Unmanned aerial vehicle charging bin and unmanned aerial vehicle assembly

Abstract

The utility model provides an unmanned aerial vehicle charging bin and an unmanned aerial vehicle assembly. The unmanned aerial vehicle charging bin comprises a first shell and a second shell. A battery and a first connecting piece are arranged on the first shell; the second shell is used for containing the unmanned aerial vehicle, and a second connecting piece is arranged on the unmanned aerial vehicle; the first shell is rotationally connected with the second shell, and when the first shell is closed relative to the second shell, the first connecting piece is in butt joint with the second connecting piece, so that the unmanned aerial vehicle is electrically connected with the battery.

Description

Technical Field

[0001] The present invention relates to the field of drone technology, and more particularly to a drone charging compartment and a drone component. Background Art

[0002] A drone is an unmanned aircraft controlled by a radio remote control device or a self-contained program control device. In recent years, with the development of drone technology, drones have been widely used in various fields, such as aerial photography, agriculture, plant protection, micro selfies, express transportation, disaster relief, surveying and mapping, news reporting, power inspection, etc. Drones consume electricity when performing tasks, and the battery life limits the flight time of drones; at the same time, due to weight and volume limitations, it is impossible to increase the battery life by infinitely expanding the battery capacity. Therefore, how to effectively charge drones and ensure their ability to continue to operate has become an important issue in the development of drone technology. Utility Model Content

[0003] One or more embodiments of the present specification provide a drone charging compartment, comprising: a first shell and a second shell; the first shell is provided with a battery and a first connecting member; the second shell is used to accommodate a drone, and the drone is provided with a second connecting member; the first shell is rotatably connected to the second shell, and when the first shell is closed relative to the second shell, the first connecting member is docked with the second connecting member, thereby electrically connecting the drone to the battery.

[0004] In some embodiments, the first connector includes a plurality of spring pins, the second connector includes a plurality of contacts, and the plurality of spring pins correspond to the plurality of contacts one by one.

[0005] In some embodiments, the second connector is a pluggable connector, one end of the second connector is a USB interface, and the other end of the second connector is provided with the multiple contacts.

[0006] In some embodiments, a first magnetic member is disposed at one end of the first connecting member facing the second connecting member, and a second magnetic member is disposed at one end of the second connecting member facing the first connecting member; the first magnetic member and the second magnetic member are disposed correspondingly.

[0007] In some embodiments, a guide groove is provided on the outer periphery of the plurality of spring pins of the first connector, and when the first connector is docked with the second connector, at least a portion of the second connector extends into the guide groove.

[0008] In some embodiments, the first shell includes a side shell and a middle shell, the side shell is detachably connected to the middle shell, and the battery is disposed between the side shell and the middle shell.

[0009] In some embodiments, a transparent observation window is provided on the first shell, and control buttons and / or a display screen are provided on the drone. When the first shell is closed relative to the second shell, the control buttons and / or the display screen correspond to the transparent observation window.

[0010] In some embodiments, metal ears are respectively provided on both sides of the first shell; the drone charging compartment also includes a shoulder strap, and both ends of the shoulder strap are respectively connected to the metal ears on both sides of the first shell.

[0011] In some embodiments, a limiting block is provided on a side of the second shell facing the first shell.

[0012] In some embodiments, a third magnetic component is disposed in the limiting block, and when the first shell is closed relative to the second shell, the third magnetic component is attracted to the first shell.

[0013] In some embodiments, a first inclined plate is provided on one side of the bottom of the second shell, and a first notch corresponding to the first inclined plate is provided at a corresponding position of the drone.

[0014] In some embodiments, a second inclined plate is provided on the other side of the bottom of the second shell, and a second notch corresponding to the second inclined plate is provided at a corresponding position of the drone; wherein the first inclined plate and the second inclined plate have different sizes, and the first notch and the second notch have different sizes.

[0015] In some embodiments, an anti-reverse positioning protrusion is provided at the bottom of the second shell, and the anti-reverse positioning protrusion corresponds to a hollow portion when the drone is placed in the second shell in the correct position.

[0016] One or more embodiments of the present specification provide a drone assembly, including the drone charging compartment and the drone described in any embodiment of the present specification. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] This specification will be further explained by way of exemplary embodiments, which will be described in detail by way of the accompanying drawings. The same numbers in the drawings represent the same structures or steps.

[0018] Figure 1 is a schematic diagram of a first state of a drone component according to some embodiments of the present specification.

[0019] Figure 2 is a schematic diagram of a second state of a drone component according to some embodiments of the present specification.

[0020] Figure 3It is a first-person perspective structural diagram of a drone charging pod according to some embodiments of this specification.

[0021] Figure 4 It is a schematic diagram of the structure of the drone charging compartment from a second perspective according to some embodiments of this specification.

[0022] Figure 5 It is a schematic diagram of the exploded structure of the drone charging compartment shown in some embodiments of this specification.

[0023] Figure 6 It is a third-perspective structural diagram of a drone charging compartment according to some embodiments of this specification.

[0024] Figure 7 It is a schematic diagram of the structure of the drone charging compartment from a fourth perspective according to some embodiments of this specification.

[0025] Figure 8 It is a partial structural schematic diagram of a drone charging compartment according to some embodiments of this specification.

[0026] Fig. 9 It is a fifth perspective structural diagram of the drone charging compartment shown in some embodiments of this specification.

[0027] Fig.10 It is a schematic diagram of a drone and a second connecting member in an unconnected state according to some embodiments of the present specification.

[0028] Fig.11 It is a schematic diagram of the connection status of the drone and the second connecting member according to some embodiments of the present specification.

[0029] Fig.12 It is a schematic diagram from another perspective of the connection status of the drone and the second connecting member shown in some embodiments of this specification.

[0030] Fig.13 It is a schematic diagram of the structure of the first connecting member shown in some embodiments of this specification.

[0031] Fig.14 It is a schematic diagram of the structure of the second connecting member shown in some embodiments of this specification.

[0032] Fig.15 It is a schematic diagram of the docking of the first connecting member and the second connecting member shown in some embodiments of this specification.

[0033] Fig.16 It is a schematic diagram of a drone and a first connecting member in an unconnected state according to some embodiments of the present specification.

[0034] Fig.17It is a schematic diagram of the connection status of the drone and the first connecting member according to some embodiments of the present specification.

[0035] Fig.18 It is a schematic diagram of an L-shaped wrench installed in a drone charging compartment according to some embodiments of this specification.

[0036] Fig.19 It is a schematic diagram of the structure of an L-shaped wrench shown in some embodiments of this specification.

[0037] Fig. 20 It is a schematic diagram of the structure of the second shell shown in some embodiments of this specification.

[0038] Fig.21 It is a first perspective schematic diagram of a drone installed in a second shell according to some embodiments of this specification.

[0039] Fig. 22 This is a second perspective schematic diagram of a drone installed in a second shell according to some embodiments of this specification.

[0040] Fig.23 It is a structural schematic diagram of a second shell according to another embodiment of the present specification.

[0041] Fig.24 It is a first perspective schematic diagram of a drone installed in a second shell according to another embodiment of the present specification.

[0042] Fig.25 It is a second perspective schematic diagram of a drone installed in a second shell according to another embodiment of the present specification.

[0043] In the figure, 100-UAV charging compartment, 110-first shell, 111-battery, 112-first connecting piece, 113-spring pin, 114-first magnetic member, 115-guide groove, 116-side shell, 117-middle shell, 118-transparent observation window, 119-metal hanging ear, 120-second shell, 121-limiting block, 122-third magnetic member, 123-first inclined plate, 124-second inclined plate, 125-anti-reverse fixed Position bump, 130-shoulder strap, 140-leather layer, 150-hinge, 160-male webbing lock buckle, 170-female lock buckle, 180-L-shaped wrench, 181 horn, 200-drone, 210-second connecting piece, 211-contact, 212-USB interface, 213-second magnetic suction piece, 220-control button, 230-display screen, 240-first missing corner, 250-second missing corner, 1000-drone component. DETAILED DESCRIPTION

[0044] In order to more clearly illustrate the technical solutions of the embodiments of this specification, the embodiments will be described in detail below with reference to the accompanying drawings. Obviously, the contents described below are some examples or embodiments of this specification. For ordinary technicians in this field, without paying creative work, the technical solutions or means disclosed in this specification can also be applied to other scenarios based on these technical contents.

[0045] Unless otherwise specified, technical terms used in this specification to describe components, elements, etc. do not refer to the singular, but may also include the plural. Generally speaking, terms such as "include", "comprise", etc. only indicate that the steps, elements, or components that have been clearly identified are included, and these steps, elements, and components do not constitute an exclusive list, such as the method or device described may also include other steps or components.

[0046] A drone is an unmanned aircraft controlled by a radio remote control device or a self-contained program control device. In recent years, drones have become increasingly popular. For example, drones can be used in aerial photography, agriculture, plant protection, micro selfies, express transportation, disaster relief, surveying and mapping, news reporting, power inspection and other fields. However, the endurance of existing drones is generally low, and it is necessary to replace the battery or charge it in time to ensure the continuous operation of the drone. To this end, some embodiments of this specification provide a drone charging compartment and a drone component; the drone charging compartment can charge the drone conveniently and in time.

[0047] Figure 1 is a schematic diagram of a first state of a drone component according to some embodiments of the present specification. Figure 2 is a schematic diagram of a second state of a drone component according to some embodiments of the present specification. Figure 3 It is a first-person perspective structural diagram of a drone charging pod according to some embodiments of this specification. Figure 4 It is a schematic diagram of the structure of the drone charging compartment from a second perspective according to some embodiments of this specification. Figure 5 It is a schematic diagram of the exploded structure of the drone charging compartment shown in some embodiments of this specification.

[0048] Some embodiments of this specification provide a drone charging compartment 100. In some embodiments, Figure 1-5 As shown, the drone charging compartment 100 may include a first shell 110 and a second shell 120; the first shell 110 is provided with a battery 111 and a first connector 112; the second shell 120 is used to accommodate the drone 200, and the drone 200 is provided with a second connector 210. The first shell 110 is rotatably connected to the second shell 120, and when the first shell 110 is closed relative to the second shell 120, the first connector 112 is docked with the second connector 210, so that the drone 200 is electrically connected to the battery 111.

[0049] In some embodiments, the battery 111 in the drone charging compartment 100 may include one or more lithium batteries, and the battery 111 can store electricity. The electrical connection between the drone 200 and the battery 111 can be understood as the electronic devices in the drone (such as drone batteries, controllers, etc.) establishing a connection with the battery 111 and being able to transmit electricity / electrical signals. When the drone 200 is electrically connected to the battery 111, the battery 111 can transmit the stored electricity to the drone battery, thereby achieving the purpose of charging the drone.

[0050] In some embodiments, Figure 5 As shown, the first shell 110 may include a side shell 116 and a middle shell 117, the side shell 116 and the middle shell 117 are detachably connected, and the battery 111 is arranged between the side shell 116 and the middle shell 117. By arranging the battery 111 between the side shell 116 and the middle shell 117, the battery 111 can be effectively protected. In some embodiments, the side shell 116 and the middle shell 117 can be detachably connected by means of screw connection, snap connection, etc. In some embodiments, a control circuit board, connecting wires, etc. can also be arranged between the side shell 116 and the middle shell 117. Through the detachable connection, it is convenient to repair and replace the battery, control circuit board, etc. between the side shell 116 and the middle shell 117.

[0051] In some embodiments, Figure 5 As shown, the outer surface of the first shell 110 and / or the second shell 120 may be provided with a veneer layer 140. The veneer layer 140 may be made of a cloth material or a leather material, and may be fixed to the outer surface of the first shell 110 and / or the second shell 120 by gluing, clamping, sewing, etc. In some embodiments, as Figure 5 As shown, the outer surfaces of the first shell 110 and the second shell 120 may be provided with a veneer layer 140. In some embodiments, the veneer layer 140 may be provided on the outer surface of only one of the first shell 110 or the second shell 120. By providing the veneer layer 140, the first shell 110 and / or the second shell 120 can be protected, and the texture and aesthetics of the charging bin can also be improved.

[0052] Figure 6 It is a third-perspective structural diagram of a drone charging compartment according to some embodiments of this specification. Figure 7 is a schematic diagram of the fourth perspective structure of the drone charging compartment according to some embodiments of this specification. Figure 4-7As shown, metal ears 119 may be provided on both sides of the first shell 110, and the drone charging compartment 100 may also include a shoulder strap 130, and the two ends of the shoulder strap 130 are respectively connected to the metal ears 119 on both sides of the first shell 110. By providing the metal ears 119 and the shoulder strap 130, the drone charging compartment can be made more convenient to carry; for example, the drone charging compartment 100 can be carried on the shoulder by the shoulder strap. In some embodiments, the drone charging compartment 100 may also include a webbing male lock buckle 160 and a female lock buckle 170. One end of the webbing male lock buckle 160 is fixedly connected to one of the first shell 110 or the second shell 120, and the other end of the webbing male lock buckle 160 is lockably connected to the other of the first shell 110 or the second shell 120 through the female lock buckle 170. For example, one end of the webbing male lock buckle 160 is fixedly connected to the second housing 120, the female lock buckle 170 is provided on the first housing 110, and the other end of the webbing male lock buckle 160 is lockably connected to the first housing 110 through the female lock buckle 170. By providing the webbing male lock buckle 160 and the female lock buckle 170, when the first housing 110 is closed relative to the second housing 120, the first housing 110 and the second housing 120 can be locked, thereby preventing the first housing 110 from being opened relative to the second housing by mistake.

[0053] Figure 8 It is a partial structural schematic diagram of a drone charging compartment according to some embodiments of this specification. Fig. 9 is a fifth perspective structural diagram of a drone charging compartment according to some embodiments of this specification. Figure 8-9 As shown, the first housing 110 and the second housing 120 can be rotatably connected by a hinge 150. In some embodiments, the maximum opening angle of the hinge can be 90-100 degrees, that is, the maximum opening angle of the first housing 110 relative to the second housing 120 is 90-100 degrees. At this time, the first housing 110 can be opened to 90 degrees relative to the second housing 120. Figure 1-3 In some embodiments, the maximum opening angle of the hinge can be 40-50 degrees, that is, the maximum opening angle of the first shell 110 relative to the second shell 120 is 40-50 degrees. At this time, the first shell 110 can be opened to 40-50 degrees relative to the second shell 120. Fig. 9 By setting the maximum opening angle of the hinge to 40-50 degrees, it is not only convenient to put the drone in and out, but also can prevent the drone from falling out accidentally when the charging compartment is opened (that is, when the first shell 110 is opened relative to the second shell 120).

[0054] Fig.10 It is a schematic diagram of a drone and a second connecting member in an unconnected state according to some embodiments of the present specification. Fig.11It is a schematic diagram of the connection status of the drone and the second connecting member according to some embodiments of the present specification. Fig.12 It is a schematic diagram from another perspective of the connection status of the drone and the second connecting member shown in some embodiments of this specification. Fig.13 It is a schematic diagram of the structure of the first connecting member shown in some embodiments of this specification. Fig.14 It is a schematic diagram of the structure of the second connecting member shown in some embodiments of this specification. Fig.15 It is a schematic diagram of the docking of the first connecting member and the second connecting member shown in some embodiments of this specification. Fig.16 It is a schematic diagram of a drone and a first connecting member in an unconnected state according to some embodiments of the present specification. Fig.17 It is a schematic diagram of the connection status of the drone and the first connecting member according to some embodiments of the present specification.

[0055] In some embodiments, Figure 10-17 As shown, the first connector 112 may include a plurality of spring pins 113, and the second connector 210 may include a plurality of contacts 211, and the plurality of spring pins 113 correspond to the plurality of contacts 211 one by one. When the first connector 112 and the second connector 210 are docked, the plurality of spring pins 113 and the plurality of contacts 211 are respectively connected to each other. In some embodiments, the plurality of spring pins 113 of the first connector 112 may be connected to the battery 111, and the plurality of contacts 211 of the second connector 210 may be connected to the electronic components of the drone (such as the drone battery, controller, etc.), so that when the first connector 112 and the second connector 210 are docked, the drone 200 is electrically connected to the battery 111. In some embodiments, the plurality of spring pins 113 of the first connector 112 may be connected to the battery 111 through a control circuit board. Through the cooperation between the spring pins and the contacts, the spring pins will be compressed to a certain extent during docking, so that the connection between the first connector 112 and the second connector 210 can be better ensured.

[0056] In some embodiments, the design forms of the first connector 112 and the second connector 210 can be interchangeable. For example, the first connector 112 can include a plurality of contacts, and the second connector 210 can include a plurality of spring pins, and the plurality of spring pins correspond to the plurality of contacts one by one.

[0057] In some embodiments, the first connector 112 may be fixedly mounted on the first housing 110. In some embodiments, the second connector 210 may be fixedly mounted on the drone 200.

[0058] In some embodiments, the second connector 210 may be a pluggable connector, one end of the second connector 210 is a USB interface 212, and the other end of the second connector 210 is provided with a plurality of contacts 211. In some embodiments, the USB interface may include a Type A interface, a Type B interface, a Type C interface, etc. By setting the second connector 210 as a pluggable connector, the charging compartment can be applied to existing drones that have adopted a USB interface for charging. The second connector 210 can convert the circuit of the USB interface into a plurality of contacts 211, so as to facilitate docking with the first connector 112, thereby realizing electrical connection between the drone and the battery. In some embodiments, when the second connector 210 is a pluggable connector, the drone charging compartment 100 may further include an L-shaped wrench 180, which can facilitate the user to pull out the second connector 210.

[0059] Fig.18 It is a schematic diagram of an L-shaped wrench installed in a drone charging compartment according to some embodiments of this specification. Fig.19 Schematic diagram of the structure of an L-shaped wrench according to some embodiments of this specification. Figure 18-19 As shown, the drone charging compartment 100 may include an L-shaped wrench 180. The L-shaped wrench 180 may include a clevis 181, and the clevis 181 may be a U-shaped or V-shaped notch. When in use, the user can use the clevis 181 to clamp the second connecting member 210, and then use the L-shaped wrench 180 to apply force to pull the second connecting member 210 out of the drone 200. In some embodiments, a placement slot may be provided on the drone charging compartment 100, and the L-shaped wrench 180 may be clamped in the prevention slot, thereby effectively preventing the L-shaped wrench 180 from being lost.

[0060] In some embodiments, Figure 13-15 As shown, a first magnetic member 114 is provided at one end of the first connecting member 112 facing the second connecting member 210, and a second magnetic member 213 is provided at one end of the second connecting member 210 facing the first connecting member 112; the first magnetic member 114 and the second magnetic member 213 are provided correspondingly. In some embodiments, one of the first magnetic member 114 or the second magnetic member 213 is a magnet, and the other is a metal member that can be attracted by a magnet. In some embodiments, both the first magnetic member 114 and the second magnetic member 213 are magnets, and can attract each other when they are close. The corresponding arrangement of the first magnetic member 114 and the second magnetic member 213 can be understood as that when the first connecting member 112 and the second connecting member 210 are docked, the first magnetic member 114 and the second magnetic member 213 are just close to each other. By providing the first magnetic member 114 and the second magnetic member 213 , the first connecting member 112 and the second connecting member 210 can be more easily aligned during docking, and the first connecting member 112 and the second connecting member 210 can be more stably docked.

[0061] In some embodiments, Figure 3 As shown, the outer periphery of the plurality of spring pins of the first connector 112 may be provided with a guide groove 115, and when the first connector 112 is docked with the second connector 210, at least a portion of the second connector 210 extends into the guide groove 115. By providing the guide groove 115, the second connector 210 can be guided and positioned when the first connector 112 and the second connector 210 are docked, so that the alignment of the first connector 112 and the second connector 210 is more convenient. At the same time, the restriction of the second connector 210 by the guide groove 115 can limit the position of the drone 200 to a certain extent, thereby reducing the shaking of the drone 200 in the charging compartment 100.

[0062] In some embodiments, a transparent observation window 118 is provided on the first housing 110, and a control button 220 and / or a display screen 230 are provided on the drone 200. When the first housing 110 is closed relative to the second housing 120, the control button 220 and / or the display screen 230 correspond to the transparent observation window 118. In some embodiments, the transparent observation window 118 can be a hollow design or realized by setting a transparent material (such as glass, acrylic, transparent plastic, etc.). By setting a transparent observation window, when the first housing 110 is closed relative to the second housing 120, the control button 220 and / or the display screen 230 can be displayed through the transparent observation window; the user can operate the control button 220 and / or view the information on the display screen 230.

[0063] In some embodiments, a power indicator light is provided on the first housing 110, and the power indicator light can be used to display the remaining power of the battery 111. In some embodiments, a control switch is provided on the first housing 110, and the control switch can be used to control the battery 111 to discharge externally. In some embodiments, a charging port is provided on the first housing 110, and the battery 111 can be charged through the charging port. In some embodiments, the charging port on the first housing 110 can integrate a discharge function, and the battery 111 can be discharged through the charging port, so as to facilitate charging of mobile phones or other electronic products.

[0064] Fig. 20 It is a schematic diagram of the structure of the second shell shown in some embodiments of this specification. Fig.21 It is a first perspective schematic diagram of a drone installed in a second shell according to some embodiments of this specification. Fig. 22 This is a second perspective schematic diagram of a drone installed in a second shell according to some embodiments of this specification.

[0065] In some embodiments, Figure 20-22As shown, a limit block 121 may be provided on the side of the second shell 120 facing the first shell 110. By providing the limit block 121, it is possible to prevent the drone 200 from tipping over or falling out after being placed into the second shell 120. In some embodiments, a third magnetic member 122 is provided in the limit block 121, and when the first shell 110 is closed relative to the second shell 120, the third magnetic member 122 can be attracted to the first shell 110. In some embodiments, the third magnetic member 122 may be a magnet, and the first shell 110 may be attracted by the magnet. In some embodiments, the third magnetic member 122 may be a magnet, and the first shell 110 may be provided with a magnet of opposite sex or a metal member that can be attracted by the magnet at a position corresponding to the third magnetic member 122, so that the third magnetic member 122 can be attracted to the first shell 110.

[0066] In some embodiments, Figure 20-22 As shown, a first inclined plate 123 is provided on one side of the bottom of the second housing 120 (the left side in the figure), and a first notch 240 corresponding to the first inclined plate 123 is provided at a corresponding position of the drone 200. When the drone 200 is placed in the second housing 120 according to a preset orientation, the drone 200 can fit exactly in the space of the second housing 120 because the first inclined plate 123 corresponds to the first notch 240; and when the drone 200 is placed in the second housing 120 according to the opposite orientation, the first inclined plate 123 will cause the drone 200 to not fit in the space of the second housing 120, thereby reminding the user that the orientation of the drone 200 is incorrect.

[0067] In some embodiments, a second inclined plate 124 is provided on the other side of the bottom of the second housing 120 (as shown on the right side in the figure), and a second notch 250 corresponding to the second inclined plate 124 is provided at a corresponding position of the drone 200; wherein, the first inclined plate 123 and the second inclined plate 124 have different sizes, and the first notch 240 and the second notch 250 have different sizes. By setting the first inclined plate 123 and the second inclined plate 124 in different sizes, when the drone 200 is placed in the second housing 120 in opposite directions, the first inclined plate 123 and the second inclined plate 124 will cause the space between the drone 200 and the second housing 120 to be unable to fit, thereby being able to remind the user that the orientation of the drone 200 is incorrect. In some embodiments, the second inclined plate 124 can be omitted. By setting the first inclined plate 123 and / or the second inclined plate 124, it is also possible to limit the placed drone 200 and reduce the shaking of the drone 200 in the second housing 120.

[0068] Fig.23 It is a structural schematic diagram of a second shell according to another embodiment of the present specification. Fig.24 It is a first perspective schematic diagram of a drone installed in a second shell according to another embodiment of the present specification. Fig.25It is a second perspective schematic diagram of a drone installed in a second shell according to another embodiment of the present specification.

[0069] In some embodiments, an anti-reverse positioning convex block 125 is provided at the bottom of the second housing 120, and the anti-reverse positioning convex block 125 corresponds to the hollowed-out portion when the drone 200 is placed in the second housing 120 in the correct position. In some embodiments, there may be multiple hollowed-out portions on the outer surface of the drone 200, and the anti-reverse positioning convex block 125 may correspond to at least one of the hollowed-out portions. When the drone 200 is placed in the second housing 120 in the correct position, the anti-reverse positioning convex block 125 may be just embedded in the hollowed-out portion, so that the drone 200 can fit exactly with the space of the second housing 120. When the drone 200 is placed in the second housing 120 in the opposite orientation, the anti-reverse positioning convex block 125 will cause the drone 200 to be unable to fit with the space of the second housing 120, thereby being able to remind the user that the orientation of the drone 200 is incorrect. By setting the anti-reverse positioning convex block 125, it is also possible to limit the placed drone 200 and reduce the shaking of the drone 200 in the second housing 120.

[0070] Some embodiments of the present specification provide a drone assembly 1000. Figure 1-2 As shown, the drone assembly 1000 may include the drone charging compartment 100 and the drone 200 of any embodiment of this specification.

[0071] The beneficial effects that may be brought about by the embodiments of this specification include but are not limited to: (1) The drone charging compartment can charge the drone conveniently and timely; (2) By providing metal ears and shoulder straps, the drone charging compartment can be made more convenient to carry; (3) By setting the maximum opening angle of the hinge, it is not only convenient to put the drone in and out, but also to prevent the drone from accidentally falling out when the charging compartment is opened; (4) By cooperating with the spring pin and the contact, the connection between the first connector and the second connector can be better guaranteed; (5) Through the anti-reverse design (such as the inclined plate, the anti-reverse positioning bump), the user can be reminded that the orientation of the drone is incorrect. It should be noted that different embodiments may produce different beneficial effects. In different embodiments, the beneficial effects that may be produced may be any one or a combination of the above, or any other possible beneficial effects.

[0072] The basic concepts have been described above. Obviously, for those skilled in the art, the above detailed disclosure is only for example and does not constitute a limitation of this specification. Although not explicitly stated here, those skilled in the art may make various modifications, improvements and corrections to this specification. Such modifications, improvements and corrections are taught in this specification, so such modifications, improvements and corrections still belong to the spirit and scope of the exemplary embodiments of this specification.

Claims

1. A drone charging compartment, characterized in that: include: a first shell and a second shell; The first housing is provided with a battery and a first connecting member; The second housing is used to accommodate a drone, and the drone is provided with a second connecting member; The first shell is rotatably connected to the second shell. When the first shell is closed relative to the second shell, the first connecting member is docked with the second connecting member, thereby electrically connecting the drone to the battery.

2. The drone charging compartment according to claim 1, characterized in that: The first connecting member includes a plurality of spring pins, and the second connecting member includes a plurality of contact points, and the plurality of spring pins correspond to the plurality of contact points one by one.

3. The drone charging compartment according to claim 2, characterized in that: The second connector is a pluggable connector, one end of the second connector is a USB interface, and the other end of the second connector is provided with the multiple contacts.

4. The drone charging compartment according to claim 2, characterized in that: A first magnetic member is disposed at one end of the first connecting member facing the second connecting member, and a second magnetic member is disposed at one end of the second connecting member facing the first connecting member; the first magnetic member and the second magnetic member are disposed correspondingly.

5. The drone charging compartment according to claim 2, characterized in that: A guide groove is provided on the outer periphery of the plurality of spring pins of the first connecting member. When the first connecting member is docked with the second connecting member, at least a portion of the second connecting member extends into the guide groove.

6. The drone charging compartment according to claim 1, characterized in that: The first shell includes a side shell and a middle shell, the side shell is detachably connected to the middle shell, and the battery is arranged between the side shell and the middle shell.

7. The drone charging compartment according to claim 1, characterized in that: The first shell is provided with a transparent observation window, and the drone is provided with control buttons and / or a display screen. When the first shell is closed relative to the second shell, the control buttons and / or the display screen correspond to the transparent observation window.

8. The drone charging compartment according to claim 1, characterized in that: Metal hanging ears are respectively provided on both sides of the first shell; the drone charging compartment also includes a shoulder strap, and both ends of the shoulder strap are respectively connected to the metal hanging ears on both sides of the first shell.

9. The drone charging compartment according to claim 1, characterized in that: A limiting block is provided on one side of the second shell facing the first shell.

10. The drone charging compartment according to claim 9, characterized in that: The limiting block is provided with a third magnetic attraction component, and when the first shell is closed relative to the second shell, the third magnetic attraction component is attracted to the first shell.

11. The drone charging compartment according to claim 1, characterized in that: A first inclined plate is provided on one side of the bottom of the second shell, and a first notch corresponding to the first inclined plate is provided at a corresponding position of the drone.

12. The drone charging compartment according to claim 11, characterized in that: A second inclined plate is provided on the other side of the bottom of the second shell, and a second notch corresponding to the second inclined plate is provided at a corresponding position of the drone; wherein the first inclined plate and the second inclined plate have different sizes, and the first notch and the second notch have different sizes.

13. The drone charging compartment according to claim 1, characterized in that: An anti-reverse positioning protrusion is provided at the bottom of the second shell, and the anti-reverse positioning protrusion corresponds to the hollowed-out portion when the drone is placed in the second shell in the correct position.

14. A drone assembly, characterized in that: The invention comprises a drone charging compartment and a drone as described in any one of claims 1 to 13.

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