Unmanned aerial vehicle garage and vehicle

Abstract

The invention relates to an unmanned aerial vehicle garage and a vehicle. The unmanned aerial vehicle garage comprises a base assembly, a parking apron and a lifting mechanism. The parking apron is used for fixing the unmanned aerial vehicle. The lifting mechanism comprises a first lifting assembly and a second lifting assembly which are rotatably connected, the first lifting assembly is rotatably connected with the base assembly, and the second lifting assembly is connected with the parking apron. Under the action of external force, the first lifting assembly can rotate relative to the base assembly, and the second lifting assembly can rotate relative to the first lifting assembly, so that the unmanned aerial vehicle garage is switched between the storage state and the opening state, and a large number of moving mechanisms and telescopic mechanisms in the related technology are omitted; and integration of the unmanned aerial vehicle garage and the vehicle is facilitated, and the carrying requirement of the vehicle is met.

Description

Technical Field

[0001] This application relates to the technical field of unmanned aerial vehicles, and particularly to an unmanned aerial vehicle storage and a vehicle. Background Art

[0002] In recent years, as a general new type of aircraft, unmanned aerial vehicles have a high degree of intelligent operation and a large field of vision. They are small in size and convenient to fly, and can better obtain environmental information that is difficult for cars to obtain. Combining cars with unmanned aerial vehicles can well solve the problem of vehicles obtaining external environmental information, improve driving safety. At the same time, unmanned aerial vehicles are becoming more and more popular in people's daily lives for shooting, performing, etc., so the combination with vehicles can also meet the convenience of carrying and transporting unmanned aerial vehicles.

[0003] Related technologies use a large number of moving mechanisms and telescopic mechanisms to achieve the centralized storage of unmanned aerial vehicles, but these mechanisms will cause the unmanned aerial vehicle storage to be too large in volume and size, occupy the internal space of the vehicle, which is not conducive to the integration of the unmanned aerial vehicle storage and the vehicle, and affects the original vehicle functions. Summary of the Invention

[0004] Embodiments of this application provide an unmanned aerial vehicle storage and a vehicle, which can reduce the volume and size of the unmanned aerial vehicle storage, and are conducive to the integration of the unmanned aerial vehicle storage and the vehicle, so as to at least partially solve the above technical problems.

[0005] To achieve the above object, according to the first aspect of this application, an unmanned aerial vehicle storage is provided, including:

[0006] A base assembly;

[0007] A landing pad for fixing an unmanned aerial vehicle; and

[0008] A lifting mechanism, including a first lifting component and a second lifting component that are rotatably connected. The first lifting component is rotatably connected to the base assembly, and the second lifting component is connected to the landing pad;

[0009] Wherein, under the action of an external force, the first lifting component can rotate relative to the base assembly, and the second lifting component can rotate relative to the first lifting component, so that the unmanned aerial vehicle storage can be switched between a storage state and an open state.

[0010] In some embodiments, when the unmanned aerial vehicle storage is in the storage state, the first lifting component and the second lifting component are deployed in the same plane; and / or

[0011] When the unmanned aerial vehicle storage is in the open state, the first lifting component is inclined relative to the second lifting component.

[0012] In some embodiments, when the unmanned aerial vehicle storage is in the open state, the landing pad can perform a lifting movement between a first position and a second position.

[0013] In some embodiments, when the landing pad is between the first position and the second position, the landing pad can swing within a predetermined spherical range to capture and fix the drone.

[0014] In some embodiments, the drone storage also includes:

[0015] A traction assembly, connected to the second lifting assembly and the landing pad, for driving the landing pad to perform a lifting motion between the first position and the second position.

[0016] In some embodiments, when the drone storage switches from the storage state to the open state, the traction assembly drives the landing pad to move to the first position, the landing pad captures and fixes the landed drone, and the traction assembly drives the landing pad to drive the drone to rise to the second position to store the drone; and / or,

[0017] When the drone storage switches from the storage state to the open state, the traction assembly drives the landing pad to drive the drone to descend from the second position to the first position, and the landing pad releases the drone to enable the drone to take off.

[0018] In some embodiments, the traction assembly includes:

[0019] A first drive assembly, fixedly connected to the second lifting assembly; and

[0020] A pulling member, the first end of the pulling member is fixedly connected to the first drive assembly, and the second end of the pulling member is fixedly connected to the landing pad;

[0021] Wherein, when the drone storage is in the open state, the pulling member causes the landing pad to swing within a predetermined spherical range, and the first drive assembly drives the pulling member to drive the landing pad to perform a lifting motion between the first position and the second position.

[0022] In some embodiments, the first drive assembly includes:

[0023] A driving member, fixedly connected to the second lifting assembly; and

[0024] An output shaft, fixedly connected to the driving member, and one end of the pulling member is connected to the output shaft;

[0025] Wherein, the driving member drives the output shaft to rotate around its own axis to drive the pulling member to perform a retracting and extending motion, so that the landing pad performs a lifting motion under the traction of the pulling member.

[0026] In some embodiments, the traction assembly further includes:

[0027] A guiding member, arranged at an interval from the output shaft, and both ends of the guiding member are fixedly connected to the second lifting assembly;

[0028] Wherein, the other end of the pulling member is connected to the guiding member so that the apron moves up and down in the direction of gravity.

[0029] In some embodiments, the extending direction of the guiding member is parallel to the extending direction of the output shaft.

[0030] In some embodiments, the drone hangar further includes:

[0031] A fixing member, located on one side of the guiding member and fixedly connected to the second lifting assembly;

[0032] Wherein, when the traction assembly drives the apron and the drone to move from the first position to the second position, the apron is adsorbed and fixed by the fixing member.

[0033] In some embodiments, the apron includes a first magnetic part, and the fixing member includes a second magnetic part;

[0034] Wherein, when the traction assembly drives the apron and the drone to move from the first position to the second position, a magnetic force is formed between the first magnetic part and the second magnetic part, and the apron is adsorbed and fixed to the fixing member by the magnetic force.

[0035] In some embodiments, the first magnetic part and / or the second magnetic part includes an electromagnet.

[0036] In some embodiments, in the top view direction, the fixing member and the apron at least partially overlap.

[0037] In some embodiments, the pulling member includes a flexible cable.

[0038] In some embodiments, the first lifting assembly includes two first cantilevers, which are opposite and spaced apart; wherein, one end of each first cantilever away from the first lifting assembly is rotatably connected to the base assembly.

[0039] In some embodiments, the lifting mechanism further includes a first rotating shaft, and both ends of the first rotating shaft are fixedly connected to the base assembly; wherein, one end of each first cantilever away from the first lifting assembly is connected to the first rotating shaft so that the two first cantilevers rotate around the first rotating shaft.

[0040] In some embodiments, the base assembly further includes two first bases, which are opposite and spaced apart; wherein, both ends of the first rotating shaft are respectively connected to the corresponding first bases.

[0041] In some embodiments, the first lifting assembly further includes a second driving assembly, the fixed end of the second driving assembly is connected to the base assembly, the output end of the second driving assembly is connected to any one of the two first cantilevers, and the second driving assembly is used to drive the first cantilever to rotate relative to the base assembly.

[0042] In some embodiments, the second driving assembly includes:

[0043] A first connecting member, one end of the first connecting member is fixedly connected to the base assembly; and

[0044] A second connecting member, one end of the second connecting member is fixedly connected to any one of the two first cantilevers, and the other end of the second connecting member is connected to the other end of the first connecting member and can telescopically move within the first connecting member to drive the first cantilever to rotate relative to the base assembly.

[0045] In some embodiments, the base assembly further includes a second base, and the second base is spaced apart from the first base; wherein, one end of the first connecting member is fixedly connected to the second base.

[0046] In some embodiments, the second driving assembly includes:

[0047] A first sliding member, connected to the base assembly; and

[0048] A second sliding member, one end of the second sliding member is slidably connected to the first sliding member, and the other end is fixedly connected to any one of the two first cantilevers;

[0049] Wherein, the second sliding member slides relative to the first sliding member to drive the first cantilever to rotate relative to the base assembly.

[0050] In some embodiments, the second driving assembly further includes:

[0051] A first locking member, located at one end of the first sliding member away from the second lifting assembly and fixedly connected to the base assembly, wherein when the drone storage is in the storage state, the second sliding member is limited by the first locking member; and / or,

[0052] A second locking member, located at one end of the first sliding member close to the second lifting assembly and fixedly connected to the base assembly, wherein when the drone storage is in the fully opened state, the second sliding member is limited by the second locking member.

[0053] In some embodiments, the first lifting assembly further includes a first support member, and the first support member is connected between the two first cantilevers for supporting the two first cantilevers.

[0054] In some embodiments, the second lifting assembly includes two second cantilevers, and the two second cantilevers are opposite and spaced apart; wherein, each second cantilever is respectively rotatably connected to one end of the corresponding first cantilever close to the first lifting assembly.

[0055] In some embodiments, the lifting mechanism further includes a second rotating shaft, and both the first cantilever and the second cantilever are connected to the second rotating shaft to enable the second cantilever to rotate relative to the first cantilever.

[0056] In some embodiments, the lifting mechanism further includes a synchronous transmission assembly connected between the first cantilever and the second cantilever for driving the rotation of the second rotating shaft to drive the second cantilever to rotate relative to the first cantilever.

[0057] In some embodiments, the synchronous transmission assembly includes:

[0058] A driving wheel fixedly connected to the first cantilever;

[0059] A driven wheel coaxially and fixedly connected to the second rotating shaft; and

[0060] A transmission member connected to the driving wheel and the driven wheel, so that the driving wheel drives the driven wheel to rotate through the transmission member, thereby causing the second rotating shaft to rotate.

[0061] In some embodiments, the plane where the second cantilever is located is parallel to the horizontal plane.

[0062] In some embodiments, the second lifting assembly further includes a second support member connected between the two second cantilevers for supporting the two second cantilevers.

[0063] In some embodiments, the drone hangar further includes:

[0064] A processor for detecting whether the apron has fixed the drone and, when detecting that the apron has fixed the drone, sending a power-off signal to the drone to cause the drone to cut off power.

[0065] According to a second aspect of the present application, there is provided a vehicle including the above drone hangar.

[0066] In some embodiments, the vehicle further includes:

[0067] A vehicle body, the vehicle body includes a hatch and a receiving cavity, the receiving cavity is arranged inside the vehicle body, and the hatch is used to close and open the receiving cavity.

[0068] In some embodiments, when the drone hangar is in a stowed state, the hatch closes the receiving cavity, and the drone hangar and the drone are located inside the receiving cavity; and / or,

[0069] When the drone hangar is in an open state, the hatch opens the receiving cavity, and the drone hangar and the drone are located outside the receiving cavity.

[0070] In some embodiments, the hatch is fixedly connected to the first lifting assembly and rotatably connected to the base assembly, and under the action of an external force, the first lifting assembly can drive the hatch to rotate relative to the base assembly.

[0071] In some embodiments, the receiving cavity is arranged at the tail of the vehicle body.

[0072] In the drone hangar and vehicle according to the embodiments of the present application, the drone hangar includes a base assembly, a landing pad, and a lifting mechanism. The lifting mechanism includes a first lifting assembly and a second lifting assembly that are rotatably connected. The first lifting assembly is rotatably connected to the base assembly, and the second lifting assembly is connected to the landing pad. Under the action of an external force, the first lifting assembly can rotate relative to the base assembly, and the second lifting assembly can rotate relative to the first lifting assembly. When the drone hangar is in the open state, the landing pad and the drone can be lifted outside the vehicle space range through the first lifting assembly and the second lifting assembly of the lifting mechanism, thereby meeting the takeoff and landing space requirements of the drone. Moreover, the drone can also land in the storage space inside the vehicle, thereby meeting the storage requirements of the drone. In this way, the drone hangar can be switched between the storage state and the open state. In addition, the lifting mechanism in the present application can eliminate a large number of moving mechanisms and telescopic mechanisms in the related art, reduce the volume size and mechanism complexity of the drone hangar, facilitate the integration of the drone hangar and the vehicle, and meet the mounting requirements of the vehicle. BRIEF DESCRIPTION OF THE DRAWINGS

[0073] In order to more clearly illustrate the technical solutions in the embodiments of the present application, the drawings required for the description of the embodiments will be briefly introduced below. Obviously, the drawings in the following description are only some embodiments of the present application. For those skilled in the art, other drawings can be obtained based on these drawings without creative efforts.

[0074] In order to more fully understand the present application and its beneficial effects, the following description will be made in conjunction with the drawings, where the same reference numerals denote the same parts in the following description.

[0075] Figure 1 is a three-dimensional structural schematic diagram of the drone hangar provided in the embodiments of the present application;

[0076] Figure 2 is Figure 1 a top view structural schematic diagram of the drone hangar in;

[0077] Figure 3 is a first three-dimensional structural schematic diagram of the drone hangar and the drone when the drone hangar is in the open state provided in the embodiments of the present application;

[0078] Figure 4 is Figure 3 a top view structural schematic diagram of the drone hangar and the drone in;

[0079] Figure 5 is a second three-dimensional structural schematic diagram of the drone hangar and the drone when the drone hangar is in the open state provided in the embodiments of the present application;

[0080] Figure 6 isFigure 5 Schematic top view structure diagram of the drone hangar and the drone in

[0081] Figure 7 Schematic three-dimensional structure diagram of the drone hangar and the drone when the drone hangar is in the storage state provided in the embodiment of the present application;

[0082] Figure 8 is Figure 7 Schematic top view structure diagram of the drone hangar and the drone in

[0083] Figure 9 Schematic three-dimensional structure diagram of a vehicle when the drone hangar is in the open state provided in the embodiment of the present application;

[0084] Figure 10 Schematic three-dimensional structure diagram of a vehicle when the drone hangar is in the storage state provided in the embodiment of the present application; and

[0085] Figure 11 Schematic connection diagram of the drone hangar and the hatch door provided in the embodiment of the present application.

[0086] Description of reference numerals:

[0087] 100, drone hangar; 200, vehicle; 201, vehicle body; 202, hatch door; 203, accommodation cavity; 300, drone;

[0088] 1, base assembly; 11, first base; 12, second base;

[0089] 2, helipad; 21, first magnetic part;

[0090] 3, lifting mechanism; 31, first lifting assembly; 311, first cantilever; 312, first support;

[0091] 32, second lifting assembly; 321, second cantilever; 322, second support; 33, first rotating shaft; 34, second rotating shaft;

[0092] 4, traction assembly; 41, first driving assembly; 411, driving member; 412, output shaft; 42, pulling member; 43, guiding member;

[0093] 5, fixing member; 51, second magnetic part;

[0094] 6, second driving assembly; 61, first connecting member; 62, second connecting member;

[0095] 7, synchronous driving assembly; 71, driving wheel; 72, driven wheel; 73, transmission member. Detailed implementation manners

[0096] The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present application. Obviously, the described embodiments are only a part of the embodiments of the present application, rather than all the embodiments. All other embodiments obtained by those skilled in the art based on the embodiments of the present application without creative efforts shall fall within the protection scope of the present application.

[0097] According to a first aspect of the present application, with reference to Figures 1-11 , the present application provides an unmanned aerial vehicle (UAV) storage 100, which includes a base assembly 1, a landing pad 2, and a lifting mechanism 3. The landing pad 2 is used to fix the UAV 300. The lifting mechanism 3 includes a first lifting component 31 and a second lifting component 32 that are rotatably connected. The first lifting component 31 is rotatably connected to the base assembly 1, and the second lifting component 32 is connected to the landing pad 2. Under the action of an external force, the first lifting component 31 can rotate relative to the base assembly 1, and the second lifting component 32 can rotate relative to the first lifting component 31, so that the UAV storage 100 can be switched between a storage state and an open state.

[0098] Through the above technical solution, when the UAV storage 100 is in the open state, the landing pad 2 and the UAV 300 can be lifted outside the space range of the vehicle 200 through the first lifting component 31 and the second lifting component 32 of the lifting mechanism 3, thus meeting the take-off and landing space requirements of the UAV 300. Moreover, the UAV 300 can also land in the storage space inside the vehicle 200, thus meeting the storage requirements of the UAV 300. In this way, the UAV storage 100 can be switched between the storage state and the open state. In addition, the lifting mechanism 3 in the present application can eliminate a large number of moving mechanisms and telescopic mechanisms in the related art, reduce the volume size and mechanism complexity of the UAV storage 100, and is conducive to the integration of the UAV storage 100 with the vehicle 200, meeting the mounting requirements of the vehicle 200.

[0099] It can be understood that, as Figures 1-4 shown, when the UAV storage 100 is switched from the storage state to the open state, the first lifting component 31 rotates relative to the base assembly 1 under the drive of an external force, the end of the first lifting component 31 connected to the second lifting component 32 rises, and the second lifting component 32 and the landing pad 2 rise synchronously under the drive of the first lifting component 31, so that the first lifting component 31, the second lifting component 32, and the landing pad 2 are located in the external space of the vehicle 200. In this way, it is convenient for the UAV 300 in the storage state to take off from the landing pad 2 or for the UAV 300 in the landing state to land on the landing pad 2.

[0100] As Figures 7-8As shown, when the drone hangar 100 switches from the open state to the storage state, the first lifting component 31 rotates relative to the base component 1 under the drive of an external force. One end of the first lifting component 31 connected to the second lifting component 32 descends downward. The second lifting component 32, the landing pad 2, and the drone 300 synchronously descend under the drive of the first lifting component 31, so that the first lifting component 31, the second lifting component 32, the landing pad 2, and the drone 300 are located in the internal storage space of the vehicle 200. In this way, the storage of the drone 300 can be achieved.

[0101] In some embodiments, when the drone hangar 100 is in the storage state, the first lifting component 31 and the second lifting component 32 are deployed in the same plane. In this way, the occupied space of the lifting mechanism 3 in the vertical direction can be reduced. Thus, when the drone hangar 100 is stored inside the vehicle 200, the space occupied by the drone hangar 100 in the vehicle 200 can be minimized, which is beneficial to achieving a compact layout. In the embodiments of the present application, when the drone hangar 100 is in the storage state, the plane where the first lifting component 31 and the second lifting component 32 are located is parallel to the plane where the vehicle 200 is located. Generally, the plane where the first lifting component 31 and the second lifting component 32 are located is parallel to the horizontal plane.

[0102] In some embodiments, when the drone hangar 100 is in the open state, the first lifting component 31 is inclined relative to the second lifting component 32. In this way, a hangar space can be formed between the first lifting component 31 and the second lifting component 32 to provide the space required for the takeoff and landing of the drone 300. For example, when the drone 300 lands, the drone 300 can first land in this hangar space and then be fixed on the landing pad 2. Again, when the drone 300 takes off, the drone 300 can take off from the landing pad 2 and then take off outside the drone hangar 100 through this hangar space.

[0103] In some embodiments, when the drone hangar 100 is in the open state, the landing pad 2 can move up and down between a first position and a second position. In this way, the landing pad 2 can adapt to the landing accuracy of the drone 300, so that the landing pad 2 is located near the landing position of the drone 300 to facilitate the landing pad 2 to capture and fix the drone 300. In the embodiments of the present application, the first position can be above the second position or below the second position. The present application does not limit this. For the sake of clearly illustrating the technical solution provided by the present application, the embodiments of the present application will be explained by taking the first position being below the second position as an example.

[0104] In the embodiments of the present application, the first position can be the lowest position to which the landing pad 2 can descend, and the second position can be the position where the landing pad 2 is located when the drone hangar 100 is in the storage state.

[0105] In some embodiments, such as Figures 1-4 shown, when the landing pad 2 is between the first position and the second position, the landing pad 2 can swing within a predetermined spherical range, that is, the landing pad 2 can freely deflect within a small range in three-dimensional space. When the landing pad 2 moves up and down between the first position and the second position, the swing radius of the landing pad 2 changes with the height of the landing pad 2. Specifically, the higher the height of the landing pad 2, the smaller its swing range; the lower the height of the landing pad 2, the larger its swing range. Wherein, the height of the landing pad 2 refers to the distance between the landing pad 2 and the base assembly 1 in the vertical direction.

[0106] It should be noted that due to technical limitations, there is usually a certain range of blind landing space (powerless blind area) when the drone 300 lands, resulting in uncontrollable landing accuracy and inability to accurately locate to a fixed point. To overcome this problem, in the related art, the mechanical landing pad 2 needs to adopt a complex centering mechanism to forcibly correct the position of the drone 300, which will result in a large volume of the drone hangar 100, occupying the internal space of the vehicle 200, being not conducive to the integration of the drone hangar 100 and the vehicle 200, and affecting the original functions of the vehicle 200.

[0107] In the embodiments of the present application, after the drone 300 enters the blind landing interval, the swing radius within the spherical range can be controlled by adjusting the height of the landing pad 2, so as to control the swing range of the landing pad 2 within the spherical range to adapt to the landing accuracy of the drone 300, thereby completing the capture and fixation of the drone 300 by the landing pad 2. Specifically, after the drone 300 enters the blind landing interval, the landing pad 2 maintains a lower height and has a larger swing range. Even if the drone 300 deviates from the theoretical landing point, it can still be captured by the landing pad 2. After the drone 300 is successfully captured by the landing pad 2, the traction assembly 4 drives the landing pad 2 to rise to increase the height of the landing pad 2 (for example, the second position), and the swing range of the landing pad 2 decreases to gradually pull the drone 300 back to the central position, thereby realizing the centering and positioning of the drone 300. It can be understood that compared with the related art, the present application can realize the centering and positioning of the drone 300 without setting a complex centering mechanism, reducing the volume of the drone hangar 100 and being conducive to the deep integration of the drone 300 and the vehicle 200.

[0108] In some embodiments, the drone hangar 100 further includes a traction assembly 4. The traction assembly 4 is connected to the second lifting assembly 32 and the landing pad 2, and is used to drive the landing pad 2 to move up and down between the first position and the second position. In the embodiments of the present application, one end of the traction assembly 4 is fixedly connected to the second lifting assembly 32, and the other end of the traction assembly 4 is fixedly connected to the landing pad 2.

[0109] In an embodiment of the present application, when the drone hangar 100 switches from the storage state to the open state, the traction assembly 4 drives the apron 2 to move to the first position, the apron 2 captures and fixes the landed drone 300, and the traction assembly 4 drives the apron 2 to drive the drone 300 to rise to the second position to store the drone 300; and / or, when the drone hangar 100 switches from the storage state to the open state, the traction assembly 4 drives the apron 2 to drive the drone 300 to descend from the second position to the first position, and the apron 2 releases the drone 300 to enable the drone 300 to take off.

[0110] In some embodiments, the traction assembly 4 includes a first driving assembly 41 and a pulling member 42. The first driving assembly 41 is fixedly connected to the second lifting assembly 32 and is used to provide driving force for the lifting movement of the apron 2. The first end of the pulling member 42 is fixedly connected to the first driving assembly 41, and the second end of the pulling member 42 is fixedly connected to the apron 2. Wherein, when the drone hangar 100 is in the open state, the apron 2 swings within a predetermined spherical range, and the first driving assembly 41 drives the pulling member 42 to pull the apron 2 to perform lifting movement between the first position and the second position.

[0111] In some embodiments, the first driving assembly 41 includes a driving member 411 and an output shaft 412. The driving member 411 is fixedly connected to the second lifting assembly 32. The output shaft 412 is fixedly connected to the driving member 411, and one end of the pulling member 42 is connected to the output shaft 412. Wherein, the driving member 411 drives the output shaft 412 to rotate around its own axis to drive the pulling member 42 to perform winding and unwinding movements, so that the apron 2 performs lifting movement under the traction of the pulling member 42.

[0112] In an embodiment of the present application, the driving member 411 may include a driving motor.

[0113] In an embodiment of the present application, the pulling member 42 is a pulling member, one end of the pulling member 42 is wound on the output shaft 412, and the other end is fixedly connected to the apron 2. The pulling member 42 may include a flexible cable, and the flexible cable includes a high-flex cable.

[0114] In some embodiments, the traction assembly 4 further includes a guiding member 43. The guiding member 43 is disposed at an interval from the output shaft 412, and both ends of the guiding member 43 are fixedly connected to the second lifting assembly 32. Wherein, the other end of the pulling member 42 is connected to the guiding member 43 to enable the apron 2 to perform lifting movement in the direction of gravity.

[0115] In an embodiment of the present application, the extending direction of the guiding member 43 is parallel to the extending direction of the output shaft 412, the guiding member 43 is a fixed shaft, and while playing a guiding role, the guiding member 43 can also play a role in supporting the second lifting assembly 32.

[0116] In some embodiments, the apron 2 captures and fixes the drone 300 by adsorption. In the embodiment of the present application, the apron 2 captures and fixes the drone 300 by magnetic adsorption. It can be understood that the embodiment of the present application integrates the structural parts such as the centering mechanism and the lifting mechanism of the drone hangar 100 in the related art, and replaces the original mechanical mechanism with electromagnetic, which is conducive to further reducing the volume of the drone hangar 100, thereby better realizing the deep integration of the drone 300 and the vehicle 200.

[0117] Specifically, the apron 2 includes a first magnetic part 21, and an adsorbable part is provided on the drone 300. For example, the drone 300 itself has soft magnetic materials or is installed with hard magnetic materials or a magnetic material is provided on the top of the drone 300. The magnetic material may include iron materials. When the drone 300 is in flight and flies into the open hangar space, the apron 2 is started. Due to the electromagnetic properties, the apron 2 can accurately capture and adsorb the drone 300 within a certain range. When the apron 2 is successfully adsorbed, the drone 300 begins to disconnect the power, and the drone 300 lands. The insufficient landing accuracy will be offset by the swing range of the apron 2. Since the apron 2 is pulled by a pulling member 42, the drone 300 will not leave the hangar space.

[0118] In some embodiments, the drone hangar 100 further includes a processor (not shown in the figure), which is used to detect whether the helipad 2 has fixed the drone 300 and send a power-off signal to the drone 300 when it is detected that the helipad 2 has fixed the drone 300, so that the drone 300 is disconnected from the power. Specifically, when the helipad 2 absorbs the drone 300, a current change will occur, and the processor determines that the helipad 2 has been successfully captured based on the current change.

[0119] In some embodiments, the drone hangar 100 further includes a fixing member 5. The fixing member 5 is located on one side of the guide member 43 and is fixedly connected to the second lifting assembly 32. When the traction assembly 4 drives the helipad 2 and the drone 300 to move from the first position to the second position, the helipad 2 is adsorbed and fixed by the fixing member 5, so that the drone 300 can move to a designated position after landing, which is conducive to the subsequent stable storage of the drone 300.

[0120] The embodiment of the present application adopts a design combining the apron 2 and the fixing member 5, so that the drone 300 is first adsorbed and fixed on the apron 2 during the landing process, and then the traction component 4 drives the apron 2 to drive the drone 300 to move upward to the second position, that is, to the vicinity of the fixing member 5, and then the apron 2 is adsorbed by the fixing member 5, so that the apron 2 and the drone 300 are adsorbed and fixed on the fixing member 5 together. Compared with the apron 2, since the fixing member 5 in the embodiment of the present application is directly fixedly connected to the second lifting component 32, it has better stability. Therefore, by fixing the apron 2 and the drone 300 on the fixing member 5, while realizing the central storage of the drone 300, a higher storage stability can be obtained.

[0121] It should be noted that since the drone 300 will produce a large shake when it stops flying, if the drone 300 is directly adsorbed onto the fixing member 5, it is equivalent to forcibly braking the drone 300, which will cause the drone 300 to be in an uncontrollable flight state, causing the drone 300 and the drone hangar 100 to be easily damaged. In view of this, in the embodiment of the present application, it is necessary to first capture and fix the drone 300 to the apron 2, and use the spherical shaking range of the pulling member 42 to offset the shaking of the drone 300 when it stops flying. After the shaking is eliminated, the apron 2 is adsorbed onto the fixing member 5, so as to realize the storage of the drone 300. This design can be suitable for storage needs in harsh working conditions such as bumps of the vehicle 200.

[0122] In some embodiments, the apron 2 and the fixed part are fixed by adsorption. In the embodiment of the present application, the apron 2 and the fixed part are fixed by magnetic adsorption. Specifically, the fixing member 5 includes a second magnetic part 51. When the traction assembly 4 drives the apron 2 and the drone 300 to move from the first position to the second position, a magnetic force is formed between the first magnetic part 21 and the second magnetic part 51, and the apron 2 is fixed to the fixing member 5 by magnetic adsorption.

[0123] In some embodiments, the second magnetic portion 51 includes an electromagnet. When the processor detects that the apron 2 captures the drone 300, the second magnetic portion 51 starts to be energized. When the apron 2 rises to the second position, an electromagnetic field is generated between the first magnetic portion 21 and the second magnetic portion 51, so that the apron 2 is adsorbed and fixed on the fixing member 5 due to the electromagnetic field, which is convenient for subsequent storage into the vehicle 200. In addition, by fixing the drone 300 by electromagnetism, vibration and other working conditions of the drone 300 in the drone hangar 100 can be avoided.

[0124] In some embodiments, in a top view, the fixing member 5 at least partially overlaps with the apron 2 to avoid the fixing member 5 and the apron 2 being too far apart so that the magnetic force formed therebetween cannot adsorb the apron 2 directly onto the fixing member 5 .

[0125] In some embodiments, the first lifting assembly 31 includes two first cantilevers 311, which are arranged at intervals relative to each other. Each end of the first cantilever 311 away from the first lifting assembly 31 is rotatably connected to the base assembly 1. Thus, when the drone hangar 100 is in the open state, the two first cantilevers 311 can rotate relative to the base assembly 1 to achieve rising or falling.

[0126] In some embodiments, the lifting mechanism 3 further includes a first rotating shaft 33, and both ends of the first rotating shaft 33 are fixedly connected to the base assembly 1. Each end of the first cantilever 311 away from the first lifting assembly 31 is connected to the first rotating shaft 33, so that the two first cantilevers 311 rotate around the first rotating shaft 33.

[0127] In some embodiments, the base assembly 1 further includes two first bases 11, which are arranged at intervals relative to each other. Both ends of the first rotating shaft 33 are respectively connected to the corresponding first bases 11. Thus, the first bases 11 serve as the mounting base of the first rotating shaft 33, used to carry the first rotating shaft 33, and can ensure that the axial center position remains unchanged when the first cantilever 311 rotates. In addition, the first bases 11 are usually fixed on the vehicle body 201 of the vehicle 200, and can transfer the weight of the first cantilever 311 and the drone 300 to the vehicle 200, which is beneficial to avoiding local stress concentration.

[0128] In some embodiments, the first lifting assembly 31 further includes a second driving assembly 6. The fixed end of the second driving assembly 6 is connected to the base assembly 1, and the output end of the second driving assembly 6 is connected to any one of the two first cantilevers 311. The second driving assembly 6 is used to drive the first cantilever 311 to rotate relative to the base assembly 1. It can be understood that the second driving assembly 6 is used to provide power for the rotation of the first cantilever 311, so that the first cantilever 311 can rotate relative to the base assembly 1 under the action of the second driving assembly 6.

[0129] In some embodiments, the second driving component 6 may adopt a push rod mechanism. Specifically, the second driving component 6 includes a first connecting piece 61 and a second connecting piece 62. One end of the first connecting piece 61 is fixedly connected to the base component 1. One end of the second connecting piece 62 is fixedly connected to any one of the two first cantilevers 311, and the other end of the second connecting piece 62 is connected to the other end of the first connecting piece 61 and can telescopically move within the first connecting piece 61 to drive the first cantilever 311 to rotate relative to the base component 1. It can be understood that during the process of the drone storage 100 switching from the storage state to the open state, the second connecting piece 62 gradually elongates within the first connecting piece 61, and the second connecting piece 62 pushes the first cantilever 311 to rotate upward. During the process of the drone storage 100 switching from the open state to the storage state, the second connecting piece 62 gradually shortens within the first connecting piece 61, and the second connecting piece 62 pulls the first cantilever 311 to rotate downward.

[0130] In the embodiments of the present application, the above push rod structure may be an electric push rod structure, and the electric push rod structure may be electrically connected to the processor to control the state of the push rod structure according to requirements.

[0131] In some embodiments, the base component 1 further includes a second base 12. The second base 12 is spaced apart from the first base 11. Wherein, one end of the first connecting piece 61 is fixedly connected to the second base 12. The second base 12 is the mounting seat of the above push rod structure, and the second base 12 can fix the push rod structure on the vehicle body 201 of the vehicle 200 to ensure that the telescopic force of the push rod structure is efficiently transmitted to the first cantilever 311.

[0132] In some other embodiments, the second driving component 6 may be a linear sliding structure. Specifically, the second driving component 6 includes a first sliding member (not shown in the figure) and a second sliding member (not shown in the figure). The first sliding member is connected to the base component 1. One end of the second sliding member is slidably connected to the first sliding member, and the other end is fixedly connected to any one of the two first cantilevers 311. Wherein, the second sliding member slides relative to the first sliding member to drive the first cantilever 311 to rotate relative to the base component 1. It can be understood that during the process of the drone storage 100 switching from the storage state to the open state, the second sliding member slides along the direction close to the end where the first cantilever 311 is connected to the first rotating shaft 33, and the second sliding member pushes the first cantilever 311 to rotate upward. During the process of the drone storage 100 switching from the open state to the storage state, the second sliding member slides along the direction away from the end where the first cantilever 311 is connected to the first rotating shaft 33, and the second sliding member pulls the first cantilever 311 to rotate downward.

[0133] In some embodiments, the second driving assembly 6 further includes a first locking member (not shown in the figure). The first locking member is located at one end of the first sliding member away from the second lifting assembly 32 and is fixedly connected to the base assembly 1. Wherein, when the drone hangar 100 is in the storage state, the second sliding member is limited by the first locking member to prevent the second sliding member from continuing to slide and driving the first cantilever 311 to rotate below the horizontal plane.

[0134] In some embodiments, the second driving assembly 6 further includes a second locking member (not shown in the figure). The second locking member is located at one end of the first sliding member close to the second lifting assembly 32 and is fixedly connected to the base assembly 1. Wherein, when the drone hangar 100 is in the fully open state, the second sliding member is limited by the second locking member.

[0135] In some embodiments, the first lifting assembly 31 further includes a first support member 312. The first support member 312 is connected between the two first cantilevers 311 and is used to support the two first cantilevers 311. The first support member 312 can be a cross beam. The number of the first support members 312 can be one or more, and the embodiments of the present application do not limit this.

[0136] In some embodiments, the second lifting assembly 32 includes two second cantilevers 321. The two second cantilevers 321 are opposite and spaced apart. Wherein, each second cantilever 321 is respectively rotatably connected to one end of the corresponding first cantilever 311 close to the first lifting assembly 31. In the embodiments of the present application, the plane where the second cantilever 321 is located is parallel to the horizontal plane to achieve the effect that the second cantilever 321 always remains parallel to the horizontal plane, providing a horizontal state for the apron 2 and facilitating the start and stop of the drone 300.

[0137] In some embodiments, the lifting mechanism 3 further includes a second rotating shaft 34. Both the first cantilever 311 and the second cantilever 321 are connected to the second rotating shaft 34 to enable the second cantilever 321 to rotate relative to the first cantilever 311. In one embodiment, the two first cantilevers 311 can be located on the outside, and the two second cantilevers 321 are located on the inside. In another embodiment, the two first cantilevers 311 can also be located on the inside, and the two second cantilevers 321 are located on the outside.

[0138] In the embodiments of the present application, the driving member 411 in the first driving assembly 41 is fixedly connected to any one of the two second cantilevers 321. The two ends of the guiding member 43 are respectively fixedly connected to the two second cantilevers 321. The two ends of the fixing member 5 are respectively fixedly connected to the two second cantilevers 321. The guiding member 43 is located between the first driving assembly 41 and the fixing member 5 and is spaced apart from the first driving assembly 41 and the fixing member 5.

[0139] In some embodiments, the lifting mechanism 3 further includes a synchronous transmission assembly, which is connected between the first cantilever 311 and the second cantilever 321 and is used to drive the second cantilever 321 to rotate relative to the first cantilever 311 by driving the rotation of the second rotating shaft 34.

[0140] In some embodiments, the synchronous transmission assembly includes a driving wheel 71, a driven wheel 72, and a transmission member 73. The driving wheel 71 is fixedly connected to the first cantilever 311. The driven wheel 72 is coaxially and fixedly connected to the second rotating shaft 34. The transmission member 73 is connected to the driving wheel 71 and the driven wheel 72, so that the driving wheel 71 drives the driven wheel 72 to rotate through the transmission member 73, thereby driving the second rotating shaft 34 to rotate. In the embodiments of the present application, the driven wheel 72 includes a synchronous motor, the driven wheel 72 includes a synchronous pulley, and the transmission member 73 includes a synchronous belt. The driving wheel 71 drives the second cantilever 321 to rotate through the driven wheel 72 and the transmission member 73, and cooperates with the first cantilever 311 for differential movement, so that the second cantilever 321 always remains parallel to the horizontal plane.

[0141] It can be understood that when the drone 300 is fixed on the apron 2, the apron 2 and the drone 300 can be lowered into the drone hangar 100 by driving the second driving assembly 6 and the synchronous transmission assembly, so as to compress the dimensional space of the drone hangar 100 in the vertical direction as a whole, which is convenient for being stored in the vehicle 200 without changing the appearance and characteristics of the existing vehicle 200.

[0142] In some embodiments, the second lifting assembly 32 further includes a second support member 322, which is connected between the two second cantilevers 321 and is used to support the two second cantilevers 321. The second support member 322 can be a cross beam, and the number of the second support members 322 can be one or more, which is not limited in the embodiments of the present application. In a top-down view, the driving motor and the output shaft 412 overlap with the second support member 322, which can reduce the volume of the drone hangar 100.

[0143] In some embodiments, the materials of the first cantilever 311, the second cantilever 321, the first rotating shaft 33, the second rotating shaft 34, and the base assembly 1 can be the same. Specifically, the first cantilever 311 and the second cantilever 321 can be made of A380 type aluminum alloy material, which has relatively high strength.

[0144] As Figures 9-11 shown, according to the second aspect of the present application, a vehicle 200 is provided. The vehicle 200 includes the above-mentioned drone hangar 100, and the vehicle 200 has all the beneficial effects of the above-mentioned drone hangar 100, which will not be elaborated herein again. The vehicle 200 can be a fuel vehicle, a plug-in hybrid vehicle, a new energy vehicle, etc., and the present application does not make specific limitations on this.

[0145] In some embodiments, the vehicle 200 further includes a vehicle body 201, which includes a hatch 202 and a receiving cavity 203. The receiving cavity 203 is disposed inside the vehicle body 201, and the hatch 202 is used to close and open the receiving cavity 203.

[0146] In some embodiments, as Figure 10 shown, when the drone hangar 100 is in the retracted state, the hatch 202 closes the receiving cavity 203, and the drone hangar 100 and the drone 300 are located inside the receiving cavity 203 to achieve the retraction of the drone hangar 100. As Figure 9 shown, when the drone hangar 100 is in the open state, the hatch 202 opens the receiving cavity 203, and the drone hangar 100 and the drone 300 are located outside the receiving cavity 203 to prepare for the landing and takeoff of the drone 300.

[0147] In some embodiments, the hatch 202 is fixedly connected to the first lifting assembly 31 and rotatably connected to the base assembly 1. Under the action of an external force, the first lifting assembly 31 can drive the hatch 202 to rotate relative to the base assembly 1. That is, when the drone hangar 100 is in the open state, the first lifting assembly 31 drives the hatch 202 to flip synchronously, so that the drone 300 and the landing pad 2 are lifted above the horizontal line of the vehicle 200, meeting the start-stop space requirements of the drone 300, facilitating the takeoff of the drone 300, and also meeting the subsequent landing requirements.

[0148] In the embodiments of the present application, the hatch 202 is fixedly connected to two first cantilevers 311 in the first lifting assembly 31. Specifically, the hatch 202 and the first cantilever 311 can adopt a welded connection form, but not limited thereto. The hatch 202 and the first cantilever 311 can also be fixedly connected by manufacturing processes such as integral casting and integral sheet metal forming.

[0149] In some embodiments, the receiving cavity 203 is disposed at the rear of the vehicle body 201, borrowing the redundant space at the rear of the vehicle. Without changing the original structure of the vehicle 200, after the drone hangar 100 is retracted into the receiving cavity 203, it will not affect the appearance of the vehicle 200. Without opening the drone hangar 100, the drone hangar 100 will not be observed by others, which is beneficial to improving the aesthetic appearance of the vehicle 200.

[0150] In some embodiments, the drone hangar 100 can be located above the storage board, and the drone hangar 100 is disposed in front of the C-pillar of the vehicle 200. In this way, the drone hangar 100 does not occupy the passenger's seating space, and thus does not affect the passenger's activity space, and the layout is more reasonable.

[0151] In the description of the present application, the terms "first" and "second" are only used for descriptive purposes and cannot be construed as indicating or implying relative importance or implicitly specifying the quantity of the indicated technical features. Thus, the features defined with "first" and "second" may explicitly or implicitly include one or more features. In the description of the present application, "a plurality of" means two or more unless otherwise specifically defined.

[0152] In the above embodiments, the descriptions of the respective embodiments have their own emphases. For the parts not detailed in a certain embodiment, reference may be made to the relevant descriptions of other embodiments.

[0153] The embodiments, implementation manners and related technical features of the present application can be combined and replaced with each other without conflict.

[0154] The above are only the preferred embodiments of the present application and do not impose any formal limitations on the present application. However, any simple modifications, equivalent changes and modifications made to the above embodiments based on the technical essence of the present application without departing from the content of the technical solution of the present application still fall within the scope of the technical solution of the present application.

Claims

1. An unmanned aircraft storage (100), characterized in that, Comprising: A base assembly (1); A landing pad (2) for fixing a drone (300); And A lifting mechanism (3), including a first lifting component (31) and a second lifting component (32) that are rotatably connected. The first lifting component (31) is rotatably connected to the base assembly (1), and the second lifting component (32) is connected to the landing pad (2); Wherein, under the action of an external force, the first lifting component (31) can rotate relative to the base assembly (1), and the second lifting component (32) can rotate relative to the first lifting component (31), so that the drone hangar (100) can be switched between a storage state and an open state.

2. The drone hangar (100) according to claim 1, characterized in that, When the drone hangar (100) is in the storage state, the first lifting component (31) and the second lifting component (32) are deployed in the same plane; and / or When the drone hangar (100) is in the open state, the first lifting component (31) is inclined relative to the second lifting component (32).

3. The drone hangar (100) according to claim 1, characterized in that, When the drone hangar (100) is in the open state, the landing pad (2) can perform a lifting movement between a first position and a second position.

4. The drone hangar (100) according to claim 3, wherein, When the landing pad (2) is between the first position and the second position, the landing pad (2) can swing within a predetermined spherical range to capture and fix the drone (300).

5. The drone hangar (100) according to claim 4, characterized in that, The drone hangar (100) further includes: A traction component (4), connected to the second lifting component (32) and the landing pad (2), for driving the landing pad (2) to perform a lifting movement between the first position and the second position.

6. The drone hangar (100) according to claim 5, characterized in that, When the drone hangar (100) is switched from the storage state to the open state, the traction component (4) drives the landing pad (2) to move to the first position, the landing pad (2) captures and fixes the landed drone (300), and the traction component (4) drives the landing pad (2) to drive the drone (300) to rise to the second position to store the drone (300); and / or, When the drone hangar (100) is switched from the storage state to the open state, the traction component (4) drives the landing pad (2) to drive the drone (300) to descend from the second position to the first position, and the landing pad (2) releases the drone (300) to enable the drone (300) to take off.

7. The drone hangar (100) according to claim 5, characterized in that, The traction component (4) includes: A first driving component (41), fixedly connected to the second lifting component (32); and A pulling member (42), the first end of the pulling member (42) is fixedly connected to the first driving component (41), and the second end of the pulling member (42) is fixedly connected to the landing pad (2); Wherein, when the drone hangar (100) is in an open state, the pulling member (42) causes the landing pad (2) to swing within a predetermined spherical range, and the first driving assembly (41) drives the pulling member (42) to drive the landing pad (2) to perform a lifting motion between the first position and the second position.

8. The drone hangar (100) according to claim 7, characterized in that, The first driving assembly (41) includes: a driving member (411) fixedly connected to the second lifting assembly (32); and an output shaft (412) fixedly connected to the driving member (411), with one end of the pulling member (42) connected to the output shaft (412); Wherein, the driving member (411) drives the output shaft (412) to rotate about its own axis to drive the pulling member (42) to perform a retracting and extending motion, so that the landing pad (2) performs a lifting motion under the traction of the pulling member (42).

9. The drone hangar (100) according to claim 8, characterized in that, The traction assembly (4) further includes: a guiding member (43) spaced apart from the output shaft (412), and both ends of the guiding member (43) are fixedly connected to the second lifting assembly (32); Wherein, the other end of the pulling member (42) is connected to the guiding member (43), so that the landing pad (2) performs a lifting motion in the direction of gravity.

10. The drone storage (100) according to claim 9, characterized in that, The extending direction of the guiding member (43) is parallel to the extending direction of the output shaft (412).

11. The drone storage (100) according to claim 9, characterized in that, The drone hangar (100) further includes: a fixing member (5) located on one side of the guiding member (43) and fixedly connected to the second lifting assembly (32); Wherein, when the traction assembly (4) drives the landing pad (2) and the drone (300) to move from the first position to the second position, the landing pad (2) is adsorbed and fixed by the fixing member (5).

12. The drone storage (100) according to claim 11, characterized in that, The landing pad (2) includes a first magnetic part (21), and the fixing member (5) includes a second magnetic part (51); Wherein, when the traction assembly (4) drives the landing pad (2) and the drone (300) to move from the first position to the second position, a magnetic force is formed between the first magnetic part (21) and the second magnetic part (51), and the landing pad (2) is adsorbed and fixed to the fixing member (5) by the magnetic force.

13. The drone hangar (100) according to claim 12, characterized in that, The first magnetic part (21) and / or the second magnetic part (51) includes an electromagnet.

14. The drone storage (100) according to claim 11, characterized in that, In the top view direction, the fixing member (5) at least partially overlaps with the landing pad (2).

15. The drone storage (100) according to claim 7, characterized in that, The pulling member (42) includes a flexible cable.

16. The drone hangar (100) according to any one of claims 1-15, characterized in that, The first lifting assembly (31) includes: two first cantilevers (311) arranged oppositely and spaced apart; Wherein, one end of each first cantilever (311) away from the first lifting assembly (31) is rotatably connected to the base assembly (1).

17. The drone hangar (100) according to claim 16, characterized in that, The lifting mechanism (3) further includes: a first rotating shaft (33), with both ends of the first rotating shaft (33) fixedly connected to the base assembly (1); Wherein, one end of each of the first cantilevers (311) away from the first lifting assembly (31) is connected to the first rotating shaft (33), so that the two first cantilevers (311) rotate around the first rotating shaft (33).

18. The drone storage (100) according to claim 17, characterized in that, The base assembly (1) further includes: Two first bases (11), which are arranged relatively and at intervals; Wherein, both ends of the first rotating shaft (33) are respectively connected to the corresponding first bases (11).

19. The drone hangar (100) according to claim 18, characterized in that, The lifting mechanism (3) further includes: A second driving assembly (6), the fixed end of the second driving assembly (6) is connected to the base assembly (1), the output end of the second driving assembly (6) is connected to any one of the two first cantilevers (311), and the second driving assembly (6) is used to drive the first cantilever (311) to rotate relative to the base assembly (1).

20. The drone storage (100) according to claim 19, characterized in that, The second driving assembly (6) includes: A first connecting member (61), one end of the first connecting member (61) is fixedly connected to the base assembly (1); and A second connecting member (62), one end of the second connecting member (62) is fixedly connected to any one of the two first cantilevers (311), and the other end of the second connecting member (62) is connected to the other end of the first connecting member (61) and can telescopically move within the first connecting member (61) to drive the first cantilever (311) to rotate relative to the base assembly (1).

21. The drone hangar (100) according to claim 20, characterized in that, The base assembly (1) further includes: A second base (12), which is arranged at an interval from the first base (11); Wherein, one end of the first connecting member (61) is fixedly connected to the second base (12).

22. The drone storage (100) according to claim 19, characterized in that, The second driving assembly (6) includes: A first sliding member, which is connected to the base assembly (1); and A second sliding member, one end of the second sliding member is slidably connected to the first sliding member, and the other end is fixedly connected to any one of the two first cantilevers (311); Wherein, the second sliding member slides relative to the first sliding member to drive the first cantilever (311) to rotate relative to the base assembly (1).

23. The drone storage (100) according to claim 22, characterized in that, The second driving assembly (6) further includes: A first locking member, which is located at one end of the first sliding member away from the second lifting assembly (32) and is fixedly connected to the base assembly (1), wherein when the drone storage (100) is in the storage state, the second sliding member is limited by the first locking member; and / or, A second locking member, which is located at one end of the first sliding member close to the second lifting assembly (32) and is fixedly connected to the base assembly (1), wherein when the drone storage (100) is in the fully opened state, the second sliding member is limited by the second locking member.

24. The drone storage (100) according to claim 16, characterized in that, The first lifting assembly (31) further includes: A first support member (312), which is connected between the two first cantilevers (311) and is used to support the two first cantilevers (311).

25. The drone hangar (100) according to claim 16, characterized in that, The second lifting assembly (32) includes: Two second cantilevers (321), which are arranged relatively and at intervals; Wherein, each of the second cantilevers (321) is respectively rotatably connected to one end of the corresponding first cantilever (311) close to the first lifting assembly (31).

26. The drone storage (100) according to claim 25, characterized in that, The lifting mechanism (3) further includes: A second rotating shaft (34) to which the first cantilever (311) and the second cantilever (321) are both connected, so that the second cantilever (321) rotates relative to the first cantilever (311).

27. The drone hangar (100) according to claim 26, characterized in that, The lifting mechanism (3) further includes: A synchronous transmission assembly connected between the first cantilever (311) and the second cantilever (321) for driving the rotation of the second rotating shaft (34) to drive the second cantilever (321) to rotate relative to the first cantilever (311).

28. The drone hangar (100) according to claim 27, characterized in that, The synchronous transmission assembly includes: A driving wheel (71) fixedly connected to the first cantilever (311); A driven wheel (72) coaxially and fixedly connected to the second rotating shaft (34); and A transmission member (73) connected to the driving wheel (71) and the driven wheel (72), so that the driving wheel (71) drives the driven wheel (72) to rotate through the transmission member (73), thereby causing the second rotating shaft (34) to rotate.

29. The drone hangar (100) according to claim 25, wherein, The plane where the second cantilever (321) is located is parallel to the horizontal plane.

30. The drone hangar (100) according to claim 25, characterized in that, The second lifting assembly (32) further includes: A second support member (322) connected between the two second cantilevers (321) for supporting the two second cantilevers (321).

31. The drone hangar (100) according to claim 1, characterized in that, The drone hangar (100) further includes: A processor for detecting whether the apron (2) has fixed the drone (300) and, when detecting that the apron (2) has fixed the drone (300), sending a power-off signal to the drone (300) so that the drone (300) cuts off power.

32. A vehicle (200), characterized in that, Including the drone hangar (100) according to any one of claims 1-31.

33. The vehicle (200) according to claim 32, characterized in that, The vehicle (200) further includes: A vehicle body (201) including a hatch (202) and a receiving cavity (203), the receiving cavity (203) being disposed inside the vehicle body (201), and the hatch (202) being used to close and open the receiving cavity (203).

34. The vehicle (200) according to claim 33, characterized in that, When the drone hangar (100) is in the retracted state, the hatch (202) closes the receiving cavity (203), and the drone hangar (100) and the drone (300) are located inside the receiving cavity (203); and / or, When the drone hangar (100) is in the open state, the hatch (202) opens the receiving cavity (203), and the drone hangar (100) and the drone (300) are located outside the receiving cavity (203).

35. The vehicle (200) according to claim 33, characterized in that, The hatch (202) is fixedly connected to the first lifting assembly (31) and rotatably connected to the base assembly (1), and under the action of an external force, the first lifting assembly (31) can drive the hatch (202) to rotate relative to the base assembly (1).

36. The vehicle (200) according to claim 33, wherein, The accommodation cavity (203) is provided at the tail of the vehicle body (201).

Images