Vehicle-mounted unmanned aerial vehicle cabin and vehicle

Abstract

The invention discloses a vehicle-mounted unmanned aerial vehicle cabin and a vehicle, the vehicle-mounted unmanned aerial vehicle cabin comprises a shell, the shell comprises an outer shell and an inner plate, the inner plate is located below the outer shell, a drainage channel is formed between the inner plate and the outer shell, the inner plate is provided with a drainage port communicated with the drainage channel, and the outer shell is provided with an air inlet opposite to the drainage channel; the air inlet assembly is located at the air inlet and connected with the shell. According to the vehicle-mounted unmanned aerial vehicle cabin, liquid entering through the air inlet can flow into the drainage channel and is drained out of the vehicle-mounted unmanned aerial vehicle cabin through the drainage opening of the drainage channel, and therefore the liquid is prevented from invading the internal structure of the vehicle-mounted unmanned aerial vehicle cabin. Meanwhile, the air inlet assembly is located at the air inlet and connected with the shell, so that the air inlet assembly prevents part of liquid from invading the internal structure of the vehicle-mounted unmanned aerial vehicle cabin through the air inlet, and the vehicle-mounted unmanned aerial vehicle cabin better gives consideration to the waterproof performance and the heat dissipation capacity.

Description

Technical Field

[0001] The present invention relates to the technical field of vehicles, and in particular to a vehicle-mounted unmanned aerial vehicle cabin and a vehicle. Background Art

[0002] As a mobile platform for carrying drones, the cabin of a vehicle-mounted drone requires a better heat dissipation system to meet the heat dissipation requirements of the cabin's internal structure. However, the cabin of a vehicle-mounted drone in the prior art mainly focuses on the optimization of heat dissipation performance, but fails to fully consider waterproof performance, resulting in the risk of liquid infiltration into the cabin when the cabin of a vehicle-mounted drone faces natural water environments such as rain, ice and snow, and daily car washing. Summary of the invention

[0003] The present invention aims to solve at least one of the technical problems existing in the prior art. To this end, the present invention proposes a vehicle-mounted UAV cabin, which better balances waterproof performance and heat dissipation capacity.

[0004] The present invention also provides a vehicle, comprising the above-mentioned vehicle-mounted UAV cabin.

[0005] According to an embodiment of the present invention, a cabin of a vehicle-mounted UAV includes: a shell, the shell includes an outer shell and an inner plate, the inner plate is located below the outer shell and a drainage channel is formed between the inner plate and the outer shell, the inner plate has a drainage port connected to the drainage channel, and the outer shell has an air inlet arranged opposite to the drainage channel; an air inlet assembly, the air inlet assembly is located at the air inlet and connected to the outer shell.

[0006] According to the vehicle-mounted drone cabin of the embodiment of the present invention, the shell includes an outer shell and an inner plate, the inner plate is located below the outer shell and a drainage channel is formed between the inner plate and the outer shell, the inner plate has a drainage port connected to the drainage channel, and the outer shell has an air inlet arranged opposite to the drainage channel, so that the liquid entering through the air inlet can flow into the drainage channel and be discharged to the outside of the vehicle-mounted drone cabin through the drainage port of the drainage channel, thereby preventing liquid from invading the internal structure of the vehicle-mounted drone cabin, so that the vehicle-mounted drone cabin can avoid water intrusion into the internal structure of the vehicle-mounted drone cabin while ensuring heat dissipation. At the same time, the air inlet component is located at the air inlet and connected to the shell, so that the air inlet component blocks part of the liquid from invading the internal structure of the vehicle-mounted drone cabin through the air inlet, so that the vehicle-mounted drone cabin can better balance waterproof performance and heat dissipation capabilities.

[0007] In some embodiments of the present invention, the housing includes a shell body and an inclined portion arranged around the shell body, the inclined portion is inclined downward at one end away from the shell body, and the air inlet is arranged on the inclined portion.

[0008] In some embodiments of the present invention, the air inlet assembly includes a plurality of first grille bars, and the plurality of first grille bars are arranged at intervals.

[0009] In some embodiments of the present invention, a plurality of the first grid bars are arranged in a vertical direction, and in a projection on a horizontal plane, two adjacent first grid bars have an overlapping area.

[0010] In some embodiments of the present invention, the size of the overlapping area is ≤15 mm.

[0011] In some embodiments of the present invention, the first grid bar includes a first section, a second section and a third section, the first section is located above the third section, and both ends of the second section in the length direction are respectively connected to an end of the first section close to the third section and an end of the third section close to the first section, and in the projection on the horizontal plane, the third section of the first grid bar located above one of two adjacent first grid bars has an overlapping area with the first section of the first grid bar located below.

[0012] In some embodiments of the present invention, one end of the first segment connected to the second segment and one end of the third segment away from the second segment are inclined downward, and the second segment is arranged horizontally.

[0013] In some embodiments of the present invention, the air inlet assembly further includes a mounting frame, the plurality of the first grille bars are located in the mounting frame and connected to the mounting frame, and the mounting frame is detachably connected to the housing.

[0014] In some embodiments of the present invention, the air inlet assembly also includes a second grille bar, which is located above the first grille bar at the top and is spaced apart, one end of the second grille bar in the width direction is connected to the mounting frame and the other end is tilted downward, and in projection on the horizontal plane, the second grille bar and the first grille bar at the top have an overlapping area.

[0015] In some embodiments of the present invention, the air inlet assembly also includes: a baffle, which extends in a ring shape along the circumferential direction of the mounting frame, and is located below the mounting frame and connected to the mounting frame; a filter, which is connected to the baffle and is located on the side of the first grille bar facing the inner plate, and is used to seal the space inside the baffle and filter the fluid in the drainage channel entering through the air inlet.

[0016] In some embodiments of the present invention, the inner peripheral wall of the baffle has a first extension portion extending toward the inner plate, and the filter screen is connected to the first extension portion.

[0017] In some embodiments of the present invention, a groove is provided on the inclined portion, the air inlet passes through the bottom wall of the groove, and the air inlet assembly is disposed in the groove.

[0018] In some embodiments of the present invention, foam is further included, and the foam is arranged between the air inlet assembly and the bottom wall of the groove.

[0019] In some embodiments of the present invention, the air inlets are multiple and spaced apart along the circumferential direction of the inclined portion, and the air inlet assemblies are multiple and correspond one-to-one to the multiple air inlets.

[0020] In some embodiments of the present invention, along the circumferential direction of the inclined portion, the downward inclination angles of one end of the inclined portion away from the shell body are the same or different.

[0021] In some embodiments of the present invention, the air inlet includes a first air inlet, a second air inlet and a third air inlet, the first air inlet and the second air inlet are spaced apart along a first direction, the first air inlet and the third air inlet are spaced apart along a third direction, the areas of the inclined portion having the first air inlet and the second air inlet are inclined downward at the same angle away from one end of the shell body, and the area of ​​the inclined portion having the third air inlet is inclined downward at a greater angle than the area of ​​the inclined portion having the first air inlet from one end of the shell body.

[0022] In some embodiments of the present invention, the inclined portion has a first lifting hole, the inner panel has a second lifting hole opposite to the first lifting hole, and the vehicle-mounted UAV cabin also includes: a blocking cover, which is arranged at the first lifting hole and is detachably connected to the outer shell, for blocking the first lifting hole.

[0023] In some embodiments of the present invention, the upper side wall of the first hanging hole has a first protrusion, and the first protrusion is located on the side of the blocking cover facing the inner plate.

[0024] In some embodiments of the present invention, the surface of the first protrusion facing the blocking cover includes a first sub-segment and a second sub-segment, the first sub-segment is located on a side of the second sub-segment close to the fixed end of the first protrusion, the end of the first sub-segment connected to the second sub-segment is inclined downward, and the end of the second sub-segment away from the first sub-segment is inclined downward, and the inclination angle of the second sub-segment is smaller than that of the first sub-segment.

[0025] In some embodiments of the present invention, the inner wall of the second hanging hole has a second extension portion extending toward the center of the second hanging hole and toward the outer shell, and the second extension portion is annular around the second hanging hole in a circumferential direction.

[0026] In some embodiments of the present invention, the aperture size of the second hanging hole is smaller than the aperture size of the first hanging hole, and the end of the second extension portion close to the center of the second hanging hole is closer to the center of the first hanging hole than the end of the first protrusion close to the center of the first hanging hole.

[0027] In some embodiments of the present invention, the surface of the inner plate facing the shell has a stop portion extending toward the shell, the stop portion is located above the second lifting hole and extends along the circumferential direction of the second lifting hole, along the radial direction of the second lifting hole, the stop portion is located radially outside the second extension portion, and along the radial direction of the first lifting hole, the stop portion is located radially outside the first protrusion.

[0028] In some embodiments of the present invention, the lower end of the blocking cover is clamped on a side of the lower side wall of the first hanging hole facing the inner plate.

[0029] In some embodiments of the present invention, the housing has a hatch, and the vehicle-mounted UAV cabin further includes a hatch assembly, and the hatch assembly is used to open or close the hatch.

[0030] In some embodiments of the present invention, a first sealing strip is provided between the door assembly and the outer shell, and the first sealing strip is provided on the door assembly and extends along a circumferential direction of the door assembly.

[0031] In some embodiments of the present invention, the outer shell has a drainage groove, which is open on top and surrounds the hatch, and the drainage groove is located below the first sealing strip and the hatch assembly. The drainage groove has a water outlet, and the water outlet is connected to the drainage channel.

[0032] In some embodiments of the present invention, the hatch assembly includes a first hatch and a second hatch arranged along a first direction, the first hatch and the second hatch are movable in directions toward and away from each other to open or close the hatch, and a second sealing strip is provided between the first hatch and the second hatch, and the second sealing strip is provided on the first hatch to seal the gap between the first hatch and the second hatch when the hatch is closed.

[0033] In some embodiments of the present invention, one end of the second hatch facing the first hatch has a third extension portion extending toward the first hatch, a portion of the third extension portion is located below the first hatch and has a water receiving trough open toward the first hatch, when the hatch is closed, the water receiving trough is located below the second sealing strip and the first hatch, and the water receiving trough is connected to the drainage trough.

[0034] A vehicle according to an embodiment of the present invention includes the above-mentioned vehicle-mounted UAV cabin.

[0035] According to the vehicle of the embodiment of the present invention, a vehicle-mounted drone cabin is provided, and the housing includes an outer shell and an inner plate, the inner plate is located below the outer shell and a drainage channel is formed between the inner plate and the outer shell, the inner plate has a drainage port connected to the drainage channel, and the outer shell has an air inlet arranged opposite to the drainage channel, so that the liquid entering through the air inlet can flow into the drainage channel and be discharged to the outside of the vehicle-mounted drone cabin through the drainage port of the drainage channel, thereby preventing liquid from invading the internal structure of the vehicle-mounted drone cabin, so that the vehicle-mounted drone cabin can avoid water ingress while ensuring heat dissipation. At the same time, the air inlet component is located at the air inlet and connected to the outer shell, so that the air inlet component blocks part of the liquid from invading the internal structure of the vehicle-mounted drone cabin through the air inlet, so that the vehicle-mounted drone cabin can better balance waterproof performance and heat dissipation capacity.

[0036] Additional aspects and advantages of the present invention will be given in part in the following description and in part will be obvious from the following description, or will be learned through practice of the present invention. BRIEF DESCRIPTION OF THE DRAWINGS

[0037] The above and / or additional aspects and advantages of the present invention will become apparent and easily understood from the description of the embodiments in conjunction with the following drawings, in which:

[0038] Figure 1 is a structural diagram of a cabin of a vehicle-mounted UAV according to an embodiment of the present invention;

[0039] Figure 2 is a top view of a cabin of a vehicle-mounted UAV according to an embodiment of the present invention;

[0040] Figure 3 is a partial structural diagram of a cabin of a vehicle-mounted UAV according to an embodiment of the present invention, wherein a first cabin door, an air inlet assembly and a plug cover are not shown;

[0041] Figure 4 is a top view of a housing according to an embodiment of the present invention;

[0042] Figure 5 is along Figure 2 Sectional view along line AA;

[0043] Figure 6 yes Figure 5 The enlarged view of the H in the middle;

[0044] Figure 7 yes Figure 5 Flow diagram of

[0045] Figure 8 is along Figure 2 Sectional view along the midline BB;

[0046] Fig. 9 is along Figure 2 Sectional view of the mid-CC line;

[0047] Fig.10 yes Fig. 9 Enlarged view of G in the middle;

[0048] Fig.11 is along Figure 2 Sectional view along the mid-DD line;

[0049] Fig.12 is along Figure 2 Sectional view along line EE;

[0050] Fig.13 is along Figure 4 Cross-sectional view along line FF.

[0051] Reference numerals:

[0052] 100. Vehicle-mounted drone cabin;

[0053] 1. Shell; 11. Shell; 111. Shell body; 1111. Hatch; 1112. Drainage groove; 1113. Water outlet; 112. Inclined portion; 1121. Air inlet; 1121a. First air outlet; 1121b. Second air outlet; 1121c. Third air outlet; 1122. Groove; 1123. First hanging hole; 1124. First protrusion; 1125. First subsection; 1126. Second subsection; 12. Inner plate; 121. Drainage outlet; 122. Second hanging hole; 123. Second extension; 124. Stopper; 13. Drainage channel;

[0054] 2. Air inlet assembly; 21. First grille bar; 211. First section; 212. Second section; 213. Third section; 22. Mounting frame; 23. Second grille bar; 24. Baffle; 241. First extension; 2411. Second protrusion; 242. Fourth extension; 25. Filter; 26. Foam;

[0055] 3. Block the cover;

[0056] 4. Hatch door assembly; 41. First sealing strip; 42. First hatch; 421. Second sealing strip; 422. Second slot; 43. Second hatch; 431. Third extension; 4311. Water receiving trough; 44. First slot. DETAILED DESCRIPTION

[0057] Embodiments of the present invention are described in detail below, examples of which are shown in the accompanying drawings, wherein the same or similar reference numerals throughout represent the same or similar elements or elements having the same or similar functions. The embodiments described below with reference to the accompanying drawings are exemplary and are only used to explain the present invention, and cannot be understood as limiting the present invention.

[0058] In the description of the present invention, it should be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside", "clockwise", "counterclockwise", "axial", "radial", "circumferential" and the like indicate positions or positional relationships based on the positions or positional relationships shown in the accompanying drawings, and are only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation on the present invention. In addition, features defined as "first" and "second" may explicitly or implicitly include one or more of the features. In the description of the present invention, unless otherwise specified, "multiple" means two or more.

[0059] In the description of the present invention, it should be noted that, unless otherwise clearly specified and limited, the terms "installed", "connected", and "connected" should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be indirectly connected through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.

[0060] The following describes a vehicle-mounted drone cabin 100 according to an embodiment of the present invention with reference to the accompanying drawings.

[0061] like Figure 1-Figure 5 , Figure 7 , Figure 8 and Fig.13 As shown, a vehicle-mounted UAV cabin 100 according to an embodiment of the present invention includes a shell 1 and an air intake assembly 2.

[0062] The shell 1 includes an outer shell 11 and an inner plate 12. The inner plate 12 is located below the outer shell 11 and a drainage channel 13 is formed between the inner plate 12 and the outer shell 11. The inner plate 12 has a drainage port 121 connected to the drainage channel 13. The outer shell 11 has an air inlet 1121 arranged opposite to the drainage channel 13.

[0063] It is understandable that the interior of the vehicle-mounted drone cabin 100 is connected to the external environment through the air inlet 1121, so that the external air can enter the interior of the vehicle-mounted drone cabin 100 through the air inlet 1121, or the heat inside the vehicle-mounted drone cabin 100 is dissipated through the air inlet 1121, thereby ensuring the heat dissipation of the internal structure of the vehicle-mounted drone cabin 100 and improving the overall reliability. At the same time, the air inlet 1121 is arranged relative to the drainage channel 13, so that the liquid entering through the air inlet 1121 can flow to the drainage channel 13 and be discharged to the outside of the vehicle-mounted drone cabin 100 through the drainage port 121 of the drainage channel 13, thereby preventing the liquid from invading the internal structure of the vehicle-mounted drone cabin 100 and achieving the waterproofing of the vehicle-mounted drone cabin 100. Therefore, through such a structure, the vehicle-mounted drone cabin 100 can ensure heat dissipation while preventing water from entering the internal structure of the vehicle-mounted drone cabin 100, so that the vehicle-mounted drone cabin 100 can take into account both waterproof performance and heat dissipation capacity.

[0064] The air inlet assembly 2 is located at the air inlet 1121 and is connected to the housing 11. Thus, the air inlet assembly 2 effectively blocks debris from entering the interior of the vehicle-mounted drone cabin 100 through the air inlet 1121, thereby effectively protecting the internal structure of the vehicle-mounted drone cabin 100 and improving overall reliability and safety. At the same time, the air inlet assembly 2 can block some liquids from invading the internal structure of the vehicle-mounted drone cabin 100 through the air inlet 1121, reducing the amount of liquid entering the vehicle-mounted drone cabin 100, thereby improving the waterproof performance of the vehicle-mounted drone cabin 100, so that the vehicle-mounted drone cabin 100 can better balance waterproof performance and heat dissipation capacity.

[0065] Furthermore, the drain port 121 is located at the lowest point of the drain channel 13. Thus, such an arrangement ensures that the liquid accumulated in the drain channel 13 can be smoothly discharged from the drain port 121, thereby avoiding liquid retention and backflow, and improving reliability.

[0066] In some embodiments, Figure 5 , Figure 7 , Figure 8 and Fig.13 As shown, the outer peripheral wall of the outer shell 11 exceeds the outer peripheral wall of the inner plate 12, and the outer peripheral wall of the outer shell 11 and the outer peripheral wall of the inner plate 12 form a drainage port 121, and the drainage port 121 is a plurality of drainage ports 121 spaced apart along the circumferential direction of the outer shell 11. Thus, through such an arrangement, the liquid in the drainage channel 13 can be discharged from the outer periphery of the vehicle-mounted drone cabin 100, further ensuring the waterproof performance of the vehicle-mounted drone cabin 100.

[0067] According to the vehicle-mounted drone cabin 100 of the embodiment of the present invention, the housing 1 includes an outer shell 11 and an inner plate 12, the inner plate 12 is located below the outer shell 11 and a drainage channel 13 is formed between the inner plate 12 and the outer shell 11, the inner plate 12 has a drainage port 121 connected to the drainage channel 13, and the outer shell 11 has an air inlet 1121 arranged opposite to the drainage channel 13, so that the liquid entering through the air inlet 1121 can flow into the drainage channel 13 and be discharged to the outside of the vehicle-mounted drone cabin 100 through the drainage port 121 of the drainage channel 13, thereby preventing the liquid from invading the internal structure of the vehicle-mounted drone cabin 100, so that the vehicle-mounted drone cabin 100 can prevent water from entering the internal structure of the vehicle-mounted drone cabin 100 while ensuring heat dissipation. At the same time, the air inlet component 2 is located at the air inlet 1121 and connected to the outer shell 11, so that the air inlet component 2 blocks part of the liquid from invading the internal structure of the vehicle-mounted drone cabin 100 through the air inlet 1121, so that the vehicle-mounted drone cabin 100 can better balance the waterproof performance and heat dissipation capacity.

[0068] In some embodiments of the present invention, Figure 2-Figure 6 As shown, the housing 11 includes a housing body 111 and an inclined portion 112 arranged around the housing body 111, the end of the inclined portion 112 away from the housing body 111 is inclined downward, and the air inlet 1121 is arranged on the inclined portion 112. It can be understood that when liquid falls on the inclined portion 112, the end of the inclined portion 112 away from the housing body 111 is inclined downward to guide the liquid, and the liquid will flow downward along the inclined portion 112, avoiding the accumulation of liquid around the air inlet 1121 and reducing the direct splashing of rainwater into the air inlet 1121, thereby reducing the intrusion of rainwater into the internal structure of the vehicle-mounted drone cabin 100 through the air inlet 1121, and improving the waterproof performance of the vehicle-mounted drone cabin 100.

[0069] In some embodiments of the present invention, Figure 2-Figure 8 As shown, the air inlet assembly 2 includes a plurality of first grille bars 21, and the plurality of first grille bars 21 are arranged at intervals. Thus, through such an arrangement, an air inlet is formed between any two adjacent first grille bars 21, and the interior of the vehicle-mounted drone cabin 100 is connected to the external environment through the air inlet. At the same time, the plurality of first grille bars 21 prevent debris and liquid from entering the interior of the vehicle-mounted drone cabin 100, thereby improving overall reliability and safety.

[0070] In some embodiments of the present invention, Figure 2-Figure 8As shown, a plurality of first grille bars 21 are arranged in the vertical direction, and in the projection on the horizontal plane, two adjacent first grille bars 21 have an overlapping area. Thus, through such an arrangement, two adjacent first grille bars 21 have an overlapping area to form a water retaining structure located in the air inlet 1121. When the liquid flows downward along the inclined portion 112 to the air inlet assembly 2, the water retaining structure formed by the overlapping area of ​​the two adjacent first grille bars 21 can effectively prevent the liquid from invading the internal structure of the vehicle-mounted UAV cabin 100, so that the liquid flows along the water retaining structure formed by the overlapping area of ​​the two adjacent first grille bars 21 to the drainage channel 13, thereby improving the waterproof performance of the air inlet assembly 2, so that the vehicle-mounted UAV cabin 100 can better balance the waterproof performance and heat dissipation capacity.

[0071] Specifically, the side of the lower first grille bar 21 close to the shell body and the side of the upper first grille bar 21 away from the shell body have an overlapping area. Thus, the water blocking effect of the air inlet assembly 2 is further ensured by such an arrangement.

[0072] It should be noted that the arrangement direction of the plurality of first grid bars 21 is not limited thereto, and may also be arranged along the circumferential direction of the inclined portion 112. At the same time, when the plurality of first grid bars 21 are arranged along the up-down direction, in the projection on the horizontal plane, two adjacent first grid bars 21 may not have overlapping areas, thereby increasing the air intake of the air inlet 1121 and improving the heat dissipation effect.

[0073] In some embodiments of the present invention, the size of the overlapped area is ≤15 mm. Thus, by limiting the upper limit of the size of the overlapped area, it is possible to ensure that the overlapped area of ​​two adjacent first grille bars 21 forms a water retaining structure located in the air inlet 1121, while ensuring that the airflow flows smoothly between the two adjacent first grille bars 21, thereby improving the overall reliability.

[0074] In some embodiments of the present invention, Figure 5 As shown, the first grid bar 21 includes a first section 211, a second section 212 and a third section 213. The first section 211 is located above the third section 213. Both ends of the second section 212 in the length direction are respectively connected to an end of the first section 211 close to the third section 213 and an end of the third section 213 close to the first section 211. In the projection on the horizontal plane, the third section 213 of the first grid bar 21 located above one of the two adjacent first grid bars 21 has an overlapping area with the first section 211 of the first grid bar 21 located below.

[0075] Thus, in the projection on the horizontal plane, the third section 213 of the first grille bar 21 located above the two adjacent first grille bars 21 and the first section 211 of the first grille bar 21 located below have an overlapping area, so that the first section 211 of the first grille bar 21 located below the two adjacent first grille bars 21 forms a water retaining structure located in the air inlet 1121. When the liquid flows downward along the inclined portion 112 to the air inlet assembly 2, the first section 211 of the first grille bar 21 located below the two adjacent first grille bars 21 can effectively prevent the liquid from invading the internal structure of the vehicle-mounted UAV cabin 100, so that the liquid flowing between the first section 211 of the two adjacent first grille bars 21 flows to the first section 211 through the second section 212 of the first grille bar 21 located below the two adjacent first grille bars 21, and flows along the length direction of the first section 211 to the drainage channel 13 for discharge, thereby ensuring the waterproof performance of the air inlet assembly 2.

[0076] In some embodiments of the present invention, Figure 5 As shown, the end of the first section 211 connected to the second section 212 and the end of the third section 213 away from the second section 212 are tilted downward, and the second section 212 is arranged horizontally. It can be understood that since the end of the inclined portion 112 away from the shell body 111 is tilted downward, the end of the first section 211 connected to the second section 212 and the end of the third section 213 away from the second section 212 are tilted downward and the second section 212 is arranged horizontally, liquid splashing is effectively reduced, and liquid is further prevented from entering the cabin 100 of the vehicle-mounted drone.

[0077] In some embodiments of the present invention, Figure 2-Figure 6 As shown, the air inlet assembly 2 further includes a mounting frame 22 , a plurality of first grille bars 21 are located in the mounting frame 22 and connected to the mounting frame 22 , and the mounting frame 22 is detachably connected to the housing 11 .

[0078] Thus, the air inlet assembly 2 is connected to the housing 11 by the detachable connection between the mounting frame 22 and the housing 11, thereby ensuring a reliable connection between the air inlet assembly 2 and the housing 11, and further ensuring the waterproof and ventilation effects of the air inlet assembly 2. At the same time, the mounting frame 22 effectively protects the plurality of first grille bars 21 located in the mounting frame 22, effectively preventing the first grille bars 21 from being deformed or damaged due to external forces, thereby ensuring the waterproof and ventilation effects of the plurality of first grille bars 21. In addition, the detachable connection between the mounting frame 22 and the housing 11 makes the installation and disassembly process between the mounting frame 22 and the housing 11 simpler and faster, thereby improving the disassembly efficiency.

[0079] In some embodiments of the present invention, Figure 2-Figure 6As shown, the air inlet assembly 2 also includes a second grille bar 23, which is located above the top first grille bar 21 and is spaced apart. One end of the second grille bar 23 in the width direction is connected to the mounting frame 22 and the other end is tilted downward. In the projection on the horizontal plane, the second grille bar 23 and the top first grille bar 21 have an overlapping area.

[0080] It can be understood that when the liquid flows downward along the inclined portion 112, one end of the second grille bar 23 in the width direction is connected to the mounting frame 22 and the other end is inclined downward, so that the liquid flows downward through the mounting frame 22 and the second grille bar 23 to the first grille bar 21 in sequence. In the projection on the horizontal plane, the second grille bar 23 and the first grille bar 21 located at the top have an overlapping area, so that the part of the overlapping area formed by the first grille bar 21 forms a water retaining structure in the air inlet 1121, thereby effectively blocking the liquid from entering the vehicle-mounted drone cabin 100, and further improving the waterproof performance of the air inlet component 2.

[0081] It should be noted that if Figure 5-Figure 7 As shown, the plurality of first grid bars 21 are arranged in the up-down direction, and the first grid bar 21 located at the top can be understood as the first grid bar 21 located at the top among the plurality of first grid bars 21 .

[0082] In some embodiments of the present invention, Figure 2-Figure 6 As shown, the air inlet assembly 2 further includes a baffle 24 and a filter 25. The baffle 24 extends in a ring shape along the circumferential direction of the mounting frame 22, the baffle 24 is located below the mounting frame 22 and connected to the mounting frame 22, and the filter 25 is connected to the baffle 24 and is located on the side of the first grid bar 21 facing the inner plate 12, and is used to block the space inside the baffle 24 and filter the fluid in the drainage channel 13 entering from the air inlet 1121.

[0083] Thus, the baffle 24 extends in a ring shape along the circumferential direction of the mounting frame 22, effectively preventing the liquid entering the air inlet 1121 from invading the internal structure of the vehicle-mounted drone cabin 100, and the liquid entering the air inlet 1121 flows into the drainage channel 13 and is discharged from the vehicle-mounted drone cabin 100, further improving the waterproof performance of the air inlet assembly 2. At the same time, the filter 25 is connected to the baffle 24 and is located on the side of the first grid bar 21 facing the inner plate 12, which is used to block the space inside the baffle 24, so that the filter 25 can form a deceleration effect on the liquid hitting the filter 25 while ensuring that the interior of the vehicle-mounted drone cabin 100 is connected to the external environment, so that the liquid can be collected at the filter 25 and penetrate downward to the inner plate 12 and flow along the upper surface of the inner plate 12 to the drainage port 121 for discharge, effectively preventing the liquid from splashing into the internal structure of the vehicle-mounted drone cabin 100. In addition, the filter 25 filters the fluid in the drainage channel 13 entering the air inlet 1121, effectively filtering the fluid entering the drainage channel 13, and improving the overall reliability.

[0084] Specifically, since the end of the inclined portion 112 away from the shell body 111 is inclined downward, the first grille bar 21, the second grille bar 23 and the mounting frame 22 can effectively prevent the liquid falling from the top to the air inlet assembly 2 and the liquid flowing downward along the inclined portion 112 to the air inlet assembly 2 from invading the internal structure of the vehicle-mounted UAV cabin 100. At the same time, the baffle 24 can effectively prevent part of the liquid flowing toward the air inlet assembly 2 that is close to the horizontal plane (for example: when the vehicle using the vehicle-mounted UAV cabin 100 is cleaned, the water gun sprays water toward the vehicle-mounted UAV cabin 100 from an angle close to the horizontal plane), and the rest of the liquid hits the filter 25, and the filter 25 forms a deceleration effect on the liquid, so that the liquid can be collected at the filter 25 and penetrate downward to the inner plate 12 and flow along the upper surface of the inner plate 12 to the drain port 121 for discharge. Thus, the air inlet assembly 2 blocks the liquid entering the air inlet 1121 at all angles from invading the internal structure of the vehicle-mounted UAV cabin 100 , thereby effectively ensuring the waterproof performance of the vehicle-mounted UAV cabin 100 .

[0085] It should be noted that the shape of the baffle 24 is not limited thereto. For example, the baffle 24 may also include a plurality of baffles spaced apart along the circumferential direction of the mounting frame 22 .

[0086] In some embodiments of the present invention, Figure 2-Figure 6 As shown, the inner peripheral wall of the baffle 24 has a first extension portion 241 extending toward the inner plate 12, and the filter 25 is connected to the first extension portion 241. Thus, the filter 25 is fixed by such a setting, and the space inside the baffle 24 is ensured, the ventilation and waterproof effects of the filter 25 are improved, and the overall reliability is improved.

[0087] In some embodiments of the present invention, Figure 2-Figure 6As shown, a groove 1122 is provided on the inclined portion 112, an air inlet 1121 penetrates the bottom wall of the groove 1122, an air inlet assembly 2 is provided in the groove 1122, and a foam 26 is provided between the air inlet assembly 2 and the bottom wall of the groove 1122. Thus, the liquid entering between the air inlet assembly 2 and the groove 1122 is first absorbed by the foam 26, so that the foam 26 plays a buffering role, and when the foam 26 absorbs the liquid and gradually reaches a saturated state, the liquid will slowly leak onto the inner plate 12 and flow along the upper surface of the inner plate 12 to the drain port 121 for discharge, thereby effectively preventing the liquid from splashing into the internal structure of the vehicle-mounted UAV cabin 100. At the same time, the foam 26 can be disassembled, which is convenient for the maintenance and disassembly of the air inlet assembly 2.

[0088] Further, a foam 26 is provided between the air inlet assembly 2 and the baffle 24 of the groove 1122, the inner peripheral wall of the baffle 24 has a first extension portion 241 and a fourth extension portion 242 extending toward the inner plate 12, the first extension portion 241 and the fourth extension portion 242 are spaced apart, the fourth extension portion 242 is located between the foam 26 and the first extension portion 241, the free end of the fourth extension portion 242 abuts against the bottom wall of the groove 1122, the free end of the first extension portion 241 has a second protrusion 2411 extending toward the center direction of the air inlet 1121, and the filter 25 is located below the second protrusion 2411 and connected to the second protrusion 2411. Thus, the position of the foam 26 is further limited by the fourth extension portion 242 to ensure the reliability of the foam 26, and the filter 25 is fixed by the second protrusion 2411.

[0089] In some embodiments, a groove 1122 is provided on the inclined portion 112, and the air inlet 1121 passes through the bottom wall of the groove 1122. The air inlet assembly 2 is arranged in the groove 1122, and the air inlet assembly 2 and the bottom wall of the groove 1122 are connected by a sealant. Thus, through such a setting, the air inlet assembly 2 is fixed at the air inlet 1121, ensuring that the air intake and waterproof effects of the air inlet assembly 2 are reliable.

[0090] In some embodiments of the present invention, Figure 1-Figure 8 As shown, the air inlets 1121 are multiple and spaced apart in the circumferential direction of the inclined portion 112, and the air inlet components 2 are multiple and correspond one-to-one to the multiple air inlets 1121. Thus, through such a setting, the interior of the vehicle-mounted drone cabin 100 is connected to the external environment through the multiple air inlets 1121, further improving the heat dissipation effect of the internal structure of the vehicle-mounted drone cabin 100. At the same time, by having multiple air inlet components 2 corresponding one-to-one to the multiple air inlets 1121, each air inlet 1121 is provided with a corresponding air inlet component 2, thereby improving the reliability of the vehicle-mounted drone cabin 100.

[0091] In some embodiments of the present invention, Figure 1-Figure 8As shown, along the circumferential direction of the inclined portion 112, the downward inclination angle of the end of the inclined portion 112 away from the shell body 111 is the same or different. It can be understood that, along the circumferential direction of the inclined portion 112, when the downward inclination angle of the end of the inclined portion 112 away from the shell body 111 is the same, the design and manufacture of the inclined portion 112 and multiple air inlet components 2 can be simplified, the grille has universality, reduces costs, and improves production efficiency. Along the circumferential direction of the inclined portion 112, when the downward inclination angle of the end of the inclined portion 112 away from the shell body 111 is different, by adjusting the inclination angle of different inclined portion 112 areas, the airflow path is optimized, so that the gas is more efficiently discharged into the vehicle-mounted drone cabin 100, and the heat dissipation performance of the vehicle-mounted drone cabin 100 is further improved. Therefore, the downward inclination angle of the end of the inclined portion 112 away from the shell body 111 can be set according to the vehicle model of the vehicle-mounted drone cabin 100, thereby improving the universality of the vehicle-mounted drone cabin 100.

[0092] In some embodiments of the present invention, Figure 1-Figure 8 As shown, the air inlet 1121 includes a first air inlet 1121a, a second air inlet 1121b and a third air inlet 1121c, the first air inlet 1121a and the second air inlet 1121b are spaced apart along a first direction, the first air inlet 1121a and the third air inlet 1121c are spaced apart along a third direction, the area of ​​the inclined portion 112 having the first air inlet 1121a and the second air inlet 1121b is tilted downward at the same angle from one end of the shell body 111, and the area of ​​the inclined portion 112 having the third air inlet 1121c is tilted downward at a greater angle than the area of ​​the inclined portion 112 having the first air inlet 1121a and the third air inlet 1121c.

[0093] Therefore, through such a setting, the fluid flow rate entering the vehicle-mounted drone cabin 100 through the third air port 1121c is greater than the fluid flow rate entering the vehicle-mounted drone cabin 100 through the first air port 1121a, and the fluid flow rate entering the vehicle-mounted drone cabin 100 through the third air port 1121c is greater than the fluid flow rate entering the vehicle-mounted drone cabin 100 through the second air port 1121b, thereby effectively ensuring the heat dissipation effect inside the vehicle-mounted drone cabin 100.

[0094] In some embodiments of the present invention, Figure 1-Figure 4 , Fig. 9 and Fig.10 As shown, the inclined portion 112 has a first hanging hole 1123, the inner plate 12 has a second hanging hole 122 opposite to the first hanging hole 1123, and the vehicle-mounted UAV cabin 100 further includes a blocking cover 3. The blocking cover 3 is disposed at the first hanging hole 1123 and is detachably connected to the outer shell 11 to block the first hanging hole 1123.

[0095] It is understandable that, during the transportation of the vehicle-mounted UAV cabin 100, the first lifting hole 1123 and the second lifting hole 122 are set, so that the lifting tools (such as lifting rings, slings, etc.) are penetrated through the first lifting hole 1123 and the second lifting hole 122, thereby realizing the transportation of the vehicle-mounted UAV cabin 100, and the setting of the first lifting hole 1123 and the second lifting hole 122 ensures the stability and safety during the transportation process, and avoids the damage of the vehicle-mounted UAV cabin 100 caused by improper transportation. At the same time, the plugging cover 3 is set at the first lifting hole 1123 to block the first lifting hole 1123, thereby effectively blocking debris and liquid from entering the vehicle-mounted UAV cabin 100 from the first lifting hole 1123, and ensuring the sealing performance of the vehicle-mounted UAV cabin 100. In addition, the plugging cover 3 is detachably connected to the shell 11, and during the transportation of the vehicle-mounted UAV cabin 100, it is convenient for the plugging cover 3 to open or block the first lifting hole 1123, thereby improving the assembly efficiency.

[0096] In some embodiments, Figure 1-Figure 4 , Fig. 9 and Fig.10 As shown, there are multiple first lifting holes 1123, and the multiple first lifting holes 1123 are spaced along the first direction and the second direction respectively, the second lifting holes 122 are multiple corresponding to the first lifting holes 1123, and the plug cover 3 is multiple corresponding to the first lifting holes 1123, wherein the first direction, the second direction and the up-down direction are perpendicular to each other. Therefore, during the transportation of the vehicle-mounted UAV cabin 100, such a setting further ensures the stability and safety of the transportation process, and avoids damage to the vehicle-mounted UAV cabin 100 caused by improper transportation.

[0097] It should be noted that when the vehicle-mounted drone cabin 100 is applied to a vehicle, the first direction can be the front and rear direction of the vehicle, in which case the second direction is the left and right direction of the vehicle; or, the first direction can be the left and right direction of the vehicle, in which case the second direction is the front and rear direction of the vehicle.

[0098] In some embodiments of the present invention, Fig. 9 and Fig.10As shown, the upper side wall of the first hanging hole 1123 has a first protrusion 1124, and the first protrusion 1124 is located on the side of the plug cover 3 facing the inner plate 12. It can be understood that since the inclined portion 112 is inclined downwardly away from the end of the shell body 111, the liquid leaking from the upper gap between the first hanging hole 1123 and the plug cover 3 first flows to the first protrusion 1124 and flows downwardly along the first protrusion 1124 to the inner plate 12, and flows along the upper surface of the inner plate 12 to the drain port 121 for discharge, so that the first protrusion 1124 blocks the liquid entering between the first hanging hole 1123 and the plug cover 3 from flowing upward or splashing to the internal structure of the vehicle-mounted drone cabin 100, thereby ensuring the waterproof performance of the vehicle-mounted drone cabin 100. At the same time, when the vehicle in which the vehicle-mounted drone cabin 100 is used is tilted at a certain angle to the road surface, the setting of the first protrusion 1124 can still effectively block the liquid from flowing upward or splashing onto the internal structure of the vehicle-mounted drone cabin 100, so that the vehicle-mounted drone cabin 100 has a certain adaptability to the road surface and ensures a waterproof effect.

[0099] In some embodiments of the present invention, Fig. 9 and Fig.10 As shown, the surface of the first protrusion 1124 facing the blocking cover 3 includes a first sub-segment 1125 and a second sub-segment 1126, the first sub-segment 1125 is located on the side of the second sub-segment 1126 close to the fixed end of the first protrusion 1124, the end of the first sub-segment 1125 connected to the second sub-segment 1126 is inclined downward, and the end of the second sub-segment 1126 away from the first sub-segment 1125 is inclined downward, and the inclination angle is smaller than that of the first sub-segment 1125.

[0100] It can be understood that since the inclined portion 112 is inclined downward at one end away from the shell body 111, the inclination angle of the second sub-segment 1126 is smaller than that of the first sub-segment 1125, so that the liquid leaking from the upper gap between the first lifting hole 1123 and the plugging cover 3 can first flow to the first sub-segment 1125 according to the planned path, and flow along the inclined surface of the first sub-segment 1125 to the second sub-segment 1126, and then flow along the inclined surface of the second sub-segment 1126 to the inner plate 12, effectively ensuring that the first protrusion 1124 blocks the liquid entering between the first lifting hole 1123 and the plugging cover 3 from flowing upward or splashing onto the internal structure of the vehicle-mounted drone cabin 100. At the same time, when the vehicle in which the vehicle-mounted UAV cabin 100 is used is driving at a certain angle to the road surface, the end connected to the second sub-segment 1126 by the first sub-segment 1125 tilts downward, and the end of the second sub-segment 1126 away from the first sub-segment 1125 tilts downward, and the inclination angle is smaller than that of the first sub-segment 1125, thereby ensuring that the liquid leaking from the upper gap between the first lifting hole 1123 and the plugging cover 3 flows along the planned path, thereby ensuring that the waterproof performance is effective.

[0101] In some embodiments of the present invention, Fig. 9and Fig.10 As shown, the lower end of the plug cover 3 is clamped to the side of the lower side wall of the first hanging hole 1123 facing the inner plate 12. Thus, the plug cover 3 is detachably connected to the outer shell 11 through such a setting, and during the transportation of the vehicle-mounted UAV cabin 100, it is convenient for the plug cover 3 to open or block the first hanging hole 1123, thereby improving assembly efficiency.

[0102] In some embodiments of the present invention, Fig. 9 and Fig.10 As shown, the inner wall of the second hanging hole 122 has a second extension portion 123 extending toward the center direction of the second hanging hole 122 and toward the housing 11, and the second extension portion 123 is annular around the second hanging hole 122 in the circumferential direction. Therefore, the liquid leaking from the gap between the first hanging hole 1123 and the plugging cover 3 can flow downward along the second extension portion 123 to the inner plate 12, and flow along the upper surface of the inner plate 12 to the drain port 121 for discharge, preventing the liquid from invading the internal structure of the vehicle-mounted drone cabin 100, thereby ensuring the waterproof performance of the vehicle-mounted drone cabin 100.

[0103] In some embodiments of the present invention, Fig. 9 and Fig.10 As shown, the aperture size of the second hanging hole 122 is smaller than the aperture size of the first hanging hole 1123, and the end of the second extension portion 123 close to the center of the second hanging hole 122 is closer to the center of the first hanging hole 1123 than the end of the first protrusion 1124 close to the center of the first hanging hole 1123. Thus, through such an arrangement, the liquid leaking from the gap between the first hanging hole 1123 and the plugging cover 3 flows along the first protrusion 1124 to the second extension portion 123, thereby effectively preventing the liquid from invading the internal structure of the vehicle-mounted drone cabin 100.

[0104] In some embodiments of the present invention, Fig. 9 and Fig.10 As shown, the surface of the inner plate 12 facing the shell 1 has a stopper 124 extending toward the shell 1, and the stopper 124 is located above the second hoisting hole 122 and extends along the circumferential direction of the second hoisting hole 122. It can be understood that since the end of the inclined portion 112 away from the shell body 111 is inclined downward, the stopper 124 effectively blocks the liquid leaking from the upper gap between the first hoisting hole 1123 and the plugging cover 3 from flowing or splashing to the internal structure of the vehicle-mounted drone cabin 100, thereby ensuring the waterproof performance of the vehicle-mounted drone cabin 100.

[0105] In the radial direction of the second hanging hole 122, the stopper 124 is located radially outside the second extension 123, and in the radial direction of the first hanging hole 1123, the stopper 124 is located radially outside the first protrusion 1124. Thus, through such an arrangement, the stopper 124 can effectively prevent the liquid leaking from the gap between the first hanging hole 1123 and the plugging cover 3 from flowing along the first protrusion 1124 to the second extension 123 and invading the internal structure of the vehicle-mounted UAV cabin 100, thereby improving the waterproof effect.

[0106] In some embodiments, Fig. 9 and Fig.10 As shown, the upper side wall of the first lifting hole 1123 has a first protrusion 1124, and the first protrusion 1124 is located on the side of the plugging cover 3 facing the inner plate 12. The surface of the first protrusion 1124 facing the plugging cover 3 includes a first sub-segment 1125 and a second sub-segment 1126. The first sub-segment 1125 is located on the side of the second sub-segment 1126 close to the fixed end of the first protrusion 1124, and the end of the first sub-segment 1125 connected to the second sub-segment 1126 is inclined downward, and the end of the second sub-segment 1126 away from the first sub-segment 1125 is inclined downward, and the inclination angle is smaller than that of the first sub-segment 1125. The inner wall of the second hanging hole 122 has a second extension portion 123 extending toward the center direction of the second hanging hole 122 and toward the outer shell 11. The second extension portion 123 is annular in the circumferential direction of the second hanging hole 122. The second extension portion 123 is located below the first protrusion 1124. The surface of the inner plate 12 facing the shell 1 has a stop portion 124 extending toward the shell 1. The stop portion 124 is located above the second hanging hole 122 and extends along the circumferential direction of the second hanging hole 122.

[0107] As a result, the liquid leaking from the upper gap between the first lifting hole 1123 and the plugging cover 3 first flows to the first sub-segment 1125, and flows along the inclined surface of the first sub-segment 1125 to the second sub-segment 1126, and then flows along the inclined surface of the second sub-segment 1126 to the second extension portion 123, and flows downward along the second extension portion 123 to the drain port 121 for discharge. At the same time, the setting of the stop portion 124 prevents the liquid flowing downward along the second extension portion 123 from invading the internal structure of the vehicle-mounted UAV cabin 100, thereby effectively ensuring the waterproof performance of the vehicle-mounted UAV cabin 100.

[0108] In some embodiments of the present invention, Figure 1-Figure 4 and Fig.11As shown, the housing 11 has a hatch 1111, and the vehicle-mounted UAV cabin 100 further includes a hatch assembly 4, which is used to open or close the hatch 1111. Thus, when the hatch 1111 is opened by the hatch assembly 4, the UAV is docked with the internal structure of the vehicle-mounted UAV cabin 100. At the same time, when the UAV is not in the cabin, the hatch 1111 is closed by the hatch assembly 4, thereby ensuring the sealing of the hatch 1111 to protect the equipment in the cabin from interference from the external environment.

[0109] In some embodiments of the present invention, Fig.11 As shown, there is a first sealing strip 41 between the door assembly 4 and the shell 11, and the first sealing strip 41 is provided on the door assembly 4 and extends along the circumferential direction of the door assembly 4. Thus, the gap between the door assembly 4 and the shell 11 is sealed by the first sealing strip 41, thereby preventing liquid from entering the vehicle-mounted UAV cabin 100 from the gap between the door assembly 4 and the shell 11, thereby ensuring the waterproof sealing performance of the vehicle-mounted UAV cabin 100.

[0110] Furthermore, the hatch assembly 4 has a first card slot 44, which extends along the circumferential direction of the hatch assembly 4. The first sealing strip 41 is clamped in the first card slot 44. When the hatch assembly 4 closes the hatch 1111, the first sealing strip 41 abuts against the housing 11. Thus, the first sealing strip 41 is fixed and the sealing effect of the first sealing strip 41 is ensured through such an arrangement.

[0111] In some embodiments of the present invention, Figure 1-Figure 4 , Fig.11 and Fig.13 As shown, the housing 11 has a drainage groove 1112, the upper part of the drainage groove 1112 is open and surrounds the hatch 1111, the drainage groove 1112 is located below the first sealing strip 41 and the hatch assembly 4, and the drainage groove 1112 has a water outlet 1113, and the water outlet 1113 is connected to the drainage channel 13. Therefore, through such an arrangement, the liquid that penetrates from the gap between the first sealing strip 41 and the hatch assembly 4 and the gap between the first sealing strip 41 and the housing 11 flows to the drainage groove 1112, flows into the drainage channel 13 through the water outlet 1113 of the drainage groove 1112, and then flows to the water outlet through the drainage channel 13 for discharge, thereby further improving the waterproof sealing performance of the vehicle-mounted UAV cabin 100.

[0112] Furthermore, the outer shell 11 includes a shell body 111 and an inclined portion 112 arranged around the shell body 111, the inclined portion 112 is inclined downward at one end away from the shell body 111, the air inlet 1121 is arranged on the inclined portion 112, the hatch 1111 is arranged on the shell body 111, and the shell body 111 has a drainage groove 1112.

[0113] Furthermore, the drainage groove 1112 extends in a ring shape along the circumferential direction of the shell body 111, and the water outlet 1113 is located at the lowest point of the drainage groove 1112. Thus, through such an arrangement, all liquids that penetrate from the gap between the first sealing strip 41 and the hatch assembly 4 and the gap between the first sealing strip 41 and the shell 11 flow to the drainage groove 1112. At the same time, the water outlet 1113 is located at the lowest point of the drainage groove 1112 to ensure that the liquid accumulated in the drainage groove 1112 can flow smoothly from the water outlet 1113 into the drainage channel 13, thereby avoiding liquid stagnation and backflow, and improving reliability. Optionally, the water outlet 1113 is a plurality of water outlets spaced apart along the length direction of the drainage groove 1112, so that the liquid in the drainage groove 1112 can flow smoothly from the plurality of water outlets 1113 into the drainage channel 13, thereby further avoiding liquid stagnation and backflow.

[0114] In some embodiments of the present invention, Figure 1-Figure 4 , Fig.12 and Fig.13 As shown, the hatch assembly 4 includes a first hatch 42 and a second hatch 43 arranged along a first direction, the first hatch 42 and the second hatch 43 are movable in directions toward and away from each other to open or close the hatch 1111, and a second sealing strip 421 is provided between the first hatch 42 and the second hatch 43, the second sealing strip 421 is provided on the first hatch 42, and is used to seal the gap between the first hatch 42 and the second hatch 43 when the hatch 1111 is closed.

[0115] Thus, the first hatch 42 and the second hatch 43 move in directions toward each other to enable the hatch assembly 4 to open the hatch 1111, and the first hatch 42 and the second hatch 43 move in directions away from each other to enable the hatch assembly 4 to close the hatch 1111. At the same time, when closing the hatch 1111, the gap between the first hatch 42 and the second hatch 43 is sealed by the second sealing strip 421, thereby preventing liquid from entering the vehicle-mounted UAV cabin 100 through the gap between the first hatch 42 and the second hatch 43, thereby ensuring the waterproof sealing performance of the vehicle-mounted UAV cabin 100.

[0116] Furthermore, the first hatch 42 has a second slot 422, which is located at one end of the first hatch 42 close to the second hatch 43, and the second sealing strip 421 is clamped in the second slot 422. When the hatch 1111 is closed, the second sealing strip 421 abuts against the second hatch 43. Thus, the second sealing strip 421 is fixed and the sealing effect of the second sealing strip 421 is ensured through such a setting.

[0117] In some embodiments of the present invention, Figure 2-Figure 4 and Fig.12As shown, one end of the second hatch 43 facing the first hatch 42 has a third extension portion 431 extending toward the first hatch 42, a portion of the third extension portion 431 is located below the first hatch 42 and has a water receiving groove 4311 open toward the first hatch 42, when the hatch 1111 is closed, the water receiving groove 4311 is located below the second sealing strip 421 and the first hatch 42, and the water receiving groove 4311 is connected to the drainage groove 1112.

[0118] Therefore, through such an arrangement, the liquid that penetrates from the gap between the second sealing strip 421 and the first hatch 42 and the gap between the second sealing strip 421 and the second hatch 43 flows to the water receiving groove 4311, and flows into the drainage groove 1112 through the water receiving groove 4311, and then flows into the drainage channel 13 through the water outlet 1113 of the drainage groove 1112, and then flows to the water outlet through the drainage channel 13 for discharge, thereby further improving the waterproof sealing performance of the vehicle-mounted drone cabin 100.

[0119] Furthermore, one end of the water receiving groove 4311 connected to the drainage groove 1112 is the lowest point of the water receiving groove 4311, thereby ensuring that the liquid accumulated in the water receiving groove 4311 can flow smoothly into the drainage groove 1112, avoiding liquid retention and backflow, and improving reliability. Furthermore, the drainage groove 1112 is annular, and both ends of the length direction of the water receiving groove 4311 are connected to the drainage groove 1112 respectively, thereby, the liquid flowing from the gap between the second sealing strip 421 and the first cabin door 42 and the gap between the second sealing strip 421 and the second cabin door 43 into the water receiving groove 4311 flows along the length direction of the water receiving groove 4311 into the drainage groove 1112, further ensuring the waterproof sealing performance of the vehicle-mounted drone cabin 100.

[0120] Next, a vehicle according to an embodiment of the present invention will be described.

[0121] The vehicle according to the embodiment of the present invention includes a vehicle-mounted drone cabin 100 .

[0122] According to the vehicle of the embodiment of the present invention, a vehicle-mounted drone cabin 100 is provided, wherein the housing 1 includes an outer shell 11 and an inner plate 12, wherein the inner plate 12 is located below the outer shell 11 and a drainage channel 13 is formed between the inner plate 12 and the outer shell 11, wherein the inner plate 12 has a drainage port 121 connected to the drainage channel 13, and the outer shell 11 has an air inlet 1121 arranged opposite to the drainage channel 13, so that the liquid entering through the air inlet 1121 can flow into the drainage channel 13 and be discharged to the outside of the vehicle-mounted drone cabin 100 through the drainage port 121 of the drainage channel 13, thereby preventing the liquid from invading the internal structure of the vehicle-mounted drone cabin 100, so that the vehicle-mounted drone cabin 100 can prevent water from entering the internal structure of the vehicle-mounted drone cabin 100 while ensuring heat dissipation. At the same time, the air inlet assembly 2 is located at the air inlet 1121 and connected to the outer shell 11, so that the air inlet assembly 2 blocks part of the liquid from invading the internal structure of the vehicle-mounted drone cabin 100 through the air inlet 1121, so that the vehicle-mounted drone cabin 100 can better balance the waterproof performance and heat dissipation capacity.

[0123] In the description of this specification, the description with reference to the terms "one embodiment", "some embodiments", "illustrative embodiments", "examples", "specific examples", or "some examples" means that the specific features, structures, materials or characteristics described in conjunction with the embodiment or example are included in at least one embodiment or example of the present invention. In this specification, the schematic representation of the above terms does not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials or characteristics described may be combined in any one or more embodiments or examples in a suitable manner.

[0124] Although the embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the claims and their equivalents.

Claims

1. A vehicle-mounted UAV cabin, characterized in that: include: A shell (1), the shell (1) comprising an outer shell (11) and an inner plate (12), the inner plate (12) being located below the outer shell (11) and forming a drainage channel (13) between the inner plate (12) and the outer shell (11), the inner plate (12) having a drainage port (121) communicating with the drainage channel (13), and the outer shell (11) having an air inlet (1121) arranged opposite to the drainage channel (13); An air intake component (2), the air intake component (2) is located at the air inlet (1121) and is connected to the housing (11).

2. The vehicle-mounted UAV cabin according to claim 1, characterized in that: The housing (11) comprises a housing body (111) and an inclined portion (112) arranged around the housing body (111); one end of the inclined portion (112) facing away from the housing body (111) is inclined downward; and the air inlet (1121) is arranged on the inclined portion (112).

3. The vehicle-mounted UAV cabin according to claim 2, characterized in that: The air inlet assembly (2) comprises a plurality of first grille bars (21), and the plurality of first grille bars (21) are arranged at intervals.

4. The vehicle-mounted UAV cabin according to claim 3, characterized in that: A plurality of the first grid bars (21) are arranged in the up-down direction, and in projection on a horizontal plane, two adjacent first grid bars (21) have an overlapping area.

5. The vehicle-mounted UAV cabin according to claim 4, characterized in that: The size of the overlapping area is ≤15mm.

6. The vehicle-mounted UAV cabin according to claim 4, characterized in that: The first grid bar (21) comprises a first section (211), a second section (212) and a third section (213); the first section (211) is located above the third section (213); two ends of the second section (212) in a length direction are respectively connected to an end of the first section (211) close to the third section (213) and an end of the third section (213) close to the first section (211); in a projection on a horizontal plane, the third section (213) of the first grid bar (21) located above one of two adjacent first grid bars (21) has an overlapping area with the first section (211) of the first grid bar (21) located below the other.

7. The vehicle-mounted UAV cabin according to claim 6, characterized in that: One end of the first section (211) connected to the second section (212) and one end of the third section (213) away from the second section (212) are inclined downward, and the second section (212) is arranged horizontally.

8. The vehicle-mounted UAV cabin according to claim 5, characterized in that: The air inlet assembly (2) further comprises a mounting frame (22), a plurality of the first grille bars (21) are located within the mounting frame (22) and connected to the mounting frame (22), and the mounting frame (22) is detachably connected to the housing (11).

9. The vehicle-mounted UAV cabin according to claim 8, characterized in that: The air inlet assembly (2) further comprises a second grille bar (23), the second grille bar (23) being located above the first grille bar (21) at the top and being arranged at an interval, one end of the second grille bar (23) in the width direction being connected to the mounting frame (22) and the other end being inclined downward, and in projection on a horizontal plane, the second grille bar (23) and the first grille bar (21) at the top have an overlapping area.

10. The vehicle-mounted UAV cabin according to claim 8, characterized in that: The air inlet assembly (2) further comprises: a baffle (24), the baffle (24) extending in a ring shape along the circumferential direction of the mounting frame (22), the baffle (24) being located below the mounting frame (22) and connected to the mounting frame (22); A filter screen (25), the filter screen (25) being connected to the baffle plate (24) and being located on a side of the first grille bar (21) facing the inner plate (12), and being used for sealing the space inside the baffle plate (24) and filtering the fluid in the drainage channel (13) entering through the air inlet (1121).

11. The vehicle-mounted UAV cabin according to claim 10, characterized in that: The inner peripheral wall of the baffle (24) has a first extension portion (241) extending toward the inner plate (12), and the filter screen (25) is connected to the first extension portion (241).

12. The vehicle-mounted UAV cabin according to claim 2, characterized in that: The inclined portion (112) is provided with a groove (1122), the air inlet (1121) penetrates the bottom wall of the groove (1122), and the air inlet assembly (2) is arranged in the groove (1122).

13. The vehicle-mounted UAV cabin according to claim 12, characterized in that: Also includes: Foam (26), the foam (26) is arranged between the air inlet component (2) and the bottom wall of the groove (1122).

14. The vehicle-mounted UAV cabin according to claim 2, characterized in that: The air inlets (1121) are a plurality of air inlets spaced apart in the circumferential direction of the inclined portion (112), and the air inlet components (2) are a plurality of air inlets corresponding one to one to the plurality of air inlets (1121).

15. The vehicle-mounted UAV cabin according to claim 14, characterized in that: Along the circumferential direction of the inclined portion (112), the ends of the inclined portion (112) that are away from the shell body (111) are inclined downward at the same or different angles.

16. The vehicle-mounted UAV cabin according to claim 14, characterized in that: The air inlet (1121) includes a first air inlet (1121a), a second air inlet (1121b) and a third air inlet (1121c), wherein the first air inlet (1121a) and the second air inlet (1121b) are spaced apart along a first direction, and the first air inlet (1121a) and the third air inlet (1121c) are spaced apart along a third direction, and the regions of the inclined portion (112) having the first air inlet (1121a) and the second air inlet (1121b) are inclined downward at the same angle away from one end of the shell body (111), and the region of the inclined portion (112) having the third air inlet (1121c) is inclined downward at a greater angle than the region of the inclined portion (112) having the first air inlet (1121a) from one end of the shell body (111).

17. The vehicle-mounted UAV cabin according to claim 2, characterized in that: The inclined portion (112) has a first hoisting hole (1123), the inner plate (12) has a second hoisting hole (122) opposite to the first hoisting hole (1123), and the vehicle-mounted UAV cabin further comprises: A blocking cover (3), the blocking cover (3) is arranged at the first hanging hole (1123) and is detachably connected to the housing (11), and is used to block the first hanging hole (1123).

18. The vehicle-mounted UAV cabin according to claim 17, characterized in that: The upper side wall of the first hanging hole (1123) has a first protrusion (1124), and the first protrusion (1124) is located on the side of the blocking cover (3) facing the inner plate (12).

19. The vehicle-mounted UAV cabin according to claim 18, characterized in that: The surface of the first protrusion (1124) facing the blocking cover (3) includes a first sub-segment (1125) and a second sub-segment (1126), the first sub-segment (1125) is located on a side of the second sub-segment (1126) close to the fixed end of the first protrusion (1124), the end of the first sub-segment (1125) connected to the second sub-segment (1126) is tilted downward, and the end of the second sub-segment (1126) away from the first sub-segment (1125) is tilted downward, and the inclination angle of the second sub-segment (1126) is smaller than that of the first sub-segment (1125).

20. The vehicle-mounted UAV cabin according to claim 18, characterized in that: The inner wall of the second hanging hole (122) has a second extension portion (123) extending toward the center of the second hanging hole (122) and toward the outer shell (11), and the second extension portion (123) is annular in the circumferential direction around the second hanging hole (122).

21. The vehicle-mounted UAV cabin according to claim 20, characterized in that: The aperture size of the second hanging hole (122) is smaller than the aperture size of the first hanging hole (1123), and the end of the second extension portion (123) close to the center of the second hanging hole (122) is closer to the center of the first hanging hole (1123) than the end of the first protrusion (1124) close to the center of the first hanging hole (1123).

22. The vehicle-mounted UAV cabin according to claim 20, characterized in that: The surface of the inner plate (12) facing the shell (1) has a stop portion (124) extending toward the shell (1); the stop portion (124) is located above the second hanging hole (122) and extends along the circumferential direction of the second hanging hole (122); along the radial direction of the second hanging hole (122), the stop portion (124) is located radially outside the second extension portion (123); along the radial direction of the first hanging hole (1123), the stop portion (124) is located radially outside the first protrusion (1124).

23. The vehicle-mounted UAV cabin according to claim 17, characterized in that: The lower end of the blocking cover (3) is clamped on a side of the lower side wall of the first hanging hole (1123) facing the inner plate (12).

24. The vehicle-mounted UAV cabin according to claim 1, characterized in that: The housing (11) has a hatch (1111), and the vehicle-mounted UAV cabin further comprises a hatch assembly (4), wherein the hatch assembly (4) is used to open or close the hatch (1111).

25. The vehicle-mounted UAV cabin according to claim 24, characterized in that: A first sealing strip (41) is provided between the door assembly (4) and the outer shell (11); the first sealing strip (41) is provided on the door assembly (4) and extends along the circumferential direction of the door assembly (4).

26. The vehicle-mounted UAV cabin according to claim 25, characterized in that: The outer shell (11) has a drainage groove (1112), the drainage groove (1112) surrounds the hatch (1111), the drainage groove (1112) is located below the first sealing strip (41) and the hatch assembly (4), and the drainage groove (1112) has a water outlet (1113), and the water outlet (1113) is connected to the drainage channel (13).

27. The vehicle-mounted UAV cabin according to claim 26, characterized in that: The hatch assembly (4) comprises a first hatch (42) and a second hatch (43) arranged along a first direction, the first hatch (42) and the second hatch (43) being movable in directions toward and away from each other to open or close the hatch (1111), a second sealing strip (421) being provided between the first hatch (42) and the second hatch (43), the second sealing strip (421) being provided on the first hatch (42) and being used to seal a gap between the first hatch (42) and the second hatch (43) when the hatch (1111) is closed.

28. The vehicle-mounted UAV cabin according to claim 27, characterized in that: One end of the second hatch (43) facing the first hatch (42) has a third extension portion (431) extending toward the first hatch (42); a portion of the third extension portion (431) is located below the first hatch (42) and has a water receiving groove (4311) open toward the first hatch (42); when the hatch (1111) is closed, the water receiving groove (4311) is located below the second sealing strip (421) and the first hatch (42); the water receiving groove (4311) is connected to the drainage groove (1112).

29. A vehicle, characterized in that: It comprises a vehicle-mounted drone cabin (100) according to any one of claims 1-28.

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