Aircraft case with anti-collision structure

Abstract

The utility model discloses an aviation case with anti -collision structure belongs to the technical field of aviation case, and its technical scheme main points include protection subassembly, anti -collision subassembly and aviation case main part, the protection subassembly sets up the surface of aviation case main part, the anti -collision subassembly sets up the inside of aviation case main part, through the setting of protection subassembly, protection subassembly can reach the effect that the aviation case main part is protected, and can be to the storage box and can be positioned handle, through the setting of anti -collision subassembly, anti -collision subassembly can reach the effect that the storage box of the storage article is provided with the buffer, thereby reduced the harm that aviation case main part is hit, thereby solved the existing traditional aviation case mostly are simple box, and mostly only through the material property of itself and provided the effect of shockproof, anti -collision for aviation case, however, the effect provided by the characteristic of material itself alone, thereby caused the problem of limited anti -collision effect.

Description

Technical Field

[0001] This utility model relates to the technical field of flight cases, and in particular to a flight case with an anti-collision structure. Background Technology

[0002] Flight cases are a new type of packaging product developed to address the problems of traditional simple wooden box packaging and transportation being unable to effectively protect high-tech products and having poor mobility. The exterior is made of multi-layer plywood bonded with ABS fireproof board and aluminum alloy frame structure, and the interior is equipped with EVA shockproof material and adjustable partitions, which have waterproof, fireproof and shockproof functions.

[0003] Most existing traditional flight cases are simple cases, and they mostly rely on the properties of their materials to provide shock and impact protection. However, the impact protection effect is limited due to the properties of the materials themselves alone.

[0004] Therefore, an aircraft case with an anti-collision structure is proposed. Utility Model Content

[0005] The purpose of this utility model is to provide a flight case with an anti-collision structure, which can solve the problem that most existing traditional flight cases are simple boxes, and most of them only rely on the material properties of the material itself to provide shock and impact protection. However, the impact protection effect is limited due to the limited effect provided by the material properties alone.

[0006] To achieve the above objectives, this utility model provides the following technical solution: a flight case with an anti-collision structure, comprising a protective component, an anti-collision component, and a flight case body. The protective component is disposed on the surface of the flight case body, and the anti-collision component is disposed inside the flight case body. The protective component includes a cushioning sponge, a slider, a storage box, and a protective pad. The cushioning sponge is fixedly connected to both sides inside the flight case body. The slider is fixedly connected to the front and rear sides of the storage box. The storage box is movably connected inside the flight case body. The protective pad is fitted onto the surface of the flight case body.

[0007] Preferably, the anti-collision component includes a buffer telescopic plate, which is fixedly connected to both sides of the storage box. A connecting plate is fixedly connected to the outer side of the buffer telescopic plate, and the outer side of the connecting plate is fixedly connected to both sides inside the main body of the flight case. A buffer pad is fixedly connected to the inner side of the connecting plate.

[0008] Preferably, a first rotating component is fixedly connected to both the front and rear sides of the connecting plate, and a rotating plate is rotatably connected to the surface of the first rotating component.

[0009] Preferably, a second rotating component is rotatably connected inside the rotating plate, and a connecting block is fixedly connected to the inner side of the second rotating component.

[0010] Preferably, the storage box has limiting grooves on both sides, and the inside of the limiting grooves is slidably connected to the inside of the connecting block.

[0011] Preferably, a protective pad is fixedly connected to the inner wall of the limiting groove, and the inner side of the protective pad is in contact with the outer side of the connecting block.

[0012] Preferably, the front and rear sides of the interior of the flight case body are provided with sliding grooves, and the interior of the sliding grooves is slidably connected to the surface of the slider.

[0013] Preferably, the cushioning sponge has grooves on both sides, and the interior of the grooves is movably connected to the surface of the connecting plate.

[0014] Compared with the prior art, the beneficial effects of this utility model are:

[0015] 1. In this application, by setting up protective components, the protective components can achieve the effect of protecting the main body of the flight case and can also limit the position of the storage box;

[0016] 2. In this application, by setting up anti-collision components, the anti-collision components can provide a cushioning effect for the storage box containing the items, thereby reducing the damage to the main body of the flight case from impact. Attached Figure Description

[0017] Figure 1 This is an overall structural diagram of the flight case with an anti-collision structure according to this utility model;

[0018] Figure 2 This is a schematic diagram showing the connection between the protective component and the anti-collision component of this utility model;

[0019] Figure 3 This is a schematic diagram of the connection of the protective components of this utility model;

[0020] Figure 4 This is a connection diagram of the anti-collision component of this utility model;

[0021] Figure 5 This is a schematic diagram showing the connection of the limiting groove, protective pad, and sliding groove of this utility model.

[0022] In the diagram, 1. Protective component; 101. Buffer sponge; 102. Slider; 103. Storage box; 104. Protective pad; 2. Anti-collision component; 201. Buffer telescopic plate; 202. Connecting plate; 203. Buffer pad; 204. First rotating component; 205. Rotating plate; 206. Second rotating component; 207. Connecting block; 3. Flight case body; 4. Limiting groove; 5. Protective pad; 6. Slide groove; 7. Groove. Detailed Implementation

[0023] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0024] Please see Figure 1-5 The present invention provides the following technical solution:

[0025] A flight case with an anti-collision structure includes a protective component 1, an anti-collision component 2, and a flight case body 3. The protective component 1 is disposed on the surface of the flight case body 3, and the anti-collision component 2 is disposed inside the flight case body 3. The protective component 1 includes a cushioning sponge 101, a slider 102, a storage box 103, and a protective pad 104. The cushioning sponge 101 is fixedly connected to both sides inside the flight case body 3, the slider 102 is fixedly connected to the front and rear sides of the storage box 103, the storage box 103 is movably connected to the inside of the flight case body 3, and the protective pad 104 is sleeved on the surface of the flight case body 3.

[0026] In this embodiment: the protective component 1 can protect the main body 3 of the flight case and limit the storage box 103. The anti-collision component 2 can provide a buffer for the storage box 103, thereby reducing the impact damage to the main body 3 of the flight case. The cushioning sponge 101 can provide a buffer for the storage box 103. The slider 102 can limit the storage box 103. The storage box 103 can provide storage adjustment for items. The storage box 103 is an existing storage device with a built-in strap limiting structure. The protective pad 104 can provide protection for the surface of the main body 3 of the flight case.

[0027] Specifically, such as Figure 4 As shown, the anti-collision component 2 includes a buffer telescopic plate 201, which is fixedly connected to both sides of the storage box 103. A connecting plate 202 is fixedly connected to the outer side of the buffer telescopic plate 201. The outer side of the connecting plate 202 is fixedly connected to both sides inside the flight case body 3. A buffer pad 203 is fixedly connected to the inner side of the connecting plate 202.

[0028] Specifically, such as Figure 4 As shown, the front and rear sides of the connecting plate 202 are fixedly connected to the first rotating member 204, and the surface of the first rotating member 204 is rotatably connected to the rotating plate 205.

[0029] Specifically, such as Figure 4 As shown, a second rotating component 206 is rotatably connected inside the rotating plate 205, and a connecting block 207 is fixedly connected to the inner side of the second rotating component 206.

[0030] In this embodiment: the buffer telescopic plate 201 is an existing telescopic device with a built-in reset buffer spring, and it can connect to the connecting plate 202. The connecting plate 202 can connect the buffer pad 203 and the first rotating member 204. The buffer pad 203 can prevent strong collisions between the buffer telescopic plate 201 and the connecting plate 202. The first rotating member 204 can connect to the rotating plate 205. The rotating plate 205 can connect to the second rotating member 206. The second rotating member 206 can connect to the connecting block 207. The connecting block 207 can limit the position of the connecting plate 202.

[0031] Specifically, such as Figure 5 As shown, the storage box 103 has limit grooves 4 on both sides, and the inside of the limit grooves 4 is slidably connected to the inside of the connecting block 207.

[0032] Specifically, such as Figure 5 As shown, a protective pad 5 is fixedly connected to the inner wall of the limiting groove 4, and the inner side of the protective pad 5 is in contact with the outer side of the connecting block 207.

[0033] In this embodiment: by setting the limiting groove 4, the limiting groove 4 can achieve the effect of limiting the sliding connection of the connecting block 207; by setting the protective pad 5, the protective pad 5 can achieve the effect of protecting the connecting block 207.

[0034] Specifically, such as Figure 5 As shown, the front and rear sides of the interior of the flight case body 3 are provided with sliding grooves 6, and the interior of the sliding grooves 6 is slidably connected to the surface of the slider 102.

[0035] Specifically, such as Figure 3 As shown, the cushioning sponge 101 has slots 7 on both sides, and the interior of the slots 7 is movably connected to the surface of the connecting plate 202.

[0036] In this embodiment: by setting the slide groove 6, the slide groove 6 can achieve the effect of limiting the sliding connection of the slider 102; by setting the slot 7, the slot 7 can achieve the effect of providing conditions for the connection between the storage box 103 and the flight case body 3.

[0037] Working principle: First, when the flight case body 3 is impacted by external forces, the protective pad 104 on its surface provides a certain buffering effect, thereby reducing the impact damage to the flight case body 3. Then, when the impact is transmitted to the interior of the flight case body 3, the internal buffer sponge 101 provides a certain protection for the storage box 103. At the same time, the connecting plate 202, when impacted, presses against the buffer telescopic plate 201, which in turn allows the buffer telescopic plate 201 to reduce the impact through its internal spring. Through repeated elimination of the impact force by the buffering force, the impact on the flight case body 3 is minimized. In addition, the straps inside the storage box 103 limit the movement of items, thereby greatly reducing the damage to the items and providing strong protection for the flight case body 3.

[0038] The above are merely preferred embodiments of the present utility model and are not intended to limit the present utility model. Any modifications, equivalent substitutions, and improvements made within the spirit and principles of the present utility model should be included within the protection scope of the present utility model.

Claims

1. A flight case with an anti-collision structure, comprising a protective component (1), an anti-collision component (2), and a flight case body (3), characterized in that: The protective component (1) is disposed on the surface of the flight case body (3), and the anti-collision component (2) is disposed inside the flight case body (3). The protective component (1) includes a cushioning sponge (101), a slider (102), a storage box (103), and a protective pad (104). The cushioning sponge (101) is fixedly connected to both sides inside the flight case body (3). The slider (102) is fixedly connected to the front and rear sides of the storage box (103). The storage box (103) is movably connected inside the flight case body (3). The protective pad (104) is fitted onto the surface of the flight case body (3).

2. The flight case with an anti-collision structure according to claim 1, characterized in that: The anti-collision component (2) includes a buffer telescopic plate (201), which is fixedly connected to both sides of the storage box (103). A connecting plate (202) is fixedly connected to the outer side of the buffer telescopic plate (201), and the outer side of the connecting plate (202) is fixedly connected to both sides inside the flight case body (3). A buffer pad (203) is fixedly connected to the inner side of the connecting plate (202).

3. The flight case with an anti-collision structure according to claim 2, characterized in that: The front and rear sides of the connecting plate (202) are fixedly connected to a first rotating member (204), and a rotating plate (205) is rotatably connected to the surface of the first rotating member (204).

4. The flight case with an anti-collision structure according to claim 3, characterized in that: The rotating plate (205) is rotatably connected to a second rotating component (206), and a connecting block (207) is fixedly connected to the inner side of the second rotating component (206).

5. The flight case with an anti-collision structure according to claim 4, characterized in that: The storage box (103) has limiting grooves (4) on both sides, and the inside of the limiting grooves (4) is slidably connected to the inside of the connecting block (207).

6. The flight case with an anti-collision structure according to claim 5, characterized in that: The inner wall of the limiting groove (4) is fixedly connected with a protective pad (5), and the inner side of the protective pad (5) is in contact with the outer side of the connecting block (207).

7. The flight case with an anti-collision structure according to claim 1, characterized in that: The front and rear sides of the interior of the flight case body (3) are provided with sliding grooves (6), and the interior of the sliding grooves (6) is slidably connected to the surface of the slider (102).

8. The flight case with an anti-collision structure according to claim 2, characterized in that: The buffer sponge (101) has slots (7) on both sides, and the interior of the slots (7) is movably connected to the surface of the connecting plate (202).

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