Material box structure, aircraft and ground carrier

By designing a detachable and connected material box structure, the problem of inconvenient transportation of agricultural drone load boxes is solved, and the stable stacking of material shells and efficient crop sowing is achieved.

CN223072750UActive Publication Date: 2025-07-08GUANGZHOU XAIRCRAFT TECH CO LTD
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Patent Information

Application Number
CN202422409500.2
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-09-30
Publication Date
2025-07-08
Estimated Expiration
2034-09-30

AI Technical Summary

Technical Problem

The existing agricultural drone load box is huge and cannot be disassembled, resulting in inconvenient transportation and increased costs.

Method used

A material box structure is designed, the material shell and the mounting piece are removably connected, and the open cross-sectional area is greater than the bottom cross-sectional area, allowing the material shell to be stable stacked, and the assembly efficiency and stability are improved through the guide structure and positioning coordination.

Benefits of technology

It realizes stable stacking of material shells, effectively utilizes storage space, reduces transportation costs, and improves crop sowing efficiency through aircraft and ground vehicles.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model provides a workbin structure, an aircraft and a ground carrier, and relates to the technical field of aircrafts. The material box structure comprises a mounting piece and a material shell. The material shells are detachably connected with the mounting pieces, openings are formed in the tops of the material shells, and the cross sectional area of the openings is larger than that of the bottoms of the material shells, so that the at least two material shells can be stacked along the openings in the state that the material shells are not connected with the mounting pieces. The mounting piece is mounted on the flying machine body or the carrier, so that the mounting piece and the material shell are driven to move through the flying machine body or the carrier, and material transportation is facilitated; the material shell and the mounting piece are connected in a separable joint mode, so that the mounting set and the material shell can be conveniently and independently disassembled; the material shells are used for containing materials, in addition, the cross sectional area of the openings of the material shells is larger than that of the bottoms of the material shells, so that the at least two material shells can be stably stacked along the openings in the state that the material shells are not connected with the mounting pieces, the storage space is effectively utilized, and the transportation cost is reduced.
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Description

Technical Field

[0001] The utility model relates to the technical field of aircraft, and more specifically, to a material box structure, an aircraft and a ground vehicle. Background Art

[0002] Currently, the load boxes used in the execution systems of agricultural drones are generally integrally formed through processes such as blow molding. However, due to their large volume and inability to be disassembled, these boxes do not have stackability, which causes inconvenience during transportation and significantly increases the cost burden. Summary of the Utility Model

[0003] The utility model provides a material box structure, an aircraft and a ground vehicle, which can achieve stable stacking of multiple material shells, thereby effectively utilizing storage space and reducing transportation costs.

[0004] Embodiments of the utility model can be implemented as follows:

[0005] In a first aspect, the utility model provides a material box structure, including:

[0006] A mounting member;

[0007] A material shell, which is detachably connected to the mounting member. An opening is provided at the top of the material shell, and the cross-sectional area of the opening is larger than that of the bottom of the material shell, so that at least two material shells can be stacked along the opening without connecting to the mounting member.

[0008] In an alternative embodiment, the mounting member is detachably connected to the opening.

[0009] In an alternative embodiment, the mounting member is detachably connected to the outer side wall of the material shell.

[0010] In an alternative embodiment, the size of the material shell decreases along the direction from the opening towards the bottom of the material shell.

[0011] In an alternative embodiment, the side wall of the material shell has a stepped structure with gradually decreasing dimensions.

[0012] In an alternative embodiment, the outer side wall of the material shell has an arc-shaped surface structure with gradually decreasing dimensions.

[0013] In an alternative embodiment, a discharge port is provided at the bottom of the material shell.

[0014] In an alternative embodiment, when the mounting member is connected to the opening, the mounting member covers a part of the opening, and the un-covered part of the opening forms the feed port of the material shell.

[0015] In an alternative embodiment, the mounting member is connected to the middle of the open end to form the feed ports on both sides of the mounting member.

[0016] In an alternative embodiment, the side wall of the material housing is provided with a guiding structure so that a plurality of the material housings can be stacked in a guided manner when stacked.

[0017] In an alternative embodiment, the mounting member is provided with a first positioning portion, and the material housing is provided with a second positioning portion;

[0018] The first positioning portion is a groove, the second positioning portion is a protrusion, and the second positioning portion can be embedded in the first positioning portion; or, the first positioning portion is a protrusion, the second positioning portion is a groove, and the first positioning portion can be embedded in the second positioning portion.

[0019] In an alternative embodiment, the mounting member is provided with a first mounting hole, and the material housing is provided with a second mounting hole. When the first positioning portion and the second positioning portion are in cooperation, the first mounting hole and the second mounting hole are correspondingly arranged, and the first mounting hole and the second mounting hole are used for installing fasteners.

[0020] In an alternative embodiment, the first mounting hole is located in the first positioning portion, and the second mounting hole is located in the second positioning portion.

[0021] In an alternative embodiment, a flanging away from the open end direction is provided at the top edge of the material housing.

[0022] In an alternative embodiment, the material housing is further provided with a plurality of support ribs, the plurality of support ribs are spaced apart, and the plurality of support ribs are all connected to the flanging and extend along the direction from the open end towards the bottom of the material housing.

[0023] In an alternative embodiment, the material housing is further provided with a strengthening structure, the strengthening structure is recessed on the outer side wall of the material housing, and the strengthening structure extends along the direction from the open end towards the bottom of the material housing.

[0024] In an alternative embodiment, the mounting member is provided with a first overlapping portion, and the material housing is provided with a second overlapping portion. The first overlapping portion includes a limiting portion and a covering edge connected to each other. The limiting portion abuts against the inner wall of the second overlapping portion, and the covering edge abuts against the top edge of the second overlapping portion.

[0025] In a second aspect, the present invention provides an aircraft, including a flying body and the material tank structure according to any one of the foregoing embodiments, and the flying body is connected to the mounting member.

[0026] In a third aspect, the present utility model provides a ground vehicle, which includes a carrier and a material box structure as described in any one of the foregoing embodiments, and the carrier is connected to the mounting member.

[0027] The beneficial effects of the material box structure, the aircraft and the ground vehicle provided by the embodiments of the present utility model include: the mounting member is installed on the aircraft body so that the mounting member and the material box can be driven by the aircraft body to fly, which facilitates the transportation of materials; the material shell is connected to the mounting member in a separable joint manner, so that it is convenient to separately disassemble and install the assembly and the material shell, and the material shell and the mounting member can also be made of different materials according to the use requirements to improve the structural stability and strength of the material box structure; the function of the material shell is to hold materials, and an opening is provided at the top of the material shell to facilitate the material shell to hold materials; in addition, the cross-sectional area of the opening of the material shell is larger than the cross-sectional area of the bottom of the material shell, so that at least two material shells can be stably stacked along the opening in a state of not being connected to the mounting member, thereby effectively utilizing the storage space and reducing the transportation cost. BRIEF DESCRIPTION OF THE DRAWINGS

[0028] In order to more clearly illustrate the technical solutions of the embodiments of the present utility model, the drawings required to be used in the embodiments will be briefly introduced below. It should be understood that the following drawings only show some embodiments of the present utility model, and thus should not be regarded as limiting the scope. For those of ordinary skill in the art, other related drawings can be obtained based on these drawings without creative efforts.

[0029] Figure 1 is an exploded view of the material box structure provided by the embodiment of the present utility model from the first perspective;

[0030] Figure 2 is an exploded view of the material box structure provided by the embodiment of the present utility model from the second perspective;

[0031] Figure 3 is a schematic diagram of the stacked state of the material shells provided by the embodiment of the present utility model;

[0032] Figure 4 is provided by the embodiment of the present utility model Figure 2 partial enlarged view;

[0033] Figure 5 is a schematic diagram of the structure of the material shell provided by the embodiment of the present utility model;

[0034] Figure 6 is provided by the embodiment of the present utility model Figure 5 partial enlarged view;

[0035] Figure 7 is one of the schematic diagrams of the outline of the material shell provided by the embodiment of the present utility model;

[0036] Figure 8 This is the second schematic diagram of the outline of the material shell provided by the embodiment of the present utility model.

[0037] Icon: 10 - bin structure; 100 - mounting part; 110 - first positioning part; 120 - first mounting hole; 130 - first overlapping part; 131 - limiting part; 132 - cover edge; 200 - material shell; 210 - open end; 211 - feed port; 220 - second positioning part; 230 - second mounting hole; 240 - flanging; 250 - support rib; 260 - strengthening structure; 270 - second overlapping part; 280 - discharge port; 290 - guiding structure. Specific embodiments

[0038] To make the objectives, technical solutions, and advantages of the embodiments of the present utility model clearer, the technical solutions in the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model. Apparently, the described embodiments are some, but not all, of the embodiments of the present utility model. Generally, the components of the embodiments of the present utility model described and illustrated in the accompanying drawings here can be arranged and designed in various different configurations.

[0039] Therefore, the following detailed description of the embodiments of the present utility model provided in the accompanying drawings is not intended to limit the scope of the claimed present utility model, but merely represents selected embodiments of the present utility model. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present utility model without creative efforts shall fall within the scope of protection of the present utility model.

[0040] It should be noted that similar reference numerals and letters denote similar items in the following drawings. Therefore, once an item is defined in one drawing, it does not need to be further defined and explained in subsequent drawings.

[0041] In the description of the present utility model, it should be noted that if terms such as "upper", "lower", "inner", "outer", etc. are used to indicate the orientation or positional relationship, it is based on the orientation or positional relationship shown in the accompanying drawings or the orientation or positional relationship in which the product of the present utility model is usually placed during use. It is only for the convenience of describing the present utility model and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus should not be construed as a limitation to the present utility model.

[0042] In addition, if terms such as "first" and "second" are used only for differential description and cannot be construed as indicating or implying relative importance.

[0043] It should be noted that the features in the embodiments of the present utility model can be combined with each other without conflict.

[0044] Currently, the load boxes adopted in the agricultural drone execution system are generally integrally formed by processes such as blow molding. However, due to their large volume and inability to be disassembled, these boxes do not have stackability, resulting in inconvenience during transportation and significantly increasing the cost burden.

[0045] Based on the above problems, the embodiments of the present utility model provide an aircraft for drones, especially applicable to the field of agricultural equipment. Sowing can be carried out through this aircraft, which is convenient, fast and efficient, significantly improving the operation efficiency.

[0046] Specifically, the aircraft includes a flight body and a material box structure. The flight body is connected to a mounting member. The material box structure can be used to load agricultural crops such as seedlings. The flight body drives the material box structure to fly and completes the spreading action through the material box structure during flight, significantly improving the agricultural operation efficiency.

[0047] Optionally, the flight body can be a rotary-wing drone, specifically a quadcopter drone. Of course, it can also be a single-rotor drone, a dual-rotor drone, a hexacopter drone, an octocopter drone, etc. The flight body can operate automatically according to a preset path, flight speed, attitude, etc., or be manually controlled by an operator.

[0048] In addition, the embodiments of the present utility model also provide a ground vehicle. The ground vehicle includes a carrier and a material box structure. The carrier is connected to the material box structure. The carrier can be an unmanned vehicle. The carrier drives the material box structure to complete the spreading action during ground travel, significantly improving the agricultural operation efficiency.

[0049] Specifically, please refer to Figures 1 to 6 , the material box structure 10 includes a mounting member 100 and a material shell 200.

[0050] Among them, the mounting member 100 is used to connect to the flight body or the carrier; the material shell 200 is detachably connected to the mounting member 100. An opening 210 is provided at the top of the material shell 200. The cross-sectional area of the opening 210 is larger than the cross-sectional area of the bottom of the material shell 200, so that at least two material shells 200 can be stacked along the opening 210 in a state where they are not connected to the mounting member 100.

[0051] In this embodiment, the material shell 200 is connected to the mounting member 100 in a separable engagement manner, so as to facilitate the separate disassembly of the mounting group and the material shell 200. Moreover, the material shell 200 and the mounting member 100 can also be made of different materials according to the usage requirements to improve the structural stability and strength of the material box structure 10. The function of the material shell 200 is to contain materials, and an opening 210 is provided at the top of the material shell 200 to facilitate the material shell 200 to contain materials. In addition, the cross-sectional area of the opening 210 of the material shell 200 is larger than the cross-sectional area of the bottom of the material shell 200, so that at least two material shells 200 can be stably stacked along the opening 210 without connecting the mounting member 100 (as shown in Figure 3 ), thereby effectively utilizing the storage space and reducing the transportation cost.

[0052] It is worth mentioning that since the mounting member 100 is connected to the flying body or the carrier, the mounting member 100 is made of a material with higher structural strength to ensure its structural strength and stability and ensure the stable flight of the aircraft. While the material shell 200 can be made of a material with relatively lower structural strength to reduce costs.

[0053] Furthermore, the mounting member 100 is detachably connected to the opening 210, which is convenient for assembly.

[0054] Specifically, the mounting member 100 is detachably connected to the outer side wall of the material shell 200.

[0055] Furthermore, the size of the material shell 200 decreases in the direction from the opening 210 towards the bottom of the material shell 200.

[0056] In this embodiment, the size of the material shell 200 gradually decreases in the direction from the opening 210 towards the bottom of the material shell 200.

[0057] The mounting member 100 is installed on the flying body or the carrier to drive the mounting member 100 and the material shell 200 to move through the flying body or the carrier, so as to facilitate material transportation. The size of the material shell 200 (which can be the length, width or height of the material shell) gradually decreases from the opening 210 downwards to the bottom direction, so as to achieve the stable stacking of multiple material shells 200 (as shown in Figure 3 ), thereby effectively utilizing the storage space and reducing the transportation cost.

[0058] As shown in Figure 3 , the size of the material shell 200 gradually decreases in the direction from the opening 210 towards the bottom of the material shell 200 to form a funnel shape.

[0059] Of course, in other embodiments of the present invention, as shown in Figure 7 , the side wall of the material shell 200 can also be a stepped structure with gradually decreasing dimensions.

[0060] Or in some other embodiments of the present invention, such as Figure 8 shown, the outer side wall of the material housing 200 is an arcuate surface structure with gradually decreasing dimensions.

[0061] It can be understood that as long as the dimensions of the material housing 200 meet the condition of decreasing along the direction from the opening 210 towards the bottom of the material housing 200, no specific limitation is made here.

[0062] Furthermore, when the mounting member 100 is connected to the opening 210, the mounting member 100 covers a part of the opening 210, and the uncovered part of the opening 210 forms the feed inlet 211 of the material housing 200.

[0063] Specifically, the mounting member 100 is connected to the middle of the opening 210 to form the feed inlets 211 on both sides of the mounting member 100, so that it is convenient to add materials through the two feed inlets 211 even when the mounting member 100 and the material housing 200 are in an assembled state.

[0064] Furthermore, the side wall of the material housing 200 is provided with a guiding structure 290, so that a plurality of material housings 200 can be stacked in a guided manner when stacked, thereby improving the stacking convenience and avoiding misaligned stacking of a plurality of material housings 200.

[0065] In this embodiment, the guiding structure 290 is in the shape of a groove or a protrusion, and the groove or the protrusion extends along the direction from the opening 210 towards the bottom of the material housing 200, so as to play a guiding role when two material housings 200 are stacked.

[0066] Furthermore, the mounting member 100 is provided with a first positioning portion 110, and the material housing 200 is provided with a second positioning portion 220.

[0067] In this embodiment, by providing the first positioning portion 110 on the mounting member 100 and the second positioning portion 220 on the material housing 200, the positioning cooperation between the first positioning portion 110 and the second positioning portion 220 facilitates the quick installation of the mounting member 100 and the material housing 200, thereby improving the assembly efficiency.

[0068] Among them, the first positioning portion 110 is a groove, and the second positioning portion 220 is a protrusion. The second positioning portion 220 can be embedded in the first positioning portion 110, so as to achieve the positioning cooperation between the first positioning portion 110 and the second positioning portion 220.

[0069] Of course, in other embodiments of the present invention, the first positioning portion 110 can also be a protrusion, and the second positioning portion 220 can also be a groove. The first positioning portion 110 can be embedded in the second positioning portion 220, and no specific limitation is made here.

[0070] Furthermore, the mounting member 100 is provided with a first mounting hole 120, and the material housing 200 is provided with a second mounting hole 230. The first mounting hole 120 and the second mounting hole 230 are correspondingly arranged, and the first mounting hole 120 and the second mounting hole 230 are used for mounting fasteners.

[0071] In this embodiment, through the positioning cooperation of the first positioning portion 110 and the second positioning portion 220, the pre-positioning of the material box structure 10 is realized. It can be understood that when the first positioning portion 110 and the second positioning portion 220 are in cooperation, the first mounting hole 120 and the second mounting hole 230 are correspondingly arranged, which facilitates the operator to sequentially pass the fastener through the first mounting hole 120 and the second mounting hole 230, thereby making the mounting member 100 and the material housing 200 firmly connected.

[0072] Optionally, the number of the first mounting holes 120 and the second mounting holes 230 is multiple. The multiple first mounting holes 120 and the multiple second mounting holes 230 are arranged in one-to-one correspondence. The fastener can be a screw or a bolt to further improve the mounting firmness.

[0073] Furthermore, the first mounting hole 120 is located in the first positioning portion 110, and the second mounting hole 230 is located in the second positioning portion 220.

[0074] In this embodiment, by arranging the first mounting hole 120 in the first positioning portion 110 and the second mounting hole 230 in the second positioning portion 220, it is convenient for the operator to install the fastener on the first positioning portion 110 and the second positioning portion 220 after the fixed cooperation of the first positioning portion 110 and the second positioning portion 220.

[0075] Optionally, the number of the first mounting holes 120 and the second mounting holes 230 is three each. The three first mounting holes 120 and the three second mounting holes 230 are arranged in one-to-one correspondence.

[0076] It should be noted that the number of the first positioning portions 110 and the second positioning portions 220 is also multiple. Specifically, at least two first positioning portions 110 are provided at both ends of the mounting member 100, and at least second positioning portions 220 are correspondingly provided on the inner wall of the material housing 200.

[0077] Furthermore, a flanging 240 away from the opening direction is provided at the top edge of the material housing 200.

[0078] In this embodiment, by providing the flanging 240 structure at the top edge of the material housing 200, the structural strength and structural stability of the material housing 200 are improved, so that the opening 210 of the material housing 200 is not easily deformed; in addition, when multiple material housings 200 are in a stacked state, the flanging 240 structure also facilitates the operator to lift the flanging 240 structure, thereby facilitating the splitting of multiple material housings 200.

[0079] Furthermore, the material housing 200 is further provided with a plurality of support ribs 250. The plurality of support ribs 250 are spaced apart, and the plurality of support ribs 250 are all connected to the flanging 240 and extend along the direction of the opening towards the bottom of the material housing 200.

[0080] In this embodiment, by providing a plurality of support ribs 250 spaced apart on the material housing 200 and connecting the support ribs 250 to the flanging 240, the structural stability and structural strength of the material housing 200 are further improved.

[0081] Furthermore, the material housing 200 is further provided with a reinforcing structure 260. The reinforcing structure 260 is recessed on the outer sidewall of the material housing 200 and extends along the direction of the opening towards the bottom of the material housing 200.

[0082] In this embodiment, by providing the recessed reinforcing structure 260 on the material housing 200, the structural stability and structural strength of the material housing 200 are further improved, thereby improving the ability of the material housing 200 to load materials.

[0083] Optionally, at least two sidewalls of the material housing 200 are provided with reinforcing mechanisms.

[0084] Furthermore, the mounting member 100 is provided with a first lapping portion 130, and the top edge of the material housing 200 is provided with a second lapping portion 270. The first lapping portion 130 includes a limiting portion 131 and a cover edge 132 connected to each other. The limiting portion 131 abuts against the inner wall of the second lapping portion 270, and the cover edge 132 abuts against the top edge of the second lapping portion 270.

[0085] In this embodiment, by the limiting portion 131 abutting against the inner wall of the second lapping portion 270 and the cover edge 132 abutting against the top edge of the second lapping portion 270, it is convenient for the mounting member 100 to be assembled with the material housing 200, and the structural strength and structural stability during the assembly of the mounting member 100 and the material housing 200 can be improved.

[0086] Furthermore, a discharge port 280 is provided at the bottom of the material housing 200, and the discharge port 280 is used for installing a broadcaster.

[0087] In this embodiment, by providing the discharge port 280 for installing a broadcaster at the bottom of the material housing 200, it is convenient for the material to be broadcast out of the material housing 200 through the broadcaster; in addition, when a plurality of material housings 200 are in a stacked state, due to the existence of the discharge port 280, a sealed space between two adjacent material housings 200 can be avoided, that is, a negative pressure phenomenon between two adjacent material housings 200 can be avoided, thereby causing difficulty in separating the material housings 200.

[0088] In summary, the embodiment of the present utility model provides a bin structure 10 and an aircraft. The mounting member 100 is installed on the aircraft body to drive the mounting member 100 and the bin to fly through the aircraft body, thereby facilitating the transportation of materials. The material shell 200 is connected to the mounting member 100 in a separable joint manner, so as to facilitate the separate disassembly of the mounting group and the material shell 200. Moreover, the material shell 200 and the mounting member 100 can also be made of different materials according to the use requirements to improve the structural stability and strength of the bin structure 10. The function of the material shell 200 is to contain materials, and an opening 210 is provided at the top of the material shell 200 to facilitate the material shell 200 to contain materials. In addition, the cross-sectional area of the opening 210 of the material shell 200 is larger than the cross-sectional area of the bottom of the material shell 200, so that at least two material shells 200 can be stably stacked along the opening 210 in a state of not being connected to the mounting member 100, thereby effectively utilizing the storage space and reducing the transportation cost.

[0089] As described above, the above is only the specific embodiment of the present utility model, but the protection scope of the present utility model is not limited thereto. Any changes or substitutions that can be easily conceived by those skilled in the art within the technical scope disclosed by the present utility model should be covered by the protection scope of the present utility model. Therefore, the protection scope of the present utility model should be subject to the protection scope of the claims.

Claims

1. A bin structure, characterized in that, Including: A mounting member (100); A material housing (200), the material housing (200) is detachably connected to the mounting member (100), an opening (210) is provided at the top of the material housing (200), and the cross-sectional area of the opening (210) is larger than the cross-sectional area of the bottom of the material housing (200), so that at least two of the material housings (200) can be stacked along the opening (210) in a state where they are not connected to the mounting member (100).

2. The bin structure according to claim 1, characterized in that The mounting member (100) is detachably connected to the opening (210).

3. The bin structure according to claim 1, characterized in that, The mounting member (100) is detachably connected to the outer side wall of the material housing (200).

4. The bin structure according to claim 1, characterized in that, The size of the material housing (200) decreases along the direction from the opening (210) towards the bottom of the material housing (200).

5. The bin structure according to claim 4, wherein The side wall of the material housing (200) is a stepped structure with a gradually decreasing size.

6. The bin structure according to claim 4, wherein, The outer side wall of the material housing (200) is an arc-shaped surface structure with a gradually decreasing size.

7. The bin structure according to claim 1, characterized in that, A discharge port (280) is provided at the bottom of the material housing (200).

8. The bin structure according to claim 1, characterized in that, When the mounting member (100) is connected to the opening (210), the mounting member (100) covers a part of the opening (210), and the non-covered part of the opening (210) forms the feed port (211) of the material housing (200).

9. The bin structure according to claim 8, characterized in that The mounting member (100) is connected to the middle of the opening (210) to form the feed ports (211) on both sides of the mounting member (100).

10. The bin structure according to claim 1, characterized in that, A guiding structure (290) is provided on the side wall of the material housing (200) so that multiple material housings (200) can be guided and stacked when stacked.

11. The bin structure according to claim 1, characterized in that, The mounting member (100) is provided with a first positioning portion (110), and the material housing (200) is provided with a second positioning portion (220); The first positioning portion (110) is a groove, the second positioning portion (220) is a protrusion, and the second positioning portion (220) can be embedded into the first positioning portion (110); or, the first positioning portion (110) is a protrusion, the second positioning portion (220) is a groove, and the first positioning portion (110) can be embedded into the second positioning portion (220).

12. The bin structure according to claim 11, wherein, The mounting member (100) is provided with a first mounting hole (120), and the material housing (200) is provided with a second mounting hole (230). When the first positioning portion (110) and the second positioning portion (220) are in cooperation, the first mounting hole (120) and the second mounting hole (230) are correspondingly arranged, and the first mounting hole (120) and the second mounting hole (230) are used for installing fasteners.

13. The bin structure according to claim 12, wherein The first mounting hole (120) is located in the first positioning portion (110), and the second mounting hole (230) is located in the second positioning portion (220).

14. The bin structure according to claim 1, characterized in that, A flanging (240) away from the opening (210) direction is provided at the top edge of the material housing (200).

15. The bin structure according to claim 14, characterized in that, The material shell (200) is further provided with a plurality of support ribs (250), the plurality of support ribs (250) are spaced apart, and the plurality of support ribs (250) are all connected to the flanging (240) and extend along the direction from the open end (210) towards the bottom of the material shell (200).

16. The bin structure according to claim 1, wherein, The material shell (200) is further provided with a strengthening structure (260), the strengthening structure (260) is recessed in the outer side wall of the material shell (200), and the strengthening structure (260) extends along the direction from the open end (210) towards the bottom of the material shell (200).

17. The bin structure according to claim 1, wherein, The mounting member (100) is provided with a first lapping portion (130), the material shell (200) is provided with a second lapping portion (270), the first lapping portion (130) includes a limiting portion (131) and a cover edge (132) connected to each other, the limiting portion (131) abuts against the inner wall of the second lapping portion (270), and the cover edge (132) abuts against the top edge of the second lapping portion (270).

18. An aircraft, characterized in that, It includes an aircraft body and a fuel tank structure according to any one of claims 1-17, and the aircraft body is connected to the mounting member (100).

19. A ground vehicle, characterized in that, It includes a carrier and a fuel tank structure according to any one of claims 1-17, and the carrier is connected to the mounting member (100).