Vehicle-mounted unmanned aerial vehicle garage and vehicle

Abstract

The utility model discloses a vehicle-mounted unmanned aerial vehicle garage and a vehicle. The vehicle-mounted unmanned aerial vehicle garage comprises an unmanned aerial vehicle garage body, the top cover assembly comprises a top cover, a sunken platform is arranged on the top cover, and at least part of the unmanned aerial vehicle garage is embedded in the sunken platform and fixedly connected with the top cover. The structure does not depend on a top cover luggage rack, mounting points are flexibly arranged, and therefore the Y-direction size of the unmanned aerial vehicle garage is reduced to the maximum extent. Meanwhile, the top cover sinks locally to form the sinking platform, the Z-direction installation height of the unmanned aerial vehicle garage can be greatly reduced, and therefore the height of the whole vehicle is reduced, the windward area of a vehicle body is reduced, wind resistance is reduced, energy consumption is reduced, and the trafficability of the vehicle is improved. The smaller unmanned aerial vehicle garage is arranged on the roof, so that the appearance is more harmonious and more attractive.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned vehicle garage technical field especially is involved in a kind of vehicle-mounted unmanned vehicle garage and vehicle. BACKGROUND

[0002] The existing top cover unmanned vehicle garage mounting structure is mostly fixed on the roof rack of the vehicle body top cover, and the unmanned vehicle garage is fixedly connected with the roof rack, which leads to high overall height, increases the wind area of the vehicle, improves the wind resistance, and further improves the energy consumption, while reducing the vehicle passability. SUMMARY

[0003] The utility model aims at at least one of the technical problems existing in prior art is solved.For this purpose, the utility model provides a vehicle-mounted unmanned vehicle garage, which is directly installed on the top cover by locally sinking the top cover of the vehicle body, so that the unmanned vehicle garage and the top cover of the vehicle body form a unified whole, which reduces the wind resistance and further reduces the energy consumption, while improving the vehicle passability.

[0004] The utility model further provides a vehicle.

[0005] According to the vehicle-mounted unmanned vehicle garage of the first aspect embodiment of the utility model, the unmanned vehicle garage is directly installed on the top cover by locally sinking the top cover of the vehicle body, so that the unmanned vehicle garage and the top cover of the vehicle body form a unified whole, which reduces the wind resistance and further reduces the energy consumption, while improving the vehicle passability.

[0006] According to the vehicle-mounted unmanned vehicle garage of the utility model embodiment, the structure does not depend on the roof rack, and the mounting point is arranged flexibly, so that the Y-direction size of the unmanned vehicle garage is minimized.Meanwhile, the sinking table is formed by locally sinking the top cover, which can greatly reduce the Z-direction installation height of the unmanned vehicle garage, thereby reducing the overall height of the vehicle, reducing the wind area of the vehicle body, reducing the wind resistance, and further reducing the energy consumption, improving the vehicle passability.In addition, the smaller unmanned vehicle garage is on the roof, which is more coordinated and beautiful in appearance.

[0007] According to some embodiments of the utility model, the top cover assembly further comprises: a first top cover cross beam arranged on the inner side of the top cover and located at the front end of the sinking table; and a second top cover cross beam arranged on the inner side of the top cover and located at the rear end of the sinking table.

[0008] According to some embodiments of the utility model, the top cover assembly further comprises: two top cover longitudinal beams arranged in parallel and spaced apart on the inner side of the top cover and located on the left and right sides of the sinking table, the front ends of the two top cover longitudinal beams are connected with the first top cover cross beam and extend backward, the two ends of the second top cover cross beam are connected with the two top cover longitudinal beams, and the first top cover cross beam, the second top cover cross beam and the two top cover longitudinal beams form a frame structure to surround the outer circumferential side of the sinking table.

[0009] According to some embodiments of the utility model, the first roof crossbeam, the second roof crossbeam and two roof longitudinal beams are respectively provided with a plurality of mounting holes, and further comprising: a plurality of connecting components, a plurality of connecting components correspond to a plurality of mounting holes one by one, and the roof assembly is fixedly connected with the unmanned vehicle garage through cooperation of the connecting components and the mounting holes.

[0010] According to some embodiments of the utility model, the connecting component comprises a bolt and a nut, the nut is embedded in the unmanned vehicle garage, and the bolt is connected with the nut through the mounting hole and the roof.

[0011] According to some embodiments of the utility model, the roof longitudinal beam comprises a first bottom plate, a first side plate, two sides of the first bottom plate are respectively connected with the first side plate, two first side plates are bent in the same direction relative to the first bottom plate, and one end of the first side plate away from the first bottom plate is provided with a first flange, and two first side plates are fixedly connected with the roof through the first flange.

[0012] According to some embodiments of the utility model, the rear end of the roof longitudinal beam extends rearward for connecting with a D column inner panel assembly of a vehicle.

[0013] According to some embodiments of the utility model, the position of the first roof crossbeam is opposite to the position of a C column of a vehicle, and the roof assembly further comprises a connecting plate, one end of the connecting plate is connected with two ends of the first roof crossbeam respectively, and the other end of the connecting plate is used for connecting a side wall assembly of a vehicle.

[0014] According to some embodiments of the utility model, the first roof crossbeam and the second roof crossbeam both comprise a second bottom plate, a second side plate, two sides of the second bottom plate are respectively connected with the second side plate, two second side plates are bent in the same direction relative to the second bottom plate, one end of the second side plate away from the second bottom plate is provided with a second flange, and two second side plates are fixedly connected with the roof through the second flange.

[0015] According to some embodiments of the utility model, the rear end of the second roof crossbeam is provided with a plurality of downward protruding bosses, and the roof assembly further comprises a roof rear crossbeam, and the second roof crossbeam is fixedly connected with the roof rear crossbeam through a plurality of bosses.

[0016] According to some embodiments of the utility model, the roof assembly further comprises a third roof crossbeam, which is arranged on the inner side of the roof assembly and located at the front end of the first roof crossbeam, and the front part of the unmanned vehicle garage is fixedly connected with the third roof crossbeam and the roof.

[0017] According to some embodiments of the present application, the sealing member is arranged between the UAV garage and the top cover.

[0018] According to some embodiments of the present application, the bottom surface of the sunken platform is formed with a plurality of reinforcing ribs, which are arranged transversely and longitudinally.

[0019] According to some embodiments of the present application, the front part of the bottom surface of the sunken platform is lower than the rear part, and the front part of the bottom surface of the sunken platform is provided with a drainage hole.

[0020] According to some embodiments of the present application, the front end position of the sunken platform is opposite to the C-pillar position of the vehicle, and the rear end position of the sunken platform is opposite to the D-pillar position of the vehicle.

[0021] According to the vehicle of the second aspect of the present application, the vehicle-mounted UAV garage is included.

[0022] Additional aspects and advantages of the present application will be in part apparent and in part pointed out hereinafter. BRIEF DESCRIPTION OF DRAWINGS

[0023] The above and / or additional aspects and advantages of the present application will become apparent and be readily appreciated from the following description, including the appended drawings.

[0024] Figure 1 is a schematic view of the appearance of the vehicle-mounted UAV garage according to the embodiments of the present application;

[0025] Figure 2 is Figure 1 is a schematic view of the cross section at A-A in FIG.

[0026] Figure 3 is Figure 2 is an enlarged schematic view of C in FIG.

[0027] Figure 4 is Figure 2 is an enlarged schematic view of D in FIG.

[0028] Figure 5 is Figure 2 is an enlarged schematic view of E in FIG.

[0029] Figure 6 is Figure 1 is a schematic view of the cross section at B-B in FIG.

[0030] Figure 7 is Figure 6 is an enlarged schematic view of F in FIG.

[0031] Figure 8 is an inner side surface schematic of a roof assembly according to an embodiment of the present utility model Figure 1 ;

[0032] Figure 9 is an inner side surface schematic of a roof assembly according to an embodiment of the present utility model Figure 2 .

[0033] Reference signs:

[0034] 1, unmanned aircraft hangar; 10, hangar shell; 2, roof assembly; 20, roof; 2001, sunken platform; 2002, reinforcing rib; 2003, drain hole; 21, first roof cross beam; 2101, second bottom plate; 2102, second side plate; 2103, second flange; 22, second roof cross beam; 2201, boss; 23, roof longitudinal beam; 2301, first bottom plate; 2302, first side plate; 2303, first flange; 24, mounting hole; 25, connecting assembly; 2501, bolt; 2502, nut; 2503, sealing gasket; 26, connecting plate; 27, roof rear cross beam; 2701, roof rear cross beam lower plate; 2702, roof rear cross beam upper plate; 28, third roof cross beam; 29, force transmission channel; 30, D-column inner plate upper section; 4, sealing element. DETAILED DESCRIPTION

[0035] The embodiments of the present utility model are described in detail below, and the embodiments described with reference to the drawings are exemplary, and the embodiments of the present utility model are described in detail below.

[0036] The embodiments of the present utility model are described in detail below, and the embodiments described with reference to the drawings are exemplary, and the embodiments of the present utility model are described in detail below. Figures 1-9 The vehicle-mounted unmanned aircraft hangar according to the embodiments of the present utility model is described below with reference to the drawings.

[0037] As shown in Figures 1-2 , the vehicle-mounted unmanned aircraft hangar comprises: an unmanned aircraft hangar 1 and a roof assembly 2, and the roof assembly 2 comprises: a roof 20, and the roof 20 is provided with a sunken platform 2001, and at least part of the unmanned aircraft hangar 1 is embedded in the sunken platform 2001 and fixedly connected with the roof 20.

[0038] Specifically, the unmanned aircraft hangar 1 is installed on the roof 20 of the vehicle, and the installation point can be flexibly designed according to the size of the unmanned aircraft, so as to minimize the Y-direction size of the unmanned aircraft. Furthermore, the sunken platform 2001 is formed by locally sinking the roof 20, and the unmanned aircraft hangar 1 is partially embedded in the sunken platform 2001 of the roof 20, so as to minimize the Z-direction size of the whole vehicle.

[0039] As shown in Figure 2As shown, the sinking amount h1 can be flexibly set according to different top cover 20 shapes, internal man-machine requirements, and in the present example, the sinking amount h1 is 40 mm. The reduction of the size of the unmanned garage 1 can effectively reduce the wind area of the whole vehicle, thereby reducing the wind resistance of the whole vehicle and reducing the energy consumption per 100 kilometers. At the same time, the reduction of the Z-direction size of the whole vehicle can effectively improve the passability of the vehicle.

[0040] According to the vehicle-mounted unmanned garage of the utility model, the structure does not rely on the luggage rack of the top cover 20, flexibly arranges the mounting point, thereby minimizing the Y-direction size of the unmanned garage 1. At the same time, the local sinking of the top cover 20 forms the sunken table 2001, which can greatly reduce the Z-direction installation height of the unmanned garage 1, thereby reducing the height of the whole vehicle, reducing the wind area of the vehicle body, reducing the wind resistance, and further reducing the energy consumption and improving the passability of the vehicle. In addition, the smaller unmanned garage 1 on the roof makes the appearance more coordinated and more beautiful.

[0041] According to some embodiments of the utility model, the top cover assembly 2 further comprises: a first top cover cross beam 21 and a second top cover cross beam 22, the first top cover cross beam 21 is arranged on the inner side of the top cover 20 and located at the front end of the sunken table 2001; the second top cover cross beam 22 is arranged on the inner side of the top cover 20 and located at the rear end of the sunken table 2001.

[0042] Referring to Figure 2 , Figure 8 and Figure 9 , the first top cover cross beam 21 and the second top cover cross beam 22 are arranged around the front end and the rear end of the sunken table 2001, which improves the structural strength and rigidity of the top cover 20 and at the same time improves the static pressure of the top cover 20, and specifically improves the structural strength and rigidity of the sunken table 2001, thereby providing a strong bearing structure for installing the unmanned garage 1.

[0043] According to some embodiments of the utility model, the top cover assembly 2 further comprises: two top cover longitudinal beams 23, the two top cover longitudinal beams 23 are arranged in parallel and spaced apart on the inner side of the top cover 20 and located on the left and right sides of the sunken table 2001, the front end of the two top cover longitudinal beams 23 is connected with the first top cover cross beam 21 and extends backward, the two ends of the second top cover cross beam 22 are connected with the two top cover longitudinal beams 23, and the first top cover cross beam 21, the second top cover cross beam 22 and the two top cover longitudinal beams 23 form a frame structure to surround the outer circumferential side of the sunken table 2001.

[0044] Referring to Figure 2 , Figure 8 and Figure 9As shown, the first roof cross beam 21, the second roof cross beam 22 and the two roof longitudinal beams 23 are welded with each other to form a frame structure of a "mouth" type, and the frame structure of the "mouth" type and the roof 20 are welded to form a closed cavity of the "mouth" type, thereby effectively improving the strength of the roof assembly 2 and further improving the reliability of the unmanned aerial vehicle garage 1.

[0045] According to some embodiments of the present application, a plurality of mounting holes 24 are arranged on the first roof cross beam 21, the second roof cross beam 22 and the two roof longitudinal beams 23 respectively.

[0046] Specifically, referring to Figures 2-7 As shown, a plurality of mounting holes 24 are arranged on the first roof cross beam 21, the second roof cross beam 22 and the two roof longitudinal beams 23 respectively, that is, a plurality of mounting points are arranged in the X direction and the Y direction of the roof 20, compared with the prior art in which the mounting points are all arranged on the roof luggage rack and only two rows of mounting points in the X direction can be designed, the unmanned aerial vehicle garage 1 of the present application is more balanced in stress, thereby realizing reliable installation of the unmanned aerial vehicle garage 1.

[0047] In an example, the connecting assembly 25 comprises a bolt 2501 and a nut 2502, the nut 2502 is embedded in the unmanned aerial vehicle garage 1, and the bolt 2501 is arranged through the mounting hole 24 and the roof 20 and connected with the nut 2502.

[0048] Specifically, referring to Figures 3-5 、 Figure 7 As shown, the nut 2502 is embedded in the unmanned aerial vehicle garage 1, and the roof 20 is also provided with a corresponding hole structure, and the bolt 2501 is arranged through the mounting hole 24 and the hole structure on the roof 20 and fixedly connected with the nut 2502 of the unmanned aerial vehicle garage 1. At the same time, in order to prevent water leakage at the mounting point, the nut 2502 on the unmanned aerial vehicle garage 1 is provided with a sealing gasket 2503.

[0049] In the present example, a plurality of mounting holes 24 are arranged on the cavity structure of the "mouth" type, a total of twenty-two, and the unmanned aerial vehicle is fixed on the roof assembly 2 by the bolt 2501, which is the main force bearing structure of the roof 20 and the unmanned aerial vehicle garage 1.

[0050] According to some embodiments of the present invention, the top cover longitudinal beam 23 includes: a first bottom plate 2301 and a first side plate 2302, the two sides of the first bottom plate 2301 are respectively connected to the first side plates 2302, the two first side plates 2302 are bent in the same direction relative to the first bottom plate 2301, and a first flange 2303 is provided at one end of the first side plate 2302 away from the first bottom plate 2301, and the two first side plates 2302 are respectively fixedly connected to the top cover 20 through the first flange 2303.

[0051] See Figure 7 As shown, the top cover longitudinal beam 23 is in a "J"-shaped structure, and the top cover longitudinal beam 23 is fixedly connected to the top cover 20 through a first flange 2303 to form a "mouth"-shaped closed cavity, further improving the structural strength and rigidity of the top cover assembly 2.

[0052] According to some embodiments of the present invention, the rear end of the roof longitudinal beam 23 extends rearward for connection with the D-pillar inner panel assembly of the vehicle.

[0053] With this arrangement, the rear end of the roof rail 23 extends rearward to connect with the D-pillar inner panel assembly. From the perspective of the entire vehicle, the connection between the roof rail 23 and the D-pillar adds a force transmission path for the roof 20, thereby improving the vehicle's torsional rigidity and the static pressure of the roof 20. Specifically, the rear end of the roof rail 23 is welded to the upper sections 30 of the D-pillar inner panels on both sides.

[0054] According to some embodiments of the present invention, the position of the first roof cross beam 21 is opposite to the C-pillar of the vehicle; the roof assembly 2 also includes: a connecting plate 26, and the two ends of the first roof cross beam 21 are respectively connected to one end of the connecting plate 26, and the other end of the connecting plate 26 is used to connect to the side assembly of the vehicle.

[0055] Reference Figure 9 As shown, the first roof cross member 21 is located in front of the sunken platform 2001 of the roof 20, near the C-pillar, and is connected to the left and right side panel assemblies via connecting plates 26. From the perspective of the entire vehicle, the first roof cross member 21 and the C-pillar form a C-ring, adding a force transmission path for the roof 20, thereby improving the vehicle's torsional rigidity and the static pressure of the roof 20.

[0056] According to some embodiments of the present invention, the first top cover cross beam 21 and the second top cover cross beam 22 both include: a second base plate 2101; a second side plate 2102, the two sides of the second base plate 2101 are respectively connected to the second side plates 2102, the two second side plates 2102 are bent in the same direction relative to the second base plate 2101, and a second flange 2103 is provided at one end of the second side plate 2102 away from the second base plate 2101, and the two second side plates 2102 are respectively fixedly connected to the top cover 20 through the second flange 2103.

[0057] Reference Figures 2-5As shown, the first roof crossbeam 21 and the second roof crossbeam 22 are both in the shape of a Chinese character 'jia', the first roof crossbeam 21 and the second roof crossbeam 22 are fixedly connected with the roof 20 through the first flange 2303 to form a closed cavity in the shape of a Chinese character 'kou', further improving the structural strength and rigidity of the roof assembly 2.

[0058] According to some embodiments of the present application, the rear end of the second roof crossbeam 22 is provided with a plurality of downward protruding bosses 2201; the roof assembly 2 further comprises: a roof rear crossbeam 27, and the second roof crossbeam 22 is fixedly connected with the roof rear crossbeam 27 through the plurality of bosses 2201.

[0059] Referring to Figure 9 As shown, the second roof crossbeam 22 is located at the rear end of the outer periphery of the sunken platform 2001, the rear side of the second roof crossbeam 22 is designed with three bosses 2201, and is welded with the roof rear crossbeam 27 lower plate and the roof rear crossbeam 27 upper plate of the roof rear crossbeam 27 to improve the Z-direction rigidity of the second roof crossbeam 22.

[0060] According to some embodiments of the present application, the roof assembly 2 further comprises: a third roof crossbeam 28, the third roof crossbeam 28 is arranged on the inner side of the roof assembly 2 and located at the front end of the first roof crossbeam 21, and the front part of the UAV hangar 1 is fixedly connected with the third roof crossbeam 28 and the roof 20.

[0061] In this way, the third roof crossbeam 28 is designed at the front part of the UAV hangar 1, which mainly serves to fix the hangar shell 10 of the UAV hangar 1. Figure 9 As shown, the third roof crossbeam 28 is also provided with mounting holes 24 like the first roof crossbeam 21 and the second roof crossbeam 22, and the UAV hangar 1 mounting point is embedded with a nut 2502, and the front part of the UAV hangar 1 is fixed through a bolt 2501.

[0062] According to some embodiments of the present application, further comprising: a sealing element 4, the UAV hangar 1 and the roof 20 are gap-fitted, and the peripheral side between the UAV hangar 1 and the roof 20 is provided with the sealing element 4.

[0063] Specifically, referring to Figure 3 As shown, a circle of sealing elements 4 is added to the peripheral side position between the hangar shell 10 of the UAV hangar 1 and the roof 20, so that the UAV hangar 1 and the roof 20 of the vehicle form a closed whole, eliminating the aerodynamic lift of the UAV hangar 1 and improving the vehicle handling.

[0064] In one example, seal 4 can be made of sealing foam or rubber. The main functions of seal 4 are: 1. Sealing and corrosion prevention: It prevents air from entering between the drone hangar 1 and the top cover 20 during high-speed driving, thereby generating aerodynamic lift. It also prevents large amounts of water from entering, which increases the corrosion resistance of the top cover 20 and the drone hangar 1. 2. Avoiding abnormal noise: Under harsh operating conditions, the gap between the drone hangar 1 and the top cover 20 will change. The hangar shell 10 and the top cover 20 are both made of hard materials. If the gap becomes smaller, the two may collide and produce abnormal noise. Adding seal 4 can slow down the reduction of the gap between the two and prevent the two from directly colliding and producing abnormal noise.

[0065] According to some embodiments of the present invention, a plurality of reinforcing ribs 2002 are formed on the bottom surface of the sink 2001 , and the plurality of reinforcing ribs 2002 are arranged in a transversely spaced manner and extend longitudinally.

[0066] Reference Figure 9 As shown, longitudinal reinforcing ribs 2002 are designed on the bottom surface of the sinking platform 2001 , and the rear ends of the reinforcing ribs 2002 can extend to the second cross beam 13 of the top cover 20 to strengthen the bottom surface rigidity of the sinking platform 2001 .

[0067] According to some embodiments of the present invention, the front bottom portion of the sinking platform 2001 is lower than the rear bottom portion, and a drainage hole 2003 is provided on the front bottom portion of the sinking platform 2001 .

[0068] Reference Figure 2 and Figure 4 As shown, the front of the bottom of the sink 2001 is slightly lower than the back. Drain holes 2003 can be added on both sides of the front of the bottom. The position of the drainage holes 2003 should be the lowest point of the entire bottom surface. A local small sink 2001 can also be designed to facilitate drainage.

[0069] According to some embodiments of the present invention, the front end of the sunken platform 2001 is opposite to the C-pillar of the vehicle, and the rear end of the sunken platform 2001 is opposite to the D-pillar of the vehicle.

[0070] See Figure 1 and Figure 8 As shown, a large sunken platform 2001 is designed in the middle of the rear of the roof 20, roughly between the C-pillar and the D-pillar, to serve as the main installation space for the drone hangar 1. The specific size of the sunken platform 2001 can be determined based on the shape of the roof 20 and the headroom requirements in the rear seats.

[0071] The vehicle according to the second embodiment of the present utility model includes an on-board drone hangar.

[0072] Compared with the existing technology, the vehicle-mounted drone library of this utility model has the following effects:

[0073] First, the unmanned aerial vehicle warehouse 1 is installed on the roof assembly 2, the roof 20 adopts a semi-submersible structure, which can minimize the size of the unmanned aerial vehicle warehouse 1. The existing structure of the unmanned aerial vehicle warehouse is installed on the luggage rack on both sides of the roof, and the position of the luggage rack determines that the Y-direction size of the unmanned aerial vehicle warehouse 1 is close to the width of the vehicle. The structure of the present application installs the unmanned aerial vehicle warehouse 1 on the sheet metal of the roof 20, and can flexibly design the installation point according to the size of the unmanned aerial vehicle, thereby minimizing the Y-direction size of the unmanned aerial vehicle. At the same time, the roof 20 is partially sunken to form a sunken table 2001, and the unmanned aerial vehicle warehouse 1 is partially embedded in the roof 20, which can minimize the Z-direction size of the whole vehicle. The reduction of the size of the unmanned aerial vehicle warehouse 1 can effectively reduce the wind area of the whole vehicle, thereby reducing the wind resistance of the whole vehicle and reducing the energy consumption per 100 kilometers. At the same time, the reduction of the Z-direction size of the whole vehicle can also effectively improve the passability of the vehicle.

[0074] Second, the roof assembly 2 and the unmanned aerial vehicle warehouse 1 are designed as a whole closed type, which eliminates the aerodynamic lift of the unmanned aerial vehicle warehouse 1 and improves the vehicle handling. The existing structure adopts a split design of the vehicle body and the unmanned aerial vehicle warehouse 1, and there is a gap between the unmanned aerial vehicle warehouse 1 and the roof 20. During high-speed driving, high-speed airflow is generated in the gap, and the unmanned aerial vehicle warehouse 1 generates aerodynamic lift F, thereby reducing the vehicle handling. The present application adopts a whole closed design of the unmanned aerial vehicle warehouse 1 and the roof assembly 2, and a sealing element 4 is added to the matching position of the warehouse shell 10 of the unmanned aerial vehicle warehouse 1 and the roof 20, so that the unmanned aerial vehicle warehouse 1 and the vehicle body form a closed whole, avoiding the defect of the existing structure that the airflow generates aerodynamic lift, and improving the vehicle handling.

[0075] Third, the unmanned aerial vehicle warehouse 1 installation structure is designed as part of the vehicle body structure, which improves the strength of the roof 20 and the static pressure of the roof 20. The existing structure of the unmanned aerial vehicle warehouse 1 is installed on the roof luggage rack, which is independent of the vehicle body structure and cannot improve the strength of the vehicle body structure. The unmanned aerial vehicle installation structure of the present application is located inside the roof 20, which is welded by two roof longitudinal beams 23, a first roof cross beam 21 and a second roof cross beam 22 to form a "mouth" type frame structure. The "mouth" type frame structure and the roof 20 form a "mouth" type closed cavity through welding, which effectively improves the strength of the roof assembly 2. At the same time, the "mouth" type structure is welded with the side wall assembly and the roof rear cross beam 27 assembly to form a whole, thereby increasing a C ring and a D ring force transmission channel 29, and further improving the static pressure of the roof 20. Therefore, the structure of the present application not only provides the installation point of the unmanned aerial vehicle warehouse 1, but also improves the strength of the vehicle body.

[0076] Fourth, the "mouth" type unmanned aerial vehicle installation structure can design multiple installation points in X and Y directions at the same time, and the force of the unmanned aerial vehicle warehouse 1 is more balanced. The existing structure of the installation point is on the roof luggage rack, which can only design two rows of installation points in X direction and no installation point in Y direction, and the force of the unmanned aerial vehicle is not balanced. The "mouth" type unmanned aerial vehicle installation structure of the present application can design multiple installation points in X and Y directions at the same time, and the force of the unmanned aerial vehicle warehouse 1 is more balanced.

[0077] In the description of the present application, it should be understood that the orientation or positional relationship indicated by the terms "center", "longitudinal", "transverse", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", "axial", "radial", "circumferential" and the like are based on the orientation or positional relationship shown in the drawings, and are only for the purpose of facilitating the description of the present application and simplifying the description, and therefore cannot be understood as indicating or implying that the device or element 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.

[0078] In the description of the present application, the description of the terms "one embodiment", "some embodiments", "illustrative 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 illustrative description of the above terms does not necessarily refer to the same embodiment or example.

[0079] Although the embodiments of the present application have been shown and described, those skilled 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 present application, and the scope of the present application is defined by the claims and their equivalents.

Claims

1. A vehicle-mounted drone hangar, characterized in that: include: drone library; The top cover assembly includes: a top cover, on which a concave sunken platform is provided, at least part of the drone hangar is embedded in the sunken platform and fixedly connected to the top cover.

2. The vehicle-mounted drone hangar according to claim 1, characterized in that: The top cover assembly further includes: a first roof crossbeam, arranged on the inner side of the roof and located at the front end of the sinking platform; The second top cover cross beam is arranged on the inner side surface of the top cover and located at the rear end of the sinking platform.

3. The vehicle-mounted drone hangar according to claim 2, characterized in that: The top cover assembly further includes: Two roof cover longitudinal beams are arranged in parallel on the inner side of the roof and on the left and right sides of the sinking platform. The front ends of the two roof cover longitudinal beams are connected to the first roof cover cross beam and extend backward. The two ends of the second roof cover cross beam are connected to the two roof cover longitudinal beams. The first roof cover cross beam, the second roof cover cross beam and the two roof cover longitudinal beams form a frame structure to be arranged around the outer periphery of the sinking platform.

4. The vehicle-mounted drone hangar according to claim 3, characterized in that: The first roof cross beam, the second roof cross beam and the two roof longitudinal beams are respectively provided with a plurality of mounting holes; and It also includes: multiple connecting components, the multiple connecting components correspond one-to-one to the multiple mounting holes, and the top cover assembly is fixedly connected to the drone hangar through the cooperation of the connecting components and the mounting holes.

5. The vehicle-mounted drone hangar according to claim 4, characterized in that: The connecting assembly includes: a bolt and a nut, the nut is embedded in the drone hangar, and the bolt passes through the mounting hole and the top cover is connected to the nut.

6. The vehicle-mounted drone hangar according to claim 3, characterized in that: The roof longitudinal beam comprises: First base plate; A first side panel, both sides of the first bottom panel are respectively connected to the first side panels, the two first side panels are bent in the same direction relative to the first bottom panel, a first flange is provided at one end of the first side panel away from the first bottom panel, and the two first side panels are respectively fixedly connected to the top cover through the first flange.

7. The vehicle-mounted drone hangar according to claim 3, characterized in that: The rear end of the roof longitudinal beam extends rearward and is used to be connected to the D-pillar inner panel assembly of the vehicle.

8. The vehicle-mounted drone hangar according to claim 2, characterized in that: The position of the first roof cross beam is opposite to the C-pillar of the vehicle; the roof assembly also includes: a connecting plate, the two ends of the first roof cross beam are respectively connected to one end of the connecting plate, and the other end of the connecting plate is used to connect to the side assembly of the vehicle.

9. The vehicle-mounted drone hangar according to claim 2, characterized in that: The first roof crossbeam and the second roof crossbeam each include: Second base plate; The second side panel, both sides of the second bottom panel are respectively connected to the second side panels, the two second side panels are bent in the same direction relative to the second bottom panel, and a second flange is provided at one end of the second side panel away from the second bottom panel, and the two second side panels are respectively fixedly connected to the top cover through the second flange.

10. The vehicle-mounted drone hangar according to claim 2, characterized in that: The rear end of the second roof crossbeam is provided with a plurality of downwardly protruding bosses; the roof assembly further comprises: a roof rear crossbeam, and the second roof crossbeam is fixedly connected to the roof rear crossbeam via the plurality of bosses.

11. The vehicle-mounted drone hangar according to claim 2, characterized in that: The roof assembly also includes: a third roof beam, which is arranged on the inner side of the roof assembly and located at the front end of the first roof beam, and the front of the drone hangar is fixedly connected to the third roof beam and the roof.

12. The vehicle-mounted drone hangar according to claim 1, characterized in that: Also includes: A sealing member is provided, wherein the drone hangar is fitted with the top cover in a clearance manner, and the sealing member is provided on the peripheral side between the drone hangar and the top cover.

13. The vehicle-mounted drone hangar according to claim 1, characterized in that: A plurality of reinforcing ribs are formed on the bottom surface of the sinking platform, and the plurality of reinforcing ribs are arranged at intervals in the transverse direction and extend in the longitudinal direction.

14. The vehicle-mounted drone hangar according to claim 1, characterized in that: The front portion of the bottom of the sinking platform is lower than the rear portion, and the front portion of the bottom of the sinking platform is provided with a drainage hole.

15. The vehicle-mounted drone hangar according to claim 1, characterized in that: The front end of the sunken platform is opposite to the C-pillar of the vehicle, and the rear end of the sunken platform is opposite to the D-pillar of the vehicle.

16. A vehicle, characterized in that: A vehicle-mounted drone hangar comprising any one of claims 1-15.

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