Heat preservation housing structure and unmanned aerial vehicle airport applying same

Abstract

The utility model discloses a heat preservation cover shell structure which comprises a plurality of heat preservation cover shell assemblies capable of forming a heat preservation inner cavity in an enclosing mode, and each heat preservation cover shell assembly comprises an outer shell body formed in an integrated plastic uptake mode and a heat insulation foam plate layer arranged on the inner side of the outer shell body. The utility model further discloses an unmanned aerial vehicle airport which comprises an unmanned aerial vehicle parking platform, and the heat preservation housing structure is arranged on the unmanned aerial vehicle parking platform. The heat preservation cover shell structure and the unmanned aerial vehicle airport applying the cover shell structure have the dual protection effects of an external protection function and an internal heat preservation function, are high in environment endurance capacity, can effectively isolate the influence of the external environment on the unmanned aerial vehicle, and are beneficial to prolonging the service life of the unmanned aerial vehicle.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, in particular to a heat preservation housing structure and an unmanned aerial vehicle airport applying the housing structure. Background Art

[0002] With the development of science and technology, unmanned aerial vehicles are more and more widely used due to their simple flight mechanism, excellent operation performance and stable flight control technology, and their applications in special fields such as aerial photography, agricultural plant protection, ecological protection, border monitoring, police security, disaster rescue, etc. are becoming more and more mature. At present, when using an unmanned aerial vehicle, a flat site needs to be found for taking off and landing. For this reason, relevant technical personnel have designed a parking apron for the unmanned aerial vehicle to park, and a protective cover is added on the parking apron to protect the unmanned aerial vehicle. However, the existing parking apron with a protective structure can only provide the protection function of preventing external physical impact for the unmanned aerial vehicle, and does not consider the influence of temperature change on the service life of the battery of the unmanned aerial vehicle, which has certain limitations. Content of the Utility Model

[0003] The technical problem to be solved by the utility model is to overcome the deficiencies of the prior art, and provide a heat preservation housing structure with a dual protection effect of external protection function and internal heat preservation function, strong environmental tolerance ability, which can effectively isolate the influence of the external environment on the unmanned aerial vehicle and is beneficial to extending the service life of the unmanned aerial vehicle, and an unmanned aerial vehicle airport applying the housing structure.

[0004] To solve the above technical problem, the utility model adopts the following technical solutions:

[0005] A heat preservation housing structure includes a number of heat preservation housing components that can enclose to form a heat preservation inner cavity. The heat preservation housing component includes an outer shell body integrally formed by thermoforming and a heat insulation foam board layer arranged on the inner side of the outer shell body.

[0006] As a further improvement of the above technical solution:

[0007] The heat preservation housing component is provided with an inner support skeleton. The outer shell body is arranged on the outer side of the inner support skeleton, and the heat insulation foam board layer is arranged on the inner side of the inner support skeleton.

[0008] An unmanned aerial vehicle airport includes an unmanned aerial vehicle parking platform, and the above heat preservation housing structure is arranged on the unmanned aerial vehicle parking platform.

[0009] As a further improvement of the above technical solution:

[0010] The number of groups of the heat preservation housing components on the unmanned aerial vehicle parking platform is set to two groups, including a first heat preservation housing component and a second heat preservation housing component.

[0011] The first thermal insulation cover assembly and the second thermal insulation cover assembly are respectively rotatably connected to both sides of the UAV parking platform through a rotation connection mechanism, and the first thermal insulation cover assembly and the second thermal insulation cover assembly can be switched between a closed state and an open state by rotation.

[0012] A first driving mechanism for driving the first thermal insulation cover assembly to rotate and a second driving mechanism for driving the second thermal insulation cover assembly to rotate are arranged inside the UAV parking platform.

[0013] The overall structure of the thermal insulation cover on the UAV parking platform is in a cuboid structure, and both the first thermal insulation cover assembly and the second thermal insulation cover assembly are provided with a top wall, a first side wall, a second side wall and a third side wall.

[0014] On the UAV parking platform, abutting bosses are respectively formed on one side corresponding to the first side wall and one side corresponding to the third side wall, and clearance recesses adapted to the abutting bosses are respectively formed on the first side wall and the third side wall.

[0015] The rotation connection mechanism includes a plurality of combined hinges. One page plate of the hinge is fixedly connected to the UAV parking platform, and the other page plate of the hinge is fixedly connected to the first thermal insulation cover assembly or the second thermal insulation cover assembly.

[0016] Both the first driving mechanism and the second driving mechanism adopt telescopic cylinders. The cylinder body of the telescopic cylinder is hinged to the UAV parking platform, and the piston rod of the telescopic cylinder is hinged to the first thermal insulation cover assembly or the second thermal insulation cover assembly.

[0017] A plurality of sets of walking wheels are arranged at the bottom of the UAV parking platform.

[0018] Compared with the prior art, the advantages of the present utility model are as follows:

[0019] First, the thermal insulation cover structure of the present utility model is composed of at least two sets of thermal insulation cover assemblies combined. An outer shell is arranged on the outside of the thermal insulation cover assembly, which can not only prevent dust, liquid, etc. from entering the inside of the cover, but also resist physical impacts caused by hail, stones, etc. An inner heat insulation foam board layer is arranged on the inside, which can effectively block the influence of the external environment of high temperature and heat or low temperature and cold. The thermal insulation cover structure utilizes the external protection function of the outer shell and the internal heat insulation function of the heat insulation foam board layer, has a dual protection effect, and has strong environmental tolerance.

[0020] II. The UAV airport of the present utility model forms an independent integrated UAV airport by arranging a heat preservation cover structure on the UAV parking platform. By closing or opening the heat preservation cover structure, the UAV can take off and land on the UAV parking platform. In the closed state, the UAV is stored in a relatively enclosed internal space, which can effectively isolate the influence of the external environment on the UAV, thereby playing a protective role for the UAV and being beneficial to extending the service life of the UAV. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] Figure 1 FIG. is a schematic structural diagram of the heat preservation cover structure on the UAV airport in a closed state.

[0022] Figure 2 FIG. is a schematic exploded view of the UAV airport.

[0023] Figure 3 FIG. is a schematic structural diagram of the heat preservation cover structure on the UAV airport in an open state.

[0024] Figure 4 FIG. is a schematic exploded view of the heat preservation cover assembly.

[0025] Figure 5 FIG. is a schematic diagram of the application scenario of the UAV airport.

[0026] LEGEND DESCRIPTION:

[0027] 1. Heat preservation cover assembly; 101. First heat preservation cover assembly; 102. Second heat preservation cover assembly; 2. Outer shell; 3. Heat insulation foam board layer; 4. Inner support skeleton; 5. UAV parking platform; 6. Rotating connection mechanism; 601. Hinge; 7. First driving mechanism; 8. Second driving mechanism; 9. Abutting boss; 10. Clearance recess; 11. Traveling wheel; 100. Top wall; 200. First side wall; 300. Second side wall; 400. Third side wall. DETAILED DESCRIPTION OF THE EMBODIMENTS

[0028] The present utility model will be further described in detail below with reference to the accompanying drawings and specific embodiments.

[0029] As Figure 1 and Figure 4As shown in the figure, the heat-insulating housing structure of this embodiment includes several groups of heat-insulating housing components 1 that can enclose to form a heat-insulating inner cavity. The heat-insulating housing component 1 includes an outer housing 2 formed by integral thermoforming and a heat-insulating foam board layer 3 arranged on the inner side of the outer housing 2. This heat-insulating housing structure is composed of at least two groups of heat-insulating housing components 1 combined. The outer side of the heat-insulating housing component 1 is provided with an outer housing 2, which can not only prevent dust, liquid, etc. from entering the inside of the housing, but also resist physical impacts caused by hail, stones, etc. The inner side is provided with a heat-insulating foam board layer 3, which can effectively block the influence of the external environment of high temperature and heat or low temperature and cold. This heat-insulating housing structure utilizes the external protection function of the outer housing 2 and the internal heat-insulating function of the heat-insulating foam board layer 3, has a dual protection effect, and has strong environmental tolerance.

[0030] It should be noted that the outer housing 2 is made of thermoforming material through integral thermoforming process. It not only has excellent physical and mechanical properties, especially excellent impact resistance, high tensile strength, bending strength, and compressive strength, but also has good heat resistance and low temperature resistance, and has stable mechanical properties within a relatively wide temperature range. Commonly used thermoforming materials on the market at present include ABS (acrylonitrile-butadiene-styrene copolymer), PVC (polyvinyl chloride), PET (polyethylene terephthalate), etc., and appropriate materials can be selected according to the actual application scenario; the heat-insulating foam board layer 3 is made of heat-insulating and heat-preserving materials. Commonly used heat-insulating and heat-preserving materials on the market at present include foam asbestos, polystyrene foam, polyurethane foam, etc., and appropriate materials can be selected according to the actual application scenario.

[0031] Preferably, the heat-insulating housing component 1 is provided with an inner support skeleton 4. The outer housing 2 is arranged on the outer side of the inner support skeleton 4, and the heat-insulating foam board layer 3 is arranged on the inner side of the inner support skeleton 4. In this embodiment, the heat-insulating housing component 1 has an inner support skeleton 4, which can improve the structural strength and load-bearing capacity of the heat-insulating housing structure.

[0032] As Figures 1 to 5 shown in the figure, the drone airport of this embodiment includes a drone parking platform 5, and the above-mentioned heat-insulating housing structure is arranged on the drone parking platform 5. This drone airport forms an independent integrated drone airport by arranging the heat-insulating housing structure on the drone parking platform 5. By closing or opening the heat-insulating housing structure, the drone can take off and land on the drone parking platform 5. In the closed state, the drone is stored in a relatively enclosed internal space, which can effectively isolate the influence of the external environment on the drone, thereby playing a protective role for the drone and being beneficial to extending the service life of the drone.

[0033] In this embodiment, the number of groups of the heat preservation cover shell assemblies 1 on the UAV parking platform 5 is set to two groups, including a first heat preservation cover shell assembly 101 and a second heat preservation cover shell assembly 102. In other embodiments, the number of groups of the heat preservation cover shell assemblies 1 can also be set to more than two groups, not limited to this embodiment.

[0034] Preferably, the first heat preservation cover shell assembly 101 and the second heat preservation cover shell assembly 102 are respectively rotatably connected to both sides of the UAV parking platform 5 through a rotation connection mechanism 6, and the first heat preservation cover shell assembly 101 and the second heat preservation cover shell assembly 102 can be switched between a closed state and an open state by rotation.

[0035] Preferably, a first driving mechanism 7 for driving the first heat preservation cover shell assembly 101 to rotate and a second driving mechanism 8 for driving the second heat preservation cover shell assembly 102 to rotate are arranged in the UAV parking platform 5.

[0036] In this embodiment, the overall structure of the heat preservation cover shell on the UAV parking platform 5 is in a cuboid structure. The first heat preservation cover shell assembly 101 and the second heat preservation cover shell assembly 102 are both provided with a top wall 100, a first side wall 200, a second side wall 300 and a third side wall 400. In other embodiments, the overall structure of the heat preservation cover shell can also be set to a semi-circular arc top structure, not limited to this embodiment.

[0037] Preferably, abutting bosses 9 are respectively formed on one side of the UAV parking platform 5 corresponding to the first side wall 200 and on one side corresponding to the third side wall 400, and clearance concave positions 10 adapted to the abutting bosses 9 are respectively formed on the first side wall 200 and the third side wall 400. In this embodiment, the abutting boss 9 is set to be semi-elliptical in shape, and the first side wall 200 and the third side wall 400 on the first heat preservation cover shell assembly 101 and the second heat preservation cover shell assembly 102 are provided with clearance concave positions 10 with a smooth arc shape adapted thereto. In the closed state, the clearance concave position 10 is in abutting contact with the abutting boss 9, which is not only simple and beautiful in appearance, but also can reduce the self-weight of the heat preservation cover shell assembly on the basis of ensuring the structural strength, realizing light weight and reducing the operating load of the first driving mechanism 7 and the second driving mechanism 8.

[0038] Preferably, the rotation connection mechanism 6 includes a plurality of hinge combinations 601. One page plate of the hinge 601 is fixedly connected to the UAV parking platform 5, and the other page plate of the hinge 601 is fixedly connected to the inner support frame 4 on the first heat preservation cover shell assembly 101 or the second heat preservation cover shell assembly 102. In this embodiment, the rotation connection mechanism 6 adopts the form of a hinge 601, and the hinge 601 is connected between the UAV parking platform 5 and the inner support frame 4, which has the advantages of simple structure, convenient and fast installation and disassembly process, and low cost.

[0039] Preferably, both the first driving mechanism 7 and the second driving mechanism 8 adopt telescopic cylinders. The cylinder body of the telescopic cylinder is hinged to the UAV parking platform 5, and the piston rod of the telescopic cylinder is hinged to the inner support frame 4 on the first heat preservation housing assembly 101 or the second heat preservation housing assembly 102. In this embodiment, the first driving mechanism 7 and the second driving mechanism 8 adopt the form of telescopic cylinders, which not only have the advantages of compact structure and small volume, are suitable for the narrow installation space inside the UAV parking platform 5, but also have strong bearing capacity and good running stability, can accurately control the opening or closing actions of the first heat preservation housing assembly 101 and the second heat preservation housing assembly 102, and meet the use requirements of fast response speed. In other embodiments, the first driving mechanism 7 and the second driving mechanism 8 can also adopt components such as chain drive mechanisms, which are not limited to this embodiment.

[0040] Preferably, a plurality of groups of walking wheels 11 are arranged at the bottom of the UAV parking platform 5. In this embodiment, four groups of walking wheels 11 are arranged at the bottom of the UAV parking platform 5, which is convenient for the staff to transfer the UAV parking platform 5, and has the advantages of good mobility, high transfer efficiency and good stability.

[0041] The above are only the preferred embodiments of the present invention, and the protection scope of the present invention is not limited to the above embodiments. For those skilled in the art of this technology, the improvements and transformations obtained without departing from the technical concept of the present invention should also be regarded as the protection scope of the present invention.

Claims

1. A heat preservation shell structure, characterized in that: The invention comprises a plurality of groups of heat-insulating shell components (1) capable of enclosing a heat-insulating inner cavity, wherein the heat-insulating shell components (1) comprise an outer shell body (2) formed by integral vacuum forming and a heat-insulating foam board layer (3) arranged on the inner side of the outer shell body (2).

2. The heat-insulating shell structure according to claim 1, characterized in that: The heat-insulating cover shell assembly (1) is provided with an inner support frame (4), the outer shell (2) is arranged on the outer side of the inner support frame (4), and the heat-insulating foam board layer (3) is arranged on the inner side of the inner support frame (4).

3. A drone airport, characterized in that: It comprises a drone parking platform (5), on which the thermal insulation cover structure according to claim 1 or 2 is arranged.

4. The drone airport according to claim 3, characterized in that: The number of groups of the heat-insulating cover shell components (1) on the drone parking platform (5) is set to two groups, including a first heat-insulating cover shell component (101) and a second heat-insulating cover shell component (102).

5. The drone airport according to claim 4, characterized in that: The first heat-insulating cover shell assembly (101) and the second heat-insulating cover shell assembly (102) are respectively rotatably connected to two sides of the drone parking platform (5) via a rotating connection mechanism (6); the first heat-insulating cover shell assembly (101) and the second heat-insulating cover shell assembly (102) can be switched between a closed state and an open state by rotating.

6. The drone airport according to claim 5, characterized in that: A first driving mechanism (7) for driving the first heat-insulating cover assembly (101) to rotate and a second driving mechanism (8) for driving the second heat-insulating cover assembly (102) to rotate are arranged in the drone parking platform (5).

7. The drone airport according to claim 6, characterized in that: The thermal insulation cover structure on the drone parking platform (5) is an overall rectangular parallelepiped structure, and the first thermal insulation cover component (101) and the second thermal insulation cover component (102) are both provided with a top wall (100), a first side wall (200), a second side wall (300) and a third side wall (400).

8. The drone airport according to claim 7, characterized in that: Abutment bosses (9) are formed on the side of the drone parking platform (5) corresponding to the first side wall (200) and the side corresponding to the third side wall (400), respectively, and air avoidance recesses (10) adapted to the abutment bosses (9) are formed on the first side wall (200) and the third side wall (400), respectively.

9. The drone airport according to claim 6, characterized in that: The rotating connection mechanism (6) comprises a plurality of combined hinges (601), one hinge of the hinge (601) being fixedly connected to the drone parking platform (5), and the other hinge of the hinge (601) being fixedly connected to the first heat-insulating cover assembly (101) or the second heat-insulating cover assembly (102); The first drive mechanism (7) and the second drive mechanism (8) both use a telescopic cylinder, the cylinder body of the telescopic cylinder is hinged to the drone parking platform (5), and the piston rod of the telescopic cylinder is hinged to the first heat-insulating cover assembly (101) or the second heat-insulating cover assembly (102).

10. The drone airport according to claim 9, characterized in that: A plurality of groups of running wheels (11) are arranged at the bottom of the drone parking platform (5).

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