Unmanned aerial vehicle hangar and vehicle

Abstract

The utility model discloses an unmanned aerial vehicle hangar and a vehicle, the unmanned aerial vehicle hangar comprises a shell, the shell is suitable for being arranged at the top of the vehicle, one side of the shell is provided with a matching part, and the matching part is suitable for defining a cabin together with the top wall of the vehicle. According to the unmanned aerial vehicle hangar, other parts do not need to be arranged between the unmanned aerial vehicle hangar and the top wall of the vehicle, the matching part of the unmanned aerial vehicle hangar and the top wall jointly define the cabin, and the space utilization rate between the unmanned aerial vehicle hangar and the top wall of the vehicle is increased.

Description

Technical Field

[0001] This utility model relates to the field of vehicle technology, and in particular to a drone hangar and vehicle. Background Technology

[0002] Unmanned aerial vehicles (UAVs) are unmanned aircraft controlled by radio remote control equipment and their own program control devices, or operated autonomously by an onboard computer, either completely or intermittently.

[0003] In related technologies, when vehicles pass through unfamiliar and complex environments (such as areas without network coverage), they can use vehicle-mounted drones to obtain first-hand, real-time traffic and environmental information along the route ahead. To facilitate drone storage, a drone hangar can be installed in the vehicle. Current technology typically involves adding a drone hangar to the roof of the vehicle, requiring corresponding mounting brackets between the roof and the hangar, resulting in low space utilization between the roof and the hangar. Utility Model Content

[0004] This utility model aims to solve at least one of the technical problems existing in the prior art. Therefore, one objective of this utility model is to provide a drone hangar where no other components are needed between the drone hangar and the vehicle's roof wall. The drone hangar's mating parts are directly connected to the roof wall to jointly define the cabin, thereby increasing the space utilization rate between the drone hangar and the vehicle's roof wall.

[0005] Another objective of this invention is to propose a vehicle that utilizes the aforementioned unmanned aerial vehicle hangar.

[0006] According to an embodiment of the present invention, a drone hangar is applied to a vehicle and includes: a housing, the housing being adapted to be disposed on the top of the vehicle, and a mating portion having a side of the housing, the mating portion being adapted to jointly define a cabin with the top wall of the vehicle.

[0007] According to the present invention, when the drone hangar is installed on the roof of a vehicle, there is no need to use other components to install the drone hangar on the vehicle, thereby avoiding other components occupying space on the drone hangar and the vehicle. Moreover, the mating part of the drone hangar is directly connected to the roof wall to jointly define the cabin. The cabin utilizes both the internal space of the drone hangar and the roof space of the vehicle, thereby effectively improving the space utilization rate between the drone hangar and the vehicle.

[0008] According to some embodiments of the present invention, a first opening is formed on the rear wall of the housing, the interior of the cabin communicates with the exterior of the housing through the first opening, and a guide is provided at the first opening.

[0009] According to some embodiments of the present application, the flow guide member comprises a plurality of flow guide plates extending in a direction perpendicular to the front-rear direction of the vehicle, and the flow guide plates are arranged at intervals.

[0010] According to some embodiments of the present application, the flow guide plate comprises a first flow guide section and two second flow guide sections, the two second flow guide sections are connected to the two sides of the first flow guide section along the width direction of the first flow guide section, and the two second flow guide sections extend in directions away from each other.

[0011] According to some embodiments of the present application, the unmanned aerial vehicle hangar further comprises a heat exchange member, the heat exchange member is arranged in the cabin, and the heat exchange member is opposite to the first opening along the front-rear direction of the vehicle.

[0012] According to some embodiments of the present application, a baffle is arranged between the heat exchange member and the rear wall of the shell, and the baffle extends downwardly along the front-rear direction of the vehicle.

[0013] According to some embodiments of the present application, the unmanned aerial vehicle hangar further comprises a controller, the controller is arranged in the cabin, and the controller is located at the front end of the cabin.

[0014] According to some embodiments of the present application, a support is arranged at the matching portion, the support is connected to the shell, and the support is adapted to be connected to the top wall, and the controller is arranged on the support.

[0015] According to some embodiments of the present application, the shell comprises a body and a door, a second opening is formed in the body, the door is movably arranged on the body to open and close the second opening, and the body and the door are adapted to jointly define the cabin with the top wall.

[0016] According to some embodiments of the present application, the unmanned aerial vehicle hangar further comprises a parking apron, the parking apron is arranged in the cabin, and the parking apron is opposite to the second opening.

[0017] According to some embodiments of the present application, the unmanned aerial vehicle hangar further comprises a lifting mechanism, the lifting mechanism is arranged in the cabin, and the lifting mechanism cooperates with the parking apron to drive the parking apron to approach and move away from the second opening.

[0018] The vehicle according to the second aspect of the present application comprises the unmanned aerial vehicle hangar according to the first aspect of the present application.

[0019] According to some embodiments of the present application, the vehicle further comprises: a vehicle body, a top wall of the vehicle body has a fitting part, a bottom wall of the fitting part is located on a side of the top wall of the vehicle body close to the center of the vehicle body, the fitting part, a part of the top wall and a shell of the UAV hangar jointly define a cabin of the UAV hangar.

[0020] According to some embodiments of the present application, the depth of the fitting part is h, wherein the h satisfies: 10mm≤h≤30mm.

[0021] According to some embodiments of the present application, the bottom wall of the fitting part extends downwardly and obliquely along the front-to-back direction of the vehicle body.

[0022] According to some embodiments of the present application, the oblique angle of the bottom wall of the fitting part is a, and the a satisfies: 1°≤a≤3°.

[0023] According to some embodiments of the present application, the fitting part is formed by concave downwardly from the top wall of the vehicle body.

[0024] According to some embodiments of the present application, at least one wire hole is formed on the top wall of the vehicle body.

[0025] According to some embodiments of the present application, a plurality of support beams are arranged on the side of the top wall of the vehicle body close to the center of the vehicle body.

[0026] The additional aspects and advantages of the present application will be partially given in the following description, partially will become obvious from the following description, or will be understood by the practice of the present application. BRIEF DESCRIPTION OF DRAWINGS

[0027] The above and / or additional aspects and advantages of the present application will become apparent and more readily appreciated from the following description of the embodiments, taken in conjunction with the accompanying drawings in which:

[0028] Figure 1 is a schematic view of a UAV hangar according to an embodiment of the present application;

[0029] Figure 2 is a schematic view of a UAV hangar according to an embodiment of the present application, wherein the specific structure of the deflector is shown;

[0030] Figure 3 is a schematic view of a UAV hangar and a UAV according to an embodiment of the present application;

[0031] Figure 3-1 is Figure 3 is an enlarged view of A part shown in the circle in figure 8;

[0032] Figure 4is a top view of a vehicle body according to an embodiment of the present application.

[0033] Reference signs:

[0034] 100, vehicle;

[0035] 1, vehicle body; 11, fitting portion; 12, wire passing hole; 13, support beam; 131, first support beam segment;

[0036] 141, curtain glass piece; 142, top wall; 143, first decorative plate; 144, first cover plate;

[0037] 145, second decorative plate; 146, spoiler; 147, second cover plate;

[0038] 2, unmanned aerial vehicle hangar;

[0039] 21, machine shell; 211, first opening; 212, flow guide piece;

[0040] 2121, flow guide plate; 2121a, first flow guide segment; 2121b, second flow guide segment;

[0041] 213, body; 2131, second opening; 214, hangar door; 215, fitting portion;

[0042] 22, machine cabin; 221, support; 23, controller;

[0043] 24, heat exchange piece; 241, third opening; 25, baffle;

[0044] 26, parking apron; 27, lifting mechanism; 28, wire harness;

[0045] 101, unmanned aerial vehicle. DETAILED DESCRIPTION

[0046] The embodiments of the present application will be described in detail below, and the embodiments described with reference to the accompanying drawings are exemplary, and the following Figures 1-3 and Figure 3-1 The unmanned aerial vehicle hangar 2 according to the first aspect of the present application is described.

[0047] As shown in Figure 1 and Figure 4 The unmanned aerial vehicle hangar 2 according to the first aspect of the present application includes a machine shell 21.

[0048] Specifically, the machine shell 21 is adapted to be arranged on the top of the vehicle 100, and one side of the machine shell 21 has a fitting portion 215 adapted to cooperatively define a machine cabin 22 with the top wall 142 of the vehicle 100.

[0049] For example, in Figure 1 andFigure 4 In the example of FIG. 1, the UAV hangar 2 is installed on the top of the vehicle 100, the bottom side of the casing 21 is open, and the fitting portion 215 is formed at a circumferential position of the bottom side of the casing 21, which is connected with the top wall 142 of the vehicle 100 to jointly define the cabin 22.

[0050] In this way, when the UAV hangar 2 is installed on the top wall 142 of the vehicle 100, the fitting portion 215 is connected with the top wall 142, and the installation between the UAV hangar 2 and the vehicle 100 does not need to rely on other components, thereby avoiding the occupation of space on the UAV hangar 2 and the vehicle 100 by the other components, and improving the space utilization of the UAV hangar 2 and the vehicle 100. In addition, the fitting portion 215 of the UAV hangar 2 is directly connected with the top wall 142 to jointly define the cabin 22, and the cabin 22 simultaneously utilizes the internal space of the UAV hangar 2 and the top space of the vehicle 100, further improving the space utilization of the UAV hangar 2 and the vehicle 100. Moreover, the space of the cabin 22 is increased by avoiding the occupation of the space of the cabin 22 by the above-mentioned other components, facilitating the placement of the UAV 101 in the cabin 22. In addition, the installation steps of the UAV hangar 2 and the vehicle 100 are simplified, thereby improving the installation efficiency of the UAV hangar 2. For example, the fitting portion 215 can be connected with the top wall 142 by fasteners (such as bolts).

[0051] According to the UAV hangar 2 of the present application, when the UAV hangar 2 is installed on the top wall 142 of the vehicle 100, the UAV hangar 2 is installed on the vehicle 100 without the aid of the above-mentioned other components, thereby avoiding the occupation of space on the UAV hangar 2 and the vehicle 100 by the above-mentioned other components, and the fitting portion 215 of the UAV hangar 2 and the top wall 142 jointly define the cabin 22, and the cabin 22 simultaneously utilizes the internal space of the UAV hangar 2 and the top space of the vehicle 100, thereby effectively improving the space utilization between the UAV hangar 2 and the vehicle 100.

[0052] According to some embodiments of the present application, referring to Figure 1 The rear wall of the casing 21 is formed with a first opening 211, the inside of the cabin 22 is communicated with the outside of the casing 21 through the first opening 211, and a flow guide 212 is arranged at the first opening 211. For example, in the example of FIG. 1, the circumferential edge of the flow guide 212 is connected with the circumferential edge of the first opening 211. Figure 1

[0053] ​In this way, the air can pass through the first opening 211, and the flow guide 212 can shield the liquid to prevent the liquid from entering the cabin 22 from the first opening 211 in a large amount, thereby preventing the liquid from flowing into the components in the cabin 22 and affecting the use of the components in the cabin 22. In addition, after the use of the unmanned aerial vehicle 101, the heat of the unmanned aerial vehicle 101 is diffused in the cabin 22, and the cold air outside the cabin 22 can flow into the cabin 22 through the first opening 211, and the heat in the cabin 22 can also flow to the outside of the cabinet 21 through the first opening 211, so that the temperature in the cabin 22 is reduced, thereby preventing the heat from damaging the components in the cabin 22, prolonging the service life of the components in the cabin 22, and enabling the unmanned aerial vehicle hangar 2 to be used normally for a long time. It should be noted that the first opening 211 can also be provided with a plurality of first openings, such as Figure 3 As shown in the drawings, two first openings 211 are provided on the rear wall of the cabinet 21 along the left-right direction, which further improves the heat dissipation capacity, but is not limited thereto.

[0054] According to some embodiments of the present application, referring to Figure 2 , Figure 3 and Figure 3-1 , the flow guide 212 includes a plurality of flow guide plates 2121, the flow guide plates 2121 extend along a direction perpendicular to the front-rear direction of the vehicle 100, and the plurality of flow guide plates 2121 are arranged at intervals. For example, in the examples of Figure 2 , Figure 3 and Figure 3-1 , the plurality of flow guide plates 2121 are arranged at intervals along the extension direction of the rear wall of the cabinet 21. Among them, the above-mentioned “direction perpendicular to the front-rear direction of the vehicle 100” can refer to any direction in the plane perpendicular to the front-rear direction. For example, it can be the left-right direction, the up-down direction or other inclined angles of the vehicle body 1, which is beneficial to the heat exchange between the inside and outside of the cabin 22. In this way, there is a gap between the two adjacent flow guide plates 2121, which effectively ensures that the airflow can flow in or out of the gap when the heat exchange member 24 is in use, facilitating the heat dissipation of the cabin 22. In addition, the plurality of flow guide plates 2121 are arranged to ensure that there is a gap, which also improves the effect of the flow guide 212 shielding the liquid, thereby effectively preventing the liquid from entering the cabin 22.

[0055] Further, referring to Figure 2 , Figure 3 and Figure 3-1 , the flow guide plate 2121 includes a first flow guide section 2121a and two second flow guide sections 2121b, the two second flow guide sections 2121b are connected to the two sides of the first flow guide section 2121a along the width direction of the first flow guide section 2121a, and the two second flow guide sections 2121b extend in directions away from each other.

[0056] For example, inFigure 2 And Figure 3-1 In the example, two second flow guide sections 2121b are connected to the front and back of the first flow guide section 2121a respectively, and the free ends of the two second flow guide sections 2121b extend in directions away from each other. That is, the lower end of the second flow guide section 2121b at the front end of the first flow guide section 2121a is connected to the front side of the first flow guide 212, and the upper end of the second flow guide section 2121b (i.e. the free end of the second flow guide section 2121b) extends upward. The second flow guide section 2121b at the back side of the first flow guide section 2121a is connected to the back side of the first flow guide 212 at the upper end of the second flow guide section 2121b, and the lower end of the second flow guide section 2121b (i.e. the free end of the second flow guide section 2121b) extends downward. Among them, the second flow guide sections 2121b corresponding to the adjacent two flow guide plates 2121 are opposite in the up-down direction, and there is a gap between the adjacent two second flow guide sections 2121b at the same side of the first flow guide section 2121a. Or in other words, the cross-sectional shape of the flow guide plate 2121 is "Z" shaped, and the two flow guide plates 2121 connected to each other are spaced apart. In this way, it is ensured that there is a gap between the adjacent two flow guide plates 2121, and heat can pass through, and the shielding effect of the multiple flow guide plates 2121 on the liquid outside the cabin 22 is improved after mutual cooperation, thereby effectively preventing the liquid from entering the cabin 22. In addition, the structure of the flow guide plate 2121 is simple and easy to form and process, thereby improving the production efficiency of the flow guide plate 2121 and improving the production efficiency of the unmanned aerial vehicle 101 warehouse.

[0057] According to some embodiments of the present application, referring to Figure 1 The unmanned aerial vehicle hangar 2 further comprises a heat exchange member 24, which is arranged in the cabin 22, and the heat exchange member 24 is opposite to the first opening 211 along the front-rear direction of the vehicle 100.

[0058] For example, in the example of Figure 1 The heat exchange member 24 is located at the rear end of the cabin 22, and the heat exchange member 24 is located in front of the flow guide member 212. The heat exchange member 24 can be provided as a heat exchange fan, and the heat exchange member 24 is formed with a third opening 241, which is formed on the side of the heat exchange member 24 facing the flow guide member 212, and the third opening 241 and the first opening 211 are opposite along the front-rear direction.

[0059] In this way, after the unmanned aerial vehicle 101 is used, the heat of the unmanned aerial vehicle 101 is diffused in the cabin 22, and the cold air outside the cabin 22 can flow into the cabin 22 through the first opening 211, and the heat exchange element 24 can exchange heat with the hot air in the cabin 22, and the heat exchange element 24 improves the heat exchange efficiency. Alternatively, the cold air can flow to the unmanned aerial vehicle 101 through the third opening 241, and the hot air at the unmanned aerial vehicle 101 can also flow out through the third opening 241 to the first opening 211. Thus, the temperature in the cabin 22 is further effectively reduced, and the components in the cabin 22 are prevented from being damaged at high temperature, thereby prolonging the service life of the components in the cabin 22 and prolonging the service life of the unmanned aerial vehicle hangar 2.

[0060] According to some embodiments of the present application, referring to Figure 1 The heat exchange element 24 and the rear wall of the cabinet 21 are provided with a baffle 25, and the baffle 25 extends downwardly along the vehicle 100 from front to back.

[0061] For example, in the example of Figure 1 The baffle 25 extends downwardly along the vehicle 100 from front to back and towards the side where the top wall 142 is located. The baffle 25 is connected to the cabinet 21, and there is a gap between the rear end of the baffle 25 and the rear wall of the cabinet 21. In this way, after the liquid enters the cabin 22 through the first opening 211, the baffle 25 can shield the liquid to prevent the liquid from contacting the components on the lower side of the baffle 25 and affecting the use of the components, so that the components on the lower side of the baffle 25 can be used normally for a long time. In addition, the baffle 25 is inclined to separate the liquid entering the cabin 22 through the flow guide 212, flow along the baffle 25, and then flow out from between the baffle 25 and the cabinet 21. For example, the liquid can flow along the cabinet 21 to the lower side of the first decorative plate 143 of the vehicle 100, and then flow into a water channel (not shown in the figure), and then flow out from the water channel to the outside of the vehicle 100. This facilitates the flow of liquid along the baffle 25, and the liquid naturally flows out of the cabin 22 to facilitate the discharge of the liquid, thereby preventing the liquid from accumulating and flowing to other components in the cabin 22 to damage the other components in the cabin 22, and thereby facilitating the normal use of the other components in the cabin 22 for a long time, and prolonging the service life of the unmanned aerial vehicle hangar 2.

[0062] According to some embodiments of the present application, referring to Figure 1 The unmanned aerial vehicle hangar 2 further comprises a controller 23, and the controller 23 is arranged in the cabin 22 and located at the front end of the cabin 22. For example, in the example of Figure 1In the example, controller 23 is positioned in front of heat exchanger 24, with a gap between them. This arrangement, placing controller 23 at the front of the cabin 22, reduces the distance between controller 23 and other components within the cabin 22 (such as UAV 101, antenna, camera, etc.). This results in a shorter wiring harness 28 spacing when controller 23 is electrically connected to other components in the cabin 22, reducing the space occupied by the harness and facilitating assembly. It also reduces the material usage of the wiring harness 28, lowering the production cost of the UAV hangar 2. Furthermore, it makes the internal layout of the cabin 22 more compact, making efficient use of the space. Additionally, positioning controller 23 and heat exchanger 24 at opposite ends of the cabin 22 avoids mutual interference during installation, reducing the difficulty of arranging and installing controller 23 and heat exchanger 24, thereby improving the assembly efficiency of the UAV 2.

[0063] Furthermore, referring to Figure 1 A bracket 221 is provided at the mating part 215. The bracket 221 is connected to the housing 21 and is adapted to be connected to the top wall 142. The controller 23 is mounted on the bracket 221. For example, in Figure 1 In the example, the controller 23 is connected to the bracket 221, which is also connected to the mating part 215. Along a plane perpendicular to the vertical direction, the cross-sectional area of ​​the bracket 221 is larger than that of the controller 23. This configuration allows the bracket 221 to support the controller 23, improving its stability and preventing it from shifting downwards after prolonged use, thus ensuring its long-term normal operation. Furthermore, the connection between the bracket 221 and the top wall 142 of the vehicle 100 enhances the stability of the bracket 221, further improving the stability of the controller 23 and the housing 21. This prevents the controller 23 and housing 21 from shaking during vehicle 100 operation, thereby extending the lifespan of the controller 23 and improving the overall stability of the UAV hangar 2.

[0064] According to some embodiments of this utility model, refer to Figure 3 The hangar 21 includes a body 213 and a door 214. A second opening 2131 is formed on the body 213. The door 214 is movably disposed on the body 213 to open and close the second opening 2131. The body 213, the door 214, and the top wall 142 together define the cabin 22. The UAV hangar 2 also includes a parking apron 26 and a lifting mechanism 27. The parking apron 26 is disposed inside the cabin 22 and is opposite to the second opening 2131. The lifting mechanism 27 is disposed inside the cabin 22 and cooperates with the parking apron 26 to move the parking apron 26 closer to and away from the second opening 2131.

[0065] For example, inFigure 3 In the example shown in FIG. 13, the second opening 2131 is in communication with the cabin 22, and the garage door 214 is matched with the second opening 2131 to open or close the cabin 22. The lifting mechanism 27 is arranged on the base of the cabin 22, and the landing pad 26 is arranged on the side of the lifting mechanism 27 away from the base of the cabin 22, and the unmanned aerial vehicle 101 is movably placed on the landing pad 26.

[0066] The process of using the unmanned aerial vehicle 101 with the unmanned aerial vehicle hangar 2 is roughly as follows:

[0067] After the controller 23 receives the work instruction, the controller 23 controls the garage door 214 to move along the left and right sides of the vehicle body 1 to open the cabin 22. Then the lifting mechanism 27 drives the landing pad 26 and the unmanned aerial vehicle 101 to move upwards to a height adjacent to the garage door 214. Then the unmanned aerial vehicle 101 is controlled to fly out of the vehicle 100, and then the lifting mechanism 27 drives the landing pad 26 to move downwards to the original position, and the garage door 214 is closed. At this time, the take-off of the unmanned aerial vehicle 101 is completed.

[0068] After the unmanned aerial vehicle 101 completes the work, the controller 23 controls the garage door 214 to move to open the cabin 22, and then the lifting mechanism 27 drives the landing pad 26 to move upwards to the height of the garage door 214. Then the unmanned aerial vehicle 101 is controlled to land back to the landing pad 26. Then, the lifting mechanism 27 drives the landing pad 26 and the unmanned aerial vehicle 101 to move downwards to the original position, and the garage door 214 is closed. At this time, the landing of the unmanned aerial vehicle 101 is completed.

[0069] In this way, the unmanned aerial vehicle 101 can be placed in the cabin 22, and the cabin 22 can also be used to install other components, so that the appearance of the body 213 is relatively simple, and the unmanned aerial vehicle hangar 2 is more beautiful. In addition, the unmanned aerial vehicle 101 can fly out of the unmanned aerial vehicle hangar 2 through the second opening 2131, or land back into the cabin 22 from the outside of the unmanned aerial vehicle hangar 2 through the second opening 2131. Before the unmanned aerial vehicle 101 is ready to take off or land, the landing pad 26 moves towards the direction of the second opening 2131 to facilitate the take-off or landing of the unmanned aerial vehicle 101, thereby improving the use performance of the unmanned aerial vehicle hangar 2. In addition, the setting of the landing pad 26 facilitates the parking of the unmanned aerial vehicle 101. It should be noted that the bottom wall of the cabin 22 is arranged horizontally along the vertical direction to ensure the landing accuracy of the unmanned aerial vehicle 101. It should be noted that the garage door 214 can be composed of one or more, which can be set according to the actual use.

[0070] According to the vehicle 100 of the second aspect of the present application, as shown in FIG. 13, the unmanned aerial vehicle hangar 2 according to the first aspect of the present application is included. Figure 4

[0071] ​According to the vehicle 100 of the utility model, the above unmanned aerial vehicle hangar 2 is adopted, and the space utilization of the top of the vehicle 100 is improved.

[0072] Further, with reference to Figure 1 and Figure 4 , the top wall 142 of the vehicle body 1 has a fitting part 11, the bottom wall of the fitting part 11 is located on the side of the top wall 142 of the vehicle body 1 close to the center of the vehicle body 1, the fitting part 11, part of the top wall 142 and the casing 21 of the unmanned aerial vehicle hangar 2 jointly define the cabin 22 of the unmanned aerial vehicle hangar 2.

[0073] For example, in the example of Figure 1 and Figure 4 , the bottom wall of the fitting part 11 is located on the lower side of the top wall 142 of the vehicle body 1, that is, the bottom surface of the fitting part 11 protrudes downward from the top wall 142 of the vehicle body 1. The unmanned aerial vehicle 101 is adapted to be placed in the cabin 22, and the position where the unmanned aerial vehicle 101 is placed can be opposite to the fitting part 11 in the up-down direction. That is to say, the casing 21 is buckled on the top wall 142 of the vehicle body 1, and jointly defines the cabin 22 with the part of the top wall 142 and the fitting part 11.

[0074] Therefore, by setting the fitting part 11, the partial space of the top of the vehicle body 1 is utilized, the height of the unmanned aerial vehicle hangar 2 is reduced in the case that the volume of the unmanned aerial vehicle hangar 2 is relatively unchanged, thereby the height of the whole vehicle 100 is reduced, the vehicle 100 is more easily passed through when passing through the components with height limit (such as limit rod or bridge hole) in life, the unmanned aerial vehicle hangar 2 is avoided from being abraded when the vehicle 100 passes through the limit rod or the bridge hole, thereby the smoothness of the vehicle 100 is improved, and the service life of the unmanned aerial vehicle hangar 2 is prolonged. In addition, in the case that the overall height of the vehicle 100 or the height of the unmanned aerial vehicle hangar 2 protruding from the top surface of the vehicle 100 is unchanged, the fitting part 11 also increases the space of the cabin 22, improves the space utilization rate of the cabin 22, facilitates the arrangement of other components in the cabin 22, reduces the production difficulty of the cabin 22, thereby the production efficiency of the unmanned aerial vehicle hangar 2 is improved. Moreover, the space of the cabin 22 is relatively large, the unmanned aerial vehicle 101 is facilitated to be placed, and the unmanned aerial vehicle 101 is facilitated to fly out and fall back from the cabin 22, collision between the unmanned aerial vehicle 101 and other components in the cabin 22 is avoided when the unmanned aerial vehicle 101 rises or falls in the cabin 22, the unmanned aerial vehicle 101 is avoided from being damaged, and the unmanned aerial vehicle 101 can be normally used for a long time. In addition, the space in the vehicle body 1 is effectively utilized, the unmanned aerial vehicle hangar 2 is facilitated to be installed on the roof, the installation difficulty of the unmanned aerial vehicle hangar 2 is reduced, and other components arranged at the top wall 142 of the vehicle body 1 are compact, thereby the space utilization rate of the vehicle body 1 is improved. Moreover, the cabin 22 is defined by the casing 21 and the top wall 142 of the vehicle body 1, and the integration of the vehicle body 1 and the unmanned aerial vehicle hangar 2 is improved. It should be noted that the vehicle 100 can be a SUV type vehicle 100, an MPV type vehicle 100 or an off-road type vehicle 100, but is not limited thereto.

[0075] According to some embodiments of the present application, referring to Figure 1The depth of the fitting part 11 is h, wherein h satisfies: 10mm≤h≤30mm. For example, when the depth of the fitting part 11 is greater than 30mm, the depth of the fitting part 11 is large, the distance between the top of the occupant in the vehicle 100 and the top of the vehicle 100 is reduced, the occupant is easy to collide with the top of the vehicle 100 and be damaged when the vehicle 100 bounces, the riding experience of the occupant is reduced, and the safety of the vehicle 100 is reduced. When the depth of the fitting part 11 is less than 10mm, the depth of the fitting part 11 is shallow, and the space in the cabin 22 can be increased only to a small extent. Therefore, by setting the depth h of the fitting part 11 to satisfy: 10mm≤h≤30mm, the depth of the fitting part 11 is reasonable, the distance between the top of the occupant in the vehicle 100 and the top of the vehicle 100 is increased, the occupant is prevented from colliding with the top of the vehicle 100 and being damaged when the vehicle 100 bounces, the head space of the occupant in the vehicle is not affected, the riding experience of the occupant is improved, and the safety of the vehicle 100 is improved. In addition, the space at the top of the vehicle body 1 is also effectively utilized, and the space utilization rate of the cabin 22 is effectively improved.

[0076] According to some embodiments of the present application, referring to Figure 1 The bottom wall of the fitting part 11 extends downwardly along the front-to-rear direction of the vehicle body 1. For example, in the example shown in Figure 1 The bottom wall of the fitting part 11 extends downwardly along the front-to-rear direction of the vehicle body 1. For example, in the example shown in The bottom wall of the fitting part 11 extends downwardly along the front-to-rear direction of the vehicle body 1. For example, in the example shown in

[0077] Further, referring to Figure 1 The bottom wall of the fitting part 11 extends downwardly along the front-to-rear direction of the vehicle body 1. For example, in the example shown in

[0078] For example, when the inclination angle of the bottom wall of the fitting portion 11 is greater than 3°, the inclination angle of the bottom wall of the fitting portion 11 is relatively large, so that the distance between the rear end of the fitting portion 11 and the top surface of the internal space of the vehicle body 1 is reduced, and the comfort of the passengers in the vehicle body 1 is reduced. When the inclination angle of the bottom wall of the fitting portion 11 is less than 1°, the inclination angle of the bottom wall of the fitting portion 11 is relatively small, and the liquid flowing onto the bottom wall of the fitting portion 11 is easy to accumulate, and other components are easy to be damaged. Therefore, by setting the inclination angle α of the bottom wall of the fitting portion 11 to satisfy 1°≤α≤3°, the inclination angle of the bottom wall of the fitting portion 11 is reasonable, the distance between the rear end of the fitting portion 11 and the top surface of the internal space of the vehicle body 1 is increased, and the comfort of the passengers in the vehicle body 1 is improved. In addition, the liquid flowing onto the bottom wall of the fitting portion 11 is avoided to accumulate, and other components are not easy to be damaged.

[0079] According to some embodiments of the present application, referring to Figure 1 , the fitting portion 11 is formed by the top wall 142 of the vehicle body 1 being recessed downward. For example, in the example of Figure 1 , the top wall 142 of the vehicle body 1 is recessed to form the fitting portion 11 towards the side away from the center of the cabin 22, that is, the fitting portion 11 is part of the top wall 142 of the vehicle body 1. Therefore, the unmanned aerial vehicle hangar 2 is arranged in an embedded manner, so that the unmanned aerial vehicle hangar 2 and the vehicle 100 are matched to realize an integrated structure, the appearance of the vehicle 100 is improved, and the appearance of the vehicle 100 is improved. In addition, the fitting portion 11 has a simple structure and is easy to form, thereby improving the production efficiency.

[0080] According to some embodiments of the present application, referring to Figure 1 , the top wall 142 of the vehicle body 1 is formed with at least one wire hole 12. For example, in the example of Figure 1 , the wire hole 12 is located on the side of the controller 23. In this way, the wire harness 28 in the unmanned aerial vehicle hangar 2 can pass through the wire hole 12 and be connected to the wire harness in the vehicle body 1 of the vehicle 100, so as to realize the connection between the components in the vehicle body 1 and the controller 23, and facilitate the normal use of the controller 23. It should be noted that the wire hole 12 can be provided with a plurality of wire holes, and in the description of the present application, "a plurality of" means two or more. For example, the wire hole 12 can be provided with two wire holes, which are respectively located on the opposite sides of the controller 23, so as to facilitate the wire harness 28 with different functions, but the present application is not limited thereto. The number and position of the wire hole 12 can be specifically set according to the actual use, so as to meet the actual demand. According to some embodiments of the present application, referring to Figure 1 , a plurality of support beams 13 are arranged on the side of the top wall 142 of the vehicle body 1 close to the center of the vehicle body 1. For example, in the example of Figure 4In the example, along the up-down direction of the vehicle body 1, the support 221, the top wall 142 of the vehicle body 1 and the support beam 13 are sequentially arranged. That is, the inner side of the top wall 142 is provided with a plurality of support beams 13, and the support beams 13 can extend in the front-rear direction, the left-right direction or other directions. In this way, the support beams 13 can support the top wall 142 and the support 221, thereby improving the rigidity and strength of the vehicle body 1 and the support 221, and improving the use performance of the vehicle body 1 and the support 221. In addition, the base of the unmanned aerial vehicle hangar 2 (for example, provided in the cabin 22, it should be pointed out that the bottom of the machine shell 21 is in an open state), the second decorative plate 145 and the wire harness 28 of the unmanned aerial vehicle hangar 2 can be fixed with a plurality of support beams 13, respectively, thereby improving the mounting stability of the base of the unmanned aerial vehicle hangar 2, the second decorative plate 145 and the wire harness 28 of the unmanned aerial vehicle hangar 2, and avoiding shaking. The support 221 of the unmanned aerial vehicle hangar 2 and the top cover of the vehicle body 1 are also connected with the support beam 13, for example, by penetrating the support 221 and the top cover with fasteners (such as bolts) and connecting with the support beam 13. Among them, the plurality of support beams 13 includes a plurality of first support beam segments 131 and a plurality of second support beam segments (not shown in the figure), the plurality of first support beam segments 131 are arranged in the front-rear direction, and the plurality of second support beam segments are arranged in the left-right direction. The first support beam segment 131 is connected with the plurality of second support beam segments.

[0081] According to some embodiments of the present application, the height of the vehicle 100 is H, wherein H satisfies: 1.82m≤H≤2m. For example, when the height of the vehicle 100 is greater than 2mm, the height of the vehicle 100 is large, and when the vehicle 100 passes through the limiting part in life, the height of the vehicle 100 is greater than the height of the limiting part, so that the vehicle 100 cannot pass through, and the vehicle 100 needs to detour, thereby prolonging the driving distance of the vehicle 100. Therefore, by setting the height H of the vehicle 100 to satisfy: 1.82m≤H≤2m, the height of the vehicle 100 is set reasonably, so that when the vehicle 100 passes through the limiting part in life, the vehicle 100 can pass through the limiting part, thereby avoiding the vehicle 100 detouring, thereby shortening the driving distance of the vehicle 100. In addition, the height of the internal space of the vehicle 100 is increased along the up-down direction, thereby avoiding the head of the occupant colliding with the top of the vehicle 100, or allowing the occupant to sit straight, thereby improving the use experience of the occupant. In addition, the appearance of the vehicle 100 is also improved, and the appearance of the vehicle 100 is improved. It should be noted that the height H of the vehicle 100 can further satisfy: 1.98m≤H≤2m, but is not limited thereto.

[0082] According to some embodiments of the present application, referring to ​The vehicle body 1 further comprises a sunroof glass 141, a top wall 142, a first decorative plate 143, a plurality of first cover plates 144, a second cover plate 147, a second decorative plate 145 and a spoiler 146. The sunroof glass 141 is located at the front side of the vehicle body 1, the spoiler 146 is located at the rear side of the vehicle body 1, the first decorative plate 143 is located between the top wall 142 and the spoiler 146, the first decorative plate 143 extends along the left-right direction of the vehicle body 1, the plurality of first cover plates 144 are respectively located at the left and right sides of the top wall 142, and the first cover plates 144 extend along the front-rear direction of the vehicle body 1, and the second decorative plate 145 is located between the top wall 142 and the first cover plates 144. The second cover plate 147 is located below the support beam 13. Alternatively, the support beam 13 is arranged between the top wall 142 and the second cover plate 147.

[0083] In this way, the sunroof glass 141, the top wall 142, the first cover plates 144 and the spoiler 146 are assembled to form the frame of the vehicle body 1, which facilitates the installation of other components of the vehicle 100 in the vehicle body 1. In addition, the first decorative plate 143 and the second decorative plate 145 can shield the structure inside the vehicle body 1, thereby improving the appearance of the vehicle 100. The UAV hangar 2 is located at the central position of the rear end of the top wall 142, and the top wall 142 is installed in cooperation with the UAV hangar 2. The second cover plate 147 can shield the components between the top wall 142 and the second cover plate 147, so that the internal modeling of the vehicle 100 is more simple and beautiful.

[0084] Other configurations and operations of the vehicle 100 according to the embodiments of the present application are known to those skilled in the art, and will not be described in detail here.

[0085] In the description of the present application, it should be understood that the orientations or positional relationships indicated by the terms "center", "longitudinal", "transverse", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "circumferential" and the like are based on the orientations or positional relationships shown in the drawings, and are only for the convenience of describing the present application and simplifying the description, and therefore cannot be understood as indicating or implying that the devices or elements referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore cannot be understood as limiting the present application.

[0086] In the description of the present application, the description of the terms "one embodiment", "some embodiments", "exemplary embodiment", "example", "specific example" or "some examples" means that the specific features, structures, materials or characteristics described in connection with the embodiment or example are included in at least one embodiment or example of the present application. In the present application, the exemplary description of the above terms does not necessarily refer to the same embodiment or example.

[0087] Although the embodiments of the utility model have been shown and described, those of ordinary skill in the art can understand that various changes, modifications, replacements and variations can be made to these embodiments without departing from the principles and purposes of the utility model, and the scope of the utility model is defined by the claims and their equivalents.

Claims

1. A drone hangar (2) for use in a vehicle (100), characterized in that, include: A housing (21) adapted to be disposed on the top of the vehicle (100), the housing (21) having a mating part (215) on one side, the mating part (215) adapted to define the cabin (22) together with the top wall (142) of the vehicle (100).

2. The unmanned aerial vehicle hangar (2) according to claim 1, characterized in that, A first opening (211) is formed on the rear wall of the housing (21), and the interior of the cabin (22) is connected to the outside of the housing (21) through the first opening (211). A guide (212) is provided at the first opening (211).

3. The unmanned aerial vehicle hangar (2) according to claim 2, characterized in that, The flow guide (212) includes: Multiple deflectors (2121) extend in a direction perpendicular to the front-rear direction of the vehicle (100), and the multiple deflectors (2121) are arranged at intervals.

4. The unmanned aerial vehicle hangar (2) according to claim 3, characterized in that, The guide plate (2121) includes a first guide section (2121a) and two second guide sections (2121b). The two second guide sections (2121b) are respectively connected to both sides of the first guide section (2121a) along the width direction of the first guide section (2121a), and the two second guide sections (2121b) extend in mutually opposite directions.

5. The unmanned aerial vehicle hangar (2) according to any one of claims 2-4, characterized in that, Also includes: A heat exchanger (24) is disposed in the engine compartment (22) and is opposite to the first opening (211) in the front-rear direction of the vehicle (100).

6. The unmanned aerial vehicle hangar (2) according to claim 5, characterized in that, A baffle (25) is provided between the heat exchanger (24) and the rear wall of the housing (21), and the baffle (25) extends downward along the vehicle (100) from front to back.

7. The unmanned aerial vehicle hangar (2) according to any one of claims 1, 2, 3, 4 and 6, characterized in that, Also includes: The controller (23) is located inside the cabin (22) and at the front of the cabin (22).

8. The unmanned aerial vehicle hangar (2) according to claim 7, characterized in that, A bracket (221) is provided at the mating part (215), the bracket (221) is connected to the housing (21), and the bracket (221) is adapted to be connected to the top wall (142). The controller (23) is provided on the bracket (221).

9. The unmanned aerial vehicle hangar (2) according to any one of claims 1, 2, 3, 4 and 8, characterized in that, The housing (21) includes a body (213) and a door (214). A second opening (2131) is formed on the body (213). The door (214) is movably disposed on the body (213) to open and close the second opening (2131). The body (213), the door (214), and the top wall (142) are adapted to define the cabin (22) together.

10. The unmanned aerial vehicle hangar (2) according to claim 9, characterized in that, Also includes: A parking apron (26) is located inside the cabin (22) and is opposite to the second opening (2131).

11. The unmanned aerial vehicle hangar (2) according to claim 10, characterized in that, Also includes: Lifting mechanism (27) is located inside the cabin (22). The lifting mechanism (27) cooperates with the parking apron (26) to move the parking apron (26) closer to and away from the second opening (2131).

12. A vehicle (100), characterized in that, Includes the unmanned aerial vehicle hangar (2) according to any one of claims 1-11.

13. The vehicle (100) according to claim 12, characterized in that, include: The vehicle body (1) has a fitting part (11) on its top wall (142). The bottom wall of the fitting part (11) is located on the side of the top wall (142) of the vehicle body (1) near the center of the vehicle body (1). The fitting part (11), a part of the top wall (142), and the shell (21) of the drone hangar (2) together define the cabin (22) of the drone hangar (2).

14. The vehicle (100) according to claim 13, characterized in that, The depth of the fitting part (11) is h, wherein h satisfies: 10mm≤h≤30mm.

15. The vehicle (100) according to claim 13 or 14, characterized in that, The bottom wall of the fitting part (11) extends downward along the vehicle body (1) from front to back.

16. The vehicle (100) according to claim 15, characterized in that, The inclination angle of the bottom wall of the fitting part (11) is α, and α satisfies: 1°≤α≤3°.

17. The vehicle (100) according to any one of claims 13, 14 and 16, characterized in that, The fitting part (11) is formed by the downward indentation of the top wall (142) of the vehicle body (1).

18. The vehicle (100) according to claim 13, characterized in that, At least one wire hole (12) is formed on the top wall (142) of the vehicle body (1).

19. The vehicle (100) according to any one of claims 13, 14, 16 and 18, characterized in that, Multiple support beams (13) are provided on the side of the top wall (142) of the vehicle body (1) near the center of the vehicle body (1).

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