Unmanned aerial vehicle multi-hangar

Abstract

The unmanned aerial vehicle multi-hangar comprises a storage assembly, a track assembly and a monitoring assembly, the storage assembly comprises a base and a storage piece which are connected with each other, and the base is suitable for being arranged on the ground; the storage part is provided with a storage cavity with one side open, and a first mounting surface, a second mounting surface and a third mounting surface which participate in forming the storage cavity, and the first mounting surface, the second mounting surface and the third mounting surface are perpendicular to one another; the rail assembly comprises a first rail and a plurality of second rails, the first rail is vertically arranged on the first mounting surface, any second rail is horizontally arranged on the first mounting surface, the second mounting surface and the third mounting surface, all the second rails are arranged at intervals, and the first rail and the second rails are arranged on the first mounting surface in an intersecting mode; the monitoring assembly comprises a monitoring piece and a driving unit which are connected with each other, and the driving unit is slidably connected with the rail assembly. The unmanned aerial vehicle multi-hangar with the structure is beneficial to reducing the cost of the unmanned aerial vehicle multi-hangar.

Description

Technical Field

[0001] The utility model relates to the technical field of parking devices, in particular to a multi-hangar for unmanned aerial vehicles. Background Art

[0002] In recent years, with the rapid development of the internet and the Internet of Things, drones have found widespread application in many areas of modern society, such as forestry, power grids, maritime security, surveying and mapping, and other related industries. Drones can perform tasks such as reconnaissance, detection, and inspection. For example, they can be used in scenarios where no one is present for extended periods of time but drone operations are still necessary, and they can monitor and inspect fixed areas.

[0003] In the existing technology, when a drone completes an operation task such as reconnaissance, detection or inspection, a drone hangar is needed to store the drone to ensure that the drone will not be damaged by the outside world, and to enable the drone to monitor and inspect the surrounding area with the hangar as the center. At the same time, the hangar can realize the fully automatic take-off and landing of the drone, as well as charging, battery replacement, and load-bearing. In order to ensure that the drone can take off and land smoothly and charge, it is necessary to set up a surveillance camera in the hangar to monitor the drone's take-off and landing process and the charging process to ensure that the drone's take-off and landing and charging can proceed normally. In order to accommodate more drones at the same time, multiple drone hangars can be merged together to form a drone multi-hangar, so that one drone multi-hangar can accommodate more drones.

[0004] However, in order to monitor the drones in each hangar, surveillance cameras need to be installed in each hangar to monitor the drones, which results in high costs for multiple hangars for drones. Utility Model Content

[0005] Therefore, the technical problem to be solved by the present invention is to overcome the defect that in order to monitor the drones in each hangar, a surveillance camera needs to be installed in each hangar to monitor the drones, thereby causing high costs for multiple hangars for drones.

[0006] To this end, the present invention provides a multi-hangar for unmanned aerial vehicles, comprising:

[0007] The storage assembly includes a base and a storage member connected to each other, wherein the base is suitable for being placed on the ground, and the storage member has a storage cavity with an opening on one side and a first mounting surface, a second mounting surface, and a third mounting surface that form the storage cavity, wherein the first mounting surface, the second mounting surface, and the third mounting surface are arranged perpendicular to each other;

[0008] The track assembly includes a first track and a plurality of second tracks. The first track is vertically arranged on the first mounting surface, and any one of the second tracks is horizontally arranged on the first mounting surface, the second mounting surface and the third mounting surface. All the second tracks are arranged at intervals, and the first track and the second tracks intersect on the first mounting surface;

[0009] The monitoring assembly includes a monitoring member and a driving unit connected to each other. The driving unit is slidably connected to the track assembly so that the driving unit drives the monitoring member to slide along the extending direction of the first track and / or the second track.

[0010] Optionally, in the above-mentioned multi-drone hangar, along the extending direction of the first track, a first rack is arranged on the first track; the driving unit includes a first telescopic member, a first driving member and a first gear. One end of the first telescopic member is connected to the monitoring member and the other end is connected to the first driving member. The driving end of the first driving member is connected to the first gear, and the first gear is meshed and connected to the first rack.

[0011] Optionally, in the above-mentioned multi-drone hangar, along the extending direction of the second track, a second rack is arranged on the second track; the driving unit further includes a second telescopic member, a second driving member and a second gear. One end of the second telescopic member is connected to the monitoring member and the other end is connected to the second driving member. The driving end of the second driving member is connected to the second gear, and the second gear is meshed and connected to the second rack.

[0012] Optionally, in the above-mentioned multi-drone hangar, the first track and all the second tracks are of an integrally formed structure, and a plurality of connecting parts are arranged at the intersection of the first track and the second tracks. All the connecting parts are arranged in an array and any two adjacent connecting parts are arranged at intervals.

[0013] Optionally, in the above-mentioned multi-drone hangar, the monitoring assembly further includes a mounting member which is adapted to be slidably connected to the track assembly, and the mounting member has a first mounting cavity and a second mounting cavity arranged at intervals. The monitoring member is arranged in the first mounting cavity, and the driving unit is arranged in the second mounting cavity.

[0014] Optionally, in the above-mentioned multi-drone hangar, a recessed part is formed on the mounting member, and clamping parts are arranged on both the first track and the second track. When connecting the mounting member and the track, the recessed part is clamped with the clamping part.

[0015] Optionally, in the above-mentioned multi-drone hangar, the monitoring component further includes a power supply component and a control component. The power supply component and the control component are both arranged in the first installation cavity, and the power supply component is electrically connected to the monitoring component, the first driving component and the second driving component. The control component is electrically connected to an external system to control the movement of the monitoring component.

[0016] Optionally, in the above-mentioned multi-drone hangar, a plurality of first installation parts are spaced apart on the second installation surface, and a plurality of second installation parts are spaced apart on the third installation surface. The first installation parts and the second installation parts are arranged in one-to-one correspondence;

[0017] It further includes a plurality of bearing components. Any one of the bearing components is suitable for bearing a drone, and both sides of any one of the bearing components are respectively suitable for slidingly connecting with a first installation part and a second installation part, so that under an external force, the bearing component enters or exits the storage cavity.

[0018] Optionally, in the above-mentioned multi-drone hangar, the bearing component includes a bearing part and a closing part connected to each other. Both sides of the bearing part are respectively suitable for slidingly connecting with the first installation part and the second installation part. The closing part is suitable for closing part of the opening when the bearing part enters the storage cavity.

[0019] Optionally, in the above-mentioned multi-drone hangar, any one of the installation parts extends from the opening towards the first installation surface, and there is a gap between the end of any one of the installation parts far from the opening and the first installation surface.

[0020] The technical solution provided by the present utility model has the following advantages:

[0021] 1. The multi-drone hangar provided by the present utility model includes a track assembly and a monitoring assembly disposed within a storage assembly. The storage assembly includes a base and a storage member connected to each other. The base can be placed on the ground, and the storage member has a storage cavity with one side open, as well as a first mounting surface, a second mounting surface, and a third mounting surface that participate in forming the storage cavity. The first mounting surface, the second mounting surface, and the third mounting surface are perpendicular to each other, and the first mounting surface is opposite to the opening, while the second mounting surface is opposite to the third mounting surface. The track assembly specifically includes a first track and several second tracks. Among them, the first track is vertically disposed on the first mounting surface, and each second track is horizontally disposed on the first mounting surface, the second mounting surface, and the third mounting surface, that is, each second track spans across the three mounting surfaces, and all the second tracks are spaced apart from each other. At the same time, the overlapping part where the first track and the second tracks intersect on the first mounting surface is provided in a coincident manner. The monitoring assembly specifically includes a monitoring member and a driving unit connected to each other. Among them, the driving unit is slidably connected to the track assembly. Thus, when the driving unit slides on the track assembly, the driving unit can drive the monitoring member to slide on the track assembly, that is, the monitoring member can slide along the extension direction of the first track or the second track, so that the monitoring member can move to the top, bottom, and both sides of the storage cavity, and further enables the monitoring member to perform all-round monitoring on the drones stored in the storage cavity, avoiding the need to arrange monitoring members at the top, bottom, and both sides of the storage cavity respectively to monitor the drones, which is beneficial to reducing the cost of the multi-drone hangar. BRIEF DESCRIPTION OF THE DRAWINGS

[0022] In order to more clearly illustrate the specific embodiments of the present utility model or the technical solutions in the prior art, the following will briefly introduce the drawings required for use in the description of the specific embodiments or the prior art. Obviously, the drawings in the following description are some embodiments of the present utility model. For those of ordinary skill in the art, without creative efforts, other drawings can also be obtained based on these drawings.

[0023] Figure 1 It is a schematic structural diagram of the multi-drone hangar provided in the embodiment of the present utility model;

[0024] Figure 2 It is a schematic structural diagram of the first perspective of the storage assembly, the track assembly, and the monitoring assembly provided in the embodiment of the present utility model; [[ID=IS=14]]

[0025] Figure 3 It is a schematic structural diagram of the second perspective of the storage assembly, the track assembly, and the monitoring assembly provided in the embodiment of the present utility model;

[0026] Figure 4 It is a schematic structural diagram of the track assembly provided in the embodiment of the present utility model;

[0027] Figure 5 The first perspective structural schematic diagram of the monitoring component provided in the embodiment of the present utility model;

[0028] Figure 6 The second perspective structural schematic diagram of the monitoring component provided in the embodiment of the present utility model;

[0029] Figure 7 The structural schematic diagram of the bearing component provided in the embodiment of the present utility model;

[0030] Explanation of reference numerals:

[0031] 1 - Storage component; 11 - Base; 12 - Storage member; 121 - First mounting surface; 122 - Second mounting surface; 1221 - First mounting portion; 123 - Third mounting surface; 1231 - Second mounting portion;

[0032] 2 - Track component; 21 - First track; 211 - First rack; 22 - Second track; 221 - Second rack; 222 - Connecting portion; 223 - Clamping portion;

[0033] 3 - Monitoring component; 31 - Monitoring member; 321 - First telescopic member; 322 - First driving member; 323 - First gear; 324 - Second telescopic member; 325 - Second driving member; 326 - Second gear; 33 - Mounting member; 331 - Concave portion;

[0034] 4 - Bearing component; 41 - Bearing member; 42 - Sealing member. Detailed implementation manners

[0035] Next, the technical solutions of the present utility model will be clearly and completely described in conjunction with the accompanying drawings. Obviously, the described embodiments are some, but not all, of the 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 protection scope of the present utility model.

[0036] In the description of the present utility model, it should be noted that the orientation or positional relationship indicated by the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. is based on the orientation or positional relationship shown in the accompanying drawings, and 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 therefore should not be construed as a limitation of the present utility model. In addition, the terms "first" and "second" are only used for descriptive purposes and cannot be construed as indicating or implying relative importance.

[0037] In the description of the present utility model, it should be noted that unless otherwise clearly specified and defined, the terms "installation", "connection", and "coupling" should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium, and it can be the communication inside two components. For those of ordinary skill in the art, the specific meanings of the above terms in the present utility model can be understood according to specific circumstances.

[0038] In addition, the technical features involved in different embodiments of the present utility model described below can be combined with each other as long as they do not conflict with each other.

[0039] Embodiment 1

[0040] This embodiment provides a multi-aircraft hangar for drones. As Figures 1 to 7 shown, it includes a storage component 1, a track component 2, and a monitoring component 3. The storage component 1 includes a base 11 and a storage member 12 that are connected to each other. The base 11 is adapted to be disposed on the ground. The storage member 12 has a storage cavity with one side being open, and a first mounting surface 121, a second mounting surface 122, and a third mounting surface 123 that participate in forming the storage cavity. The first mounting surface 121, the second mounting surface 122, and the third mounting surface 123 are perpendicularly arranged pairwise; the track component 2 includes a first track 21 and a plurality of second tracks 22. The first track 21 is vertically disposed on the first mounting surface 121. Any one of the second tracks 22 is horizontally disposed on the first mounting surface 121, the second mounting surface 122, and the third mounting surface 123. All the second tracks 22 are spaced apart from each other, and the first track 21 and the second tracks 22 intersect on the first mounting surface 121; the monitoring component 3 includes a monitoring member 31 and a driving unit that are connected to each other. The driving unit is slidably connected to the track component 2 so that the driving unit drives the monitoring member 31 to slide along the extending direction of the first track 21 and / or the second track 22.

[0041] The multi-drone hangar with the above structure, through the track assembly 2 and the monitoring assembly 3 arranged in the storage assembly 1. Among them, the storage assembly 1 includes a base 11 and a storage member 12 connected to each other. The storage member 12 is a storage box in this embodiment. The base 11 can be placed on the ground, and the storage member 12 has a storage cavity with one side open, and a first mounting surface 121, a second mounting surface 122, and a third mounting surface 123 that participate in forming the storage cavity. The first mounting surface 121, the second mounting surface 122, and the third mounting surface 123 are perpendicular to each other, and the first mounting surface 121 is opposite to the opening, and the second mounting surface 122 is opposite to the third mounting surface 123. The track assembly 2 specifically includes a first track 21 and several second tracks 22. Among them, the first track 21 is vertically arranged on the first mounting surface 121, and each second track 22 is horizontally arranged on the first mounting surface 121, the second mounting surface 122, and the third mounting surface 123, that is, each second track 22 straddles the three mounting surfaces, and all the second tracks 22 are spaced apart from each other. At the same time, the overlapping part where the first track 21 and the second tracks 22 intersect on the first mounting surface 121 is arranged in coincidence.

[0042] In addition, the monitoring assembly 3 specifically includes a monitoring member 31 and a driving unit connected to each other. The monitoring member 31 is a monitoring camera in this embodiment. Among them, the driving unit is slidably connected to the track assembly 2. When the driving unit slides on the track assembly 2, the driving unit can drive the monitoring member 31 to slide on the track assembly 2, that is, the monitoring member 31 can slide along the extension direction of the first track 21 or the second track 22, so that the monitoring member 31 can move to the top, bottom, and both sides of the storage cavity, and further enables the monitoring member 31 to perform omnidirectional monitoring on the drones stored in the storage cavity, avoiding the need to arrange monitoring members 31 at the top, bottom, and both sides of the storage cavity respectively to monitor the drones, which is beneficial to reducing the cost of the multi-drone hangar.

[0043] Among them, when the monitoring member 31 moves to the second mounting surface 122 and the third mounting surface 123, since the charging ports of the drones are mainly arranged on both sides of them, the monitoring member 31 can monitor the charging situation of the drones stored in the storage cavity to observe whether the drones are successfully charged. When the monitoring member moves to the first mounting surface 121, the monitoring member can monitor the takeoff and landing of the drones to observe whether the drones can take off or land smoothly.

[0044] Specifically, a main unit and a WI-FI router are further disposed in the storage cavity. Among them, the main unit can emit WI-FI signals, so that the WI-FI router can receive the WI-FI signals emitted by the main unit and transmit the WI-FI signals to the monitoring member 31. Furthermore, the monitoring member 31 can monitor the drone through the WI-FI signals and send the monitored situation to the management platform through the WI-FI signals.

[0045] The multi-drone hangar provided in this embodiment, as Figures 1 to 6 shown, along the extension direction of the first track 21, a first rack 211 is disposed on the first track 21; the driving unit includes a first telescopic member 321, a first driving member 322 and a first gear 323. One end of the first telescopic member 321 is connected to the monitoring member 31, and the other end is connected to the first driving member 322. The driving end of the first driving member 322 is connected to the first gear 323, and the first gear 323 is meshed and connected to the first rack 211.

[0046] For the multi-drone hangar with the above structure, through the first rack 211 disposed on the first track 21 and the driving unit including the first telescopic member 321, the first driving member 322 and the first gear 323, the first telescopic member 321 and the first driving member 322 are respectively a first telescopic rod and a first motor in this embodiment. Among them, the first rack 211 is disposed along the extension direction of the first track 21. One end of the first telescopic member 321 is connected to the monitoring member 31, and the other end is connected to the first driving member 322. The driving end of the first driving member 322 is connected to the first gear 323, and the first gear 323 can be meshed and connected to the first rack 211. Thus, when it is necessary to move the monitoring member 31 in the vertical direction in the storage cavity, the first telescopic member 321 can be used to drive the first gear 323 to mesh with the first rack 211. Furthermore, under the drive of the first driving member 322, the first gear 323 can rotate and can drive the first driving member 322, the first telescopic member 321 and the monitoring member 31 to slide on the first track 21, so as to realize the movement of the monitoring member 31 in the vertical direction in the storage cavity.

[0047] The multi-drone hangar provided in this embodiment, as Figures 1 to 6 shown, along the extension direction of the second track 22, a second rack 221 is disposed on the second track 22; the driving unit further includes a second telescopic member 324, a second driving member 325 and a second gear 326. One end of the second telescopic member 324 is connected to the monitoring member 31, and the other end is connected to the second driving member 325. The driving end of the second driving member 325 is connected to the second gear 326, and the second gear 326 is meshed and connected to the second rack 221.

[0048] The multi-drone hangar with the above structure, through the second rack 221 arranged on the second track 22 and the drive unit further including a second telescopic member 324, a second drive member 325 and a second gear 326. The second telescopic member 324 and the second drive member 325 are respectively a second telescopic rod and a second motor in this embodiment. Among them, the second rack 221 is arranged along the extending direction of the second track 22. One end of the second telescopic member 324 is connected to the monitoring member 31, and the other end is connected to the second drive member 325. The drive end of the second drive member 325 is connected to the second gear 326. The second gear 326 can be meshed and connected with the first rack 211. Thus, when it is necessary to move the monitoring member 31 in the horizontal direction in the storage cavity, the second telescopic member 324 can be used to drive the second gear 326 to mesh with the second rack 221. Then, under the drive of the second drive member 325, the second gear 326 can rotate and can drive the second drive member 325, the second telescopic member 324 and the monitoring member 31 to slide on the second track 22, so as to realize the movement of the monitoring member 31 in the horizontal direction in the storage cavity.

[0049] The multi-drone hangar provided in this embodiment, as Figures 1 to 4 shown, the first track 21 and all the second tracks 22 are of an integrally formed structure, and a plurality of connecting parts 222 are arranged at the intersection of the first track 21 and the second track 22. All the connecting parts 222 are arranged in an array, and any two adjacent connecting parts 222 are spaced apart.

[0050] For the multi-drone hangar with the above structure, by setting the first track 21 and the second track 22 to be of an integrally formed structure and a plurality of connecting parts 222 arranged at the intersection of the first track 21 and the second track 22. The connecting parts 222 are connecting blocks in this embodiment. Thus, when installing the track assembly 2 in the storage cavity, the first track 21 and the second track 22 can be directly installed in the storage cavity at the same time, which is beneficial to improving the installation efficiency of the track assembly 2.

[0051] In addition, all the connecting parts 222 are specifically arranged in an array at the intersection of the first track 21 and the second track 22, and every two adjacent connecting parts 222 are spaced apart. Thus, when the gear passes through the intersection of the first track 21 and the second track 22, the gear can be meshed with the arrayed connecting parts 222, and in both the horizontal direction and the vertical direction, the gear can be meshed with the arrayed connecting parts 222. This ensures the normal movement of the monitoring member 31 in the vertical direction and the horizontal direction, and the monitoring member 31 can also switch the moving direction through the connecting parts 222 at the intersection of the first track 21 and the second track 22.

[0052] The multi-drone hangar provided in this embodiment, as Figures 1 to 6As shown, the monitoring component 3 further includes a mounting member 33, which is adapted to be slidably connected to the rail assembly 2. The mounting member 33 has a first mounting cavity and a second mounting cavity arranged at intervals. The monitoring member 31 is arranged in the first mounting cavity, and the driving unit is arranged in the second mounting cavity.

[0053] For the multi-drone hangar with the above structure, by providing that the monitoring component 3 further includes a mounting member 33, which is a mounting shell in this embodiment. The mounting member 33 is slidably connected to the rail assembly 2, and the mounting member 33 has a first mounting cavity and a second mounting cavity arranged at intervals. Among them, the monitoring member 31 is arranged in the first mounting cavity, and the driving unit is arranged in the second mounting cavity. Thus, when the gear of the driving unit moves on the rack of the rail assembly 2, the driving unit can drive the mounting member 33 and the monitoring member 31 to move on the rail assembly 2.

[0054] The multi-drone hangar provided in this embodiment, as Figure 4 and Figure 6 shown, a recess 331 is formed on the mounting member 33, and clamping portions 223 are arranged on both the first rail 21 and the second rail 22. When connecting the mounting member 33 and the rail, the recess 331 is clamped with the clamping portion 223.

[0055] For the multi-drone hangar with the above structure, through the recess 331 formed on the mounting member 33 and the clamping portions 223 arranged on the first rail 21 and the second rail 22, the recess 331 is a recessed groove in this embodiment, and the clamping portion 223 is a clamping strip in this embodiment. When connecting the mounting member 33 and the rail, the recess 331 can be clamped with the clamping portion 223. Thus, when the mounting member 33 slides relative to the rail, the recess 331 can slide relative to the clamping portion 223, which provides a guiding function for the sliding of the mounting member 33, and the mutually clamped recess 331 and clamping portion 223 can also enhance the connection strength between the mounting member 33 and the rail.

[0056] The multi-drone hangar provided in this embodiment, as Figure 5 and Figure 6 shown, the monitoring component 3 further includes a power supply component and a control component. The power supply component and the control component are both arranged in the first mounting cavity, and the power supply component is electrically connected to the monitoring member 31, the first driving member 322, and the second driving member 325. The control component is electrically connected to an external system to control the movement of the monitoring component 3.

[0057] The multi-drone hangar with the above structure, by providing that the monitoring component 3 further includes a power supply component and a control component, the power supply component and the control component are respectively a battery and a control chip in this embodiment. Among them, both the power supply component and the control component are arranged in the first installation cavity, and the power supply component is electrically connected to the monitoring component 31, the first driving component 322, and the second driving component 325, so as to provide power for the normal operation of the monitoring component 31, the first driving component 322, and the second driving component 325. The control component is electrically connected to the external system, so that under the instruction of the external system, the control component can control the movement of the monitoring component 3.

[0058] The multi-drone hangar provided in this embodiment, as Figures 1 to 3 shown, a plurality of first installation parts 1221 are spaced apart on the second installation surface 122, and a plurality of second installation parts 1231 are spaced apart on the third installation surface 123. The first installation parts 1221 and the second installation parts 1231 are arranged in one-to-one correspondence; it further includes a plurality of carrying components 4. Any one of the carrying components 4 is suitable for carrying a drone, and both sides of any one of the carrying components 4 are respectively suitable for sliding connection with a first installation part 1221 and a second installation part 1231, so that under the action of an external force, the carrying component 4 can enter or exit the storage cavity.

[0059] The multi-drone hangar with the above structure, through a plurality of first installation parts 1221 opened on the second installation surface 122, a plurality of second installation parts 1231 opened on the third installation surface 123, and a plurality of carrying components 4 arranged between the second installation surface 122 and the third installation surface 123. The first installation part 1221 and the second installation part 1231 are respectively a first installation groove and a second installation groove in this embodiment. The first installation part 1221 and the second installation part 1231 are arranged in one-to-one correspondence. The carrying component 4 can carry a drone, and both sides of each carrying component 4 can respectively slide connection with the first installation part 1221 and the second installation part 1231. Thus, under the action of an external force, the carrying component 4 can slide relative to the first installation part 1221 and the second installation part 1231, so that the carrying component 4 can enter or exit the storage cavity, and the drone carried by the carrying component 4 can also enter or exit the storage cavity.

[0060] Specifically, by respectively opening a plurality of first installation parts 1221 and second installation parts 1231 on the second installation surface 122 and the third installation surface 123, a carrying component 4 can be arranged between each pair of corresponding first installation part 1221 and second installation part 1231, so that all the carrying components 4 together divide the storage cavity into a plurality of carrying cavities, and each carrying cavity can place a drone, thus realizing the setting of the multi-drone hangar of the storage component 1.

[0061] Meanwhile, the monitoring member 31 can move to any one of the bearing cavities through the first track 21. When the monitoring member 31 moves to a bearing cavity through the first track 21, the monitoring member 31 can monitor the take-off and landing conditions of the drones in the bearing cavity, and the monitoring member 31 can also move to the second mounting surface 122 and the third mounting surface 123 through the second track 22, so as to monitor the charging conditions of the drones in the bearing cavity.

[0062] The multi-drone hangar provided in this embodiment, such as Figure 7 shown, the bearing assembly 4 includes a bearing member 41 and a closing member 42 that are connected to each other. Both sides of the bearing member 41 are respectively adapted to be slidably connected to the first mounting portion 1221 and the second mounting portion 1231. The closing member 42 is adapted to close part of the opening when the bearing member 41 enters the storage cavity.

[0063] For the multi-drone hangar with the above structure, by setting the bearing assembly 4 to include a bearing member 41 and a closing member 42, the bearing member 41 and the closing member 42 are respectively a bearing plate and a closing plate in this embodiment. Among them, the bearing member 41 can carry the drones, and both sides of the bearing member 41 can be respectively slidably connected to the first mounting portion 1221 and the second mounting portion 1231, so that the bearing member 41 can drive the drones to enter or exit the storage cavity. When the bearing member 41 enters the storage cavity, the closing member 42 can close part of the opening, so as to protect various components arranged in the storage cavity.

[0064] Specifically, when the drones on the bearing member 41 need to take off, since a multi-drone hangar has multiple bearing members 41 and one monitoring member 31, therefore, when the drones on multiple bearing members 41 need to take off, these drones need to take off in sequence so that the monitoring member 31 can monitor the take-off conditions of these drones in sequence. Similarly, when multiple drones flying outside need to land on the bearing member 41, these drones also need to land in sequence, so that the monitoring member 31 can monitor the landing conditions of these drones in sequence.

[0065] It should be noted that when the monitoring member 31 needs to monitor the take-off and landing conditions of multiple drones, the host installed in the storage cavity needs to be used to plan the take-off and landing of these drones, and the position of the monitoring member 31 is adjusted through the WIFI signal sent by the WIFI router, so that these drones can take off or land in sequence, and the monitoring member 31 can timely monitor the drones that need to take off or land.

[0066] The multi-drone hangar provided in this embodiment, such as Figure 2 and Figure 3As shown, any installation part extends from the opening towards the first installation surface 121, and there is a gap between the end of any installation part far from the opening and the first installation surface 121.

[0067] For the multi-drone hangar with the above structure, by setting the installation part to extend from the opening towards the first installation surface 121 and having a gap between the end of the installation part far from the opening and the first installation surface 121, when the carrying component 4 enters the storage cavity, the monitoring component 3 can move within the gap and monitor the drones arranged on the carrying component 4.

[0068] The monitoring process of the multi-drone hangar provided by the present utility model is as follows:

[0069] First, the main machine receives the signal that the drone is ready to land and emits a WI FI signal. The router then transmits this WI FI signal to the monitoring member 31, and the monitoring member 31 moves to the first installation surface 121 under the instruction of this WI FI signal. At the same time, the carrying component 4 exits the carrying cavity to receive the drone. At this time, the monitoring member 31 monitors the landing situation of the drone. Next, the carrying component 4 drives the received drone into the carrying cavity. At this time, the monitoring member 31 monitors the storage situation of the drone. Then, the monitoring member 31 moves to the second installation surface 122 and the third installation surface 123 under the instruction of the WI FI signal to monitor the charging situation of the drones in the carrying cavity. Finally, the carrying component 4 drives the drone out of the carrying cavity, and the drone is ready to take off. At this time, the monitoring member 31 monitors the take-off situation of the drone. Thus, the monitoring component 3 completes the monitoring of the landing, storage, charging, and take-off situations of the drones.

[0070] The multi-drone hangar provided by the present utility model includes a track assembly 2 and a monitoring assembly 3 disposed within a storage assembly 1. The storage assembly 1 includes a base 11 and a storage member 12 connected to each other. The base 11 can be placed on the ground, and the storage member 12 has a storage cavity with one side open, as well as a first mounting surface 121, a second mounting surface 122, and a third mounting surface 123 that participate in forming the storage cavity. The first mounting surface 121, the second mounting surface 122, and the third mounting surface 123 are perpendicular to each other pairwise, and the first mounting surface 121 is opposite to the opening, and the second mounting surface 122 is opposite to the third mounting surface 123. The track assembly 2 specifically includes a first track 21 and a plurality of second tracks 22. Among them, the first track 21 is vertically disposed on the first mounting surface 121, and each second track 22 is horizontally disposed on the first mounting surface 121, the second mounting surface 122, and the third mounting surface 123, that is, each second track 22 straddles the three mounting surfaces and all the second tracks 22 are spaced apart from each other. At the same time, the overlapping part of the first track 21 and the second tracks 22 on the first mounting surface 121 is set to coincide. The monitoring assembly 3 specifically includes a monitoring member 31 and a driving unit connected to each other. Among them, the driving unit is slidably connected to the track assembly 2. Thus, when the driving unit slides on the track assembly 2, the driving unit can drive the monitoring member 31 to slide on the track assembly 2, that is, the monitoring member 31 can slide along the extension direction of the first track 21 or the second tracks 22, so that the monitoring member 31 can move to the top, bottom, and both sides of the storage cavity, and further enables the monitoring member 31 to perform all-round monitoring of the drones stored in the storage cavity, avoiding the need to arrange monitoring members 31 at the top, bottom, and both sides of the storage cavity respectively to monitor the drones, which is beneficial to reducing the cost of the multi-drone hangar.

[0071] Obviously, the above embodiments are merely examples given for clear illustration and not limitations on the implementation manners. For those of ordinary skill in the art, other different forms of changes or variations can be made based on the above description. It is not necessary and impossible to enumerate all the implementation manners here. And the obvious changes or variations derived therefrom are still within the protection scope of the present utility model.

Claims

1. A multi-drone hangar, characterized in that, Comprising: A storage component (1), including a base (11) and a storage member (12) connected to each other. The base (11) is adapted to be disposed on the ground. The storage member (12) has a storage cavity with one side being open, and a first mounting surface (121), a second mounting surface (122), and a third mounting surface (123) that participate in forming the storage cavity. The first mounting surface (121), the second mounting surface (122), and the third mounting surface (123) are perpendicular to each other in pairs. An orbit component (2), including a first orbit (21) and a plurality of second orbits (22). The first orbit (21) is vertically disposed on the first mounting surface (121). Any one of the second orbits (22) is horizontally disposed on the first mounting surface (121), the second mounting surface (122), and the third mounting surface (123). All the second orbits (22) are spaced apart from each other, and the first orbit (21) and the second orbits (22) intersect on the first mounting surface (121). A monitoring component (3), including a monitoring member (31) and a driving unit connected to each other. The driving unit is slidably connected to the orbit component (2) so that the driving unit drives the monitoring member (31) to slide along the extending direction of the first orbit (21) and / or the second orbit (22).

2. The multi-aircraft hangar for unmanned aerial vehicles according to claim 1, wherein Along the extending direction of the first orbit (21), a first rack (211) is disposed on the first orbit (21). The driving unit includes a first telescopic member (321), a first driving member (322), and a first gear (323). One end of the first telescopic member (321) is connected to the monitoring member (31), and the other end is connected to the first driving member (322). The driving end of the first driving member (322) is connected to the first gear (323), and the first gear (323) is meshed with the first rack (211).

3. The multi-drone hangar according to claim 2, characterized in that, Along the extending direction of the second orbit (22), a second rack (221) is disposed on the second orbit (22). The driving unit further includes a second telescopic member (324), a second driving member (325), and a second gear (326). One end of the second telescopic member (324) is connected to the monitoring member (31), and the other end is connected to the second driving member (325). The driving end of the second driving member (325) is connected to the second gear (326), and the second gear (326) is meshed with the second rack (221).

4. The multi-drone hangar according to claim 3, characterized in that, The first orbit (21) and all the second orbits (22) are of an integrally formed structure, and a plurality of connecting portions (222) are disposed at the intersection of the first orbit (21) and the second orbits (22). All the connecting portions (222) are arranged in an array, and any two adjacent connecting portions (222) are spaced apart.

5. The multi-aircraft hangar for unmanned aerial vehicles according to claim 4, characterized in that, The monitoring component (3) further includes a mounting member (33). The mounting member (33) is adapted to be slidably connected to the rail component (2), and the mounting member (33) has a first mounting cavity and a second mounting cavity which are spaced apart. The monitoring member (31) is disposed in the first mounting cavity, and the driving unit is disposed in the second mounting cavity.

6. The multi-drone hangar according to claim 5, characterized in that, A recessed portion (331) is formed on the mounting member (33). Clamping portions (223) are provided on both the first rail (21) and the second rail (22). When connecting the mounting member (33) and the rail, the recessed portion (331) is clamped with the clamping portion (223).

7. The multi-aircraft hangar for drones according to claim 6, characterized in that, The monitoring component (3) further includes a power supply member and a control member. The power supply member and the control member are both disposed in the first mounting cavity, and the power supply member is electrically connected to the monitoring member (31), the first driving member (322), and the second driving member (325). The control member is electrically connected to an external system to control the movement of the monitoring component (3).

8. The multi-drone hangar according to claim 1, characterized in that A plurality of first mounting portions (1221) are spaced apart on the second mounting surface (122), and a plurality of second mounting portions (1231) are spaced apart on the third mounting surface (123). The first mounting portions (1221) and the second mounting portions (1231) are arranged in one-to-one correspondence. It further includes a plurality of carrying components (4). Any one of the carrying components (4) is adapted to carry a drone, and both sides of any one of the carrying components (4) are respectively adapted to be slidably connected to a first mounting portion (1221) and a second mounting portion (1231), so that under an external force, the carrying component (4) enters or exits the storage cavity.

9. The multi-aircraft hangar for unmanned aerial vehicles according to claim 8, wherein, The carrying component (4) includes a carrying member (41) and a closing member (42) which are connected to each other. Both sides of the carrying member (41) are respectively adapted to be slidably connected to the first mounting portion (1221) and the second mounting portion (1231). The closing member (42) is adapted to close a part of the opening when the carrying member (41) enters the storage cavity.

10. The multi-aircraft hangar for unmanned aerial vehicles according to claim 9, wherein Any one of the mounting portions extends from the opening towards the first mounting surface (121), and there is a gap between the end of any one of the mounting portions away from the opening and the first mounting surface (121).

Images