Drawer type unmanned aerial vehicle hangar

Abstract

The drawer type unmanned aerial vehicle hangar comprises a hangar body, a bearing structure and a control structure, the hangar body is provided with a containing cavity, and one side of the containing cavity is open; the bearing structure comprises a driving assembly and a bearing part, the driving assembly is arranged in the containing cavity, the bearing part is suitable for bearing the unmanned aerial vehicle, and the driving end of the driving assembly is connected with the bearing part to drive the bearing part to drive the unmanned aerial vehicle to enter or exit from the containing cavity; the control structure comprises a control piece and a detection piece which are electrically connected, the control piece is arranged in the containing cavity and electrically connected with the driving assembly, and the detection piece is arranged at the end, away from the driving assembly, of the bearing piece and electrically connected with the control piece; the detection part is suitable for detecting distance information between the bearing part and the object and transmitting the distance information to the control part, so that the control part controls the driving assembly to rotate forwards or be closed or rotate backwards or be closed according to the distance information. The drawer type unmanned aerial vehicle hangar with the structure is beneficial to improving the safety of the unmanned aerial vehicle hangar.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, and particularly relates to a drawer-type unmanned aerial vehicle hangar. Background Art

[0002] In recent years, with the rapid development of the Internet and the Internet of Things, unmanned aerial vehicle products have been widely used in many fields of modern society, such as related industries like forestry, power grids, sea areas, surveying and mapping, etc. Unmanned aerial vehicles can complete tasks such as reconnaissance, detection, and inspection. For example, they can be used in scenarios where no one has visited for a long time but where unmanned aerial vehicle operations are required, and can monitor and inspect fixed areas, etc.

[0003] In the prior art, when an unmanned aerial vehicle completes tasks such as reconnaissance, detection, or inspection, an unmanned aerial vehicle hangar is needed to store the unmanned aerial vehicle to ensure that the unmanned aerial vehicle is not damaged by the outside world, and enable the unmanned aerial vehicle to take the hangar as the center and conduct operations such as monitoring and inspection of the surrounding area. At the same time, the hangar can realize functions such as automatic takeoff and landing of the unmanned aerial vehicle, charging, battery replacement, and payload. For a drawer-type unmanned aerial vehicle hangar, most of them use a drawer-type apron to carry the unmanned aerial vehicle. That is, when the unmanned aerial vehicle needs to land in the hangar for charging, the apron can retract outside the hangar, so that the unmanned aerial vehicle can land on the apron. And after the unmanned aerial vehicle lands on the apron, the apron can drive the unmanned aerial vehicle to retract into the hangar, and then charge the unmanned aerial vehicle. When the unmanned aerial vehicle needs to take off, the apron can drive the unmanned aerial vehicle to retract outside the hangar, so that the unmanned aerial vehicle can take off smoothly. And after the unmanned aerial vehicle takes off, the apron can retract into the hangar to avoid damage to the apron by the outside world.

[0004] However, most of the existing drawer-type unmanned aerial vehicle hangars are deployed outdoors, and the movement of the apron on them is straight in and out. When there are pedestrians passing by or obstacles in front of the apron, it may cause harm to pedestrians during the process of the apron being pushed out, or the pushing motor may be blocked due to the obstruction of the obstacle and then the motor may be burned out, resulting in low safety. Summary of the Utility Model

[0005] Therefore, the technical problem to be solved by the utility model is to overcome the defect that the existing drawer-type unmanned aerial vehicle hangar may cause harm to pedestrians in front or be blocked by obstacles in front during the process of the apron being pushed out, resulting in the blocking of the pushing motor and then the burning out of the motor, and thus having low safety.

[0006] For this reason, the utility model provides a drawer-type unmanned aerial vehicle hangar, including:

[0007] A library body having a receiving cavity with one side open;

[0008] A carrying structure, comprising a driving component and a carrier. The driving component is arranged in the accommodation cavity. The carrier is adapted to carry a drone, and a driving end of the driving component is connected to the carrier to drive the carrier to drive the drone into or out of the accommodation cavity;

[0009] A control structure, comprising a control member and a detection member which are electrically connected. The control member is arranged in the accommodation cavity and is electrically connected to the driving component. The detection member is arranged at an end of the carrier away from the driving component and is electrically connected to the control member;

[0010] Wherein, the detection member is adapted to detect distance information between the carrier and an object, and transmit the distance information to the control member, so that the control member controls the driving component to rotate forward or close and rotate backward or close according to the distance information.

[0011] Optionally, the above drawer-type drone hangar further comprises a plurality of partition members. All the partition members are arranged in the accommodation cavity at intervals to divide the accommodation cavity into a plurality of storage cavities. The carrying structure and the control structure are arranged in any one of the storage cavities.

[0012] Optionally, for the above drawer-type drone hangar, the driving component comprises a driving member, a guiding member and a connecting member. The driving member and the guiding member are both arranged on the partition member. The connecting member is slidably connected to the guiding member, and two ends of the connecting member are respectively connected to the carrier and a driving end of the driving member, so that under the drive of the driving member, the connecting member is adapted to drive the carrier to enter or exit the storage cavity.

[0013] Optionally, for the above drawer-type drone hangar, the guiding member has a guiding cavity. The driving member is arranged in the guiding cavity. The connecting member is adapted to extend into the guiding cavity to be connected to the driving end of the driving member and is slidably connected to the guiding member.

[0014] Optionally, for the above drawer-type drone hangar, the driving component further comprises an adapter. The adapter is arranged in the guiding cavity, and one end of the adapter is connected to the driving end of the driving member and the other end is connected to the connecting member.

[0015] Optionally, for the above drawer-type drone hangar, the adapter is provided with threads, and a threaded hole is formed in the connecting member. The connecting member is adapted to be threadedly connected to the threads on the adapter through the threaded hole.

[0016] Optionally, in the above-mentioned drawer-type drone hangar, a yield portion is provided on the carrier, and one end of the connecting member connected to the carrier is suitable for extending into the yield portion and connecting with the carrier, and when the carrier enters the storage cavity, the guide member is arranged in the yield portion.

[0017] Optionally, in the above-mentioned drawer-type drone hangar, at least three of the drive components are arranged in any of the storage cavities, the three drive components are arranged at intervals on the partition, and one drive component is respectively arranged at both ends of the partition.

[0018] Optionally, in the above-mentioned drawer-type drone hangar, the supporting structure also includes a closing member, which is connected to an end of the supporting member away from the driving assembly, and the closing member and the supporting member are vertically arranged so that when the supporting member enters the storage cavity, the closing member closes part of the opening.

[0019] Optionally, in the above-mentioned drawer-type UAV hangar, an anti-slip member is provided on the bearing member, and when the UAV lands on the bearing member, the UAV contacts the anti-slip member.

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

[0021] 1. The drawer - type UAV hangar provided by the present utility model, through the load - bearing structure and control structure arranged in the hangar body, the hangar body has a receiving cavity with one side open. The load - bearing structure includes a driving component and a load - bearing member. Among them, the driving component is arranged in the receiving cavity, and the load - bearing member can carry the UAV, and the driving end of the driving component is connected to the load - bearing member. Thus, driven by the driving component, the load - bearing member can drive the UAV to enter or exit the receiving cavity, and then realize the operations of UAV landing storage and take - off preparation. The control structure specifically includes a control part and a detection part which are electrically connected. Among them, the control part is arranged in the receiving cavity and is electrically connected to the driving component, and the detection part is arranged at one end of the load - bearing member far from the driving component and is electrically connected to the control part. And the detection part can detect the distance between the load - bearing member and the object in front of it, and can transmit the detected distance information to the control part, so that the control part can control the forward rotation or shutdown and reverse rotation and shutdown of the driving component according to the distance information. That is, when the load - bearing member drives the UAV to exit the receiving cavity, if there is an object in front of the load - bearing member, then the detection part can detect the distance between the end of the load - bearing member far from the driving component and the object. And when the distance allows the load - bearing member to completely exit the receiving cavity and the control part receives the distance information, the control part will not control the driving component to shut down, but still control the driving component to rotate forward to drive the load - bearing member to completely exit the receiving cavity. And when the distance does not allow the load - bearing member to completely exit the receiving cavity, the control part will, after receiving the distance information, control the driving component to shut down and control the driving component to rotate in reverse, so that the load - bearing member drives the UAV to re - enter the receiving cavity, to avoid the end of the load - bearing member far from the driving component colliding with the object and causing damage to the object and the load - bearing member, and to avoid the situation that after the load - bearing member collides with the object, the driving component still drives the load - bearing member to exit the receiving cavity, resulting in damage due to the driving component being unable to drive the load - bearing member to move. Therefore, by installing the control structure in the receiving cavity, damage to the load - bearing structure and the object can be avoided, which is beneficial to improving the safety of the UAV 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 following - described drawings are some embodiments of the present utility model. For those of ordinary skill in the art, without creative efforts, other drawings can be obtained based on these drawings.

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

[0024] Figure 2 It is a schematic structural diagram of the load - bearing structure provided in the embodiment of the present utility model;

[0025] Figure 3 This is the working flowchart of the drawer - type UAV hangar provided in the embodiment of the present utility model;

[0026] Explanation of reference numerals:

[0027] 1 - Library body;

[0028] 2 - Bearing structure; 21 - Driving component; 211 - Guide; 212 - Connecting piece; 22 - Carrier;

[0029] 31 - Detection piece; 4 - Partition piece; 5 - UAV. Specific implementation manners

[0030] 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 part of the embodiments of the present utility model, rather than all of them. 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.

[0031] 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 drawings. It is only for the convenience of describing the present utility model and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus cannot be understood as a limitation to the present utility model. In addition, the terms "first" and "second" are only used for descriptive purposes and cannot be understood as indicating or implying relative importance.

[0032] In the description of the present utility model, it should be noted that unless otherwise clearly specified and limited, the terms "installation", "connection", and "connection" 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 directly connected or indirectly connected through an intermediate medium, and it can be the communication inside two elements. 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 situations.

[0033] 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.

[0034] Embodiment

[0035] This embodiment provides a drawer - type UAV hangar, as Figures 1 to 3As shown in the figure, it includes a library body 1, a bearing structure 2 and a control structure. The library body 1 has a receiving cavity with one side open; the bearing structure 2 includes a driving component 21 and a bearing member 22. The driving component 21 is arranged in the receiving cavity. The bearing member 22 is suitable for bearing the drone 5, and the driving end of the driving component 21 is connected to the bearing member 22 to drive the bearing member 22 to drive the drone 5 to enter or exit the receiving cavity; the control structure includes a control member and a detection member 31 which are electrically connected. The control member is arranged in the receiving cavity and is electrically connected to the driving component 21. The detection member 31 is arranged at one end of the bearing member 22 away from the driving component 21 and is electrically connected to the control member; wherein, the detection member 31 is suitable for detecting the distance information between the bearing member 22 and an object, and transmitting the distance information to the control member, so that the control member controls the driving component 21 to rotate forward or close and rotate backward or close according to the distance information.

[0036] For the drawer-type drone hangar with the above structure, through the bearing structure 2 and the control structure arranged in the library body 1, the library body 1 has a receiving cavity with one side open. The bearing structure 2 includes a driving component 21 and a bearing member 22. The bearing member 22 is a helipad in this embodiment. Among them, the driving component 21 is arranged in the receiving cavity, and the bearing member 22 can bear the drone 5. The driving end of the driving component 21 is connected to the bearing member 22. Thus, driven by the driving component 21, the bearing member 22 can drive the drone 5 to enter or exit the receiving cavity, and then realize the operations of landing storage and takeoff preparation of the drone 5. The control structure specifically includes a control member and a detection member 31 which are electrically connected. The control member and the detection member 31 are an MCU control board and a distance sensor respectively in this embodiment. Among them, the control member is arranged in the receiving cavity and is electrically connected to the driving component 21. The detection member 31 is arranged at one end of the bearing member 22 away from the driving component 21 and is electrically connected to the control member. The detection member 31 can detect the distance between the bearing member 22 and the object in front of it, and can transmit the detected distance information to the control member, so that the control member can control the forward rotation or closing and reverse rotation and closing of the driving component 21 according to the distance information.

[0037] Specifically, when the carrier 22 drives the UAV 5 to exit the accommodation cavity, if there is an object at the front end of the carrier 22, the detector 31 can detect the distance between the end of the carrier 22 away from the drive assembly 21 and the object. And when the distance allows the carrier 22 to completely exit the accommodation cavity and the control member receives the distance information, the control member does not control the drive assembly 21 to close, but still controls the drive assembly 21 to rotate forward to drive the carrier 22 to completely exit the accommodation cavity. When the distance does not allow the carrier 22 to completely exit the accommodation cavity, the control member will, after receiving the distance information, control the drive assembly 21 to close and control the drive assembly 21 to rotate reversely, so that the carrier 22 drives the UAV 5 to re-enter the accommodation cavity to avoid the end of the carrier 22 away from the drive assembly 21 colliding with the object and causing damage to the object and the carrier 22, and can avoid the situation that after the carrier 22 collides with the object, the drive assembly 21 still drives the carrier 22 to exit the accommodation cavity, resulting in damage to the drive assembly 21 due to its inability to drive the carrier 22 to move.

[0038] Therefore, by installing the control structure in the accommodation cavity, damage to the carrier structure 2 and the object can be avoided, which is beneficial to improving the safety of the UAV hangar.

[0039] The drawer-type UAV hangar provided in this embodiment, as Figure 1 shown, further includes a plurality of partition members 4. All the partition members 4 are arranged at intervals in the accommodation cavity to divide the accommodation cavity into a plurality of storage cavities, and a carrier structure 2 and a control structure are arranged in any one of the storage cavities.

[0040] For the drawer-type UAV hangar with the above structure, through the plurality of partition members 4 arranged in the accommodation cavity, the partition members 4 are partition plates in this embodiment, and all the partition members 4 are arranged at intervals in the accommodation cavity, so as to divide the accommodation cavity into a plurality of storage cavities, and a carrier structure 2 and a control structure are arranged in each storage cavity, thereby enabling a UAV hangar to accommodate multiple UAVs 5 at the same time.

[0041] The drawer-type UAV hangar provided in this embodiment, as Figure 1 and Figure 2 shown, the drive assembly 21 includes a drive member, a guide member 211 and a connecting member 212. The drive member and the guide member 211 are both arranged on the partition member 4. The connecting member 212 is slidably connected to the guide member 211, and both ends of the connecting member 212 are respectively connected to the carrier 22 and the drive end of the drive member, so as to drive the carrier 22 to enter or exit the storage cavity under the drive of the drive member.

[0042] For the drawer - type UAV hangar with the above - mentioned structure, by setting that the driving assembly 21 includes a driving member, a guiding member 211 and a connecting member 212. The driving member, the guiding member 211 and the connecting member 212 are respectively a driving motor, a guiding housing and a connecting rod in this embodiment. Among them, both the driving member and the guiding member 211 are arranged on the partition member 4, the connecting member 212 is slidably connected to the guiding member 211, and both ends of the connecting member 212 are respectively connected to the bearing member 22 and the driving end of the driving member. Thus, under the drive of the driving member, the connecting member 212 can slide relative to the guiding member 211 and drive the bearing member 22 to enter or exit the storage cavity, and further realize that the bearing member 22 drives the UAV 5 to enter or exit the storage cavity, so as to prepare for the landing storage and take - off operation of the UAV 5.

[0043] The drawer - type UAV hangar provided in this embodiment, as Figure 2 shown, the guiding member 211 has a guiding cavity, the driving member is arranged in the guiding cavity, the connecting member 212 is adapted to extend into the guiding cavity to be connected to the driving end of the driving member, and is slidably connected to the guiding member 211.

[0044] For the drawer - type UAV hangar with the above - mentioned structure, by setting that the guiding member 211 has a guiding cavity, so that the driving member can be arranged in the guiding cavity, and when the connecting member 212 is slidably connected to the guiding member 211, one end of the connecting member 212 can extend into the guiding cavity to be connected to the driving end of the driving member. Furthermore, under the drive of the driving end of the driving member, the connecting member 212 can drive the bearing member 22 to enter or exit the storage cavity, and enable the UAV 5 to enter or exit the storage cavity.

[0045] The drawer - type UAV hangar provided in this embodiment, as Figure 2 shown, the driving assembly 21 further includes an adapter. The adapter is arranged in the guiding cavity, and one end of the adapter is connected to the driving end of the driving member, and the other end is connected to the connecting member 212.

[0046] For the drawer - type UAV hangar with the above - mentioned structure, by setting that the driving assembly 21 further includes an adapter, the adapter is a connecting rod in this embodiment. The adapter is specifically arranged in the guiding cavity of the guiding member 211, and both ends of the adapter are respectively connected to the driving end of the driving member and the end of the connecting member 212 far from the bearing member 22. Thus, under the drive of the driving member, the adapter can drive the connecting member 212 to slide relative to the guiding member 211, and enable the connecting member 212 to drive the bearing member 22 to enter or exit the storage cavity.

[0047] The drawer - type UAV hangar provided in this embodiment, as Figure 2 shown, the adapter is provided with threads, and a threaded hole is formed in the connecting member 212. The connecting member 212 is adapted to be threadedly connected to the threads on the adapter through the threaded hole.

[0048] For the drawer - type UAV hangar with the above - mentioned structure, through the threads provided on the adapter and the threaded holes opened on the connecting member 212, the connecting member 212 can be threadedly connected to the threads on the adapter through the threaded holes. Thus, when the driving end of the driving member drives the adapter to rotate, the connecting member 212 can move on the adapter through the threaded connection with the adapter and slide relative to the guiding member 211. At the same time, the connecting member 212 can also drive the bearing member 22 to enter or exit the storage cavity.

[0049] The drawer - type UAV hangar provided in this embodiment, as Figure 2 shown, a relief portion is opened on the bearing member 22. One end of the connecting member 212 connected to the bearing member 22 is adapted to extend into the relief portion to be connected to the bearing member 22. And when the bearing member 22 enters the storage cavity, the guiding member 211 is arranged in the relief portion.

[0050] For the drawer - type UAV hangar with the above - mentioned structure, through the relief portion opened on the bearing member 22, the relief portion is a relief groove in this embodiment. Thus, one end of the connecting member 212 connected to the bearing member 22 can extend into the relief portion to be connected to the bearing member 22. And when the driving member drives the connecting member 212 to slide relative to the guiding member 211 and drives the bearing member 22 to enter the storage cavity, the guiding member 211 can extend into the relief portion on the bearing member 22, thereby avoiding the situation that the bearing member 22 cannot enter the storage cavity due to the blockage of the guiding member 211.

[0051] The drawer - type UAV hangar provided in this embodiment, as Figure 2 shown, at least three driving assemblies 21 are arranged in any storage cavity. The three driving assemblies 21 are spaced apart on the partition member 4, and one driving assembly 21 is respectively arranged at both ends of the partition member 4.

[0052] For the drawer - type UAV hangar with the above - mentioned structure, by arranging three driving assemblies 21 in each storage cavity, the three driving assemblies 21 are spaced apart on the partition member 4, and one driving assembly 21 is respectively arranged at both ends of each partition member 4. Thus, when the driving assembly 21 drives the connecting member 212 to drive the bearing member 22 to move, since there are multiple driving assemblies 21, the process of the connecting member 212 driving the bearing member 22 to move is relatively stable, so as to avoid the situation that the UAV 5 on the bearing member 22 falls off the bearing member 22 due to the relatively jerky movement of the bearing member 22, thereby being beneficial to improving the movement stability of the bearing member 22.

[0053] The drawer - type UAV hangar provided in this embodiment, as Figure 1 and Figure 2As shown, the bearing structure 2 further includes a closing member, which is connected to the end of the bearing member 22 away from the driving assembly 21, and the closing member and the bearing member 22 are vertically arranged so that when the bearing member 22 enters the storage cavity, the closing member closes part of the opening.

[0054] For the drawer-type UAV hangar with the above structure, by providing that the bearing structure 2 further includes a closing member, which is a closing plate in this embodiment, and the closing member is specifically connected to the end of the bearing member 22 away from the driving assembly 21, and the closing member and the bearing member 22 are vertically arranged. Thus, when the driving member drives the connecting member 212 to drive the bearing member 22 into the storage cavity, the closing member can close part of the opening, and this part of the opening is specifically the opening corresponding to a single storage cavity, so as to protect the UAV 5 in the storage cavity.

[0055] The drawer-type UAV hangar provided in this embodiment, as Figure 1 and Figure 2 shown, anti-slip members are provided on the bearing member 22, and when the UAV 5 lands on the bearing member 22, the UAV 5 contacts the anti-slip members.

[0056] For the drawer-type UAV hangar with the above structure, by providing anti-slip members on the bearing member 22, which are anti-slip pads in this embodiment, when the UAV 5 lands on the bearing member 22, the UAV 5 can contact the anti-slip members, thereby increasing the friction between the UAV 5 and the bearing member 22, and avoiding the situation that when the bearing member 22 drives the UAV 5 to move, the UAV 5 slides relative to the bearing member 22 and falls off the bearing member 22, causing damage to the UAV 5.

[0057] The drawer - type UAV hangar provided by the utility model includes a bearing structure 2 and a control structure arranged in the library body 1. The library body 1 has an accommodating cavity with one side open. The bearing structure 2 includes a driving component 21 and a bearing member 22. Among them, the driving component 21 is arranged in the accommodating cavity, and the bearing member 22 can carry the UAV 5. The driving end of the driving component 21 is connected to the bearing member 22. Thus, driven by the driving component 21, the bearing member 22 can drive the UAV 5 to enter or exit the accommodating cavity, and then realize the operations of landing storage and take - off preparation of the UAV 5. The control structure specifically includes a control part and a detection part 31 which are electrically connected. Among them, the control part is arranged in the accommodating cavity and is electrically connected to the driving component 21. The detection part 31 is arranged at one end of the bearing member 22 far from the driving component 21 and is electrically connected to the control part. The detection part 31 can detect the distance between the bearing member 22 and the object in front of it, and can transmit the detected distance information to the control part. Thus, the control part can control the forward rotation or shutdown and reverse rotation and shutdown of the driving component 21 according to the distance information. That is, when the bearing member 22 drives the UAV 5 to exit the accommodating cavity, if there is an object in front of the bearing member 22, then the detection part 31 can detect the distance between the end of the bearing member 22 far from the driving component 21 and the object. And when the distance allows the bearing member 22 to completely exit the accommodating cavity and the control part receives the distance information, the control part will not control the driving component 21 to shut down, but still control the driving component 21 to rotate forward to drive the bearing member 22 to completely exit the accommodating cavity. When the distance does not allow the bearing member 22 to completely exit the accommodating cavity, the control part will, after receiving the distance information, control the driving component 21 to shut down and control the driving component 21 to rotate reversely, so that the bearing member 22 drives the UAV 5 to re - enter the accommodating cavity, to avoid the end of the bearing member 22 far from the driving component 21 colliding with the object and causing damage to the object and the bearing member 22, and can avoid the situation that after the bearing member 22 collides with the object, the driving component 21 still drives the bearing member 22 to exit the accommodating cavity, resulting in damage due to the driving component 21 being unable to drive the bearing member 22 to move. Therefore, by installing the control structure in the accommodating cavity, damage to the bearing structure 2 and the object can be avoided, which is beneficial to improving the safety of the UAV 5 hangar.

[0058] Obviously, the above - mentioned embodiments are merely examples for clear illustration and not limitations on the implementation manners. For those of ordinary skill in the art, other different forms of changes or modifications can be made based on the above description. It is not necessary and impossible to list all the implementation manners here. And the obvious changes or modifications derived therefrom are still within the protection scope of the utility model.

Claims

1. A drawer-type UAV hangar, characterized in that, include: A storage body (1) having a receiving cavity with an opening on one side; The bearing structure (2) comprises a driving component (21) and a bearing member (22), wherein the driving component (21) is arranged in the accommodating cavity, the bearing member (22) is suitable for carrying the drone (5), and the driving end of the driving component (21) is connected to the bearing member (22) so as to drive the bearing member (22) to drive the drone (5) to enter or exit the accommodating cavity; A control structure, comprising an electrically connected control member and a detection member (31), wherein the control member is arranged in the accommodating cavity and is electrically connected to the driving assembly (21), and the detection member (31) is arranged at one end of the bearing member (22) away from the driving assembly (21) and is electrically connected to the control member; The detection member (31) is suitable for detecting distance information between the carrier (22) and the object, and transmitting the distance information to the control member, so that the control member controls the driving component (21) to rotate forward or close and rotate backward or close according to the distance information.

2. The drawer-type drone hangar according to claim 1, wherein It also includes a plurality of partitions (4), all of which are arranged at intervals in the accommodating cavity to divide the accommodating cavity into a plurality of storage cavities, and the bearing structure (2) and the control structure are arranged in any one of the storage cavities.

3. The drawer-type UAV hangar according to claim 2, characterized in that, The driving assembly (21) comprises a driving member, a guiding member (211) and a connecting member (212); the driving member and the guiding member (211) are both arranged on the partition (4); the connecting member (212) is slidably connected to the guiding member (211), and the two ends of the connecting member (212) are respectively connected to the supporting member (22) and the driving end of the driving member, so that under the drive of the driving member, the connecting member (212) is suitable for driving the supporting member (22) to enter or exit the storage cavity.

4. The drawer-type UAV hangar according to claim 3, wherein, The guide member (211) has a guide cavity, the driving member is arranged in the guide cavity, and the connecting member (212) is suitable for extending into the guide cavity to be connected to the driving end of the driving member and is slidably connected to the guide member (211).

5. The drawer-type UAV hangar according to claim 4, wherein, The driving assembly (21) further comprises a connecting piece, which is arranged in the guide cavity, and one end of the connecting piece is connected to the driving end of the driving piece, and the other end of the connecting piece is connected to the connecting piece (212).

6. The drawer-type UAV hangar according to claim 5, wherein, The adapter is provided with a thread, the connecting piece (212) is provided with a threaded hole, and the connecting piece (212) is suitable for being threadedly connected to the thread on the adapter through the threaded hole.

7. The drawer-type UAV hangar according to claim 6, wherein, The carrier (22) is provided with a yielding portion, and one end of the connecting member (212) connected to the carrier (22) is suitable for extending into the yielding portion to be connected to the carrier (22), and when the carrier (22) enters the storage cavity, the guide member (211) is arranged in the yielding portion.

8. The drawer-type UAV hangar according to claim 2, wherein, At least three of the driving components (21) are arranged in any one of the storage cavities. The three driving components (21) are arranged on the partition member (4) at intervals, and one driving component (21) is arranged at each of the two ends of the partition member (4).

9. The drawer-type drone hangar according to claim 8, wherein, The carrying structure (2) further includes a closing member. The closing member is connected to one end of the carrying member (22) away from the driving component (21), and the closing member and the carrying member (22) are vertically arranged so that when the carrying member (22) enters the storage cavity, the closing member closes part of the opening.

10. The drawer-type UAV hangar according to claim 9, wherein, Anti-slip members are arranged on the carrying member (22). When the drone (5) lands on the carrying member (22), the drone (5) contacts the anti-slip members.

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