Anti-collision and anti-vibration aviation case
By adopting hinged hinge and splicing structure on the aircraft box, combining engineering plastic materials and multiple functional designs, the problems of traditional aircraft box in terms of maneuverability, loading and unloading convenience and environmental protection are solved, and more efficient collision and shock-proofing are achieved. Effects and lightweight properties.
Patent Information
- Application Number
- CN202421206290.0
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-05-30
- Publication Date
- 2025-01-07
- Estimated Expiration
- 2034-05-30
AI Technical Summary
Traditional anti-collision and shock-proof aircraft boxes have shortcomings in poor maneuverability, inconvenient loading and unloading, unenvironmental protection, single sealing effect and weight increase, and cannot effectively protect high-end products.
A flight box consisting of the upper cover and the lower box is designed, adopting a hinged hinge structure, splicing through the front side plate, the rear side plate, the left side plate, the right side plate and the bottom plate, and grooves are set on the plate, Reinforcement ribs, snaps and wheel compartments are used to enhance structural strength and lightweight properties, while providing detachable and marking area functions.
It achieves better structural strength and lightweight, meets the requirements of anti-collision and shock, and is also characterized by easy loading and unloading, handling and space saving, and is suitable for multiple use.
Smart Images

Figure CN222311181U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of aviation boxes, in particular to an anti-collision and anti-vibration aviation box. Background Art
[0002] With the development of global economic integration and the widespread use of high-tech products, more and more high-end packaging carriers are needed. Traditional packaging products such as wooden boxes and iron boxes have poor mobility, inconvenient loading and unloading, and are not environmentally friendly. They cannot meet the requirements of existing high-end products for packaging carriers. Aviation boxes are mainly widely used in precision instrument industry, exhibition industry, stage lighting industry, LED optoelectronic industry, military industry, medical equipment industry, multimedia audio-visual industry, etc. Some anti-collision and shockproof aviation boxes use a single shock-absorbing spring and waterproof rubber strip for shock absorption and waterproofing, and increase the thickness to increase its anti-collision effect. There are many shortcomings. The single and fixed spring cannot fully protect the items in the aviation box. The sealing effect is single and cannot be effectively waterproofed multiple times. The increased thickness increases the weight of the aviation box, which is not conducive to carrying. For this reason, we propose an anti-collision and shockproof aviation box. Utility Model Content
[0003] The technical problem to be solved by the utility model is to overcome the existing defects and provide an anti-collision and shock-proof aviation box, which can effectively solve the problems in the background technology.
[0004] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: an anti-collision and shock-proof aviation box, comprising an upper cover and a lower box body; the upper cover is hingedly connected to the rear side of the upper surface of the lower box body by a hinge, and is spliced by a front side panel, a rear side panel, a left side panel, a right side panel and a bottom panel, an inwardly recessed cover opening groove is provided on the front side of the upper cover, wheels with brakes are fixedly connected to the four corners of the bottom panel, grooves of different lengths are provided on the inner sides of the upper cover, the front side panel, the rear side panel, the left side panel and the right side panel, and grooves of different lengths are provided on the outer side of the bottom panel.
[0005] Furthermore, a plurality of reinforcing ribs perpendicular to the grooves are provided on the inner side of the upper cover to increase the structural strength.
[0006] Furthermore, the left and right sides and the bottom of the front side panel and the rear side panel are provided with outwardly extending buckles, and correspondingly, the edges of the left side panel, the right side panel and the bottom panel are provided with a plurality of slots, the sides of the front side panel and the rear side panel are respectively connected with the left side panel and the right side panel by buckles, and the bottom is connected with the bottom panel by buckles, and the buckle connection is convenient for assembly and disassembly.
[0007] Furthermore, the upper cover and the lower box body are made of engineering plastics, which are both light and strong.
[0008] Furthermore, inwardly recessed wheel compartments are provided at the four corners of the upper cover, and the size and position of the wheel compartments are adapted to the wheels provided at the lower part of the bottom plate, so as to facilitate the stacking of multiple aviation boxes.
[0009] Furthermore, a plurality of inwardly recessed hasp lock installation positions are provided at the connection between the upper cover and the front side plate for installing the hasp lock.
[0010] Furthermore, a first identification area is provided on the outer side of the front side plate for mounting an identification plate.
[0011] Furthermore, handle grooves are provided on the outer sides of the left side plate and the right side plate, and handles are fixedly provided on the handle grooves to facilitate the transportation of the aviation box.
[0012] Furthermore, a second identification area is provided on the outer sides of the left side plate and the right side plate for installing identification plates.
[0013] Compared with the prior art, the utility model has the following advantages:
[0014] 1. All the upper covers, front side panels, rear side panels, left side panels, right side panels, and the inner or outer sides of the bottom panels are provided with grooves of varying lengths, which can not only reduce the overall finishing, but also increase the structural strength. The whole is made of engineering plastics to meet the requirements of anti-collision and shockproof.
[0015] 2. The lower box body is composed of the front side panel, the rear side panel, the left side panel, the right side panel and the bottom panel. It can be disassembled when not in use, so as not to take up space. BRIEF DESCRIPTION OF THE DRAWINGS
[0016] Figure 1 It is a front view of the utility model;
[0017] Figure 2 It is a bottom view of the utility model;
[0018] Figure 3 It is a top view of the utility model;
[0019] Figure 4 It is a three-dimensional diagram of the utility model;
[0020] Figure 5 The utility model is a cross-sectional view Figure 1 ;
[0021] Figure 6 The utility model is a cross-sectional view Figure 2 .
[0022] In the figure: 1 upper cover, 11 wheel compartment, 2 lower box body, 21 front side panel, 22 rear side panel, 23 left side panel, 24 right side panel, 25 bottom panel, 3 cover opening slot, 4 buckle lock installation position, 5 identification area 1, 6 wheels, 7 handle slot, 8 handle, 9 identification area 2, 10 hinge. DETAILED DESCRIPTION
[0023] 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.
[0024] See also Figure 1-6 The present embodiment provides a technical solution: an anti-collision and shock-proof aviation box, comprising an upper cover 1 and a lower box body 2; the upper cover 1 is hingedly connected to the rear side of the upper surface of the lower box body 2 by a hinge 10, and is spliced by a front side panel 21, a rear side panel 22, a left side panel 23, a right side panel 24 and a bottom panel 25, an inwardly recessed cover opening groove 3 is provided on the front side of the upper cover 1, wheels 6 with brakes are fixedly connected to the four corners of the bottom panel 25, grooves of different lengths are provided on the inner sides of the upper cover 1, the front side panel 21, the rear side panel 22, the left side panel 23 and the right side panel 24, and grooves of different lengths are provided on the outer side of the bottom panel 25.
[0025] Among them, the inner side of the upper cover 1 is also provided with a plurality of reinforcing ribs perpendicular to the groove to increase the structural strength; the left and right sides and the bottom of the front side panel 21 and the rear side panel 22 are provided with buckles extending outward, and correspondingly, the edges of the left side panel 23, the right side panel 24 and the bottom panel 25 are provided with a plurality of slots, and the front side panel 21 and the rear side panel 22 are respectively connected with the left side panel 23 and the right side panel 24 by buckles on both sides, and the bottom is connected with the bottom panel 25 by buckles, which is convenient for assembly and disassembly; the upper cover 1 and the lower box body 2 are made of engineering plastics, which are both light and strong.
[0026] Among them, inwardly recessed wheel compartments 11 are provided at the four corners of the upper cover 1, and the size and position of the wheel compartments 11 are adapted to the wheels 6 provided at the lower part of the bottom plate 25, so as to facilitate the stacking of multiple air boxes; a plurality of inwardly recessed buckle lock installation positions 4 are provided at the connection between the upper cover 1 and the front side plate 21 for installing buckle locks; an identification area 1 5 is provided on the outer side of the front side plate 21 for installing identification plates; handle grooves 7 are provided on the outer sides of the left side plate 23 and the right side plate 24, and handles 8 are fixedly provided on the handle grooves 7 for convenient transportation of the air boxes; an identification area 2 9 is also provided on the outer sides of the left side plate 23 and the right side plate 24 for installing identification plates; an identification area 2 9 is also provided on the outer sides of the left side plate 23 and the right side plate 24 for installing identification plates, and the identification plates can display relevant information of the goods.
[0027] The anti-collision and shockproof aviation box has grooves of different lengths on the inner or outer sides of all panels including the upper cover 1, the front side panel 21, the rear side panel 22, the left side panel 23, the right side panel 24, and the bottom panel 25, which can reduce the overall arrangement and increase the structural strength. The whole is made of engineering plastics to meet the requirements of anti-collision and shockproof. The lower box body 2 is spliced by the front side panel 21, the rear side panel 22, the left side panel 23, the right side panel 24 and the bottom panel 25, which can be disassembled when not in use, so as not to occupy space.
[0028] The above description is only an embodiment of the present invention, and does not limit the patent scope of the present invention. Any equivalent structure or equivalent process transformation made by using the contents of the specification and drawings of the present invention, or directly or indirectly applied in other related technical fields, are also included in the patent protection scope of the present invention.
Claims
1. An anti-collision and shock-proof aviation box, characterized by: The invention comprises an upper cover (1) and a lower box body (2); the upper cover (1) is hingedly connected to the rear side of the upper surface of the lower box body (2) by a hinge (10), and is composed of a front side plate (21), a rear side plate (22), a left side plate (23), a right side plate (24) and a bottom plate (25); an inwardly recessed cover opening groove (3) is provided on the front side of the upper cover (1); wheels (6) with brakes are fixedly connected at the four corners of the bottom plate (25); grooves of different lengths are provided on the inner sides of the upper cover (1), the front side plate (21), the rear side plate (22), the left side plate (23) and the right side plate (24); and grooves of different lengths are provided on the outer side of the bottom plate (25).
2. The anti-collision and anti-vibration aviation box according to claim 1, characterized in that: The inner side of the upper cover (1) is also provided with a plurality of reinforcing ribs perpendicular to the groove.
3. The anti-collision and anti-vibration aviation box according to claim 1, characterized in that: The left and right sides and the bottom of the front side plate (21) and the rear side plate (22) are provided with buckles extending outward, and correspondingly, the edges of the left side plate (23), the right side plate (24) and the bottom plate (25) are provided with a plurality of buckle grooves, and the two sides of the front side plate (21) and the rear side plate (22) are respectively connected with the left side plate (23) and the right side plate (24) by buckles, and the bottom is connected with the bottom plate (25) by buckles.
4. The anti-collision and anti-vibration aviation box according to claim 1, characterized in that: The upper cover (1) and the lower box body (2) are made of engineering plastics.
5. The anti-collision and anti-vibration aviation box according to claim 1, characterized in that: Inwardly recessed wheel compartments (11) are arranged at the four corners of the upper cover (1), and the size and position of the wheel compartments (11) are adapted to the wheels (6) arranged at the lower part of the bottom plate (25).
6. The anti-collision and anti-vibration aviation box according to claim 1, characterized in that: A plurality of inwardly recessed hasp lock installation positions (4) for installing locks are provided at the connection between the upper cover (1) and the front side plate (21).
7. The anti-collision and anti-vibration aviation box according to claim 1, characterized in that: A marking area 1 (5) is arranged on the outer side of the front side plate (21).
8. The anti-collision and anti-vibration aviation box according to claim 1, characterized in that: The outer sides of the left side plate (23) and the right side plate (24) are both provided with a handle groove (7), and a handle (8) is fixedly provided on the handle groove (7).
9. The anti-collision and anti-vibration aviation box according to claim 8, characterized in that: The outer sides of the left side plate (23) and the right side plate (24) are also provided with a marking area 2 (9).