CN214382006U - Unmanned aerial vehicle basic station and unmanned aerial vehicle system - Google Patents

Abstract

The utility model provides an unmanned aerial vehicle basic station and unmanned aerial vehicle system, wherein, unmanned aerial vehicle basic station includes: a housing (10); the unmanned aerial vehicle charging system comprises an operating platform (20) arranged in a shell (10), wherein the operating platform (20) is at least used for charging a battery of the unmanned aerial vehicle, the operating platform (20) at least separates the interior of the shell (10) into a first cavity (11) and a second cavity (12), the first cavity (11) is used for accommodating the unmanned aerial vehicle, and a cavity air inlet part (21) and a cavity air outlet part (22) which are communicated with the first cavity (11) are arranged on the operating platform (20); air conditioner (30), set up in second cavity (12), the internal circulation air inlet portion (31) and the cavity air-out portion (22) intercommunication of air conditioner (30), the internal circulation air-out portion (32) and the cavity air inlet portion (21) direct intercommunication of air conditioner (30), the cold air current that air conditioner (30) refrigeration produced can be by cavity air inlet portion (21) direct access first cavity (11) to cool off unmanned aerial vehicle's battery.

Description

Unmanned aerial vehicle basic station and unmanned aerial vehicle system

Technical Field

The application relates to the technical field of unmanned aerial vehicle base stations, in particular to an unmanned aerial vehicle base station and an unmanned aerial vehicle system.

Background

Because unmanned aerial vehicle's battery duration is limited, generally need charge unmanned aerial vehicle's battery through the unmanned aerial vehicle basic station. Some unmanned aerial vehicle basic stations's that have now inside has two cavities, and wherein, a cavity is used for placing unmanned aerial vehicle, and the embedding has the air conditioner in another cavity. The air conditioning that air conditioner refrigeration produced is let in earlier in the cavity that is equipped with the air conditioner, and the intercommunicating pore between two cavities of rethread enters into the cavity of placing unmanned aerial vehicle to carry out cooling to unmanned aerial vehicle's battery. However, in the above manner, the cold air generated by the air conditioner is introduced into the two chambers, and the space requiring refrigeration is large, so that the requirement on the refrigeration performance (such as the refrigeration capacity) of the air conditioner is high. And the air conditioner volume that refrigeration performance is high is often great, will increase the holistic size in unmanned aerial vehicle basic station like this, also be convenient for simultaneously arranging of other parts in unmanned aerial vehicle basic station.

SUMMERY OF THE UTILITY MODEL

The embodiment of the application provides an unmanned aerial vehicle basic station and unmanned aerial vehicle system.

In a first aspect, an embodiment of the present application provides an unmanned aerial vehicle base station, including: a housing; the operation platform is arranged in the shell and at least used for charging a battery of the unmanned aerial vehicle, the operation platform at least divides the interior of the shell into a first cavity and a second cavity, the first cavity is used for accommodating the unmanned aerial vehicle, and the operation platform is provided with a cavity air inlet part and a cavity air outlet part which are communicated with the first cavity; the air conditioner sets up in the second cavity, and the inner loop air inlet portion and the cavity air-out portion intercommunication of air conditioner, the inner loop air-out portion and the direct intercommunication of cavity air inlet portion of air conditioner, the cold air current that the air conditioner refrigeration produced can be directly got into first cavity by cavity air inlet portion to cool off unmanned aerial vehicle's battery.

Further, the internal circulation air inlet part is directly communicated with the cavity air outlet part.

Further, still include: and the first air duct structure is arranged between the cavity air inlet part and the internal circulation air outlet part and/or between the cavity air outlet part and the internal circulation air inlet part.

Furthermore, one end of the first air duct structure is connected to the operating platform, and the other end of the first air duct structure is attached to the air conditioner or has a gap with the air conditioner; or one end of the first air duct structure is connected to the air conditioner, and the other end of the first air duct structure is attached to the operating platform or a gap is formed between the other end of the first air duct structure and the operating platform.

Further, the casing includes main part and cover body portion, and the second cavity is located the main part, and first cavity is located cover body portion, and cover body portion selectively opens or closes, and the unmanned aerial vehicle basic station still includes: the first heat insulation structure is arranged on the cover body part to insulate the first cavity.

Further, the first cavity is located above the second cavity.

Further, the quantity of cavity air inlet portion is the same with the quantity of unmanned aerial vehicle's battery, and when unmanned aerial vehicle was located operation platform's assigned position, cavity air inlet portion and unmanned aerial vehicle's battery one-to-one.

Further, cavity air inlet portion is two along first direction symmetry setting.

Further, when unmanned aerial vehicle was located operation platform's assigned position, the first direction and the coincidence of the central line of unmanned aerial vehicle's fuselage or perpendicular.

Furthermore, the two air outlet parts of the cavity are symmetrically arranged along a second direction, and the second direction is vertical to the first direction.

Further, the cavity air outlet part comprises a cavity air outlet and a fan arranged at the cavity air outlet, the cavity air inlet part is of a fan-free structure, and/or the internal circulation air inlet part comprises an internal circulation air inlet and a fan arranged at the internal circulation air inlet, and the internal circulation air outlet part is of a fan-free structure, wherein airflow of the internal circulation air outlet part is led into the first cavity through the cavity air inlet part by the fan, and the airflow in the first cavity is led into the internal circulation air inlet part and/or the second cavity through the cavity air outlet part.

Further, the casing includes main part and cover body portion, and the second cavity is located the main part, and first cavity is located cover body portion, and cover body portion selectively opens or closes, and operation platform connects on the main part, and operation platform has the open mode that can open the second cavity and the closed mode that seals the second cavity.

Further, one side of the operation platform is pivotally connected to the main body part; alternatively, the operation platform is integrally detachably connected to the main body.

Further, the outer circulation air inlet portion of air conditioner includes outer circulation air intake and the dust-proof structure of detachably setting in outer circulation air intake department, and when operation platform was in the open mode, dust-proof structure can be carried out the dismouting by the opening of second cavity.

Furthermore, the shell is provided with an external air inlet part and an external air outlet part, the external air inlet part is communicated with the external circulation air inlet part of the air conditioner, the external air outlet part is communicated with the external circulation air outlet part of the air conditioner, and the external air inlet part and the external air outlet part are symmetrically arranged on two opposite sides of the shell; and/or the external circulation air inlet part and the external circulation air outlet part are symmetrically arranged on two sides of the air conditioner.

Further, the casing has outside air-out portion, and outside air-out portion communicates with the extrinsic cycle air-out portion of air conditioner, and the unmanned aerial vehicle basic station still includes: the second air duct structure is arranged between the external air outlet part and the external circulating air outlet part; and the second heat insulation structure is arranged on the second air duct structure so as to insulate the air flow channel of the second air duct structure.

Further, still include: and the electric module is arranged in the second cavity and is positioned on the circumferential outer side of the air conditioner.

Further, the height of the projection of the electrical module in the radial direction of the air conditioner is less than or equal to the height of the projection of the air conditioner in the radial direction thereof.

Further, the electric module comprises a strong current module, a weak current module or a power supply module.

In a second aspect, the present application provides an unmanned aerial vehicle system, including unmanned aerial vehicle and the unmanned aerial vehicle basic station that is used for at least charging to unmanned aerial vehicle's battery, the unmanned aerial vehicle basic station is foretell unmanned aerial vehicle basic station.

Because the internal circulation air-out portion and the cavity air inlet portion direct intercommunication of air conditioner, the cold air current that the air conditioner refrigeration produced can directly get into first cavity by cavity air inlet portion to cool off unmanned aerial vehicle's battery. That is to say, the air conditioner mainly refrigerates to first cavity, can reduce the refrigerated space of needs like this to reduce the requirement to the refrigeration performance (like the refrigeration volume) of air conditioner, and then can reduce the overall dimension of unmanned aerial vehicle basic station, also be favorable to arranging of other parts in unmanned aerial vehicle basic station.

Drawings

Fig. 1 is a schematic structural diagram of a drone base station according to one embodiment of the present application;

fig. 2 is a schematic structural diagram of an air conditioner of the drone base station of fig. 1;

FIG. 3 is a schematic view of another angle of the air conditioner of FIG. 2;

fig. 4 is a schematic internal structural diagram of the drone base station of fig. 1;

fig. 5 is a schematic structural view of another angle of the drone base station of fig. 1;

fig. 6 is a schematic cross-sectional structural view of the drone base station of fig. 5;

fig. 7 is a schematic structural diagram of the operation platform of the drone base station of fig. 1 in an open state.

It is noted that the drawings are not necessarily to scale and are merely illustrative in nature and not intended to obscure the reader.

Description of reference numerals:

10. a housing; 11. a first cavity; 12. a second cavity; 13. a main body portion; 14. a cover body portion; 15. an external air inlet portion; 16. an external air outlet part; 17. a heat dissipating section; 18. a side cover; 20. an operating platform; 21. a cavity air inlet part; 22. a cavity air outlet part; 30. an air conditioner; 31. an internal circulation air inlet part; 311. an internal circulation air inlet; 312. a fan; 32. an internal circulation air outlet part; 33. an external circulation air inlet part; 331. an external circulation air inlet; 332. a dust-proof structure; 34. an external circulation air outlet part; 40. a first air duct structure; 50. a second air duct structure; 60. a second thermally insulating structure; 71. a strong current module mounting position; 72. a weak current module mounting position; 73. a current power module mounting position; 74. and a standby power supply module mounting position.

Detailed Description

In order to make the objects, technical solutions and advantages of the present application more clear, the technical solutions of the present application will be described below in detail and completely with reference to the accompanying drawings of the embodiments of the present application. It should be apparent that the described embodiment is one embodiment of the present application and not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the described embodiments of the application without any inventive step, are within the scope of protection of the application.

It is to be noted that, unless otherwise defined, technical or scientific terms used herein shall have the ordinary meaning as understood by those of ordinary skill in the art to which this application belongs. If the description "first", "second", etc. is referred to throughout, the description of "first", "second", etc. is used only for distinguishing similar objects, and is not to be construed as indicating or implying a relative importance, order or number of technical features indicated, it being understood that the data described in "first", "second", etc. may be interchanged where appropriate. If "and/or" is presented throughout, it is meant to include three juxtapositions, exemplified by "A and/or B" and including either scheme A, or scheme B, or schemes in which both A and B are satisfied. Furthermore, spatially relative terms, such as "above," "below," "top," "bottom," and the like, may be used herein for ease of description to describe one element or feature's spatial relationship to another element or feature as illustrated in the figures, and should be understood to encompass different orientations in use or operation in addition to the orientation depicted in the figures.

The application provides an unmanned aerial vehicle basic station can be used to carry out multiple type operation to unmanned aerial vehicle through unmanned aerial vehicle basic station. For example, charging a battery of the drone, replacing a battery or parts of the drone, interacting data with the drone, etc. In some embodiments of the present application, the drone base station is primarily used to charge the battery of the drone.

Fig. 1 shows a schematic structural diagram of an unmanned aerial vehicle base station according to an embodiment of the present application. Fig. 2 shows a schematic structural diagram of the air conditioner 30 of the drone base station of fig. 1. Fig. 3 shows a schematic view of another angle of the air conditioner 30 of fig. 2. Fig. 4 shows a schematic internal structural diagram (top view) of the drone base station of fig. 1. Fig. 5 shows a schematic structural view of another angle of the drone base station of fig. 1. Fig. 6 shows a longitudinal cross-sectional structural schematic diagram of the drone base station of fig. 5. Fig. 7 shows a schematic structural diagram of the operation platform 20 of the drone base station of fig. 1 in an open state.

As shown in fig. 1 to 7, in some embodiments of the present application, the drone base station includes a housing 10, an operation platform 20, and an air conditioner 30. The operation platform 20 is disposed in the housing 10. The operation platform 20 is used at least for charging the battery of the drone. The operation platform 20 divides the interior of the housing 10 into at least a first chamber 11 and a second chamber 12. First cavity 11 is used for holding unmanned aerial vehicle. The operation platform 20 is provided with a cavity air inlet portion 21 and a cavity air outlet portion 22 which are communicated with the first cavity 11. The air conditioner 30 is disposed in the second chamber 12. The internal circulation air inlet part 31 of the air conditioner 30 is communicated with the cavity air outlet part 22. The internal circulation air outlet part 32 of the air conditioner 30 is directly communicated with the cavity air inlet part 21. The term "directly connected" means that the cold airflow generated by the air conditioner 30 does not flow into the second cavity 12 or a small amount of cold airflow (which does not affect the cooling effect of the air conditioner 30 and can be ignored) flows into the second cavity 12, and all or most of the cold airflow directly enters the first cavity 11.

Because the internal circulation air outlet portion 32 of the air conditioner 30 is directly communicated with the cavity air inlet portion 21, cold air flow generated by refrigeration of the air conditioner 30 can directly enter the first cavity 11 through the cavity air inlet portion 21 so as to cool the battery of the unmanned aerial vehicle. That is to say, air conditioner 30 mainly refrigerates to first cavity 11, can reduce the refrigerated space of needs like this to reduce the requirement to the refrigeration performance (like the refrigerating output) of air conditioner 30, and then can reduce the overall size of unmanned aerial vehicle basic station, also be favorable to arranging of other parts in unmanned aerial vehicle basic station.

It should be noted that the cavity formed by the operating platform 20 dividing the inside of the casing 10 is not limited to the first cavity 11 and the second cavity 12, and in other embodiments, there may be another cavity formed by the operating platform 20 dividing, and at this time, the cold air flow generated by the refrigeration of the air conditioner 30 mainly enters the first cavity 11 provided with the unmanned aerial vehicle. In addition, the cold air current that air conditioner 30 refrigeration produced enters into and mainly is used for cooling the battery of the unmanned aerial vehicle in charging behind the first cavity 11, and of course, above-mentioned cold air current also can be used for cooling the battery or the unmanned aerial vehicle's of charging before, after other parts.

As shown in fig. 6 and 7, in some embodiments of the present application, the inner circulation air inlet portion 31 is in direct communication with the chamber air outlet portion 22. That is to say, the air flow after heat exchange in the first cavity 11 does not flow into the second cavity 12 or a trace amount of air flow (negligible) flows into the second cavity 12, and all or most of the air flow after heat exchange directly enters the air conditioner 30 from the internal circulation air inlet portion 31 to perform the next step of refrigeration, so that the internal circulation of the air conditioner 30 is substantially completely performed in the first cavity 11 and the air conditioner 30, and is not performed in the second cavity 12, thereby improving the refrigeration effect of the air conditioner 30, and preventing the air flow with higher temperature after heat exchange from affecting other components in the second cavity 12. Of course, in other embodiments not shown in the drawings, the internal circulation air inlet 31 and the cavity air outlet 22 may not be directly connected, for example, the internal circulation air inlet 31 is connected to the second cavity 12, and the cavity air outlet 22 is also connected to the second cavity 12, at this time, the air flow after heat exchange will enter the second cavity 12 first and then enter the air conditioner 30 through the internal circulation air inlet 31.

It should be noted that there are various ways of directly communicating the internal circulation air outlet portion 32 with the cavity air inlet portion 21/the internal circulation air inlet portion 31 with the cavity air outlet portion 22. For example, as shown in fig. 6 and 7, in some embodiments of the present application, the drone base station further includes a first air duct structure 40, the first air duct structure 40 being disposed between the cavity air inlet 21 and the internal circulation air outlet 32 and/or between the cavity air outlet 22 and the internal circulation air inlet 31. The air channel inside the first air channel structure 40 forms an air channel, and when the first air channel structure 40 is arranged between the cavity air inlet part 21 and the internal circulation air outlet part 32, the air channel is used for communicating the cavity air inlet part 21 and the internal circulation air outlet part 32; when the first air duct structure 40 is disposed between the internal circulation air inlet portion 31 and the cavity air outlet portion 22, the air duct is used for communicating the internal circulation air inlet portion 31 and the cavity air outlet portion 22. Therefore, the air flow passing through the internal air duct of the first air duct structure 40 can directly enter the first cavity 11 from the cavity air inlet 21 or enter the air conditioner 30 from the internal circulation air inlet 31, so as to directly communicate the internal circulation air outlet 32 with the cavity air inlet 21/the internal circulation air inlet 31 with the cavity air outlet 22. Of course, the manner of realizing the "direct communication" is not limited to this, and in other embodiments, the internal circulation air outlet portion 32 and the cavity air inlet portion 21/the internal circulation air inlet portion 31 and the cavity air outlet portion 22 may be directly attached or nested.

Specifically, as shown in fig. 6 and 7, one end of the first air duct structure 40 is connected to the operation platform 20, and may specifically correspond to the position of the cavity air inlet 21 or the cavity air outlet 22, and the other end of the first air duct structure is attached to the air conditioner 30 or has a gap with the air conditioner 30, and may specifically correspond to the position of the internal circulation air inlet 31 or the internal circulation air outlet 32. At this time, one end of the first air duct structure 40 close to the air conditioner 30 is not connected to the air conditioner 30, and if the operation platform 20 is detachably or movably provided with respect to the housing 10, the whole first air duct structure 40 can be detached or moved along with the operation platform 20. When the end of the first air duct structure 40 is attached to the air conditioner 30, no gap is formed between the first air duct structure 40 and the air conditioner 30, the cold air flow generated by the air conditioner 30 can be guided to the cavity air inlet portion 21 through the first air duct structure 40, and the heat-exchanged air flow flowing out of the cavity air outlet portion 22 can be guided to the internal circulation air inlet portion 31 through the first air duct structure 40. When there is a gap between the end of the first air duct structure 40 and the air conditioner 30, the gap needs to be small enough not to affect the cooling effect of the air conditioner 30. That is, even if the air flow flows into the second chamber 12 at the gap, only a slight amount of the air flow may be so, and most of the air flow may directly enter the first chamber 11 or enter the inside of the air conditioner 30. Of course, in other embodiments, if the operation platform 20 and the housing 10 do not move relatively, both ends of the first air duct structure 40 may be directly connected to the operation platform 20 and the air conditioner 30.

It should be noted that, in other embodiments of the present application, one end of the first air duct structure 40 may be connected to the air conditioner 30, and the other end of the first air duct structure may be attached to the operation platform 20 or have a gap with the operation platform 20. At this time, one end of the first air duct structure 40 close to the operation platform 20 is not connected to the operation platform 20, if the operation platform 20 is detachable or movable relative to the housing 10, no matter when the operation platform 20 is detached or moved, the first air duct structure 40 is integrally connected to the air conditioner 30, and the action of the operation platform 20 is not affected.

As shown in fig. 1 and 4-7, in some embodiments of the present application, the housing 10 includes a main body portion 13 and a cover body portion 14. The second cavity 12 is located within the body portion 13. The first cavity 11 is located within the mask body 14. The cover body portion 14 can be selectively opened or closed. Preferably, the internal space enclosed by the main body 13 forms the second cavity 12, the internal space enclosed by the cover part 14 forms the first cavity 11, the operation platform 20 is disposed at the top opening of the main body 13, and the operation platform 20 is flush with or recessed in the edge of the top opening of the main body 13. When the cover body portion 14 is opened, the unmanned aerial vehicle descends to or is moved to the operation platform 20, and then the cover body portion 14 is closed, so that the unmanned aerial vehicle is protected.

Preferably, in some embodiments of the present application, the drone base station further comprises a first thermal insulation structure (not shown in the figures) provided on the casing portion 14 to thermally insulate the first cavity 11. The first heat insulating structure may be in various forms, for example, it includes an insulating layer provided on the inner or outer side of the housing portion 14; alternatively, the cover body portion 14 itself is made of a heat insulating material so that the cover body portion 14 forms the first heat insulating structure. Because air conditioner 30 mainly refrigerates to first cavity 11, only need set up on cover somatic part 14 to carry out thermal-insulated first heat-proof structure to first cavity 11 can, compare in the mode that whole casing 10 all set up heat-proof structure, technology is simpler, and the structure is simplified more. In addition, particularly in some embodiments, the heat dissipation portion 17 is disposed on the sidewall of the housing 10, the heat dissipation portion 17 is communicated with the second cavity 12, and the heat inside the second cavity 12 can be dissipated through the heat dissipation portion 17. The heat dissipation portion 17 is applicable to various cases, for example, in the case where the air flow enters the second cavity 12 after the heat exchange, the heat can be dissipated through the heat dissipation portion 17; alternatively, other members provided in the second cavity 12 need to dissipate heat, and the heat dissipation portion 17 may be used. The form of the heat dissipation portion 17 is not limited, and may be, for example, a heat dissipation hole, a heat dissipation grid, or the like.

As shown in fig. 1, 5 and 6, in some embodiments of the present application, the first cavity 11 is located above the second cavity 12. The cold airflow generated by the refrigeration of the air conditioner 30 is introduced into the first cavity 11 from bottom to top, so that the heat dissipation of the battery of the unmanned aerial vehicle is facilitated. In addition, second cavity 12 is located the below of first cavity 11 completely, and two cavities do not have the part of overlapping in the horizontal direction, and the respective space of two cavities can be designed great, and the part of being convenient for more obtains arranging, the holding of also being convenient for simultaneously and operation unmanned aerial vehicle. In other embodiments not shown in the drawings, the first cavity 11 and the second cavity 12 may also be horizontally disposed; or, the part of the first cavity 11 close to the periphery is wrapped outside the second cavity 12; alternatively, the portion of the second cavity 12 near the periphery is wrapped outside the first cavity 11.

As shown in fig. 2 to 4 and 7, in some embodiments of the present application, the number of the cavity air inlets 21 is the same as the number of the batteries of the unmanned aerial vehicle, and when the unmanned aerial vehicle is located at the designated position of the operating platform 20, the cavity air inlets 21 correspond to the batteries of the unmanned aerial vehicle one to one, so that the cold air flow generated by the refrigeration of the air conditioner 30 can be directly blown to the batteries of the unmanned aerial vehicle through the cavity air inlets 21, thereby improving the cooling effect on the batteries. Of course, the position and number of the cavity air inlet portions 21 are not limited to this, and in other embodiments, the number of the cavity air inlet portions 21 may not be equal to the number of the batteries of the unmanned aerial vehicle, and may not correspond to the batteries of the unmanned aerial vehicle, as long as it is ensured that the airflow can enter the first cavity 11.

It should be noted that the cavity air inlet 21 and the internal circulation air outlet 32 of the air conditioner 30 are also in a one-to-one correspondence relationship, for example, in the embodiment shown in the drawings, the cavity air inlet 21 and the internal circulation air outlet 32 are aligned in the vertical direction. Of course, in other embodiments, the cavity air inlet portion 21 and the internal circulation air outlet portion 32 may not be aligned in the vertical direction, but slightly staggered, and at this time, the direct communication between the two can also be realized through the first air duct structure 40. Therefore, the description of the number and positional relationship of the cavity air inlet portions 21 to each other is also applicable to the internal circulation air outlet portion 32. Likewise, the description of the number and positional relationship of the chamber outlet portions 22 to each other is equally applicable to the inner circulation air inlet portion 31.

Preferably, in some embodiments of the present application, the cavity air inlet portion 21 (or the internal circulation air outlet portion 32) is two symmetrically arranged along the first direction. Because unmanned aerial vehicle's battery also is two of symmetry setting usually, two cavity air inlet portion 21 (or inner loop air-out portion 32) respectively with two batteries one-to-one. When the drone is in a designated position (e.g., a charging position for charging) of the operating platform 20, the first direction coincides with or is perpendicular to a centerline of the body of the drone. When the first direction coincides with the center line of the unmanned aerial vehicle body, two batteries of the unmanned aerial vehicle are respectively positioned on the left side and the right side of the unmanned aerial vehicle body; when the central line of first direction and unmanned aerial vehicle fuselage is perpendicular, two batteries of unmanned aerial vehicle are arranged along the fore-and-aft direction of fuselage respectively. Further, the cavity air outlet part 22 (or the internal circulation air inlet part 31) is two symmetrically arranged along the second direction, the second direction is perpendicular to the first direction, the arrangement mode of the cavity air outlet part 22 (or the internal circulation air inlet part 31) and the cavity air inlet part 21 (or the internal circulation air outlet part 32) is convenient for arrangement of components such as an evaporator inside the air conditioner 30, and air flow can better flow through the battery of the unmanned aerial vehicle. In the embodiment shown in the figures, two cavity air inlet portions 21 (or inner circulation air outlet portions 32) and two cavity air outlet portions 22 (or inner circulation air inlet portions 31) are arranged in a matrix.

It should be noted that the arrangement modes of the cavity air inlet portion 21 (or the internal circulation air outlet portion 32) and the cavity air outlet portion 22 (or the internal circulation air inlet portion 31) are not limited to this, and in other embodiments, the arrangement modes may be arranged in other forms according to the cooling requirements of the internal evaporator and the air duct of the air conditioner 30, the battery of the unmanned aerial vehicle, or other components. For example, according to the different designated positions of the unmanned aerial vehicle, the two cavity air inlet portions 21 (or the internal circulation air outlet portion 32) and the two cavity air outlet portions 22 (or the internal circulation air inlet portion 31) can be integrally rotated by a certain angle, and the relative position relationship between the two cavity air inlet portions 21 (or the internal circulation air outlet portion 32) and the two cavity air outlet portions 22 (or the internal circulation air inlet portion 31) is not changed.

In some embodiments of the present application, the cavity air outlet portion 22 includes a cavity air outlet and a fan disposed at the cavity air outlet, and the cavity air inlet portion 21 is of a fan-less structure, and/or, as shown in fig. 3, the internal circulation air inlet portion 31 includes an internal circulation air inlet 311 and a fan 312 disposed at the internal circulation air inlet 311, and the internal circulation air outlet portion 32 is of a fan-less structure. The air flow of the internal circulation air outlet part 32 is introduced into the first cavity 11 through the cavity air inlet part 21 by the fan, and the air flow in the first cavity 11 is guided into the internal circulation air inlet part 31 and/or the second cavity 12 through the cavity air outlet part 22. Because the air current of cavity air inlet portion 21 and internal circulation air-out portion 32 is the cold air current after the air conditioner 30 refrigeration, if set up cavity air inlet portion 21 or internal circulation air-out portion 32 to adopt the form of fan, the fan can increase the air current here, and the strong air current directly blows to the higher unmanned aerial vehicle battery of temperature or other positions and easily forms the condensation on the surface, probably influences unmanned aerial vehicle and charges and other operations. Therefore, the cavity air outlet part 22 and/or the internal circulation air inlet part 31 can be set to be in a fan form, so that the function of forming and guiding air flow is achieved, and meanwhile, the generation of condensation can be prevented.

As shown in fig. 7, in some embodiments of the present application, an operation platform 20 is connected to the main body 13, and the operation platform 20 has an open state capable of opening the second cavity 12 and a closed state closing the second cavity 12. When the operation platform 20 is in the open state, the air conditioner 30 and/or other components in the second chamber 12 can be mounted, dismounted, maintained, cleaned, and the like through the open port of the second chamber 12, so that the operation is more convenient. Specifically, one side of the operation platform 20 is pivotably connected to the main body portion 13; alternatively, the operation platform 20 may be integrally detachably attached to the main body 13. The pivotal connection of the operation platform 20 includes, but is not limited to, one operation platform 20, and the second cavity 12 can be completely enclosed by one operation platform 20; the other is that the operation platform 20 is multiple (for example, two), the outer side of each operation platform 20 is pivotally connected with the main body 13, when each operation platform 20 is in the closed state, the multiple operation platforms 20 are spliced or overlapped, and together enclose the second cavity 12.

Further, as shown in fig. 3, the external circulation air intake part 33 of the air conditioner 30 includes an external circulation air intake 331 and a dust-proof structure 332 detachably disposed at the external circulation air intake 331. The dust-proof structure 332 can filter the external air, thereby preventing impurities such as dust from entering the inside of the air conditioner 30. When the operation platform 20 is in the open state, the dust-proof structure 332 can be removed from the opening of the second cavity 12, so as to facilitate maintenance, cleaning or replacement. Specifically, in some embodiments, the dust-proof structure 332 may be of a pull-out type, that is, the dust-proof structure 332 is slidably connected to the external circulation air inlet 331, and when the operation platform 20 is in the open state, the dust-proof structure 332 may be pulled out through the opening at the top of the second cavity 12. The specific type of the dust-proof structure 332 may be various, and for example, may be a dust screen, a dust plate, or the like.

As shown in fig. 1 and 4-7, in some embodiments of the present application, the housing 10 has an external air inlet portion 15 and an external air outlet portion 16. The "external air inlet portion" refers to a member directly contacting with the outside and supplying external air, and the "external air outlet portion" refers to a member directly contacting with the outside and supplying air to the outside. The external air inlet portion 15 communicates with an external circulation air inlet portion 33 of the air conditioner 30, and the external air outlet portion 16 communicates with an external circulation air outlet portion 34 of the air conditioner 30. Wherein, the external air inlet part 15 and the external air outlet part 16 are symmetrically arranged at two opposite sides of the shell 10; and/or the external circulation air inlet part 33 and the external circulation air outlet part 34 are symmetrically arranged at two sides of the air conditioner 30. On one hand, the external air inlet part 15 and the external air outlet part 16 are parts which can be directly seen from the outside, and the two parts are symmetrically arranged, so that the appearance is more attractive and complete; on the other hand, the external circulation air inlet part 33 and the external circulation air outlet part 34 are symmetrically arranged on two sides of the air conditioner 30, so that the flow direction of the external circulation air flow of the air conditioner 30 is simpler, and the arrangement of internal components of the air conditioner 30 is convenient.

Preferably, the unmanned aerial vehicle basic station still includes second wind channel structure 50 and second heat-proof structure 60, and second wind channel structure 50 sets up between outside air-out portion 16 and outer circulation air-out portion 34 to guide the air-out. A second insulating structure 60 is provided on the second air duct structure 50 to insulate the air flow passage of the second air duct structure 50. The second heat insulating structure 60 may take various forms, for example, the second heat insulating structure 60 includes an insulating layer disposed inside or outside the second air duct structure 50; alternatively, the second air duct structure 50 itself is made of a thermal insulating material, such that the second air duct structure 50 forms the second insulating structure 60. Since the temperature of the air flow in the external circulation air outlet portion 34 of the air conditioner 30 is high, the inside of the second air duct structure 50 through which the air flow flows is insulated, so that the heat in the air flow is prevented from being diffused into the second cavity 12, and other components in the second cavity 12 are prevented from being affected. In addition, the unmanned aerial vehicle basic station can also include third wind channel structure, and third wind channel structure sets up between outside air inlet portion 15 and extrinsic cycle air inlet portion 33 to guide the air inlet.

In some embodiments of the present application, the drone base station further includes an electrical module disposed within the second cavity 12 and located circumferentially outside of the air conditioner 30. Since these electric modules do not need to be cooled by the cold airflow generated by the cooling of the air conditioner 30, they can be disposed at positions (such as the positions of the second air duct structure 50 and the third air duct structure) that are circumferentially outside the air conditioner 30 and avoid the external circulation of the air conditioner 30, so that the arrangement of the components in the second chamber 12 is more compact and the integration level is higher. At the same time, the heat generated by the electric module can be dissipated through the heat dissipating portion 17 on the side wall of the housing 10. Further, a height of a projection of the electrical module in a radial direction of the air conditioner 30 is equal to or less than a height of a projection of the air conditioner 30 in a radial direction thereof, wherein the "radial direction" refers to a direction perpendicular to a longitudinal center line of the air conditioner 30. That is, the electrical module does not protrude from the air conditioner 30 in the direction of the longitudinal center line of the air conditioner 30, so that the size of the second chamber 12 can be minimized, thereby making the structure more compact and reducing the overall size.

In particular, the type of electrical module may be various. In the specific embodiment shown in the figures, the electrical module comprises a strong current module, a weak current module (control module) or a power module, wherein the power module comprises a current power module and a standby power module. As shown in fig. 1, 4, 5 and 7, the air conditioner 30 has a first side, a second side, a third side and a fourth side sequentially connected in a circumferential direction, the external circulation air inlet portion 33 and the external circulation air outlet portion 34 are respectively disposed on the first side and the third side, a strong current module mounting location 71 and a standby power module mounting location 74 are disposed on an outer side of the second side, a weak current module mounting location 72 and a current power module mounting location 73 are disposed on an outer side of the fourth side, the strong current module mounting location 71 is used for mounting a strong current module, the weak current module mounting location 72 is used for mounting a weak current module, the current power module mounting location 73 is used for mounting a current power module, and the standby power module mounting location 74 is used for mounting a standby power module. A side cover 18 is provided on the outer wall of the main body 13 at a position corresponding to the second side, the side cover 18 is disposed adjacent to the strong electric module mounting position 71, the side cover 18 is openable from the outside, and the strong electric module can be exposed after opening, thereby facilitating the operation of the strong electric module.

In the specific embodiment that fig. 1-7 show, place the middle part of main part 13 in the air conditioner 30 to interior circulation, the extrinsic cycle business turn over wind structure of air conditioner 30 has carried out redesign, compares in the present mode of transplanting standard air conditioner product whole to the unmanned aerial vehicle basic station, and the structure is compacter, and the integrated level is higher, and the position design of each part more is adapted to the product demand, and the overall arrangement is more reasonable.

The application also provides an unmanned aerial vehicle system, including unmanned aerial vehicle and the unmanned aerial vehicle basic station that is used for at least charging unmanned aerial vehicle's battery, the unmanned aerial vehicle basic station is foretell unmanned aerial vehicle basic station. The base station may also be used to perform other types of operations on the drone. For example, the battery or parts of the drone are replaced, data interaction with the drone is performed, and the like. In some embodiments of the present application, the drone base station is primarily used to charge the battery of the drone.

For the embodiments of the present application, it should also be noted that, in a case of no conflict, the embodiments of the present application and features of the embodiments may be combined with each other to obtain a new embodiment.

The above description is only for the specific embodiments of the present application, but the scope of the present application is not limited thereto, and the scope of the present application shall be subject to the scope of the claims.

Claims (20)

1. An unmanned aerial vehicle basic station, its characterized in that includes:

a housing (10);

the unmanned aerial vehicle comprises a shell (10), an operating platform (20) and a control panel, wherein the operating platform (20) is arranged in the shell (10), the operating platform (20) is at least used for charging a battery of the unmanned aerial vehicle, the operating platform (20) at least separates the interior of the shell (10) into a first cavity (11) and a second cavity (12), the first cavity (11) is used for accommodating the unmanned aerial vehicle, and a cavity air inlet part (21) and a cavity air outlet part (22) which are communicated with the first cavity (11) are arranged on the operating platform (20);

air conditioner (30), set up and be in second cavity (12), the inner loop air inlet portion (31) of air conditioner (30) with cavity air-out portion (22) intercommunication, the inner loop air-out portion (32) of air conditioner (30) with cavity air inlet portion (21) directly communicates, the cold air stream that air conditioner (30) refrigeration produced can by cavity air inlet portion (21) directly gets into first cavity (11), with right unmanned aerial vehicle's battery cools off.

2. The drone base station of claim 1,

the internal circulation air inlet part (31) is directly communicated with the cavity air outlet part (22).

3. The drone base station of claim 1 or 2, further comprising:

the first air channel structure (40) is arranged between the cavity air inlet part (21) and the internal circulation air outlet part (32) and/or between the cavity air outlet part (22) and the internal circulation air inlet part (31).

4. The drone base station of claim 3,

one end of the first air duct structure (40) is connected to the operating platform (20), and the other end of the first air duct structure is attached to the air conditioner (30) or a gap is formed between the other end of the first air duct structure and the air conditioner (30); or,

one end of the first air duct structure (40) is connected to the air conditioner (30), and the other end of the first air duct structure is attached to the operating platform (20) or a gap is formed between the operating platform (20).

5. The drone base station of claim 1,

the casing (10) includes main part (13) and cover body portion (14), second cavity (12) are located in main part (13), first cavity (11) are located in cover body portion (14), cover body portion (14) can selectively open or close, the unmanned aerial vehicle base station still includes:

a first heat insulation structure provided on the cover body portion (14) to insulate the first cavity (11).

6. The drone base station of claim 1,

the first cavity (11) is located above the second cavity (12).

7. The drone base station of claim 1,

the quantity of cavity air inlet portion (21) with the quantity of unmanned aerial vehicle's battery is the same, works as unmanned aerial vehicle is located during the assigned position of operation platform (20), cavity air inlet portion (21) with unmanned aerial vehicle's battery one-to-one.

8. The drone base station of claim 7,

the two cavity air inlet parts (21) are symmetrically arranged along the first direction.

9. The drone base station of claim 8,

when the unmanned aerial vehicle is located the assigned position of operation platform (20), first direction with the coincidence of the central line of unmanned aerial vehicle's fuselage or perpendicular.

10. The drone base station of claim 8 or 9,

the cavity air outlet parts (22) are symmetrically arranged along a second direction, and the second direction is perpendicular to the first direction.

11. The drone base station of claim 7,

the cavity air outlet part (22) comprises a cavity air outlet and a fan arranged at the cavity air outlet, the cavity air inlet part (21) is of a fan-free structure, and/or the internal circulation air inlet part (31) comprises an internal circulation air inlet (311) and a fan (312) arranged at the internal circulation air inlet (311), and the internal circulation air outlet part (32) is of a fan-free structure,

wherein, through the fan will the air current of inner loop air-out portion (32) warp cavity air inlet portion (21) introduce to first cavity (11), and will the air current warp in first cavity (11) cavity air-out portion (22) guide to in inner loop air inlet portion (31) and/or in second cavity (12).

12. The drone base station of claim 1,

the casing (10) comprises a main body part (13) and a cover body part (14), the second cavity (12) is located in the main body part (13), the first cavity (11) is located in the cover body part (14), the cover body part (14) can be selectively opened or closed, the operating platform (20) is connected to the main body part (13), and the operating platform (20) has an opening state capable of opening the second cavity (12) and a closing state capable of closing the second cavity (12).

13. The drone base station of claim 12,

one side of the operating platform (20) is pivotally connected to the main body part (13); alternatively, the operation platform (20) is integrally detachably connected to the main body (13).

14. The drone base station of claim 12 or 13,

the external circulation air inlet part (33) of the air conditioner (30) comprises an external circulation air inlet (331) and a dustproof structure (332) which is detachably arranged at the external circulation air inlet (331), and when the operating platform (20) is in the open state, the dustproof structure (332) can be disassembled and assembled through the open port of the second cavity (12).

15. The drone base station of claim 1,

the shell (10) is provided with an external air inlet part (15) and an external air outlet part (16), the external air inlet part (15) is communicated with an external circulation air inlet part (33) of the air conditioner (30), the external air outlet part (16) is communicated with an external circulation air outlet part (34) of the air conditioner (30), wherein,

the external air inlet part (15) and the external air outlet part (16) are symmetrically arranged at two opposite sides of the shell (10); and/or the presence of a gas in the gas,

the external circulation air inlet part (33) and the external circulation air outlet part (34) are symmetrically arranged on two sides of the air conditioner (30).

16. The drone base station of claim 1,

casing (10) have outside air-out portion (16), outside air-out portion (16) with the extrinsic cycle air-out portion (34) intercommunication of air conditioner (30), the unmanned aerial vehicle basic station still includes:

the second air duct structure (50) is arranged between the external air outlet part (16) and the external circulating air outlet part (34);

and the second heat insulation structure (60) is arranged on the second air duct structure (50) so as to insulate the airflow channel of the second air duct structure (50).

17. The drone base station of claim 1, further comprising:

an electrical module disposed within the second cavity (12) and located circumferentially outward of the air conditioner (30).

18. The drone base station of claim 17,

the height of the projection of the electrical module along the radial direction of the air conditioner (30) is less than or equal to the height of the projection of the air conditioner (30) along the radial direction thereof.

19. The drone base station of claim 17 or 18,

the electric module comprises a strong current module, a weak current module or a power supply module.

20. A drone system comprising a drone and a drone base station for at least charging a battery of the drone, the drone base station being the drone base station of any one of claims 1 to 19.

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