Tray for air transportation
By designing pallets for air transport and using lashing components to secure the pallets inside the aircraft cabin, the problem of vehicle displacement or damage caused by aircraft turbulence has been solved, thus improving stability and safety during transportation.
Patent Information
- Application Number
- CN202423276054.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-30
- Publication Date
- 2025-11-11
- Estimated Expiration
- 2034-12-30
AI Technical Summary
During air transport of automobiles, turbulence can cause vehicles to shift or be damaged inside the cabin.
Design an air transport pallet, including a pallet body and a fastening assembly. The pallet has pre-drilled holes. The fastening assembly consists of a first limiting member, a connecting rod, a second limiting member, and a fastening ring. The connecting rod is fixed in the pre-drilled holes by limiting the connection, and the fastening ring connects the pallet to the inner wall of the aircraft cabin to prevent displacement or damage.
It effectively prevents the container from shifting or being damaged during aircraft turbulence, thus improving the stability and safety of transportation.
Smart Images
Figure CN223534132U_ABST
Abstract
Description
Technical Field
[0001] This application relates to the field of aviation carrying equipment technology, and in particular to a pallet for air transport. Background Technology
[0002] Currently, air transport of automobiles primarily serves ordinary vehicles. The process involves using specialized transport racks and aviation pallets to secure and reinforce the cars before safely loading the assembled vehicles into the aircraft cargo hold, thus completing the air transport mission. However, during flight, the aircraft may encounter turbulence, causing the installed equipment or vehicles to shift or even be damaged within the cabin. Utility Model Content
[0003] In view of this, the purpose of this application is to provide a pallet for air transport to prevent automobiles from shifting or being damaged due to turbulence during air transport.
[0004] For the purposes described above, this application provides a pallet for air transport, comprising:
[0005] The container plate body has pre-drilled holes;
[0006] The fastening assembly includes a first limiting member, a connecting rod, a second limiting member, and a fastening ring. The connecting rod is connected between the first limiting member and the second limiting member. The fastening ring is connected to the side of the first limiting member away from the connecting rod. The connecting rod passes through a pre-drilled hole. The first limiting member is located on one side of the container plate body, and the second limiting member is located on the other side of the container plate body to prevent the connecting rod from disengaging from the pre-drilled hole.
[0007] Optionally, the first limiting member is a rectangular limiting plate, which can limit the connecting rod together with the second limiting member through the reserved hole.
[0008] Optionally, the second limiting member has a mounting groove on the side near the first limiting member, and the connecting rod extends and retracts in the mounting groove.
[0009] Optionally, the mounting groove is threadedly connected to the connecting rod.
[0010] Optionally, a limiting protrusion is fixedly connected to the side of the container plate body near the first limiting member. The limiting protrusion is located on one side of the reserved hole and abuts against the first limiting member to limit the shaking of the first limiting member.
[0011] Optionally, a gasket is provided between the container plate body and the first limiting member to fill the gap between the container plate body and the first limiting member.
[0012] Optionally, the gasket gradually thickens from one side to the other to fill gaps of different sizes between the container plate body and the first limiting member.
[0013] Optionally, the container plate body is provided with wheel limiting holes.
[0014] As can be seen from the above, this application provides a pallet for air transport, including a pallet body and a fastening assembly. The pallet has a pre-drilled hole. The fastening assembly includes a first limiting member, a second limiting member, a connecting rod, and a fastening ring. The fastening assembly uses the limiting action of the first and second limiting members to restrict the connecting rod within the pre-drilled hole, thereby fixing the fastening assembly to the pallet. The fastening ring on the fastening assembly provides a connection point for a pull rope or zipper, facilitating the connection of the pull rope or zipper between the pallet body and the aircraft cabin wall, thereby preventing the pallet body from shifting or being damaged during aircraft turbulence. Attached Figure Description
[0015] To more clearly illustrate the technical solutions in this application or related technologies, the drawings used in the description of the embodiments or related technologies will be briefly introduced below. Obviously, the drawings described below are only embodiments of this application. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.
[0016] Figure 1 This is a schematic diagram of the structure of an embodiment of this application;
[0017] Figure 2 This is a schematic diagram showing the structure of the container pallet body according to an embodiment of this application;
[0018] Figure 3 This is a schematic diagram of the structure of the fastening assembly shown in the embodiments of this application;
[0019] Figure 4 This is a schematic diagram of the structure of the gasket shown in the embodiment of this application.
[0020] Reference numerals: 1. Container plate body; 11. Reserved hole; 12. Wheel limiting hole; 2. Fastening assembly; 21. First limiting component; 22. Connecting rod; 221. Mounting groove; 23. Second limiting component; 24. Fastening ring; 3. Limiting protrusion; 4. Gasket. Detailed Implementation
[0021] To make the objectives, technical solutions, and advantages of this application clearer, the following detailed description is provided in conjunction with specific embodiments and the accompanying drawings.
[0022] It should be noted that, unless otherwise defined, the technical or scientific terms used in the embodiments of this application should have the ordinary meaning understood by one of ordinary skill in the art to which this application pertains. The terms "first," "second," and similar terms used in the embodiments of this application do not indicate any order, quantity, or importance, but are merely used to distinguish different components. Terms such as "comprising" or "including" mean that the element or object preceding the word encompasses the elements or objects listed after the word and their equivalents, without excluding other elements or objects. Terms such as "connected" or "linked" are not limited to physical or mechanical connections, but can include electrical connections, whether direct or indirect. Terms such as "upper," "lower," "left," and "right" are only used to indicate relative positional relationships; when the absolute position of the described object changes, the relative positional relationship may also change accordingly.
[0023] As mentioned in the background, current air transport of automobiles primarily serves ordinary vehicles. The process involves using specialized transport racks and aviation pallets to securely reinforce the cars before safely loading the assembled vehicles into the aircraft cargo hold, thus completing the air transport mission. However, during flight, the aircraft may encounter turbulence, causing the installed equipment or vehicles to shift or even be damaged within the cabin.
[0024] To address the aforementioned problems, this application provides a pallet for air transport.
[0025] The following is in conjunction with the appendix Figure 1-4 The embodiments of this application will be described in detail below.
[0026] like Figure 1 , Figure 2 and Figure 3 As shown, an air transport pallet includes:
[0027] The container plate body 1 is provided with a reserved hole 11;
[0028] The fastening assembly 2 includes a first limiting member 21, a connecting rod 22, a second limiting member 23, and a fastening ring 24. The connecting rod 22 is connected between the first limiting member 21 and the second limiting member 23. The fastening ring 24 is connected to the side of the first limiting member 21 away from the connecting rod 22. The connecting rod 22 passes through a pre-drilled hole 11. The first limiting member 21 is located on one side of the container plate body 1, and the second limiting member 23 is located on the other side of the container plate body 1 to prevent the connecting rod 22 from disengaging from the pre-drilled hole 11.
[0029] Specifically, the stabilization assembly 2 is fixed to the container plate body 1 through the reserved holes 11. The stabilization ring 24 on the stabilization assembly 2 provides a connection position for the pull rope or zipper, which facilitates the pull rope or zipper to connect the container plate body 1 to the inner wall of the aircraft cabin, thereby preventing the container plate body 1 from shifting or being damaged under the condition of aircraft turbulence. In addition, the container plate body 1 is provided with multiple reserved holes 11, which are respectively set at the four corners of the container plate body 1. Each reserved hole 11 corresponds to a stabilization assembly 2, which facilitates the overall fixation of the container plate body 1 and further improves the stability of the container plate body 1.
[0030] Furthermore, the first limiting member 21 is located on one side of the container plate body 1, the second limiting member 23 is located on the other side of the container plate, and the connecting rod 22 is located between the first limiting member 21 and the second limiting member 23 and passes through the reserved hole 11. The first limiting member 21 and the second limiting member 23 can abut against the container plate body 1, thereby preventing the connecting rod 22 from disengaging from the reserved hole 11, and thus completing the connection between the fastening assembly 2 and the container plate body 1.
[0031] In summary, in this application, the fastening assembly 2 restricts the connecting rod 22 in the reserved hole 11 through the limiting effect of the first limiting member 21 and the second limiting member 23, thereby fixing the fastening assembly 2 to the container plate. The fastening ring 24 on the fastening assembly 2 provides a connection position for the pull rope or zipper, which facilitates the pull rope to connect the container plate body 1 to the inner wall of the aircraft cabin, thereby preventing the container plate body 1 from being displaced or damaged under the condition of aircraft turbulence.
[0032] like Figure 1 and Figure 3 As shown, in some embodiments, the first limiting member 21 is a rectangular limiting plate, which can limit the connecting rod 22 together with the second limiting member 23 through the reserved hole 11.
[0033] Specifically, the reserved hole 11 is also rectangular to facilitate the passage of the first limiting member 21. When the fastening assembly 2 needs to be installed on the container plate body 1, the first limiting member 21 is passed through the reserved hole 11, and then the fastening ring 24 is rotated. The first limiting member 21 rotates synchronously and the two sides of the first limiting member 21 abut against the container plate body 1, thereby cooperating with the second limiting member 23 to complete the limiting of the connecting rod 22.
[0034] In this embodiment, the rectangular limiting plate can provide a foundation for the installation of the fastening component 2 on the container plate body 1 through the reserved hole 11. After the rectangular limiting plate passes through the reserved hole 11, the installation of the fastening component 2 on the container plate body 1 can be achieved simply by rotating the rectangular limiting plate, thereby improving the efficiency of installing the fastening component 2 on the container plate body 1.
[0035] like Figure 3As shown, in some embodiments, the second limiting member 23 has a mounting groove 221 on the side near the first limiting member 21, and the connecting rod 22 extends and retracts in the mounting groove 221.
[0036] In this embodiment, the second limiting member 23 has an installation groove 221 on the side near the first limiting member 21. The connecting rod 22 extends and retracts in the installation groove 221 to adapt to the container plate body 1 of different thicknesses, thereby increasing the versatility of the fastening assembly 2.
[0037] In some embodiments, the mounting groove 221 is threadedly connected to the connecting rod 22.
[0038] In this embodiment, the mounting groove 221 is threadedly connected to the connecting rod 22, which can improve the connection stability between the second limiting member 23 and the connecting rod 22, thereby enhancing the stability of the fastening assembly 2 on the container plate body 1, and also making the fastening assembly 2 adaptable to container plate bodies 1 of different thicknesses, increasing the versatility of the fastening assembly 2.
[0039] like Figure 1 As shown, in some embodiments, a limiting protrusion 3 is fixedly connected to the side of the container plate body 1 near the first limiting member 21. The limiting protrusion 3 is provided on one side of the reserved hole 11 and abuts against the first limiting member 21 to limit the shaking of the first limiting member 21.
[0040] In this embodiment, the limiting protrusion 3 is provided on the side of the container plate body 1 near the first limiting member 21 and adjacent to the side of the reserved hole 11. The limiting protrusion 3 abuts against the side of the first limiting member 21, restricting the shaking of the first limiting member 21 in the mounting groove 221, thereby enhancing the stability of the entire fastening assembly 2.
[0041] like Figure 1 and Figure 4 As shown, in some embodiments, a gasket 4 is provided between the container plate body 1 and the first limiting member 21 to fill the gap between the container plate body 1 and the first limiting member 21.
[0042] In this embodiment, the gasket 4 fills the gap between the container plate body 1 and the first limiting member 21, preventing the fastening assembly 2 from shaking and causing the first limiting member 21 to detach from the reserved hole 11, thereby increasing the stability of the fastening assembly 2 installed on the container plate body 1 and thus increasing the stability of the container plate body 1 during aircraft transportation.
[0043] In some embodiments, the gasket 4 gradually thickens from one side to the other to fill gaps of different sizes between the container plate body 1 and the first limiting member 21.
[0044] Specifically, the gasket 4 is a U-shaped gasket 4, with the opening side of the U-shaped gasket 4 gradually thickening towards the tail. In use, the opening side of the U-shaped gasket 4 is inserted into the gap between the container plate body 1 and the first limiting member 21 until the fastening assembly 2 is stable. The U-shaped gasket 4 is inserted into the gap between the first limiting member 21 and the container plate body 1 on both sides, avoiding uneven force on both sides of the first limiting member 21 and further increasing the stability of the fastening assembly 2.
[0045] In this embodiment, the gasket 4 gradually thickens from one side to the other, that is, the thickness of the gasket 4 is different at different positions, so as to fill the gaps of different sizes between the container plate body 1 and the first limiting member 21, thereby increasing the versatility and practicality of the gasket 4.
[0046] like Figure 2 As shown, in some embodiments, the container plate body 1 is provided with wheel limiting holes 12.
[0047] In this embodiment, the wheel limiting hole 12 can restrict the movement of the vehicle wheels, thereby enhancing the stability of the vehicle during transportation.
[0048] In summary, in this application, the fastening assembly 2 restricts the connecting rod 22 within the reserved hole 11 through the limiting effect of the first limiting member 21 and the second limiting member 23, thereby fixing the fastening assembly 2 to the container plate. The fastening ring 24 on the fastening assembly 2 provides a connection position for the pull rope or zipper, which facilitates the pull rope or zipper to connect the container plate body 1 to the inner wall of the aircraft cabin, thereby preventing the container plate body 1 from shifting or being damaged under the condition of aircraft turbulence.
[0049] The first limiting member 21 in this application is a rectangular limiting plate. The rectangular limiting plate can pass through the reserved hole 11 to provide a foundation for the fastening component 2 to be installed on the container plate body 1. After the rectangular limiting plate passes through the reserved hole 11, the installation of the fastening component 2 on the container plate body 1 can be achieved simply by rotating the rectangular limiting plate, thereby improving the efficiency of installing the fastening component 2 on the container plate body 1.
[0050] The gasket 4 in this application fills the gap between the container plate body 1 and the first limiting member 21, preventing the fastening assembly 2 from shaking and causing the first limiting member 21 to detach from the reserved hole 11, thereby increasing the stability of the fastening assembly 2 installed on the container plate body 1 and thus increasing the stability of the container plate body 1 during aircraft transportation.
[0051] Those skilled in the art should understand that the discussion of any of the above embodiments is merely exemplary and is not intended to imply that the scope of this application is limited to these examples; under the concept of this application, the technical features of the above embodiments or different embodiments can also be combined, the steps can be implemented in any order, and there are many other variations of different aspects of the embodiments of this application as described above, which are not provided in detail for the sake of brevity.
[0052] Additionally, to simplify the description and discussion, and to avoid obscuring the embodiments of this application, the well-known power / ground connections to integrated circuit chips and other components may or may not be shown in the provided drawings. Furthermore, the apparatus may be shown in block diagram form to avoid obscuring the embodiments of this application, and this also takes into account the fact that the details of the implementation of these block diagram apparatuses are highly dependent on the platform on which the embodiments of this application will be implemented (i.e., these details should be fully within the understanding of those skilled in the art). While specific details (e.g., circuits) have been set forth to describe exemplary embodiments of this application, it will be apparent to those skilled in the art that the embodiments of this application can be implemented without these specific details or with variations thereof. Therefore, these descriptions should be considered illustrative rather than restrictive.
[0053] Although this application has been described in conjunction with specific embodiments thereof, many substitutions, modifications, and variations of these embodiments will be apparent to those skilled in the art from the foregoing description. For example, other memory architectures may use the embodiments discussed.
[0054] The embodiments of this application are intended to cover all such substitutions, modifications, and variations that fall within the broad scope of the claims of this application. Therefore, any omissions, modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the embodiments of this application should be included within the protection scope of this application.
Claims
1. A pallet for air transport, characterized in that, include: The container plate body (1) is provided with a reserved hole (11); The fastening assembly (2) includes a first limiting member (21), a connecting rod (22), a second limiting member (23), and a fastening ring (24). The connecting rod (22) is connected between the first limiting member (21) and the second limiting member (23). The fastening ring (24) is connected to the side of the first limiting member (21) away from the connecting rod (22). The connecting rod (22) passes through a pre-drilled hole (11). The first limiting member (21) is located on one side of the container plate body (1), and the second limiting member (23) is located on the other side of the container plate body (1) to restrict the connecting rod (22) from disengaging from the pre-drilled hole (11).
2. The air transport pallet according to claim 1, characterized in that, The first limiting member (21) is a rectangular limiting plate, which can limit the connecting rod (22) together with the second limiting member (23) through the reserved hole (11).
3. The air transport pallet according to claim 2, characterized in that, The second limiting member (23) has an installation groove (221) on the side near the first limiting member (21), and the connecting rod (22) extends and retracts in the installation groove (221).
4. The air transport pallet according to claim 3, characterized in that, The mounting groove (221) is threadedly connected to the connecting rod (22).
5. A pallet for air transport according to claim 2, characterized in that, The container plate body (1) is fixedly connected to a limiting protrusion (3) on the side near the first limiting member (21). The limiting protrusion (3) is located on one side of the reserved hole (11) and abuts against the first limiting member (21) to limit the shaking of the first limiting member (21).
6. The air transport pallet according to claim 1, characterized in that, A gasket (4) is provided between the container plate body (1) and the first limiting member (21) to fill the gap between the container plate body (1) and the first limiting member (21).
7. A pallet for air transport according to claim 6, characterized in that, The gasket (4) gradually thickens from one side to the other to fill the gaps of different sizes between the container plate body (1) and the first limiting member (21).
8. A pallet for air transport according to claim 1, characterized in that, The container plate body (1) is provided with wheel limiting holes (12).