Novel aviation container plate

Abstract

The utility model discloses a novel aviation packaging plate in the technical field of aviation packaging plates, which is reasonable in structure, and is characterized in that a frame profile is matched with an upper panel and a lower panel to form the integral aviation packaging plate, and a plurality of groups of reinforcing ribs are paved between the upper panel and the lower panel to form a plurality of groups of reinforcing ribs. The upper panel, the lower panel and the reinforcing ribs are matched, the rivets for fastening sequentially penetrate through the upper panel, the lower panel and the reinforcing ribs, the reinforcing ribs are installed and fixed, and meanwhile the reinforcing ribs are high in rigidity and strength, so that the overall strength and rigidity of the aviation packaging plate are improved; the situation that the aviation container plate deforms due to the influence of the weight of goods in the loading and transporting process is avoided as much as possible, the four inner corners of the frame profile are provided with the plug corners A and fixed through the bolts, and the four outer corners are plugged into the plug corners B, so that the overall strength and rigidity of the four inner corners and the four outer corners of the frame profile are improved, and the service life of the aviation container plate is prolonged. And deformation and damage of the frame profile caused by impact or collision are reduced as much as possible.

Description

Technical Field

[0001] The utility model relates to the technical field of aviation container plates, in particular to a novel aviation container plate. Background Art

[0002] Air pallet technology refers to the technology used for loading and transporting cargo for air cargo. An air pallet is a cargo container of standard size, usually used to load cargo and transport it by aircraft. Air pallet technology includes the design, manufacture, maintenance and management of air pallets to ensure the safe and efficient transportation of cargo. At present, during the process of loading cargo, air pallets are easily affected by the weight of the cargo and the loading position, which causes the air pallet to deform. At the same time, during the transportation of air pallets, the four corners of the air pallet are inevitably affected by impact or collision, causing deformation and damage to the four corners of the air pallet, thereby reducing the durability of the air pallet and affecting the overall strength and rigidity of the air pallet.

[0003] Therefore, it is necessary to develop a new type of aviation container. Utility Model Content

[0004] The utility model aims to provide a novel aviation container board, which is formed by matching a frame profile with an upper panel and a lower panel to form an integral aviation container board, and paving an array of reinforcing ribs between the upper panel and the lower panel, so that the rivets used for fastening are sequentially penetrated through the upper panel, the lower panel and the reinforcing ribs to achieve installation and fixation of the reinforcing ribs, and at the same time, the reinforcing ribs have strong rigidity and strength, thereby increasing the overall strength and rigidity of the aviation container board, and avoiding the deformation of the aviation container board caused by the weight of the goods during loading and transportation as much as possible. By installing plug corners A at the four inner corners of the frame profile and fixing them with bolts, and plugging corners B at the four outer corners, the overall strength and rigidity of the four inner and outer corners of the frame profile are increased, and the deformation and damage caused by impact or collision of the frame profile are minimized, so as to solve the problem of low strength and easy deformation and damage of the aviation container board proposed in the above background technology.

[0005] To achieve the above object, the utility model provides the following technical solutions: a novel aviation container panel, comprising a frame profile, an upper panel is installed at the inner front end of the frame profile, and a lower panel is installed at the inner rear end of the frame profile;

[0006] Reinforcing ribs are installed between opposite sides of the upper panel and the lower panel.

[0007] Preferably, rivet holes A are provided on the surfaces of the upper panel and the lower panel, and rivet holes B are provided on the surfaces of the reinforcing ribs.

[0008] Preferably, the rivet hole B and the rivet hole A are fixed by rivets.

[0009] Preferably, locking grooves are provided on the surfaces of the frame profiles, and limiting blocks are provided on the outer walls on both sides of the frame profiles.

[0010] Preferably, the insides of the four inner corners of the frame profile are all provided with plug corners A, and the insides of the four outer corners of the frame profile are all provided with plug corners B.

[0011] Compared with the prior art, the beneficial effects of the utility model are:

[0012] An integral aviation container is formed by matching the frame profile with the upper panel and the lower panel, and an array of reinforcing ribs are laid between the upper panel and the lower panel, so that the rivets used for fastening penetrate the upper panel, the lower panel and the reinforcing ribs in sequence to achieve installation and fixation of the reinforcing ribs. At the same time, the reinforcing ribs have strong rigidity and strength, thereby increasing the overall strength and rigidity of the aviation container, and avoiding deformation caused by the weight of the cargo during loading and transportation of the aviation container as much as possible. By installing plug corners A at the four inner corners of the frame profile and fixing them with bolts, and plugging corners B at the four outer corners, the overall strength and rigidity of the four inner and outer corners of the frame profile are increased, and the deformation and damage caused by impact or collision of the frame profile are minimized, thereby effectively improving the durability of the aviation container, and effectively increasing the rigidity and strength of the aviation container. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Figure 1 The overall structural diagram provided by the utility model;

[0014] Figure 2 A schematic diagram of a top-view cross-sectional structure provided by the utility model;

[0015] Figure 3 The utility model provides Figure 1 A magnified view of the structure at A;

[0016] Figure 4 The utility model provides Figure 1 Enlarged view of the structure at B in the figure.

[0017] In the figure: 1. frame profile; 2. upper panel; 3. lower panel; 4. reinforcing rib; 5. rivet hole A; 6. rivet hole B; 7. locking groove; 8. limit block; 9. corner plug A; 10. corner plug B. DETAILED DESCRIPTION

[0018] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0019] The utility model provides the following technical solutions: a new type of aviation container board, please refer to Figure 1-4 , comprising a frame profile 1, an upper panel 2 is installed at the inner front end of the frame profile 1, and a lower panel 3 is installed at the inner rear end of the frame profile 1;

[0020] Reinforcing ribs 4 are installed between the opposite sides of the upper panel 2 and the lower panel 3, rivet holes A5 are opened on the surfaces of the upper panel 2 and the lower panel 3, rivet holes B6 are opened on the surfaces of the reinforcing ribs 4, and the rivet holes B6 are fixed to the rivet holes A5 by rivets. The upper panel 2 and the lower panel 3 are butted together, and the frame profiles 1 on the four sides are diagonally welded to form an integral aviation container. Before the upper panel 2 and the lower panel 3 are butted together, an array of reinforcing ribs 4 are laid between them, and several rivet holes B6 are opened on the surfaces of the reinforcing ribs 4. Several rivet holes A5 are opened on the surfaces of the upper panel 2 and the lower panel 3 accordingly, so that the rivets used for fastening penetrate the rivet holes B6 and the rivet holes A5 for locking, so as to achieve the installation and fixing of the reinforcing ribs 4. At the same time, the reinforcing ribs 4 have strong rigidity and strength, thereby increasing the overall strength and rigidity of the aviation container, and avoiding the deformation of the aviation container due to the weight of the goods during loading and transportation as much as possible;

[0021] The surface of the frame profile 1 is provided with a locking groove 7. A plurality of locking grooves 7 are provided on the surface of the frame profile 1. According to the cargo being loaded on the upper panel 2 on the aviation container, the locking buckle on one end of the strap is inserted into the locking groove 7 to fix the cargo. Limiting blocks 8 are provided on both sides of the outer wall of the frame profile 1. An array of limiting blocks 8 is provided on the outer wall of the longer side of the frame profile 1. According to the spacing between the two groups of limiting blocks 8, the prior art technology for fixing the aviation container by air transportation can be applied. The fixing method is to use an inverted L-shaped bracket, which is inserted into the spacing between the two groups of limiting blocks 8, to fix the position of the aviation container, so as to prevent the aviation container from shifting and falling during transportation.

[0022] Corner plugs A9 are provided inside the four inner corners of the frame profile 1, and corner plugs B10 are provided inside the four outer corners of the frame profile 1. The four inner corners of the frame profile 1 are installed with corner plugs A9 and fixed with bolts, and the four outer corners are stuffed with corner plugs B10 to increase the overall strength and rigidity of the four inner and outer corners of the frame profile 1 and minimize the deformation and damage of the frame profile 1 caused by impact or collision.

[0023] Working principle: When using the utility model, the upper panel 2 and the lower panel 3 are butt-jointed, and the frame profiles 1 on the four sides are diagonally welded to form an integral aviation container. Before the upper panel 2 and the lower panel 3 are butt-jointed, an array of reinforcing ribs 4 are laid between them, and a plurality of rivet holes B6 are opened on the surface of the reinforcing ribs 4. A plurality of rivet holes A5 are correspondingly opened on the surfaces of the upper panel 2 and the lower panel 3, so that the rivets used for fastening penetrate the rivet holes B6 and the rivet holes A5 for locking, so as to achieve the installation and fixing of the reinforcing ribs 4. At the same time, the reinforcing ribs 4 have strong rigidity and strength, so as to increase the overall strength and rigidity of the aviation container, and try to avoid the deformation caused by the weight of the cargo during the loading and transportation of the aviation container. By opening a plurality of locking grooves 7 on the surface of the frame profile 1, according to the cargo loaded on the upper panel 2 on the aviation container, the upper end of the strap is fastened by the upper end of the strap. The lock is inserted into the lock groove 7 to fix the cargo. By setting an array of limit blocks 8 on the outer wall of the longer side of the frame profile 1, according to the spacing between the two groups of limit blocks 8, it can be applied to the prior art of aviation transportation to fix the aviation container. The fixing method is to use an inverted L-shaped bracket, which is inserted into the spacing between the two groups of limit blocks 8, so as to fix the position of the aviation container to prevent the aviation container from shifting and falling during transportation. By installing plug corners A9 at the four inner corners of the frame profile 1 and fixing it with bolts, and plug corners B10 are inserted into the four outer corners, the overall strength and rigidity of the four inner and outer corners of the frame profile 1 are increased, and the deformation and damage caused by impact or collision of the frame profile 1 are minimized, the durability of the aviation container is effectively improved, and the rigidity and strength of the aviation container are also effectively increased.

[0024] Although the present invention has been described above with reference to the embodiments, various modifications may be made thereto and parts thereof may be replaced with equivalents without departing from the scope of the present invention. In particular, as long as there is no structural conflict, the various features in the embodiments disclosed in the present invention may be used in combination with each other in any manner, and the fact that these combinations are not exhaustively described in this specification is only for the sake of omitting space and saving resources. Therefore, the present invention is not limited to the specific embodiments disclosed herein, but includes all technical solutions falling within the scope of the claims.

Claims

1. A novel aviation container, comprising a frame profile (1), characterized in that: An upper panel (2) is installed at the inner front end of the frame profile (1), and a lower panel (3) is installed at the inner rear end of the frame profile (1); Reinforcing ribs (4) are installed between the upper panel (2) and the lower panel (3) on opposite sides.

2. A novel aviation pallet according to claim 1, characterized in that: The surfaces of the upper panel (2) and the lower panel (3) are both provided with rivet holes A (5), and the surfaces of the reinforcing ribs (4) are both provided with rivet holes B (6).

3. A novel aviation pallet according to claim 2, characterized in that: The rivet hole B (6) is fixed to the rivet hole A (5) by rivets.

4. A novel aviation pallet according to claim 1, characterized in that: The surface of the frame profile (1) is provided with a locking groove (7), and the outer walls on both sides of the frame profile (1) are provided with a limiting block (8).

5. A novel aviation pallet according to claim 1, characterized in that: Corner plugs A (9) are provided inside the four inner corners of the frame profile (1), and corner plugs B (10) are provided inside the four outer corners of the frame profile (1).

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