An aircraft pod

Abstract

The application relates to an aircraft box which comprises an aircraft box body, the aircraft box body comprises a bottom plate, a top cover plate, a top baffle and side insertion tongues, the top baffle is connected with the side insertion tongues, the top baffle is connected with the top cover plate, the two sides of the top baffle are connected with first auxiliary insertion tongues, the aircraft box body is provided with a first annular block for inserting the first auxiliary insertion tongues, the side, away from the top cover plate, of the top baffle is connected with a second auxiliary insertion tongue, and the bottom plate is provided with a second annular block for inserting the second auxiliary insertion tongue. The first auxiliary insertion tongues on the two sides of the top baffle are inserted into the first annular block, the relative positions of the top baffle and the box body can be fixed from the two sides of the top; the second auxiliary insertion tongue on the other side of the top baffle is inserted into the second annular block of the bottom plate, a "pulling type fixing" is formed from the vertical direction of the top cover and the bottom plate, and only the positions of the first auxiliary insertion tongues and the second auxiliary insertion tongue need to be found from the outside of the box body, the insertion tongues can be pulled out by being gently pushed outwards, and gap insertion opening is not needed.

Description

Technical Field

[0001] This application relates to the field of packaging box technology, and in particular to an airplane box. Background Technology

[0002] Currently, corrugated boxes are a common type of packaging widely used in the transportation and storage of various goods. Traditional corrugated boxes have a simple structure, mainly consisting of a base, top cover, top baffle, and side latches, which are used to close the box. However, with increasing demands for packaging stability in logistics transportation, traditional corrugated boxes are prone to top cover flipping outwards or box deformation due to external forces during transport, affecting the integrity of the packaging and the safety of the goods.

[0003] In the prior art, the existing airplane box includes a box body and a cover plate that closes on the box body. The cover plate has a front buckle plate connected to the end opposite to the box body. Side buckle plates are connected to both sides of the front buckle plate. The two sides of the box body have inner side plates and outer side plates from the inside to the outside. A slot is formed between the inner side plates and the outer side plates for the side buckle plates to be inserted. This solution greatly increases the stability and practicality of the contents.

[0004] Regarding the aforementioned technologies, the main drawback of existing airplane boxes is that they cannot simultaneously ensure both high stability and ease of opening. Solutions that increase the fixing strength often sacrifice the ease of opening, while solutions that emphasize ease of opening are difficult to meet the stability requirements during transportation. Summary of the Invention

[0005] To address the main shortcomings of existing aircraft boxes, which are unable to simultaneously ensure high stability and ease of opening, and the fact that solutions to increase fixing strength often sacrifice ease of opening, this application provides an aircraft box.

[0006] This application provides an aircraft box, which adopts the following technical solution: An aircraft box includes an aircraft box body, which includes a bottom plate, a top cover plate, a top baffle plate, and side tongues. The top baffle plate is connected to the side tongues and the top cover plate. First auxiliary tongues are connected to both sides of the top baffle plate. The aircraft box body is provided with a first annular block for inserting the first auxiliary tongues. A second auxiliary tongue is connected to the side of the top baffle plate away from the top cover plate. A second annular block for inserting the second auxiliary tongue is provided on the bottom plate.

[0007] By adopting the above technical solution, the first auxiliary tongues on both sides of the top baffle are inserted into the first annular block, which can fix the relative position of the top baffle and the box body from the top two sides; the second auxiliary tongue on the other side of the top baffle is inserted into the second annular block of the bottom plate, which forms a "pull-type fixation" from the vertical direction of the top cover and the bottom plate, which is equivalent to forming a triple fixation from "both sides + top and bottom", greatly reducing the probability of the top cover flipping outward and the box body deforming. At the same time, when opening, you only need to find the positions of the first auxiliary tongue and the second auxiliary tongue from the outside of the box body, and gently push outward to pull out the tongue, without the need for gap insertion to open, thereby reducing damage to the aircraft box and making it easier for users to open.

[0008] Preferably, the bottom plate is connected to outer side plates on both the left and right sides, and an inner side plate is connected to the side of the outer side plate away from the bottom plate. A front baffle is connected to the front side of the bottom plate, and a rear baffle is connected to the rear side of the bottom plate. The top cover plate is connected to the bottom plate through the rear baffle. Handle plates are connected to both sides of the front and rear baffles. Side insert plates are connected to both the left and right sides of the top cover plate.

[0009] By adopting the above technical solution, the outer side panels and inner side panels on the left and right sides of the base plate form a "double-layer folding structure". During assembly, the outer side panels can be erected along the edge of the base plate, and the inner side panels are folded inward to fit the inner side of the outer side panels. This is equivalent to forming a "double-layer wall thickness" on the left and right sides of the box. After the front baffle (front side of the base plate) and the rear baffle (rear side of the base plate) are erected, they form a "four-sided enclosure" structure with the outer side panels on the left and right sides, upgrading the base plate from "planar support" to "three-dimensional frame support". This makes the bottom and middle structure of the entire box more stable and reduces the sagging of the base plate caused by the weight of the internal items.

[0010] Preferably, the inner side plate is connected to a buckle on the side away from the outer side plate, and the bottom plate has a slot for cooperating with the buckle.

[0011] By adopting the above technical solution, after the buckle is fixed, one end of the inner side plate is connected to the outer side plate, and the other end is fixed to the bottom plate by the buckle, forming a "triangular support" (the most mechanically stable structure) together with the outer side plate and the bottom plate. This structure can transfer the side force (such as compression and collision) to the bottom plate through the inner side plate, disperse the local pressure, and avoid the side plate from tearing due to excessive force at a single point.

[0012] Preferably, the surface of the outer side plate has a first opening for use with the first auxiliary tongue, and the first auxiliary tongue is inserted into the first opening through the first annular block.

[0013] By adopting the above technical solution, through the cooperation of "first auxiliary tongue → first annular block → first opening", it is equivalent to adding an "anchor point" on each side of the top baffle: after the first auxiliary tongue is inserted into the first opening of the outer side plate, the two sides of the top baffle are firmly fixed to the outer side plate (the edge of the opening forms a lateral limit on the tongue). No matter how the box shakes, the top baffle cannot shift to the left or right, ensuring that the top is always in a tight closed state, and preventing internal items from falling or getting dusty due to the top gap.

[0014] Preferably, the base plate has a second opening for use with the second auxiliary tongue, and the second auxiliary tongue is inserted into the second opening through the second annular block.

[0015] By adopting the above technical solution, through the cooperation of "second auxiliary tongue → second annular block → second opening", it is equivalent to adding a "longitudinal anchor point" between the top baffle and the bottom plate: the tongue first passes through the first annular block (initial positioning), and then inserts into the second opening of the bottom plate (deep fixation). The edge of the opening will form a rigid constraint on the tongue in "up and down + front and back", which completely avoids the displacement of the tongue in the longitudinal direction. Even if the box is subjected to impact from above and below, the top baffle can be firmly "held" to ensure that the top always maintains a stable closed distance with the bottom plate and will not loosen due to external force.

[0016] Preferably, the top baffle has two semi-circular grooves on the side away from the top cover plate, and the semi-circular grooves are symmetrically distributed on the top baffle.

[0017] By adopting the above technical solution, when opening the aircraft box, pushing the first auxiliary tongue and the second auxiliary tongue will cause the top baffle to move and create a gap. Then, the user can open the aircraft box by placing their finger in the semi-circular groove, which makes it easier for the user to open the aircraft box.

[0018] Preferably, a dotted crease is provided at the connection between the outer side panel and the inner side panel, and the dotted crease is used for folding the outer side panel and the inner side panel together.

[0019] By adopting the above technical solution, the dotted crease reduces the rigidity of the material at the connection point by "partially cutting the material fibers". When folding, only a light force is needed to bend naturally along the crease. Users with less strength, such as the elderly and children, can operate it easily. After folding, the crease is flat and wrinkle-free, and the appearance is more regular, making it easier for users to fold.

[0020] In summary, this application includes at least one of the following beneficial technical effects: 1. The first auxiliary tongues on both sides of the top baffle are inserted into the first annular block, which can fix the relative position of the top baffle and the box body from the top sides; the second auxiliary tongue on the other side of the top baffle is inserted into the second annular block of the bottom plate, which forms a "pull-type fixation" from the vertical direction of the top cover and the bottom plate. This is equivalent to forming a triple fixation from "both sides + top and bottom", which greatly reduces the probability of the top cover flipping outward and the box body deforming. At the same time, when opening, you only need to find the position of the first auxiliary tongue and the second auxiliary tongue from the outside of the box body, and gently push outward to pull out the tongue. There is no need to insert it through a gap to open it, thereby reducing damage to the aircraft box and making it easier for users to open. 2. When opening the aircraft box, pushing the first auxiliary tongue and the second auxiliary tongue will cause the top baffle to move and create a gap. Then, the user can open the aircraft box by placing their fingers in the semi-circular groove, which makes it easier for the user to open the aircraft box. 3. The dotted crease reduces the rigidity of the material at the joint by "partially cutting the material fibers". When folding, only a light force is needed to bend naturally along the crease. Users with less strength, such as the elderly and children, can operate it easily. After folding, the crease is flat and wrinkle-free, and the appearance is more regular, making it easier for users to fold. Attached Figure Description

[0021] Figure 1 This is a schematic diagram of the unfolded external structure of the airplane box; Figure 2 This is a schematic diagram of the internal structure of the unfolded airplane box.

[0022] Reference numerals: 100, Airplane box body; 101, Base plate; 102, Top cover plate; 103, Top baffle; 104, Side latch; 105, First auxiliary latch; 106, First annular block; 107, Second auxiliary latch; 108, Second annular block; 109, Outer side plate; 110, Inner side plate; 111, Front baffle; 112, Rear baffle; 113, Handle plate; 114, Side insert plate; 115, Buckle; 116, Locking opening; 117, First opening; 118, Second opening; 119, Semicircular groove; 120, Dashed crease. Detailed Implementation

[0023] The following is in conjunction with the appendix Figure 1 - Appendix Figure 2 This application will be described in further detail.

[0024] This application discloses an airplane box.

[0025] Reference Figure 1An aircraft case includes an aircraft case body 100, wherein the aircraft case body 100 includes a bottom plate 101, a top cover plate 102, a top baffle 103, and side tongues 104. The top baffle 103 is connected to the side tongues 104 and the top cover plate 102. First auxiliary tongues 105 are connected to both sides of the top baffle 103. The aircraft case body 100 is provided with a first annular block 106 for inserting the first auxiliary tongues 105. A second auxiliary tongue 107 is connected to the side of the top baffle 103 away from the top cover plate 102. A second annular block 108 is provided on the bottom plate 101 for inserting the second auxiliary tongue 107. The first auxiliary tongues 106 on both sides of the top baffle 103 are connected to the side tongues 104. The auxiliary tongue 105 is inserted into the first annular block 106, which can fix the relative position of the top baffle 103 and the box body from both sides. The second auxiliary tongue 107 on the other side of the top baffle 103 is inserted into the second annular block 108 of the bottom plate 101, which forms a "pull-type fixation" from the vertical direction of the top cover and the bottom plate 101. This is equivalent to forming a triple fixation from "both sides + top and bottom", which greatly reduces the probability of the top cover flipping outward and the box body deforming. At the same time, when opening, you only need to find the position of the first auxiliary tongue 105 and the second auxiliary tongue 107 from the outside of the box body and gently push outward to pull out the tongue. There is no need to insert it through a gap to open it, thereby reducing damage to the box and making it easier for users to open.

[0026] refer to Figure 1 and Figure 2 The base plate 101 has outer side plates 109 connected to both its left and right sides. An inner side plate 110 is connected to the side of the outer side plate 109 furthest from the base plate 101. A front baffle 111 is connected to the front of the base plate 101, and a rear baffle 112 is connected to the rear of the base plate 101. The top cover plate 102 is connected to the base plate 101 via the rear baffle 112. Handle plates 113 are connected to both sides of the front baffle 111 and the rear baffle 112. Side insert plates 114 are connected to both the left and right sides of the top cover plate 102. The outer side plates 109 and inner side plates 110 on the left and right sides of the base plate 101... The plate 110 forms a "double-layer folding structure". During assembly, the outer plate 109 can be erected along the edge of the bottom plate 101, and the inner plate 110 is folded inward to fit the inner side of the outer plate 109. This is equivalent to the left and right sides of the box forming a "double-layer wall thickness". After the front baffle 111 and the rear baffle 112 are erected, they form a "four-sided enclosure" structure with the outer plates 109 on the left and right sides, upgrading the bottom plate 101 from "planar support" to "three-dimensional frame support", making the bottom and middle structure of the entire box more stable and reducing the sagging of the bottom plate 101 caused by the weight of the internal items.

[0027] refer to Figure 1 and Figure 2The inner side plate 110 is connected to a buckle 115 on the side away from the outer side plate 109. The bottom plate 101 has a slot 116 that works with the buckle 115, and the slot 116 is located at the connection between the outer side plate 109 and the bottom plate 101. After being fixed by the buckle 115, one end of the inner side plate 110 is connected to the outer side plate 109, and the other end is fixed to the bottom plate 101 by the buckle 115, forming a "triangular support" together with the outer side plate 109 and the bottom plate 101. This structure can transfer the lateral force to the bottom plate 101 through the inner side plate 110, disperse the local pressure, and avoid the side plate from tearing due to excessive stress at a single point.

[0028] refer to Figure 1 and Figure 2 The outer side panel 109 has a first opening 117 on its surface that works in conjunction with the first auxiliary tongue 105. The first auxiliary tongue 105 is inserted into the first opening 117 via the first annular block 106. Through the cooperation of "first auxiliary tongue 105 → first annular block 106 → first opening 117", it is equivalent to adding an "anchor point" on each side of the top baffle 103. After the first auxiliary tongue 105 is inserted into the first opening 117 of the outer side panel 109, the two sides of the top baffle 103 are firmly fixed to the outer side panel 109. No matter how the box shakes, the top baffle 103 cannot shift to the left or right, ensuring that the top is always in a tightly closed state and preventing internal items from falling out or getting dusty due to gaps in the top.

[0029] refer to Figure 1 and Figure 2 The base plate 101 has a second opening 118 that works in conjunction with the second auxiliary tongue 107. The second auxiliary tongue 107 is inserted into the second opening 118 through the second annular block 108. Through the cooperation of "second auxiliary tongue 107 → second annular block 108 → second opening 118", it is equivalent to adding a "longitudinal anchor point" between the top baffle 103 and the base plate 101: the tongue first passes through the first annular block 106 and then inserts into the second opening 118 of the base plate 101. The edge of the opening will form a rigid constraint on the tongue in the "up and down + front and back" direction, which completely avoids the displacement of the tongue in the longitudinal direction. Even if the box is subjected to impact from above and below, the top baffle 103 can be firmly "held" to ensure that the top always maintains a stable closed distance with the base plate 101 and will not loosen due to external force.

[0030] refer to Figure 2 Two semi-circular grooves 119 are provided on the side of the top baffle 103 away from the top cover plate 102. The semi-circular grooves 119 are symmetrically distributed on the top baffle 103. When the aircraft box is opened, the top baffle 103 will move and create a gap by pushing the first auxiliary tongue 105 and the second auxiliary tongue 107. Then, the user can open the aircraft box by placing his / her finger in the semi-circular groove 119, which makes it easier for the user to open the aircraft box.

[0031] refer to Figure 2 A dotted crease 120 is provided at the connection between the outer side panel 109 and the inner side panel 110. The dotted crease 120 is used for folding the outer side panel 109 and the inner side panel 110. The dotted crease 120 reduces the rigidity of the material at the connection by "partially cutting the material fibers". When folding, only a little force is needed to bend naturally along the crease. Users with less strength, such as the elderly and children, can operate it easily. After folding, the crease is flat and wrinkle-free, and the appearance is more regular, which makes it easier for users to fold.

[0032] The implementation principle of this application embodiment is as follows: In implementation, the front baffle 111 and the rear baffle 112 are folded inward, then the handle plate 113 is folded inward, then the inner side plate 110 and the outer side plate 109 are folded inward, so that the buckle 115 on the inner side plate 110 is engaged in the slot 116 on the bottom plate 101, then the top cover plate 102 is folded downward, so that the side insert plate 114 is inserted into the box body, the top baffle 103 is folded and located on the front baffle 111, so that the side tongue 104 is inserted into the gap between the folded outer side plate 109 and the inner side plate 110, and then the first auxiliary tongue 105 is inserted into the first annular block 106, with the end of the first auxiliary tongue 105 away from the top baffle 103. Insert the first auxiliary tongue 105 into the first opening 117, and simultaneously insert the second auxiliary tongue 107 on the top baffle 103 into the second annular block 108, and insert the second auxiliary tongue 107 into the second opening 118 to fix the box body, thereby making the connection between the boxes more secure. When opening the carton, the user only needs to push the first auxiliary tongue 105 and the second auxiliary tongue 107, so that the first auxiliary tongue 105 and the second auxiliary tongue 107 push the top baffle 103 to move away from the front baffle 111. Then the user opens the box body through the semi-circular groove 119, which makes it easier for the user to open and avoids the user having to pry open the gap by hand, thus reducing damage to the box body.

[0033] The above are all preferred embodiments of this application, and are not intended to limit the scope of protection of this application. Therefore, all equivalent changes made in accordance with the structure, shape and principle of this application should be covered within the scope of protection of this application.

Claims

1. An airplane case, comprising an airplane case body (100), the airplane case body (100) including a bottom plate (101), a top cover plate (102), a top baffle (103), and a side tongue (104), characterized in that, The top baffle (103) is connected to the side tongue (104), the top baffle (103) is connected to the top cover plate (102), the top baffle (103) is connected to the two sides of the top baffle (103) with first auxiliary tongues (105), the aircraft box body (100) is provided with a first annular block (106) for inserting the first auxiliary tongue (105), the top baffle (103) is connected to the side away from the top cover plate (102) with a second auxiliary tongue (107), and the bottom plate (101) is provided with a second annular block (108) for inserting the second auxiliary tongue (107). The bottom plate (101) is connected to outer side plates (109) on both the left and right sides, and an inner side plate (110) is connected to the side of the outer side plate (109) away from the bottom plate (101). The inner side plate (110) is connected to a buckle (115) on the side away from the outer side plate (109), and the bottom plate (101) is provided with a slot (116) that cooperates with the buckle (115). The outer side plate (109) has a first opening (117) on its surface that is used in conjunction with the first auxiliary tongue (105). The first auxiliary tongue (105) is inserted into the first opening (117) through the first annular block (106). The base plate (101) has a second opening (118) for use with the second auxiliary tongue (107), and the second auxiliary tongue (107) is inserted into the second opening (118) through the second annular block (108).

2. The airplane box according to claim 1, characterized in that, The front side of the base plate (101) is connected to a front baffle (111), the rear side of the base plate (101) is connected to a rear baffle (112), the top cover plate (102) is connected to the base plate (101) through the rear baffle (112), the front baffle (111) and the rear baffle (112) are connected to handle plates (113) on both sides, and the left and right sides of the top cover plate (102) are connected to side insert plates (114).

3. The airplane box according to claim 1, characterized in that, The top baffle (103) has two semi-circular grooves (119) on the side away from the top cover plate (102), and the semi-circular grooves (119) are symmetrically distributed on the top baffle (103).

4. The airplane box according to claim 1, characterized in that, A dotted crease (120) is provided at the connection between the outer side panel (109) and the inner side panel (110), and the dotted crease (120) is used for folding the outer side panel (109) and the inner side panel (110) together.

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