjected to vertical force, but the horizontal buffer component 302 can also provide horizontal buffering protection for objects placed inside the buffer liner 3. Furthermore, the top positioning component 303 can effectively buffer and protect objects placed inside the buffer liner 3 from the top, thereby achieving all-round protection for objects placed inside the buffer liner 3.
[0037] Please refer to Figures 1 to 6 As shown, the vertical buffer assembly 301 includes two mounting blocks 3011 fixedly connected to the inner wall side of the housing 1. The two mounting blocks 3011 are fixedly connected to each other by a buffer slide rod 3012. Two symmetrically arranged buffer sliders 3013 are slidably connected on the buffer slide rod 3012. A buffer spring 3014 is sleeved on the buffer slide rod 3012 located between the buffer sliders 3013 and the mounting blocks 3011. When an object inside the buffer liner 3 is subjected to vertical force, it can provide good vertical buffer protection for the object under the elastic action of the buffer spring 3014.
[0038] Please refer to Figures 1 to 6As shown, the lateral buffer assembly 302 includes a side buffer plate 3021. The side of the side buffer plate 3021 is provided with a plurality of side buffers 3023 arranged at equal intervals. The side buffers 3023 include buffer shells 30231 fixedly connected to the side of the inner wall of the housing 1. A side buffer spring 30232 is fixedly connected to the inner wall of the buffer shell 30231. A buffer rod 30233 is fixedly connected to the side of the side buffer spring 30232, and the other end of the buffer rod 30233 is fixedly connected to the side of the side buffer plate 3021. When the object inside the buffer liner 3 is subjected to a lateral force, it can play a lateral buffering and protection role for the object inside the buffer liner 3 under the elastic force of the side buffer spring 30232.
[0039] Please refer to Figures 1 to 6 As shown, a top positioning component 303 is provided at the bottom of the lid 2. The top positioning component 303 includes an elastic rubber shell 3031 fixedly connected to the bottom of the lid 2. Several vertical buffer springs 3032 are arranged at equal intervals inside the elastic rubber shell 3031. By setting the horizontal buffer component 302, not only can the object placed inside the buffer liner 3 be effectively buffered and protected from the top, but the object placed inside the buffer liner 3 can also be positioned, thereby increasing the stability of the object placed inside the buffer liner 3.
[0040] Please refer to Figures 1 to 6 As shown, a vertical buffer pad 3033 is fixedly connected to the bottom of the elastic rubber shell 3031, and a side buffer pad 3022 is provided on the side of the side buffer plate 3021 away from the side buffer 3023. The vertical buffer pad 3033 and the side buffer pad 3022 provide good buffer protection for objects placed inside the buffer liner 3.
[0041] The working principle of this utility model is as follows: not only by setting the vertical buffer component 301, when an object inside the buffer liner 3 is subjected to vertical force, it can provide good vertical buffer protection under the elastic action of the buffer sleeve spring 3014; not only by setting the horizontal buffer component 302, when an object inside the buffer liner 3 is subjected to horizontal force, it can provide horizontal buffer protection under the elastic action of the side buffer spring 30232; and by setting the top positioning component 303, it can not only effectively buffer and protect the object placed inside the buffer liner 3 from the top, but also position the object placed inside the buffer liner 3, thereby increasing the stability of the object placed inside the buffer liner 3, and thus achieving all-round protection for the object placed inside the buffer liner 3.
[0042] The foregoing description illustrates and describes several preferred embodiments of the present invention. However, as previously stated, it should be understood that the present invention is not limited to the forms disclosed herein and should not be construed as excluding other embodiments. It can be used in various other combinations, modifications, and environments, and can be altered within the scope of the present invention's conception through the foregoing teachings or related technical or knowledge. Any modifications and variations made by those skilled in the art that do not depart from the spirit and scope of the present invention should be within the protection scope of the appended claims.
Claims
1. An internal cushioning function aviation case with multi-angle cushioning module, comprising a case body (1), characterized in that, The top of the box (1) is provided with a box cover (2) matched with the box (1), the inside of the box (1) is provided with a multi-directional buffering protection buffer inner container (3), both sides of the buffer inner container (3) are provided with vertical buffering assemblies (301), both sides of the inner wall of the buffer inner container (3) are provided with horizontal buffering assemblies (302).
2. The inner cushioning function aviation case with multi-angle cushioning module according to claim 1, characterized in that: The vertical buffering assembly (301) comprises two mounting blocks (3011) fixedly connected to the side surface of the inner wall of the box (1), two buffering slide rods (3012) are fixedly connected between the two mounting blocks (3011), two symmetrically arranged buffering slide blocks (3013) are slidably connected to the buffering slide rods (3012), and buffering sleeve springs (3014) are sleeved on the buffering slide rods (3012) between the buffering slide blocks (3013) and the mounting blocks (3011).
3. The inner cushioning function aviation case with multi-angle cushioning module according to claim 2, characterized in that: The horizontal buffering assembly (302) comprises a side buffering plate (3021), and a plurality of side buffers (3023) are arranged at equal distances on the side surface of the side buffering plate (3021).
4. The inner cushioning function aviation case with multi-angle cushioning module according to claim 3, characterized in that: The side buffer (3023) comprises a buffering shell (30231) fixedly connected to the side surface of the inner wall of the box (1), a side buffering spring (30232) is fixedly connected to the inner wall of the buffering shell (30231), a buffering rod (30233) is fixedly connected to the side surface of the side buffering spring (30232), and the other end of the buffering rod (30233) is fixedly connected to the side surface of the side buffering plate (3021).
5. The inner cushioning function aviation case with multi-angle cushioning module according to claim 4, characterized in that: The bottom of the box cover (2) is provided with a top positioning assembly (303).
6. The inner cushioning function of the aviation case with multi-angle cushioning module according to claim 5, characterized in that: The top positioning assembly (303) comprises an elastic rubber shell (3031) fixedly connected to the bottom of the box cover (2), and a plurality of vertical buffering springs (3032) are arranged at equal distances in the elastic rubber shell (3031).
7. The inner cushioning function case with multi-angle cushioning modules according to claim 6, characterized in that: The bottom of the elastic rubber shell (3031) is fixedly connected with a vertical buffering pad (3033).
8. The inner cushioning function case with multi-angle cushioning modules according to claim 7, characterized in that: The side buffering plate (3021) is provided with a side buffering pad (3022) away from the side buffer (3023).
Citation Information
Patent Citations
Shockproof aviation case
CN212173172U