Air-drop box body of unmanned offender

Abstract

The utility model relates to an unmanned attacker air-drop box body, which comprises a shell and a shell cover, the shell cover is detachable relative to the shell, a built-in assembly is arranged in the shell, the built-in assembly comprises a lining group and a cellular board group, and the cellular board group is wrapped outside the lining group. The built-in assembly formed by combining the cellular board set and the lining set is arranged in the shell, the lining set is wrapped and covered through the cellular board set, kinetic energy is absorbed, and meanwhile the lining set is buffered; and the lining group is formed by combining the first lining and the second lining, so that the attacker and the matching of the attacker are protected and are convenient to place and take, and the timeliness of use is improved.

Description

TECHNICAL FIELD

[0001] The utility model relates to military technology field especially, relate to a kind of unmanned attack aircraft air-drop box. BACKGROUND

[0002] Attack aircraft air-drop box, usually refers to in military operation, from air drop is loaded with attack aircraft equipment and supporting, therefore attack aircraft air-drop box has extensive application prospect and important strategic value in military operation. They not only provide an efficient, fast means of material supply and tactical deployment, but also provide flexible and diverse combat options and support methods for troops. With the continuous progress of science and technology and the continuous change of military demand, the application of attack aircraft air-drop box will be more extensive and in-depth, but this box design has its specific function and requirement to ensure safety, stability and practicability in air-drop process and after landing. SUMMARY

[0003] In view of the above-mentioned prior art defects, the utility model aims at providing a kind of unmanned attack aircraft air-drop box to solve one or more problems in prior art.

[0004] To achieve the above-mentioned purpose, the technical scheme of the utility model is as follows:

[0005] A kind of unmanned attack aircraft air-drop box, including shell and shell cover, the shell cover is detachable relative to the shell, inner component is provided in the shell, the inner component includes inner lining group and honeycomb plate group, the honeycomb plate group is wrapped in the inner lining group.

[0006] Further, the inner lining group includes first inner lining and second inner lining, the first inner lining and the second inner lining are sequentially arranged along the first direction.

[0007] Further, the first inner lining surface is respectively provided with first recess, second recess and third recess.

[0008] Further, the first inner lining surface is also provided with first protruding portion and fourth recess, the first protruding portion is matched in the fourth recess.

[0009] Further, the first inner lining surface is also provided with through hole, the through hole penetrates the first inner lining along the first direction.

[0010] Further, the second inner lining surface is provided with aperture.

[0011] Further, the honeycomb plate group includes first honeycomb plate and second honeycomb plate;The first honeycomb plate and the second honeycomb plate are respectively arranged along the second direction and third direction and are abutted to the shell surface.

[0012] Further, the honeycomb plate group further comprises a third honeycomb plate, which is arranged in parallel to the inner lining group and connected to the first honeycomb plate and the second honeycomb plate.

[0013] Further, the box further comprises an induction port, which is arranged on the shell cover.

[0014] Further, the shell cover is further provided with a ventilation hole.

[0015] Compared with the prior art, the beneficial technical effects of the utility model are as follows:

[0016] The utility model discloses a shell body is arranged with the inner package component formed by the honeycomb plate group and the inner lining group combination in the shell body, and the honeycomb plate group is covered to the inner lining group, and the inner lining group is protected while being convenient to take out by the first inner lining and the second inner lining combination, and the utility model discloses a kind of unmanned attack aircraft air-drop box body. BRIEF DESCRIPTION OF DRAWINGS

[0017] Figure 1 An unmanned attack aircraft air-drop box body structure explosion schematic diagram of an embodiment of the utility model is shown.

[0018] Figure 2 A first inner lining structure schematic diagram of an embodiment of the utility model is shown. Figure I .

[0019] Figure 3 A first inner lining structure schematic diagram of an embodiment of the utility model is shown. Figure II .

[0020] Mark in drawing: 1, shell body;2, shell cover;201, ventilation hole;3, inner package component;301, inner lining group;3011, first inner lining;30111, first recess;30112, second recess;30113, third recess;30114, first protruding portion;30115, fourth recess;30116, through hole;3012, second inner lining;30121, orifice;302, honeycomb plate group;3021, first honeycomb plate;3022, second honeycomb plate;3023, third honeycomb plate;4, induction port. DETAILED DESCRIPTION

[0021] In order to make the purpose, technical scheme and advantages of the utility model more clearly, the following will make further detailed description of the utility model of a kind of unmanned attack aircraft air-drop box body combining with the drawings and specific implementation. According to the following description, the advantages and features of the utility model will be more clearly. It should be noted that the drawings are very simplified and all use non-precise scale, the orientation or position relationship indicated by the terms "center", "lateral", "length", "width", "height", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "side" and the like are based on the orientation or position relationship shown in the drawings, not indicating or implying that the indicated unmanned attack aircraft air-drop box body or element must have a particular orientation, be constructed and operated in a particular orientation, so it cannot be understood as a limitation on the utility model, only for the purpose of conveniently and clearly assisting in the description of the utility model implementation. In order to make the purpose, features and advantages of the utility model more obvious and easy to understand, please refer to the drawings.

[0022] It should be understood that the structures, proportions, sizes and the like shown in the drawings attached to the specification are only used to cooperate with the content disclosed in the specification for understanding and reading by those skilled in the art, and are not used to limit the implementation of the utility model, so they do not have technical significance, any modification of structure, change of proportion relationship or adjustment of size, without affecting the effect and purpose that the utility model can produce, should still fall within the scope covered by the technical content disclosed by the utility model.

[0023] The specific structure of the unmanned attack aircraft air-drop box body is described below:

[0024] Please refer to Figures 1 to 3 The attack aircraft air-drop box body of the embodiment includes a shell 1 and a shell cover 2, the shell cover 2 is detachable relative to the shell 1, an inner assembly 3 is arranged in the shell 1, the inner assembly 3 includes an inner lining assembly 301 and a honeycomb plate assembly 302, the honeycomb plate assembly 302 is wrapped outside the inner lining assembly 301 to protect the inner lining assembly 301.

[0025] Further, the inner lining assembly 301 includes a first inner lining 3011 and a second inner lining 3012, the first inner lining 3011 and the second inner lining 3012 are sequentially arranged along a first direction. Preferably, a plurality of first inner linings 3011 and one second inner lining 3012 are arranged in the embodiment, and the second inner lining 3012 is arranged at the uppermost position of the shell 1.

[0026] Further, the first inner liner 3011 is provided with a first recessed part 30111, a second recessed part 30112 and a third recessed part 30113. Preferably, the first recessed part 30111 is used for placing an attacking machine, the second recessed part 30112 is used for placing a battery, and the third recessed part 30113 is used for placing a fuse.

[0027] Further, the first inner liner 3011 is provided with a first protruding part 30114 and a fourth recessed part 30115. The first protruding part 30114 is arranged on the upper surface of the first inner liner 3011, and the fourth recessed part 30115 is arranged on the lower surface of the first inner liner 3011. The first protruding part 30114 is matched with the fourth recessed part 30115, thereby achieving stacking of the first inner liner 3011.

[0028] Further, the first inner liner 3011 is provided with a through hole 30116 penetrating the first inner liner 3011 along a first direction. Preferably, the through hole 30116 is used for placing a cannonball.

[0029] Further, the second inner liner 3012 is provided with an aperture 30121 for facilitating taking of the second inner liner 3012.

[0030] Further, the honeycomb plate group 302 includes a first honeycomb plate 3021 and a second honeycomb plate 3022 arranged along a second direction and a third direction respectively and abutting against the surface of the shell 1. Preferably, in the embodiment, the first direction and the second direction are the long side direction and the short side direction of the shell 1 respectively.

[0031] Further, the honeycomb plate group 302 further includes a third honeycomb plate 3023 arranged parallel to the inner liner group 301 and connected to the first honeycomb plate 3021 and the second honeycomb plate 3022, i.e. arranged on the bottom surface of the shell 1.

[0032] Further, the box further includes an induction port 4 arranged on the shell cover 2 for inducing and capturing the real-time logistics state of the box. The shell cover 2 is further provided with a ventilation hole 201 for balancing the storage environment inside the shell 1.

[0033] Any combination of the technical features in the above-described embodiments can be made. In order to make the description concise, all possible combinations of the technical features in the above-described embodiments are not described, however, as long as the combination of the technical features does not exist, it should be considered as the scope of the description.

[0034] The above-described embodiments only express several implementation manners of the utility model, the description is more specific and detailed, but can not therefore be understood as the limitation of the utility model patent range. It should be pointed out that for ordinary skilled person in the art, without departing from the utility model concept, several modifications and improvements can be made, which belong to the protection range of the utility model. Therefore, the protection range of the utility model patent should be subject to the appended claims.

Claims

1. A drop container for an unmanned attack aircraft, comprising a shell and a cover, wherein the cover is detachable relative to the shell, characterized in that: The housing is provided with an internal assembly, which includes an inner liner assembly and a honeycomb panel assembly, with the honeycomb panel assembly enclosing the inner liner assembly. The inner liner assembly includes a first inner liner and a second inner liner, which are arranged sequentially along a first direction. The surface of the first inner liner is provided with a first recess, a second recess, and a third recess. The surface of the first inner liner is also provided with a first protrusion and a fourth recess, with the first protrusion engaging with the fourth recess. The surface of the first inner liner is also provided with a through hole, which penetrates the first inner liner along the first direction. The surface of the second inner liner is provided with an opening.

2. The unmanned attack aircraft airdrop container as described in claim 1, characterized in that: The honeycomb panel assembly includes a first honeycomb panel and a second honeycomb panel; the first honeycomb panel and the second honeycomb panel are respectively disposed along a second direction and a third direction and abut against the surface of the housing.

3. The unmanned attack aircraft airdrop container as described in claim 2, characterized in that: The honeycomb panel assembly further includes a third honeycomb panel, which is arranged parallel to the inner lining assembly and connected to the first honeycomb panel and the second honeycomb panel.

4. The unmanned attack aircraft airdrop container as described in claim 3, characterized in that: The enclosure also includes a sensing port, which is located on the cover.

5. The unmanned attack aircraft airdrop container as described in claim 4, characterized in that: The cover is also provided with ventilation holes.

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