Unmanned aerial vehicle (UAV) take-off and landing equipment, UAV take-off and landing systems and vehicles

Abstract

This application relates to a drone take-off and landing device, a drone take-off and landing system, and a vehicle. The drone take-off and landing device includes a platform base plate, a top cover plate, and a connecting assembly. A parking space is formed on one side of the platform base plate, and the top cover plate is used to cover or open the parking space. The connecting assembly is connected to the top cover plate and has an extended state and a retracted state. When the connecting assembly is in the retracted state, the top cover plate covers the parking space. When the connecting assembly is in the extended state, the top cover plate opens the parking space. In this way, the connecting assembly can drive the top cover plate to open the parking space, allowing the drone take-off and landing system to allow the drone to take off and land without moving the drone, avoiding damage to the drone during transportation and improving the reliability of the drone take-off and landing device.

Description

Technical Field

[0001] This application relates to the field of vehicle-mounted drone take-off and landing technology, and in particular to a drone take-off and landing device, a drone take-off and landing system, and a vehicle. Background Technology

[0002] A vehicle-mounted drone is a drone device that can be used in conjunction with a vehicle. It can be easily placed in a vehicle and used at any time. For example, it can quickly take off to provide real-time information to the driver when aerial reconnaissance or photography is required. While driving, the drone can be used to preview road conditions ahead, greatly improving driving safety and traffic flow in congested or complex terrain areas. When traveling in the wild, vehicle-mounted drones can also be used to survey the surrounding environment and find routes. In emergencies, vehicle-mounted drones can take off quickly to assist in rescue operations, such as searching for missing persons.

[0003] In related technologies, a container is used to store vehicle-mounted drones, with a parking space inside. An exit is located on the side of the container. When a drone needs to take off, it must first be transported out of the container through this exit before taking off; when a drone needs to land, it must land on the side of the container before being transported back in. However, when the vehicle moves, the drone is easily detached from the transport device during transport and may fall or collide with the container, resulting in damage. This makes the existing drone take-off and landing devices unreliable. Summary of the Invention

[0004] This application provides a drone take-off and landing device to at least partially solve the above-mentioned technical problems.

[0005] To achieve the above objectives, according to a first aspect of this application, a drone take-off and landing device is provided, comprising:

[0006] The platform base has a parking space on one side;

[0007] Top cover plate, used to cover or open the parking space; and

[0008] A connecting component is connected to the upper cover plate, and the connecting component has an extended state and a retracted state.

[0009] When the connecting component is in the retracted state, the upper cover can cover the stopping space; when the connecting component is in the extended state, the upper cover can open the stopping space.

[0010] Optionally,

[0011] The platform base plate can move along a first direction, and along the first direction, the platform base plate includes a first end and a second end that are disposed opposite to each other;

[0012] The upper cover plate includes a third end and a fourth end that are disposed opposite to each other. In the retracted state, the third end is disposed close to the first end and the fourth end is disposed close to the second end.

[0013] When switching from the retracted state to the extended state, the third end moves toward the direction closer to the second end.

[0014] Optionally, the UAV take-off and landing device further includes a drive motor and a power distribution device. The drive motor is driven to the power distribution device, and the power distribution device is driven to the platform base plate and the connecting assembly, respectively. The drive motor is used to drive the platform base plate to move along a first direction and drive the connecting assembly to switch between an extended state and a retracted state through the power distribution device.

[0015] Optionally, the power distribution device includes a drive gear, a rack, and a driven gear shaft. The drive gear is driven to the output shaft of the drive motor. The rack is fixedly connected to the platform base plate and extends along the first direction. The rack meshes with the drive gear and the driven gear shaft respectively. The driven gear shaft is driven to the connecting assembly to drive the upper cover plate.

[0016] Optionally, the connecting assembly includes a drive crank, a first connecting rod, a second connecting rod, a connecting rod base, and a connecting rod upper seat, the connecting rod upper seat being fixedly connected to the upper cover plate; the driven gear shaft being drivenly connected to the drive crank; one end of the first connecting rod being hinged to the drive crank, and the other end of the first connecting rod being hinged to the middle of the second connecting rod; one end of the second connecting rod being hinged to the connecting rod base, and the other end of the second connecting rod being connected to the connecting rod upper seat; the drive crank drives the second connecting rod to rotate via the first connecting rod, thereby switching the connecting assembly between an extended state and a retracted state.

[0017] Optionally, the connecting assembly further includes a third link, a fourth link, a fifth link, and a pin; one end of the third link is hinged to the end of the second link away from the link base, and the other end of the third link is hinged to the link upper seat; one end of the fourth link is hinged to the link upper seat, and the other end of the fourth link is hinged to one end of the fifth link; the end of the fifth link away from the fourth link is hinged to the link base; the pin is fixed in the middle of the second link; the fourth link has a waist-shaped hole in the middle, and the pin passes through the waist-shaped hole, allowing the fourth link to rotate around the pin and slide along the length of the waist-shaped hole; the fourth link and the third link are arranged in parallel, and the second link and the fifth link are arranged in parallel; the link base, the second link, the third link, the fourth link, the fifth link, the link upper seat, and the pin cooperate so that when the second link stops rotating around the link base, the upper cover plate stops rotating around the third link.

[0018] Optionally, the connecting assembly further includes a buffer pad disposed on the drive crank; when the connecting assembly is in the extended state, the buffer pad abuts against the connecting rod base to impede rotation of the drive crank; and / or

[0019] When the connecting assembly is in the retracted state, the buffer pad abuts against the connecting rod base to prevent the drive crank from rotating; and / or

[0020] A first limiting block is provided on the base of the connecting rod. When the connecting assembly is in the extended state, the first limiting block abuts against the fifth connecting rod; and / or

[0021] The upper seat of the connecting rod is provided with a second limiting block. When the connecting assembly is in the extended state, the second limiting block abuts against the fourth connecting rod.

[0022] Optionally, two sets of the connecting components are provided, with the two sets of connecting components respectively located on both sides of the platform base plate, and arranged in a direction perpendicular to the first direction.

[0023] Optionally, the UAV take-off and landing device further includes a guide mechanism, which includes a slider and a slide rail that are slidably connected. The slide rail extends along the length of the rack, and one of the slider and the slide rail is fixedly connected to the platform base plate.

[0024] Optionally, two sets of the guiding mechanism are provided, with the two sets of guiding mechanisms spaced apart and arranged in a direction perpendicular to the first direction.

[0025] According to a second aspect of this application, a drone take-off and landing system is also provided, including the aforementioned drone take-off and landing device and the drone.

[0026] Optionally, the drone take-off and landing system is applied to a vehicle, the vehicle including a rear windshield and a shelf arranged opposite each other, the drone take-off and landing device being disposed between the rear windshield and the shelf; the rear windshield is provided with a take-off and landing opening, the take-off and landing opening communicating with the parking space; the platform base plate is used to park the drone, when the connecting component is in the extended state, the upper cover plate is away from the take-off and landing opening to open the take-off and landing opening; when the connecting component is in the retracted state, the upper cover plate covers the take-off and landing opening.

[0027] Optionally,

[0028] When the upper cover plate covers the landing port, the projection of the UAV landing system is within the projection of the vehicle along the x-axis and / or y-axis and / or z-axis; and / or

[0029] When the upper cover opens the landing port, the projection of the UAV landing system is within the projection of the vehicle along the x-axis and / or z-axis.

[0030] Optionally, a charging port is provided on the platform base plate, and a charging plug is provided on the drone. When the drone is parked on the platform base plate, the charging plug can be plugged into the charging port.

[0031] Optionally, the charging port is a magnetic charging interface, the charging plug is a support frame, the support frame is provided with magnetic charging contacts, and the magnetic charging interface and the magnetic charging contacts can be attracted to each other.

[0032] Optionally, the platform base plate is provided with alignment marks, and the drone is provided with a downward-looking camera, which is used to identify the alignment marks.

[0033] Optionally, the drone take-off and landing device further includes a enclosure; when the connecting component is in the retracted state, the rear windshield, the enclosure, and the upper cover enclose the parking space.

[0034] Optionally, at least a portion of the side of the enclosure panel abuts against the side of the rear windshield; the portion of the side of the enclosure panel that abuts against the rear windshield is provided with a sealing structure and / or a water guide groove; and / or

[0035] When the connecting assembly is in the retracted state, the upper cover plate and the rear windshield are used to form a side connection of the landing port, and a sealing structure and / or a water guide groove are provided at the connection position of the upper cover plate and the rear windshield.

[0036] Optionally, a cooling fan is provided on the enclosure.

[0037] Optionally, the UAV take-off and landing device further includes a temperature sensor for acquiring temperature information within the landing space.

[0038] According to a third aspect of this application, a vehicle is also provided, including a rear windshield, a shelf, and a drone disposed opposite to each other, as well as a drone take-off and landing device or a drone take-off and landing system as described above.

[0039] Optionally, the vehicle also includes a streaming rearview mirror for acquiring images during the takeoff or landing of the drone.

[0040] In the drone take-off and landing device of this application embodiment, the drone can be placed on the platform base plate and then stored in the parking space. When the connecting components are in the extended state, the upper cover opens the parking space, allowing the drone to take off directly from the parking space without needing to be transported. When the drone needs to land, the connecting components can also be extended, allowing the drone to land directly in the parking space without needing to land on one side and be transported into the parking space. In summary, the drone take-off and landing device of this application embodiment allows the drone to take off or land without needing to be transported into or out of the parking space, thus avoiding damage to the drone during transportation and improving the reliability of the drone take-off and landing device.

[0041] Other features and advantages of this application will be described in detail in the following detailed description section. Attached Figure Description

[0042] 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 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.

[0043] To gain a more complete understanding of this application and its beneficial effects, the following description will be provided in conjunction with the accompanying drawings, wherein the same reference numerals in the following description denote the same parts.

[0044] Figure 1 This is a schematic diagram of the overall structure of the vehicle provided in an exemplary embodiment of this disclosure;

[0045] Figure 2 This is a schematic diagram of the structure of the unmanned aerial vehicle take-off and landing system provided in the exemplary embodiment of this disclosure when the connecting components are in the extended state;

[0046] Figure 3This is a schematic diagram of the structure of the enclosure, platform base plate, cooling fan and slide rail of the unmanned aerial vehicle take-off and landing device provided in an exemplary embodiment of this disclosure;

[0047] Figure 4 This is a first-view structural schematic diagram of the power distribution device of the unmanned aerial vehicle take-off and landing device provided in an exemplary embodiment of this disclosure;

[0048] Figure 5 This is a second-view structural schematic diagram of the power distribution device of the unmanned aerial vehicle take-off and landing device provided in an exemplary embodiment of this disclosure;

[0049] Figure 6 This is a schematic diagram of the structure of the connection component of the unmanned aerial vehicle take-off and landing device provided in an exemplary embodiment of this disclosure;

[0050] Figure 7 This is a schematic diagram of the structure of the drone take-off and landing system provided in an exemplary embodiment of this disclosure when the drone lands.

[0051] Explanation of reference numerals in the attached figures:

[0052] 100. Drones; 200. Helipad space; 300. Rear windshield; 400. Tailgate;

[0053] 210, Top cover; 210a, Third end; 210b, Fourth end; 220, Front panel; 230, Left panel; 240, Right panel; 250, Base plate; 260, Heatsink; 270, Cooling fan;

[0054] 510. Drive motor; 520. Drive gear; 530. Rack; 540. Driven gear shaft; 550. Connecting assembly; 560. Slider; 570. Slide rail; 580. Platform base plate; 580a. First end; 580b. Second end;

[0055] 5501, Drive crank; 5502, First connecting rod; 5503, Second connecting rod; 5504, Third connecting rod; 5505, Connecting rod upper seat; 5506, Fourth connecting rod; 5507, Fifth connecting rod; 5508, First limiting block; 5509, Buffer pad; 5510, Connecting rod base; 5511, Second limiting block; 5512, Pin;

[0056] 110. Downward-facing camera; 120. Support bracket; 130. Magnetic charging contacts; 5801. Magnetic charging interface; 5802. QR code;

[0057] 600, Central control panel; 700, Streaming media rearview mirror; 800, Central integrated controller; 900, Vehicle-mounted drone controller. Detailed Implementation

[0058] 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 a part of the embodiments of this application, and not all of them. All other embodiments obtained by those skilled in the art based on the embodiments of this application without creative effort are within the protection scope of this application.

[0059] To achieve the above objectives, according to the first aspect of this application, a drone take-off and landing device is provided, with reference to... Figure 1 The drone take-off and landing device can be installed between the vehicle's storage rack and the rear windshield 300. Of course, in some other embodiments, the drone take-off and landing device can also be installed in the vehicle's trunk, passenger compartment, or roof, etc.

[0060] According to a first aspect of this application, a drone take-off and landing device is provided, with reference to... Figure 5 It includes a platform base plate 580, a top cover plate 210, and a connecting assembly 550. A parking space 200 is formed on one side of the platform base plate 580, and the drone 100 is positioned within this parking space 200 when it is placed on the platform base plate 580. Figure 5 In the shown configuration, the connecting component 550 is in the extended state, and the upper cover 210 opens the parking space 200, allowing the drone to take off directly from the parking space 200. (Refer to reference...) Figure 2 and Figure 1 ,visible Figure 2 The connecting component 550 is also in an extended position, the parking space 200 is open, and the drone can take off directly. Figure 1 In the state shown, the connecting component 550 is in the retracted state. Figure 1 In the illustrated embodiment, the upper cover 210 and the rear windshield are aligned on the same plane, thus covering the parking space 200 and safely parking the drone on the platform base 580. In summary, whether taking off or landing, the drone only needs the connecting component 550 extended to open the parking space 200 with the upper cover 210 open. The drone can then fly into the parking space 200 to park on the platform base 580, or take off from the platform base 580 and fly out of the parking space 200. Therefore, no additional transport mechanism is needed. When taking off, the drone is first transported out of the parking space 200 using a transport mechanism before taking off; similarly, when landing, it does not need to land next to the parking space 200 before being transported into it using a transport mechanism. This avoids damage to the drone during transport and improves the reliability of the drone takeoff and landing device.

[0061] The connecting component 550 is connected to the upper cover 210, allowing the upper cover 210 to move as the connecting component 550 switches between an extended and retracted state. The connecting component 550 can be, as in the embodiments described below, a power input that allows it to move under power. Alternatively, it can be a simple guide mechanism, whereby a user pushes the upper cover 210, which moves under the guidance of the connecting component 550 to open or close the stopping space 200. For example, the guide mechanism can be two relatively sliding guide rails, one fixedly connected to the upper cover 210 and the other fixedly connected to the left plate 230 or right plate 240, allowing the upper cover 210 to move under the guidance of the guide rails.

[0062] refer to Figure 2 and Figure 7 In some embodiments, the platform base plate 580 can move along a first direction, which is equivalent to the parking space 200 also moving along the first direction. (See reference...) Figure 7 The platform base plate 580 includes a first end 580a and a second end 580b disposed opposite to each other, and the upper cover plate 210 includes a third end 210a and a fourth end 210b disposed opposite to each other. When the connecting assembly 550 is in the retracted state, the third end 210a is positioned closer to the first end 580a, and the fourth end 210b is positioned closer to the second end 580b. When the connecting assembly 550 switches from the retracted state to the extended state, the third end 210a moves toward the direction closer to the second end 580b. Figure 7 In the illustrated embodiment, the third end 210a is close to the second end 580b. This allows the upper cover 210 to open the parking space 200 when the connecting assembly 550 is in the extended state after the platform base plate 580 moves along the first direction, enabling the drone to fly out of or land in the parking space 200. However, due to the movement of the platform base plate 580, the parking space 200 is moved away from the main body of the vehicle on which the drone take-off and landing device is installed, for example... Figure 7 As can be seen, the parking space 200 is moved away from the vehicle body due to the platform base plate 580 moving in the first direction. If the UAV take-off and landing device is installed on a ship, the movement of the platform base plate 580 in the first direction can move the parking space 200 away from the hull. Furthermore, since the UAV takes off or lands from the parking space 200, the movement of the platform base plate 580 in the first direction allows the UAV to stay as far away from the main body of the vehicle as possible during take-off and landing, avoiding collisions and damage, and further improving the reliability of the UAV take-off and landing system.

[0063] refer to Figure 4 and Figure 5In some embodiments, the drone take-off and landing device further includes a drive motor 510 and a power distribution device. When the drone take-off and landing device is mounted on a vehicle, the drive motor 510 is fixed in relative position to the vehicle. For example, the drive motor 510 can be directly fixedly connected to a shelf or fixedly connected to a base plate 250, wherein the base plate 250 is fixed to the vehicle by being fixedly connected to the left plate 230, right plate 240, and front plate 220 (the left plate 230, right plate 240, and front plate 220 can be fixedly connected to the rear windshield 300 and / or directly fixedly connected to the shelf to be fixedly connected to the vehicle). The drive motor 510 is driven by the power distribution device, so that the drive motor 510 can input the rotational torque power of the output shaft into the power distribution device. The power distribution device is also driven by the platform base plate 580 and the connecting assembly 550, respectively. This allows the drive motor 510 to drive the platform base plate 580 to move in a first direction and to switch the connecting assembly 550 between extended and retracted states. This is equivalent to driving the upper cover plate 210 to move between the open stopping space 200 and the covered stopping space 200. The power distribution device can be a gearbox with one input end and two output shafts. The input end receives power from the drive motor 510, and each of the two output ends is connected to a rubber wheel. The first rubber wheel abuts against the platform base plate 580, driving the platform base plate 580 to move by rolling. The other rubber wheel abuts against the upper cover plate 210, driving the upper cover plate 210 to move by rotating (in this embodiment, the upper cover plate 210 can be slidably connected to the left or right plate via a guide rail). In these embodiments, the upper cover plate 210 and the platform base plate 580 move simultaneously, i.e., the linkage between the upper cover plate 210 and the platform base plate 580 is realized through the power distribution device. This shortens the switching time between the open state (the state where the parking space 200 is open) and the closed state (the state where the parking space 200 is covered) of the UAV take-off and landing device, and improves the efficiency of UAV 100 take-off and landing. In addition, it also makes it less likely for the platform base plate 580 and the upper cover plate 210 to interfere with each other, because the power distribution device can also ensure that they do not interfere with each other mechanically (for example, by changing the gearbox parameters and changing the rotation speed of the two rubber wheels to maintain their rotation speed at a preset value so that the upper cover plate 210 and the platform base plate 580 always maintain a suitable motion phase), without the need to set up a control system to monitor the motion phase of the platform base plate 580 and the upper cover plate 210 to avoid their motion interference. The use of control systems often requires the use of sensors, such as photoelectric encoders or displacement switches, to determine the motion phase of the upper cover plate 210 and the platform base plate 580 in order to avoid them interfering with each other. Therefore, the use of mechanical structures also reduces the complexity of the system and improves the reliability of the system operation.Of course, in some embodiments, a dual-motor approach can also be adopted, with two motors driving the upper cover plate 210 and the platform base plate 580 respectively. This can provide greater driving force and is suitable for larger vehicles or drone 100 take-off and landing systems.

[0064] refer to Figure 4 and Figure 5 In some embodiments, the power distribution device includes a drive gear 520, a rack 530, and a driven gear shaft 540. The drive gear 520 is drivenly connected to the output shaft of a drive motor 510, so that the drive motor 510 can drive the drive gear 520 to rotate. The rack 530 is fixedly connected to the platform base plate 580 and extends in a first direction. The rack 530 also meshes with both the drive gear 520 and the driven gear shaft 540, so that when the drive gear 520 rotates, the drive rack 530 moves in the first direction, thereby driving the platform base plate 580 to move in the first direction. Figure 7 In the illustrated embodiment, by setting a suitable rotation direction of the drive motor 510, the platform chassis can be controlled to move towards the rear of the vehicle (i.e., into the open state) or away from the rear of the vehicle (i.e., into the closed state). Since the rack 530 meshes with the driven gear shaft 540, the driven gear shaft 540 rotates when the rack 530 moves. The driven gear shaft 540 is driven by the connecting assembly 550, allowing the power output from the driven gear shaft 540 to switch between extended and retracted states via the drive connecting assembly 550, thereby driving the upper cover plate 210 to move and achieving linkage between the upper cover plate 210 and the platform base plate 580. A rubber wheel can also be provided on the output shaft of the driven gear shaft 540 for sliding of the upper cover plate 210 in embodiments where it is slidably connected to the left or right plate. In these embodiments, the gear ratio between the drive gear 520 and the driven gear shaft 540 can be adjusted to ensure that the upper cover plate 210 and the platform base plate 580 do not interfere with each other.

[0065] refer to Figure 6In some embodiments, the power distribution device further includes a connecting assembly 550, which includes a drive crank 5501, a first connecting rod 5502, a second connecting rod 5503, a connecting rod base 5510, and a connecting rod upper seat 5505. The connecting rod base 5510 is fixed in relative position to the vehicle, for example, it can be directly fixed to a shelf, or fixedly connected to a structure such as the left plate 230, right plate 240, or bottom plate 250. The connecting rod upper seat 5505 is fixedly connected to the upper cover plate 210. The driven gear shaft 540 is drivenly connected to the drive crank 5501, so that rotation of the driven gear shaft 540 can drive rotation of the drive crank 5501. One end of the first connecting rod 5502 is hinged to the drive crank 5501, and the other end is hinged to the middle of the second connecting rod 5503. One end of the second connecting rod 5503 is hinged to the connecting rod base 5510. This effectively forms a speed adjustment mechanism, which adjusts the speed of the drive crank 5501 and the speed of the second connecting rod 5503. When the speed of the drive crank 5501 is higher than the speed of the second connecting rod 5503, it is equivalent to amplifying the torque on the drive crank 5501 and increasing the driving force. When the speed of the drive crank 5501 is lower than the speed of the second connecting rod 5503, it is equivalent to increasing the speed of the second connecting rod 5503, thus accelerating the movement speed of the upper cover plate 210. In general, it is equivalent to further adjusting the speed of the second connecting rod 5503, ensuring that the movement phase of the upper cover plate 210 does not interfere with the movement of the platform base plate 580. The other end of the second link 5503 is connected to the upper link seat 5505. This connection can be a direct hinge, or it can be an indirect connection to the upper link seat 5505 via a hinge to the third link 5504, as described in the embodiments below. In any case, the second link 5503 needs to allow the upper cover plate 210 to open or close the stopping space 200 when rotating, which is equivalent to switching the connecting assembly 550 between an extended and retracted state. In summary, in these embodiments, the connecting assembly 550 provides further speed adjustment to avoid interference between the upper cover plate 210 and the platform base plate 580. Furthermore, the lever structure is simple, reliable, and low-cost.

[0066] refer to Figure 6 and Figure 7In some embodiments, the connecting assembly 550 further includes a third link 5504, a fourth link 5506, a fifth link 5507, and a pin 5512; one end of the third link 5504 is hinged to the end of the second link 5503 away from the link base 5510, and the other end of the third link 5504 is hinged to the upper link seat 5505; one end of the fourth link 5506 is hinged to the upper link seat 5505, and the other end of the fourth link 5506 is hinged to one end of the fifth link 5507; the end of the fifth link 5507 away from the fourth link 5506 is hinged to the link base 5510; the pin 5512 is fixed to the middle of the second link 5503; and the fourth link 5506 has a waist-shaped opening in the middle. A hole is formed in the bore, through which the pin 5512 passes, allowing the fourth link 5506 to rotate around the pin 5512 and slide along the length of the bore. The fourth link 5506 is arranged parallel to the third link 5504, and the second link 5503 and the fifth link 5507 are arranged parallel to each other. The link base 5510, the second link 5503, the third link 5504, the fourth link 5506, the fifth link 5507, the link upper seat 5505, and the pin 5512 cooperate to form a limiting position. Thus, when the second link 5503 stops rotating at any position, the upper cover 210 will not rotate either; that is, when the second link stops rotating around the link base, the upper cover 210 also stops rotating around the third link. Generally, if... Figure 7 As shown, the upper cover plate 210 has a tendency to rotate under the action of gravity and the force of the connecting rod upper seat 5505, that is, as Figure 7 In the case of the upper cover 210, there is a tendency for it to rotate clockwise around the connecting rod upper seat 5505, but this can easily cause the upper cover 210 to come into direct contact with the vehicle, which may require contact with the vehicle body (e.g., on the vehicle body). Figure 7 The rear tailgate 400 shown is provided with a scratch-resistant surface to prevent the cover plate 210 from scratching the vehicle's body panels. Alternatively, when the drone landing gear is mounted on other vehicles, if the cover plate 210 rotates freely, a scratch-resistant surface also needs to be provided on the vehicle's body panels to prevent scratches. However, due to the coordination of the connecting rod base 5510, the second connecting rod 5503, the third connecting rod 5504, the fourth connecting rod 5506, the fifth connecting rod 5507, the connecting rod upper seat 5505, and the pin 5512 to form a limiting position, the cover plate 210 can maintain a definite position at every moment during rotation under the drive of the connecting assembly 550, and will not rotate arbitrarily around the pin 5512 on the connecting rod upper seat 5505 under the action of gravity. This allows the cover plate 210 to avoid rubbing against the vehicle's body panels during movement through the setting of geometric parameters. It also reduces the resistance during the movement of the cover plate 210 and reduces the driving force required for the cover plate 210.

[0067] refer to Figure 6In some embodiments, the connecting assembly 550 further includes a buffer pad 5509 disposed on the drive crank 5501. When the connecting assembly 550 is in the deployed state, the buffer pad 5509 abuts against the connecting rod base 5510 to prevent the drive crank 5501 from rotating. It is understood that when the UAV landing device moves from the closed state to the open state, the upper cover 210 and the connecting rod possess kinetic energy during the movement. However, the open state is a stationary state, therefore the kinetic energy of the upper cover 210 and the connecting rod needs to be dissipated quickly, which can cause impact. Therefore, the flexible buffer pad 5509 is used to dissipate such impact, preventing damage to the connecting assembly 550.

[0068] refer to Figure 6 In some embodiments, when the connecting assembly 550 is in the retracted state, the buffer pad 5509 abuts against the connecting rod base 5510 to prevent the drive crank 5501 from rotating. Similarly, when the upper cover 210 and the connecting assembly 550 move from the moving state to the stationary closed state, kinetic energy needs to be dissipated. Therefore, the buffer pad 5509 can also mitigate impact and protect the connecting assembly 550 in these embodiments.

[0069] refer to Figure 6 In some embodiments, a first limiting block 5508 is provided on the connecting rod base 5510. When the connecting assembly 550 is in the extended state, the first limiting block 5508 abuts against the fifth connecting rod 5507, thus preventing the fifth connecting rod 5507 from rotating. If the connecting assembly 550 is in the extended state and the connecting rod can still rotate freely, the motor needs to have a self-locking capability to stop the movement of the connecting rod. However, such motors are often expensive. Therefore, providing the first limiting block 5508 can reduce manufacturing costs and also improve the stability of the upper cover plate 210 position when it is open, preventing it from hitting the vehicle body.

[0070] refer to Figure 6 In some embodiments, a second limiting block 5511 is provided on the connecting rod upper seat 5505. When the connecting assembly 550 is in the extended state, the second limiting block 5511 abuts against the fourth connecting rod 5506 to prevent the fourth connecting rod 5506 from rotating. Like the first limiting block 5508, the second limiting block 5511 can also improve the stability of the upper cover plate 210 in the open state. However, compared with the first limiting block 5508, the second limiting block 5511 is provided on the connecting rod upper seat 5505, thus having a better effect of preventing the upper cover plate 210 from rotating around the axis on the connecting rod upper seat 5505.

[0071] refer to Figure 4In some embodiments, two sets of connecting components 550 are provided, with the two sets of connecting components 550 respectively located on both sides of the platform base plate 580 and arranged perpendicular to the first direction. This can improve the load-bearing capacity of the connecting components 550, and the driven gear shaft 540 can also be provided with two output ends to drive the drive cranks 5501 of the two sets of connecting components 550 respectively, without the need to provide more motors.

[0072] refer to Figure 4 In some embodiments, the UAV take-off and landing device further includes a guiding mechanism, which includes a slider 560 and a slide rail 570. One of the slider 560 and the slide rail 570 is fixedly connected to the platform base plate 580, which is equivalent to the platform base plate being slidably connected to the other of the slider and the slide rail. The other of the slider 560 and the slide rail 570 can be fixedly connected to a vehicle, for example... Figure 2 In the illustrated embodiment, the position of the slide rail 570 can be fixed to the shelf, for example, it can be fixed to the base plate 250 or directly to the shelf, or even fixed to the left plate 230 or the right plate 240. The slide rail 570 is slidably connected to the slider 560, and the slide rail 570 extends along the length direction of the rack 530. In this way, the slider 560 and the slide rail 570 cooperate to make the platform base plate 580 run more stably in the first direction.

[0073] refer to Figure 4 In some embodiments, two sets of guiding mechanisms are provided, spaced apart and arranged perpendicular to the first direction. These two guiding mechanisms guide the movement of the platform base plate, further improving the stability of the platform base plate's movement.

[0074] refer to Figure 7 According to a second aspect of this application, a drone take-off and landing system is also provided, including a drone and the aforementioned drone take-off and landing device, and thus has all the technical effects of the aforementioned drone take-off and landing device, which will not be repeated here.

[0075] refer to Figure 7 In some embodiments, the drone takeoff and landing system is applied to a vehicle, which includes a rear windshield 300 and a shelf positioned opposite each other. The rear windshield 300 also serves as the observation window for the rearview mirror inside the vehicle, allowing the driver to observe the situation behind the vehicle through the rear windshield 300. And for... Figure 1In the illustrated embodiment, for a sedan, the shelf can refer to the partition between the trunk and the passenger compartment. For a hatchback, it can be an added trunk partition, essentially a platform for installing a drone landing gear. The rear windshield 300 and the shelf are positioned opposite each other, but this does not mean that the rear windshield 300 and the shelf cannot contact each other; rather, it means that they are at least partially spaced apart. This spaced-out portion can form an installation space for installing the drone landing gear and parking the drone 100.

[0076] The drone take-off and landing equipment is at least partially located in the installation space, for example in... Figure 3 In the illustrated embodiment, combined with Figure 2 It can be seen that the left plate 230, right plate 240, front plate 220, cooling fan 270, and other structures are all located within the installation space, while the upper cover plate 210 is exposed outside the installation space. The platform base plate 580 and connecting assembly 550 extend out of the installation space when the UAV take-off and landing device is in the open state; however, when the UAV take-off and landing device is in the open state... Figure 3 When shown in the closed state, both are within the installation space.

[0077] A landing hatch is provided on the rear windshield, which connects to the parking space 200, allowing the drone to take off or land. When the connecting assembly 550 is extended, the upper cover 210 moves away from the landing hatch to open it, allowing the drone 100 to fly into or out of the parking space 200. When the connecting assembly 550 is retracted, the upper cover 210 covers the landing hatch to close the rear windshield 300. This provides a more enclosed parking environment for the drone 100 in rainy or dusty conditions, preventing damage from rain or excessive wear on moving parts from dust. When the drone's takeoff and landing device is in the extended position... Figure 2 When it is in the open state as shown.

[0078] exist Figure 2In the illustrated embodiment, the platform base plate 580 moves in the first direction, i.e., towards the vehicle's x-axis, allowing the drone 100 to move towards the rear of the vehicle to create installation space. In these embodiments, the landing opening can be appropriately smaller to meet the vertical take-off and landing requirements of the drone 100. Although the drone 100 can turn arbitrarily in the air and has a very high degree of freedom of movement, its control is complex due to the unknown surrounding environment during take-off or landing, making it prone to collisions with obstacles. Therefore, vertical and rapid take-off and landing can improve the success rate of the drone 100's take-off and landing. The vehicle's rear windshield 300 is often also angled. If the drone 100 needs to take off and land vertically with the landing opening open, the projection of the landing opening along the vehicle's z-axis must completely surround the drone 100, which often requires a large landing opening. However, the rear windshield 300 is also often an important safety device for the vehicle, usually made of laminated glass, and needs to be protected from breakage in a vehicle collision to avoid injuring the driver and passengers. Therefore, it is often not advisable to set a large opening, as this would result in excessive reduction of strength. Since the platform base plate 580 can transport the drone 100 out of the installation space, the size of the landing opening only needs to be large enough for the drone 100 to enter and exit the installation space along the vehicle's x-axis. This significantly reduces the required size of the landing opening and ensures the strength of the rear windshield 300. For some vehicle models where the rear windshield 300 is closer to the ground, such as SUVs, it is almost impossible to completely surround the drone 100 with the projection of the landing opening along the vehicle's z-axis. The design of the platform base plate 580 also facilitates the application of this invention to such vehicles.

[0079] When the top cover 210 covers the landing port, the projection of the UAV landing system is within the vehicle's projection along the vehicle's x-axis. This ensures that installing the UAV landing system on the vehicle does not increase the vehicle's overall height or width, preventing the vehicle from more easily encountering obstacles outside the vehicle and improving the flexibility of the UAV landing system's installation.

[0080] When the top cover 210 covers the landing port, the projection of the UAV landing system is within the vehicle's projection along the vehicle's y-axis. This ensures that installing the UAV landing system on the vehicle does not increase the vehicle's overall height or length, preventing the vehicle from more easily encountering obstacles outside the vehicle and improving the flexibility of the UAV landing system's installation.

[0081] When the top cover 210 covers the landing port, the projection of the UAV landing system is within the vehicle's projection along the vehicle's z-axis. This ensures that installing the UAV landing system on the vehicle does not increase the vehicle's overall width or length, preventing the vehicle from more easily encountering obstacles outside the vehicle and improving the flexibility of the UAV landing system's installation.

[0082] When the top cover 210 opens the landing port, the projection of the UAV landing system is within the vehicle's projection along the vehicle's x-axis. This means that even when the UAV landing system is installed on the vehicle and the system is open for takeoff and landing, it does not increase the vehicle's overall height or width. This allows for safer UAV takeoff and landing operations while the vehicle is in motion, improving the safety of the UAV landing system application.

[0083] When the top cover 210 opens the landing port, the projection of the UAV landing system is within the vehicle's projection along the vehicle's z-axis. This means that even when the UAV landing system is installed on the vehicle and the system is open for takeoff and landing, it does not increase the vehicle's overall length or width. This allows for safer UAV takeoff and landing operations while the vehicle is in motion, improving the safety of the UAV landing system application.

[0084] refer to Figure 7 In some embodiments, a charging port is provided on the platform base plate 580, and a charging plug is provided on the drone 100. When the drone 100 is parked on the platform base plate 580, the charging plug can be plugged into the charging port. This allows the drone 100 to be charged while stored, improving its ease of use. The power for the charging port can come from an onboard power source, such as the alternator or battery of a conventional gasoline vehicle or the power battery of a new energy vehicle. The plug and port can also be equipped with communication interfaces, allowing the drone 100 to communicate with the vehicle and, consequently, with the user, further enhancing usability.

[0085] refer to Figure 7 In some embodiments, the charging port is a magnetic charging interface 5801, and the charging plug is a support frame 120. The support frame 120 is provided with magnetic charging contacts 130. The magnetic charging interface 5801 and the magnetic charging contacts 130 are mutually attracted to achieve an electrical connection. Thus, the drone 100 only needs to be parked in a preset position to automatically complete the electrical connection between the magnetic charging interface 5801 and the magnetic charging contacts 130, eliminating the need for manual operation. This improves the ease of use of the drone 100 and also increases the success rate of the connection between the magnetic charging interface 5801 and the magnetic charging contacts 130. Once the drone 100 is parked on the platform base plate 580, the charging port and charging plug are connected, which also helps to secure the drone 100 and prevent it from shifting during vehicle operation.

[0086] refer to Figure 7In some embodiments, an alignment mark is provided on the platform base plate 580, and a downward-facing camera 110 is provided on the drone 100. The downward-facing camera 110 is used to identify the alignment mark. The alignment mark can be a QR code 5802 or some asymmetrical graphic. The drone 100 can identify the alignment mark through a visual solution to determine the position of the drone 100, ensuring that the drone 100 is accurately parked in the preset position, avoiding collisions with other parts of the vehicle body, and ensuring successful connection between the magnetic charging interface 5801 and the magnetic charging contact 130.

[0087] refer to Figure 3 In some embodiments, the drone take-off and landing device also includes a enclosure, which, when the connecting assembly 550 is in the retracted state, encloses the parking space 200 with the rear windshield, enclosure, and top cover 210. This allows the parking space 200 to be relatively enclosed, preventing interference from external dust and rain, and preventing noise and heat from the drone's operation from interfering with the vehicle's pilot. Figure 3 In the illustrated embodiment, the enclosure includes a left panel 230 and a right panel 240 disposed opposite each other in the y-axis direction of the vehicle, and a front panel 220 disposed opposite to the top cover 210 in the x-axis direction of the vehicle. However, the enclosure can also be a continuous arc-shaped panel, and its shape can be set according to specific needs. The drone 100 can be parked in the parking space 200. In this way, the drone 100 has an independent parking space 200 for storage, which completely separates the drone 100 from the passenger cabin, reduces the impact of drone 100 noise on passengers, and provides a simpler take-off and landing environment for the drone 100, avoiding interference with the take-off and landing of the drone 100 when users place items on the shelf. In addition, the top cover 210, left panel 230, right panel 240 and front panel 220 can all be made of transparent materials, such as glass or resin, which can provide the driver with a wider rear view. Of course, these four can also be opaque. In this embodiment, a streaming media rearview mirror 700 can be set to allow the driver to compensate for the rear view.

[0088] refer to Figures 1 to 3 The side panel at least partially mates with the side of the rear windshield, for Figure 3 In the illustrated embodiment, at least partially, the sides of the left panel 230, the right panel 240, and the front panel 220 mate with the side of the rear windshield 300. The portions of the panels that mate with the rear windshield 300 are provided with a sealing structure and / or a water-guiding channel. The sealing structure may be a waterproof sleeve fitted onto the sides of the left panel 230, right panel 240, and front panel 220, or an applied sealant, to prevent water from entering the parking space 200 and damaging the drone 100. The water-guiding channel can drain water if it accidentally spills onto the mating area, preventing water accumulation and damage to the drone 100.

[0089] When the connecting assembly 550 is in the retracted state, the upper cover 210 and the rear windshield 300 form a side connection for the take-off and landing port. A sealing structure and / or a water-guiding channel are provided at the connection point between the upper cover 210 and the rear windshield 300. The sealing structure can be a waterproof sleeve fitted onto the side of the upper cover 210, or an applied sealant, to prevent water from entering the landing space 200 and damaging the drone 100. The water-guiding channel can drain water if it accidentally spills onto the connection point, preventing water accumulation and damage to the drone 100.

[0090] refer to Figure 3 In some embodiments, a cooling fan 270 is provided on the enclosure. The cooling fan 270 can be used in conjunction with the heat sink 260 or used independently. The cooling fan 270 can dissipate heat from the drone 100 when it is charging or when the temperature inside the parking space 200 is abnormally high due to factors such as light or ambient temperature, thus preventing the drone 100 from overheating and being damaged.

[0091] refer to Figure 1 and Figure 3 In some embodiments, the drone take-off and landing device also includes a temperature sensor for acquiring temperature information within the parking space 200. The temperature sensor can be located either inside or outside the parking space, depending on its form. For example, when the temperature sensor is a thermistor, it can be located inside the parking space; when it is an infrared temperature sensor, it is located outside. In these embodiments, the vehicle can be equipped with an onboard drone controller 900. The onboard drone controller 900 receives signals from the temperature sensor to obtain the internal temperature of the parking space 200. When the temperature inside the parking space 200 exceeds a preset safe temperature, the onboard drone controller 900 can control the activation of the cooling fan 270 to rapidly cool the interior of the parking space 200, reducing the probability of overheating damage to the drone 100 and the risk of charging fire. Simultaneously, the onboard drone controller 900 can also output the temperature information to the vehicle's central integrated controller 800, which displays the temperature information on the vehicle's central control screen 600 for operator monitoring.

[0092] refer to Figure 1 According to a third aspect of this application, a vehicle is also provided, including a rear windshield 300, a shelf, and a drone, as well as the aforementioned drone take-off and landing device or system. The vehicle may be a gasoline-powered vehicle, a plug-in hybrid electric vehicle, or a new energy vehicle, etc., and this disclosure does not specifically limit it.

[0093] refer to Figure 1In some embodiments, the vehicle also includes a streaming rearview mirror 700, which is used to acquire images during the takeoff or landing of the drone 100. This allows for manual intervention during the takeoff and landing of the drone 100, preventing it from colliding with obstacles. It also compensates for the lost rear view during takeoff and landing, improving driving safety. In these embodiments, the operator can issue takeoff and landing commands for the drone 100 via the vehicle's central control screen 600. Upon receiving the command, the central integrated controller 800 immediately issues an activation command to the streaming rearview mirror 700, enabling the streaming rearview mirror 700 to be activated simultaneously with the drone 100's takeoff and landing while driving, monitoring the environment behind the vehicle and improving driving safety.

[0094] In the description of this application, the terms "first" and "second" are used for descriptive purposes only and should not be construed as indicating or implying relative importance or implicitly specifying the number of technical features indicated. Therefore, a feature defined as "first" or "second" may explicitly or implicitly include one or more features. In the description of this application, "multiple" means two or more, unless otherwise explicitly specified.

[0095] In the above embodiments, the descriptions of each embodiment have different focuses. For parts not described in detail in a certain embodiment, please refer to the relevant descriptions in other embodiments.

[0096] The embodiments, implementation methods, and related technical features of this application can be combined and substituted for each other without conflict.

[0097] The above are merely preferred embodiments of this application and are not intended to limit this application in any way. Any modifications, equivalent changes, or alterations made to the above embodiments based on the technical essence of this application without departing from the scope of the technical solution of this application shall still fall within the scope of the technical solution of this application.

Claims

1. An unmanned aerial vehicle landing gear, characterized in that, The utility model relates to a kind of unmanned aerial vehicle landing device, including: Platform base, one side is formed with parking space; Upper cover plate, for covering or opening the parking space; Connecting assembly, connected with the upper cover plate, the connecting assembly has extension state and retracted state; Wherein, the connecting assembly can make the upper cover plate cover the parking space when the connecting assembly is in retracted state;The connecting assembly can make the upper cover plate open the parking space when the connecting assembly is in extension state, the connecting assembly includes drive crank, first connecting rod, second connecting rod, connecting rod base, connecting rod upper seat, third connecting rod, fourth connecting rod, fifth connecting rod and pin shaft, the connecting rod upper seat is fixedly connected with the upper cover plate;And Power distribution device, the power distribution device is driven connection with the drive crank, one end of the first connecting rod is hinged with the drive crank, the other end of the first connecting rod is hinged with the middle part of the second connecting rod;One end of the second connecting rod is hinged with the connecting rod base, the other end of the second connecting rod is connected with the connecting rod upper seat;The drive crank drives the second connecting rod to rotate by the first connecting rod, to make the connecting assembly switch between extension state and retracted state; One end of the third connecting rod is hinged with the end of the second connecting rod away from the connecting rod base, the other end of the third connecting rod is hinged with the connecting rod upper seat, one end of the fourth connecting rod is hinged with the connecting rod upper seat, the other end of the fourth connecting rod is hinged with one end of the fifth connecting rod, the end of the fifth connecting rod away from the fourth connecting rod is hinged with the connecting rod base, the pin shaft is fixed in the middle part of the second connecting rod, the fourth connecting rod middle part is provided with a waist type hole, the pin shaft passes through the waist type hole, so that the fourth connecting rod can rotate around the pin shaft and slide along the length direction of the waist type hole;The fourth connecting rod is arranged in parallel with the third connecting rod, and the second connecting rod and the fifth connecting rod are arranged in parallel;The connecting rod base, the second connecting rod, the third connecting rod, the fourth connecting rod, the fifth connecting rod, the connecting rod upper seat and the pin shaft cooperate, so that when the second connecting rod stops rotating around the connecting rod base, the upper cover plate stops rotating around the third connecting rod.

2. The unmanned aerial vehicle landing device according to claim 1, wherein: The platform base is movable in a first direction, and in the first direction, the platform base includes oppositely arranged first and second ends; The upper cover plate includes oppositely arranged third and fourth ends, and in the retracted state, the third end is arranged close to the first end, and the fourth end is arranged close to the second end; When switching from the retracted state to the extended state, the third end moves towards the second end.

3. The UAV landing device of claim 1 or 2, wherein, The unmanned aerial vehicle landing device further includes a drive motor, the drive motor is drivingly connected with the power distribution device, and the power distribution device is drivingly connected with the platform base and the connecting assembly respectively;The drive motor is used to drive the platform base to move in the first direction and drive the connecting assembly to switch between the extended state and the retracted state through the power distribution device.

4. The UAV landing gear of claim 3, wherein, The power distribution device comprises a driving gear, a rack and a driven gear shaft, the driving gear is drivingly connected with an output shaft of the driving motor; the rack is fixedly connected on the platform bottom plate and extends along the first direction, the rack is respectively engaged with the driving gear and the driven gear shaft; The driven gear shaft is drivingly connected with the connecting assembly to drive the upper cover plate.

5. The UAV landing gear of claim 4, wherein, The driven gear shaft is drivingly connected with the driving crank.

6. The UAV landing gear of claim 1, wherein, The connecting assembly further comprises a buffer pad, the buffer pad is arranged on the driving crank; when the connecting assembly is in the extended state, the buffer pad abuts against the connecting rod base to hinder the rotation of the driving crank; and / or When the connecting assembly is in the retracted state, the buffer pad abuts against the connecting rod base to hinder the rotation of the driving crank; and / or The connecting rod base is provided with a first limiting block, when the connecting assembly is in the extended state, the first limiting block abuts against the fifth connecting rod; and / or The connecting rod base is provided with a second limiting block, when the connecting assembly is in the extended state, the second limiting block abuts against the fourth connecting rod.

7. The drone landing device of claim 6, wherein, The connecting assembly is provided with two sets, the two sets of connecting assemblies are arranged on the two sides of the platform bottom plate and the arrangement direction is perpendicular to the first direction.

8. The UAV landing gear of claim 4, wherein, The unmanned aerial vehicle landing device further comprises a guide mechanism, the guide mechanism comprises a sliding block and a sliding rail which are slidingly connected, the sliding rail extends along the length direction of the rack, one of the sliding block and the sliding rail is fixedly connected with the platform bottom plate.

9. The UAV landing gear of claim 8, wherein, The guide mechanism is provided with two sets, the two sets of guide mechanisms are arranged at intervals and the arrangement direction is perpendicular to the first direction.

10. An unmanned aerial vehicle landing system, characterized by, The unmanned aerial vehicle landing system comprises the unmanned aerial vehicle landing device and an unmanned aerial vehicle.

11. The drone landing system of claim 10, wherein, The unmanned aerial vehicle landing system is applied to a vehicle, the vehicle comprises oppositely arranged rear windshield glass and a storage rack, the unmanned aerial vehicle landing device is arranged between the rear windshield glass and the storage rack; the rear windshield glass is provided with a landing port, the landing port is communicated with the parking space; the platform bottom plate is used for parking the unmanned aerial vehicle, when the connecting assembly is in the extended state, the upper cover plate is away from the landing port to open the landing port; when the connecting assembly is in the retracted state, the upper cover plate covers the landing port.

12. The unmanned aerial vehicle landing system according to claim 11, wherein when the upper cover plate covers the landing port, the projection of the unmanned aerial vehicle landing system in the vehicle is within the projection of the vehicle along the x-axis and / or y-axis and / or z-axis of the vehicle; and / or when the upper cover plate opens the landing port, the projection of the unmanned aerial vehicle landing system in the vehicle is within the projection of the vehicle along the x-axis and / or z-axis of the vehicle.

13. The drone landing system of claim 10, wherein, The platform bottom plate is provided with a charging socket, the unmanned aerial vehicle is provided with a charging plug, when the unmanned aerial vehicle is parked on the platform bottom plate, the charging plug can be plugged with the charging socket.

14. The drone landing system of claim 13, wherein, The charging socket is a magnetic charging interface, the charging plug is a support frame, the support frame is provided with a magnetic charging contact, and the magnetic charging interface and the magnetic charging contact can be attracted to each other.

15. The drone landing system of claim 10, wherein, The platform bottom plate is provided with an alignment mark, and the unmanned aerial vehicle is provided with a downward-looking camera, which is used to identify the alignment mark.

16. The drone landing system of claim 11, wherein, The unmanned aerial vehicle landing device further comprises a coaming; when the connecting assembly is in the retracted state, the rear windshield, the coaming and the upper cover plate enclose the parking space.

17. The drone landing system of claim 16, wherein, The side edge of the coaming is at least partially in abutment with the side surface of the rear windshield; the portion of the side edge of the coaming in abutment with the rear windshield is provided with a sealing structure and / or a water guide groove; And / or When the connecting assembly is in the retracted state, the upper cover plate and the rear windshield are used to form the side edge abutment of the landing port, and the position of the abutment of the upper cover plate and the rear windshield is provided with a sealing structure and / or a water guide groove.

18. The drone landing system of claim 16, wherein, The coaming is provided with a cooling fan.

19. The drone landing system of claim 18, wherein, The unmanned aerial vehicle landing device further comprises a temperature sensor, which is used to obtain temperature information in the parking space.

20. A vehicle characterized by The vehicle further comprises a streaming rearview mirror, which is used to obtain images during the take-off or landing of the unmanned aerial vehicle.

21. The vehicle of claim 20, wherein, The vehicle further comprises a streaming rearview mirror, which is used to obtain images during the take-off or landing of the unmanned aerial vehicle.

Images