Helipad, vehicle-mounted drone cabin and vehicle

Abstract

This application relates to the field of unmanned aerial vehicle (UAV) technology, and discloses a landing platform, a vehicle-mounted UAV cabin, and a vehicle. The landing platform includes a centering mechanism and a landing pad. The centering mechanism includes a first centering section and a second centering section. The first and second centering sections are installed on the bearing plane of the landing pad and are configured to push the UAV towards the center of the bearing plane for fixing and positioning the UAV. The bearing plane is used to park the UAV. Each of the first and second centering sections includes two opposing centering units, which can move along the bearing plane towards or away from each other, and the movement direction of the first centering section is perpendicular to the movement direction of the second centering section. Both the first and second centering sections pass through a first plane, which is parallel to the bearing plane. The landing platform provided by this application eliminates errors generated during UAV centering and improves the accuracy of the centering operation.

Description

Technical Field

[0001] This application relates to the field of unmanned aerial vehicle (UAV) technology, specifically to a parking platform, a vehicle-mounted UAV cabin, and a vehicle. Background Technology

[0002] With the continuous development of drones, drones are widely used in various fields and industries. Among them, vehicle-mounted drones are favored by users because they are easy to use in conjunction with cars and have strong mobility.

[0003] Cars travel at high speeds, and drones are affected by factors such as airflow, making it difficult for them to land precisely at the designated location for storage or battery swapping. Usually, it is necessary to center the drone and move it to the designated location.

[0004] In related technologies, the centering device of a drone may have errors during the centering operation, which may interfere with subsequent operations such as storage and battery swapping. Summary of the Invention

[0005] In view of this, this application provides a parking platform, a vehicle-mounted drone cabin, and a vehicle, which eliminates the errors generated by the drone during centering and improves the accuracy of centering operations.

[0006] Specifically, the embodiments of this application include the following technical solutions:

[0007] The first aspect of this application provides a parking platform for use in the cabin of a vehicle-mounted unmanned aerial vehicle, the parking platform including a centering mechanism and a parking apron;

[0008] The centering mechanism includes a first centering section and a second centering section;

[0009] The first centering section and the second centering section are installed on the bearing plane of the landing pad and are configured to push the UAV toward the center of the bearing plane to fix and position the UAV. The bearing plane is used to park the UAV.

[0010] Both the first centering section and the second centering section include two centering units arranged opposite to each other. The two centering units can move along the bearing plane in a direction that is closer to or farther from each other, and the moving direction of the first centering section is perpendicular to the moving direction of the second centering section.

[0011] Both the first centering portion and the second centering portion pass through the first plane, which is parallel to the bearing plane.

[0012] Optionally, the two centering units of the first centering section are located between the two centering units of the second centering section, and the length of the centering unit of the first centering section is less than the length of the centering unit of the second centering section.

[0013] Optionally, the centering mechanism further includes a charging unit connected to at least one of the first centering part and the second centering part, and at least a portion of the charging unit protrudes from the contact surface between the first centering part and / or the second centering part and the drone, for contacting the drone and charging the drone.

[0014] Optionally, the parking platform further includes a triggering mechanism, which is connected to the parking platform and to the centering mechanism and the UAV signal respectively. The triggering mechanism is configured to send a power-on or power-off signal to the UAV according to the operating status of the centering mechanism.

[0015] A second aspect of this application provides a vehicle-mounted drone cabin, the vehicle-mounted drone cabin including the aforementioned parking platform.

[0016] Optionally, the vehicle-mounted UAV cabin also includes a cabin body, a lifting mechanism, and a moving mechanism;

[0017] The interior of the cabin has a receiving cavity, and one side of the receiving cavity is open.

[0018] The lifting mechanism is located on the side of the parking platform away from the bearing plane and is connected to the parking platform;

[0019] The lifting mechanism has an extended state and a retracted state, wherein in the extended state, the bearing plane is flush with the top of the cabin;

[0020] The moving mechanism is movably connected to the receiving cavity and to the lifting mechanism to drive the stopping platform to extend or retract from the opening.

[0021] Optionally, the vehicle-mounted drone cabin also includes a spoiler, which is located on the side of the cabin where the opening is provided and is connected to the top surface of the cabin, for the purpose of diverting the airflow flowing through the top surface.

[0022] Optionally, the vehicle-mounted drone cabin also includes a camera unit, and the spoiler has a mounting opening, the opening direction of which faces the center of the bearing plane, and at least a portion of the camera unit is located within the mounting opening.

[0023] Optionally, the vehicle-mounted drone cabin also includes a temperature control mechanism connected to the cabin body, used to regulate the real-time temperature inside the containment cavity.

[0024] A third aspect of this application provides a vehicle that includes the aforementioned vehicle-mounted unmanned aerial vehicle (UAV) cabin.

[0025] The beneficial effects of the technical solutions provided in this application include at least the following:

[0026] The landing platform, vehicle-mounted UAV cabin, and vehicle provided in this application embodiment, by setting a first centering section and a second centering section on the landing pad, can push the UAV to the center area of ​​the landing pad, thereby achieving the fixation and positioning of the UAV. In related technologies, the centering devices have limiting components of different heights in different directions, which do not interfere with each other, but may result in errors along the length or width direction of the UAV during centering. However, in this application, both the first and second centering sections pass through the same plane parallel to the bearing plane. During the centering operation, the first and second centering sections limit the UAV in two mutually perpendicular directions at the same height, eliminating potential errors in the length or width direction during centering, improving the accuracy of the centering operation, and reducing the risk of inaccurate centering affecting subsequent operations. Attached Figure Description

[0027] To more clearly illustrate the technical solutions in the embodiments of this application, the accompanying drawings used in the description of the embodiments will be briefly introduced below. Obviously, the accompanying drawings described below are only some embodiments of this application. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0028] Figure 1 This paper shows a first structural schematic diagram of the vehicle-mounted unmanned aerial vehicle (UAV) cabin provided in an embodiment of this application;

[0029] Figure 2 This illustration shows a first structural diagram of the first centralization section provided in an embodiment of this application;

[0030] Figure 3 This illustration shows a second structural diagram of the first centralization section provided in an embodiment of this application;

[0031] Figure 4 A schematic diagram of the centralization mechanism provided in an embodiment of this application is shown;

[0032] Figure 5 This diagram illustrates the connection relationship between the triggering structure, the centering mechanism, and the UAV provided in an embodiment of this application.

[0033] Figure 6 This paper shows a second structural schematic diagram of the vehicle-mounted unmanned aerial vehicle cabin provided in an embodiment of this application;

[0034] Figure 7 A schematic diagram of the structure of the turbulence section provided in an embodiment of this application is shown.

[0035] 1. Centralization mechanism; 11. First centralization section; 12. Second centralization section; 13. Charging section;

[0036] 2. Helipad; 21. Load-bearing surface;

[0037] 3. Triggering mechanism;

[0038] 4. Hull; 41. Reception cavity; 42. Blowout section; 421. Mounting opening; 43. Camera section; 44. Top surface;

[0039] 5. Lifting mechanism; 51. Enclosed section;

[0040] 6. Moving mechanism;

[0041] 7. Temperature control mechanism; 71. Heating section; 72. Cooling section. Detailed Implementation

[0042] The technical solutions of the embodiments of this application will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of this application, not all embodiments. Based on the embodiments of this application, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of this application. To make the technical solutions and advantages of this application clearer, the parking platform, vehicle-mounted UAV cabin, and vehicle will be described in detail below with reference to the accompanying drawings.

[0043] With the continuous development of drones, drones are widely used in various fields and industries. Among them, vehicle-mounted drones are favored by users because they are easy to use in conjunction with cars and have strong mobility.

[0044] Cars travel at high speeds, and drones are affected by factors such as airflow, making it difficult for them to land precisely at the designated location for storage or battery swapping. Usually, it is necessary to center the drone and move it to the designated location.

[0045] However, drone parking platforms in related technologies typically include two sets of centering components, one set positioned above the other, with the two sets moving independently. Therefore, during centering, the upper centering rod may become misaligned with the intended position (the drone's parking location) after movement, resulting in errors in the drone's length or width along the parking platform. This can interfere with subsequent operations such as storage and battery swapping.

[0046] In response, this application provides a parking platform for use in the cabin of a vehicle-mounted unmanned aerial vehicle, such as... Figure 1 As shown, the landing platform includes a centering mechanism 1 and a landing pad 2. The centering mechanism 1 includes a first centering section 11 and a second centering section 12. The first centering section 11 and the second centering section 12 are mounted on the bearing plane 21 of the landing pad 2 and are configured to push the UAV towards the center of the bearing plane 21 for fixing and positioning the UAV. The bearing plane 21 is used to park the UAV. Each of the first centering section 11 and the second centering section 12 includes two centering units arranged opposite each other. The two centering units can move along the bearing plane 21 in a direction closer to or farther from each other, and the movement direction of the first centering section 11 is perpendicular to the movement direction of the second centering section 12. The first centering section 11 and the second centering section 12 both pass through a first plane, which is parallel to the bearing plane 21. Here, the first plane is a virtual plane, and the definition associated with the first plane indicates that when the bearing plane 21 is in a horizontal position, the first centering section 11 and the second centering section 12 are approximately at the same height.

[0047] The landing platform provided in this application, by setting a first centering part 11 and a second centering part 12 on the landing pad 2, can push the drone to the center area of ​​the landing pad 2, thereby achieving the fixation and positioning of the drone. In related technologies, the centering components in different directions have different heights and do not interfere with each other, which may result in errors along the length or width direction of the drone during centering. However, in this application, the first centering part 11 and the second centering part 12 both pass through the same plane parallel to the landing pad 2. During the centering operation, the first centering part 11 and the second centering part 12 limit the drone in two mutually perpendicular directions at the same height, eliminating potential errors in the length or width direction during centering, improving the accuracy of the centering operation, and reducing the risk of inaccurate centering affecting subsequent operations.

[0048] In some embodiments, the first plane may be in contact with the bearing plane 21 of the landing pad 2, or it may be spaced apart from the bearing plane 21. Those skilled in the art can adjust the height of the centering mechanism 1 according to the specific structure of the UAV.

[0049] In order to enable the first centering portion 11 and the second centering portion 12 to pass through the same plane (the first plane), in some embodiments of this application, such as Figure 1 As shown, the two centering units of the first centering section 11 are located between the two centering units of the second centering section 12, and the length of the centering unit of the first centering section 11 is less than the length of the centering unit of the second centering section 12.

[0050] In the parking platform provided in this application embodiment, the first centering part 11 is located between the two centering units of the second centering part 12. When both the first centering part 11 and the second centering part 12 move towards the center of the parking apron 2 and reach the extreme position, the two centering units of the first centering part 11 and the two centering units of the second centering part 12 respectively abut against each other and jointly form a rectangular limiting area, pushing the UAV to the limiting area to achieve fixing and positioning of the UAV. The center of the limiting area coincides with the center of the bearing plane 21, completing the centering operation.

[0051] It should be noted that the drone may include four columns perpendicular to the bearing plane 21, with a propeller at the end of the column away from the bearing plane 21. The drone may also include two supports for abutting against the bearing plane 21 to provide support for the drone.

[0052] After the drone lands on the landing pad 2, the second central section 12 contacts the four pillars, and the first central section 11 abuts against the two supports respectively, jointly applying a driving force to push the drone toward the center of the bearing surface 21.

[0053] In some embodiments, the landing platform may further include a magnetic attraction mechanism, which is installed on the surface of the landing pad 2 away from the bearing plane 21, and the center of the magnetic attraction mechanism is on the same straight line as the center of the bearing plane 21. When the drone lands on the landing pad 2 and is moved to the center of the bearing plane 21 by the centering mechanism 1, the magnetic attraction mechanism can be activated to attract the drone, thereby further securing the drone and preventing it from falling off due to bumps or vibrations during vehicle movement, thus enhancing the stability of the drone when parked.

[0054] In some embodiments, such as Figure 3 As shown, the centering unit in the first centering section 11 and / or the second centering section 12 can be an arc-shaped surface facing away from the UAV. The arc-shaped surface protrudes in a direction away from the center of the landing pad 2, which can reduce the wind resistance of the first centering section 11 and / or the second centering section 12 when the vehicle moves forward, and avoid the first centering section 11 and / or the second centering section 12 from being unstable due to the influence of air resistance, thereby improving the operability and safety of the centering mechanism 1.

[0055] In some embodiments, the helipad 2 is provided with two first slide rails and two second slide rails. The extension direction of the first slide rail is perpendicular to the extension direction of the second slide rail. A drive mechanism is provided at the bottom of the helipad 2. The drive mechanism passes through the first slide rail and the second slide rail and is connected to the first centering part 11 and the second centering part 12 respectively, so as to drive the first centering part 11 and the second centering part 12 to move along the slide rail.

[0056] Currently, conventional vehicle-mounted drones typically charge themselves using a wireless charging module installed in the drone's cabin. This charging method is relatively slow and has a low energy conversion rate.

[0057] Alternatively, a simple robotic arm can be installed in the drone's cabin to replace the drone's battery, achieving rapid full charging. While this method is more efficient than wireless charging modules, it requires an additional robotic arm inside the cabin, increasing the number of parts and the cost of the robotic arm. Furthermore, the accuracy of the robotic arm is difficult to meet requirements when the vehicle is in motion.

[0058] Therefore, in some embodiments of this application, such as Figure 2 and Figure 3 As shown, the centering mechanism 1 may further include a charging section 13, which is connected to at least one of the first centering section 11 and the second centering section 12, and at least a portion of the charging section 13 protrudes from the contact surface between the first centering section 11 and / or the second centering section 12 and the drone, for contacting the drone and charging the drone.

[0059] In the parking platform provided in this application embodiment, a charging unit 13 is provided on the centering mechanism 1. When the drone moves to the center of the parking apron 2, the charging unit 13 comes into contact with the drone and automatically charges the drone. Compared with wireless charging, the charging efficiency is higher, and there is no need to set up additional complex devices and parts to replace the drone's battery, realizing the drone can be charged at any time.

[0060] It should be noted that the location of the charging unit 13 corresponds to the charging location of the drone. Those skilled in the art can select and adjust the location of the charging unit 13 according to the specific structure of the drone.

[0061] Optionally, the charging unit 13 is a contact charging device, which can be connected to the vehicle's battery or other power supply device to charge the drone when it comes into contact with the drone.

[0062] In some embodiments of this application, such as Figure 5 As shown, the parking platform may also include a triggering mechanism 3, which is connected to the parking platform and to the centering mechanism 1 and the UAV signal respectively. The triggering mechanism 3 is configured to send a power-on or power-off signal to the UAV according to the operating status of the centering mechanism 1.

[0063] The triggering mechanism 3 is signal-connected to the centering mechanism 1 and the drone respectively. When the centering mechanism 1 pushes the drone to the center position of the bearing plane 21, the centering mechanism 1 stops moving. At this time, the triggering mechanism 3 sends a shutdown signal to the drone to realize the automatic shutdown of the drone. When the drone needs to take off, the centering mechanism 1 moves away from the drone. When the centering mechanism 1 moves to the limit position (the ends of the first and second slide rails mentioned above) and stops moving, the triggering mechanism 3 sends a power-on signal to the drone to realize the automatic power-on of the drone.

[0064] Furthermore, the drone, in conjunction with the centering mechanism, enables automatic power on / off, which not only makes it more convenient to use but also prevents the drone's battery from running out of power unexpectedly during long standby periods, thereby extending battery life.

[0065] In addition, some types of drones are equipped with a power button, which needs to be pressed to turn the drone on and off.

[0066] Therefore, in some embodiments, the landing platform may further include a pressing mechanism connected to the landing pad 2, which can extend or retract to perform a pressing action. When the drone needs to be turned on or off, the power button can be pressed or released by extending or retracting the pressing mechanism, thereby realizing the automatic power on / off of the drone.

[0067] This application also provides a vehicle-mounted drone cabin, which includes the aforementioned parking platform.

[0068] In some embodiments of this application, such as Figure 6 As shown, the vehicle-mounted drone cabin may also include a cabin body 4, a lifting mechanism 5, and a moving mechanism 6; the cabin body 4 has an internal cavity 41, and one side of the cavity 41 is open; the lifting mechanism 5 is located on the side of the parking platform away from the bearing plane 21 and is connected to the parking platform; the lifting mechanism 5 has an extended state and a retracted state, wherein in the extended state, the bearing plane 21 is flush with the top of the cabin body 4; the moving mechanism 6 is movably connected to the cavity 41 and connected to the lifting mechanism 5 to drive the parking platform to extend or retract from the open side.

[0069] In related technologies, the vehicle-mounted drone cabin, with the landing pad 2 extending out and located in the rear area of ​​the cabin, aims to reduce airflow disturbance to the drone during vehicle movement and improve the drone's stability during takeoff and landing. However, with this configuration, the drone's propeller may collide with the cabin during takeoff and landing, potentially causing damage to both the drone and the cabin.

[0070] In the vehicle-mounted drone cabin provided in this application embodiment, a lifting mechanism 5 is provided below the landing pad 2. Before the drone takes off or lands, the lifting mechanism 5 raises the landing pad 2 to a position level with the top of the cabin, and then the drone takes off or lands. The drone's propeller will not collide with the cabin, thus improving the safety of the drone during takeoff and landing.

[0071] In some embodiments, such as Figure 6 As shown, a closing part 51 can be provided on the side of the lifting mechanism 5 away from the cabin 4. The closing part 51 is connected to the lifting mechanism 5 and moves with the lifting mechanism 5 to close or open the cabin 4.

[0072] Optionally, the closed part 51 is a baffle.

[0073] Optionally, the lifting mechanism 5 is a scissor-type lifting platform.

[0074] In some embodiments, the moving mechanism 6 may include a slide rail and a sliding member. The slide rail is disposed on either the cabin 4 or the lifting mechanism 5, and the sliding member is disposed on the other. The sliding member slides in cooperation with the slide rail, and under the drive of an external driving device, the platform can be extended or retracted.

[0075] Optionally, the slider is a block.

[0076] As can be seen from the above embodiments, in order to avoid the drone from colliding with the cabin during take-off and landing, the lifting mechanism 5 will raise the landing pad 2 to a position level with the top of the cabin 4. At this time, if the vehicle is in motion, the airflow may interfere with the take-off and landing of the drone.

[0077] In some embodiments of this application, such as Figure 6 and Figure 7 As shown, the vehicle-mounted drone cabin may also include a spoiler 42, which is located on the side of the cabin 4 with an opening and connected to the top surface 44 of the cabin 4, and is used to divert the airflow flowing through the top surface 44.

[0078] The spoiler 42 extends in the same direction as the vehicle's movement and is located directly in front of the helipad 2 in the same direction as the vehicle's movement. When the drone is parked on the helipad 2, it is positioned behind the spoiler 42, which diverts the airflow, thereby reducing airflow interference with the drone.

[0079] Optionally, such as Figure 5 As shown, the spoiler 42 is a shark fin type spoiler.

[0080] Optionally, there may be multiple spoilers 42, which are spaced apart along the width of the cabin 4.

[0081] Those skilled in the art can select and adjust the number and size of the aerodynamic components 42 according to actual needs.

[0082] Furthermore, a guide surface is formed at the front end of the cabin 4. The guide surface is an arc-shaped surface extending from front to back. During the vehicle's movement, the guide surface is used to guide the airflow on the front side of the cabin 4 to the space above the cabin 4, reducing the wind resistance experienced by the cabin 4. It can also work with the spoiler 42 to further reduce the interference of airflow on the take-off and landing of the UAV.

[0083] In some embodiments of this application, such as Figure 6 As shown, the vehicle-mounted drone cabin may also include a camera unit 43, and the spoiler 42 has an installation opening 421. The opening direction of the installation opening 421 is towards the center of the landing pad 2, and at least a part of the camera unit 43 is located inside the installation opening 421.

[0084] In the vehicle-mounted drone cabin provided in this application embodiment, by setting up a camera unit 43, the real-time status of the drone can be monitored at any time and fed back to the display device in the vehicle, so that the user can keep track of the drone's status at any time. In addition, with the centering mechanism 1, it is easier to determine whether the drone has moved to the center of the bearing plane 21, avoiding centering errors.

[0085] In addition, by placing the camera unit 43 inside the mounting opening 421 of the spoiler 42, the space required for arranging the camera unit 43 is saved, and the camera unit 43 is protected from being exposed to the external environment and affected by factors such as airflow and rain and snow.

[0086] Optionally, the photography unit 43 includes multiple cameras capable of monitoring and providing feedback on multiple areas of the helipad 2. Those skilled in the art can select and adjust the number of cameras according to actual needs; for example, the number of cameras could be three.

[0087] Currently, vehicle-mounted drone cabins are typically located on the roof of vehicles, making takeoff and landing more convenient. However, these cabins are exposed to the elements, and direct sunlight or cold weather can directly affect the cabin's internal temperature, thus impacting the drones parked inside.

[0088] High temperatures can cause the internal electronic devices of a drone to overheat, affecting their performance and stability, while excessively low temperatures may cause electronic components to malfunction. Temperature also has a direct impact on the performance of the drone's internal battery. High temperatures accelerate the battery aging process, shorten battery life, and may even lead to overheating, combustion, or explosion of the battery, while low temperatures may reduce the battery's charge capacity and shorten flight time.

[0089] Therefore, in some embodiments of this application, such as Figure 5As shown, the vehicle-mounted drone cabin may also include a temperature control mechanism 7, which is connected to the cabin body 4 and is used to regulate the real-time temperature inside the containment cavity 41 to ensure that the temperature inside the cabin is kept within a predetermined temperature range and is not too high or too low, thereby affecting the performance of the drone and its battery life.

[0090] In some embodiments, the temperature control mechanism 7 may include a heating section 71 and a cooling section 72, which are mounted on the outer surface of the cabin 4 and are used to heat up when the cabin temperature is low and to cool down when the temperature is high.

[0091] In some embodiments, a temperature sensor is provided inside the cabin 4. The temperature sensor is connected to the controller inside the vehicle and feeds back the temperature inside the accommodating cavity 41 to the controller. The controller controls the heating unit 71 and the cooling unit 72 to work or shut down according to the temperature signal.

[0092] Optionally, the heating section 71 is a resistance heater, or the cooling section 72 is a cooling diode, or both of the above.

[0093] This application also provides a vehicle that includes the aforementioned vehicle-mounted unmanned aerial vehicle cabin.

[0094] In the vehicle provided in this application embodiment, by setting a first centering part 11 and a second centering part 12 on the helipad 2, the drone can be moved to the center area of ​​the helipad 2, thereby achieving the fixation and positioning of the drone. Furthermore, both the first centering part 11 and the second centering part 12 pass through the same plane parallel to the helipad 2. When performing the centering operation, the first centering part 11 and the second centering part 12 limit the drone in two mutually perpendicular directions at the same height, eliminating the possible errors in the length or width direction of the drone during centering, improving the accuracy of the centering operation, and reducing the risk of subsequent operations being affected by inaccurate centering.

[0095] In addition, the adoption of the aforementioned vehicle-mounted drone cabin eliminates the centering error before and after drone take-off and landing, making it more convenient to use drones in conjunction with vehicles and providing users with a better user experience.

[0096] In this application, the terms "first" and "second" are used for descriptive purposes only and should not be construed as indicating or implying relative importance. The term "multiple" refers to two or more unless otherwise expressly defined.

[0097] Other embodiments of this application will readily occur to those skilled in the art upon consideration of the specification and practice of the invention disclosed herein. This application is intended to cover any variations, uses, or adaptations of this application that follow the general principles of this application and include common knowledge or customary techniques in the art not disclosed herein. The specification and examples are to be considered exemplary only.

[0098] It should be understood that this application is not limited to the precise structure described above and shown in the accompanying drawings, and various modifications and changes can be made without departing from its scope. The scope of this application is limited only by the appended claims.

Claims

1. A vehicle-mounted unmanned aerial vehicle (UAV) cabin, comprising a parking platform, characterized in that, The parking platform includes a centering mechanism (1) and a parking apron (2); The centering mechanism (1) includes a first centering section (11) and a second centering section (12); The first centering part (11) and the second centering part (12) are installed on the bearing plane (21) of the landing pad (2) and are configured to push the UAV toward the center of the bearing plane (21) to fix and position the UAV. The bearing plane (21) is used to park the UAV. The first centering section (11) and the second centering section (12) each include two centering units arranged opposite to each other. The two centering units can move along the bearing plane (21) in a direction that is closer to or farther away from each other, and the moving direction of the first centering section (11) is perpendicular to the moving direction of the second centering section (12). The first centering portion (11) and the second centering portion (12) both pass through the first plane, which is parallel to the bearing plane (21). The vehicle-mounted drone cabin also includes a cabin body (4), a lifting mechanism (5), and a moving mechanism (6); The interior of the cabin (4) has a receiving cavity (41), and one side of the receiving cavity (41) is open; The lifting mechanism (5) is located on the side of the parking platform away from the bearing plane (21) and is connected to the parking platform; The lifting mechanism (5) has an extended state and a retracted state, wherein in the extended state, the bearing plane (21) is flush with the top of the cabin (4); The moving mechanism (6) is movably connected to the receiving cavity (41) and connected to the lifting mechanism (5) to drive the stopping platform to extend or retract from the opening; The vehicle-mounted drone cabin also includes a spoiler (42), which is located on the side of the cabin (4) where the opening is provided and is connected to the top surface (44) of the cabin (4) for diverting the airflow flowing through the top surface (44), wherein the extension direction of the spoiler (42) is the same as the direction of vehicle movement.

2. The vehicle-mounted unmanned aerial vehicle cabin according to claim 1, characterized in that, The two centering units of the first centering section (11) are located between the two centering units of the second centering section (12), and the length of the centering unit of the first centering section (11) is less than the length of the centering unit of the second centering section (12).

3. The vehicle-mounted unmanned aerial vehicle cabin according to claim 1, characterized in that, The centering mechanism (1) further includes a charging unit (13), which is connected to at least one of the first centering unit (11) and the second centering unit (12), and at least a portion of the charging unit (13) protrudes from the contact surface between the first centering unit (11) and / or the second centering unit (12) and the drone, for contacting the drone and charging the drone.

4. The vehicle-mounted unmanned aerial vehicle cabin according to claim 1, characterized in that, The shutdown platform also includes a triggering mechanism (3), which is connected to the shutdown platform and connected to the centering mechanism (1) and the UAV signal respectively. The triggering mechanism (3) is configured to send a power-on or power-off signal to the UAV according to the operating status of the centering mechanism (1).

5. The vehicle-mounted unmanned aerial vehicle cabin according to claim 1, characterized in that, The vehicle-mounted drone cabin also includes a camera unit (43), and the spoiler (42) has an installation opening (421) with the opening direction of the installation opening (421) facing the center of the bearing plane (21). At least a portion of the camera unit (43) is located inside the installation opening (421).

6. The vehicle-mounted unmanned aerial vehicle cabin according to any one of claims 1 to 5, characterized in that, The vehicle-mounted drone cabin also includes a temperature control mechanism (7), which is connected to the cabin body (4) and is used to regulate the real-time temperature inside the containment cavity (41).

7. A vehicle, characterized in that, The vehicle includes the vehicle-mounted unmanned aerial vehicle cabin as described in any one of claims 1 to 6.

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