Gliding type unmanned aerial vehicle transfer bin

Abstract

The utility model discloses a gliding type unmanned aerial vehicle transfer bin, and relates to the technical field of gliding type unmanned aerial vehicle transportation, the gliding type unmanned aerial vehicle transfer bin comprises a bin body, a launching port arranged on one side of the bin body, a plurality of bearing assemblies distributed in the bin body at intervals, and a sliding piece, the sliding piece is provided with a plurality of abutting parts, and the abutting parts abut against the bearing assemblies. The bearing assembly is driven to rotate. The unmanned aerial vehicle is installed on the bearing assembly, the bearing assembly is rotationally connected with the bin body, the sliding piece is slidably connected with the bin body, the sliding piece is provided with the abutting part, the abutting part can abut against the bearing assembly by sliding the sliding piece, the bearing assembly is driven to rotate relative to the bin body, and then the posture of the unmanned aerial vehicle is adjusted; a necessary inclination angle is provided for takeoff of the unmanned aerial vehicle, the unmanned aerial vehicle can fly out of the launching port and can be adjusted to be horizontal, installation and stabilization of the unmanned aerial vehicle are facilitated, the task execution efficiency and safety of the unmanned aerial vehicle are improved, the operation process is simplified, and the cost is reduced.

Description

TECHNICAL FIELD

[0001] The utility model relates to gliding unmanned plane transportation technical field, especially in a gliding unmanned plane transfer storehouse. BACKGROUND

[0002] In the rapid development of unmanned plane technology, gliding unmanned plane because its unique flight performance and flexibility, in reconnaissance, monitoring, search and rescue and many other fields have been widely used. In order to realize the effective deployment and rapid response of gliding unmanned plane, usually need to store unmanned plane in the dedicated transfer storehouse, in order to transport to the task area quickly.

[0003] The traditional gliding unmanned plane transfer storehouse design is relatively simple, mainly with a certain interval unmanned plane is arranged in the storehouse, to ensure the safety and stability of unmanned plane in the transportation process. However, this design mainly focuses on the storage and transportation function of unmanned plane, and ignores the synergy with unmanned plane launch task, specifically, the traditional transfer storehouse when unmanned plane takes off, often only as a simple storage and take out tool, cannot provide effective assistance for the takeoff of unmanned plane. Especially for gliding unmanned plane, its takeoff process needs a certain inclination angle and speed to produce enough lift, but direct inclination setting is not convenient for the fixation and placement of unmanned plane, the traditional transfer storehouse cannot meet this demand. UTILITY MODEL CONTENT

[0004] The main purpose of the utility model is to propose a gliding unmanned plane transfer storehouse aims at solving the problem that the traditional transfer storehouse cannot help the takeoff of unmanned plane.

[0005] To achieve the above purpose, the gliding unmanned plane transfer storehouse provided by the utility model comprises:

[0006] The storehouse is provided with a launch port on one side, and a first slide is formed in the storehouse, and the length direction of the first slide is parallel to the plane where the launch port is located;

[0007] A plurality of bearing assemblies are distributed in the storehouse at intervals, and the bearing assemblies are rotationally connected to the inner walls of the storehouse on the two sides adjacent to the launch port;

[0008] A sliding part is slidingly inserted into the first slide, the sliding part is provided with a plurality of abutting portions, the abutting portions abut against the bearing assemblies, and the bearing assemblies are driven to rotate by the abutting portions.

[0009] In an embodiment, the bearing assembly is provided with a connecting column, the storehouse is provided with a connecting sleeve, the connecting sleeve sleeves the connecting column, and the bearing assembly is rotationally connected to the storehouse through the connecting column;

[0010] The bearing assembly further includes a limit pin, and the connecting column and the connecting sleeve both abut against the limit pin to limit the connecting column from being separated from the connecting sleeve, and the limit pin partially protrudes from the connecting sleeve to remove the limit pin.

[0011] In one embodiment, a limiting notch with an arc-shaped cross-section is provided on the side surface of the connecting sleeve along the circumferential direction, and the connecting column is provided with an installation opening corresponding to the limiting notch. The limiting pin passes through the limiting notch and is inserted into the installation opening to limit the rotation angle of the connecting column relative to the connecting sleeve.

[0012] In one embodiment, the supporting assembly includes a partition and a support frame, the connecting column is fixedly connected to the side of the support frame close to the first slide, and a second slide is provided on the side opposite to the supporting frame and the connecting column, and the partition is inserted into the support frame through the second slide.

[0013] In one embodiment, the support frame includes a baffle and two support rails, the second slide is arranged in the support rail, and the connecting column is fixedly connected to the side of the support rail close to the first slide, and the two support rails are fixedly connected to the baffle on the side away from the launch port.

[0014] In one embodiment, the bearing assembly further includes a positioning pin, the support frame is provided with a first positioning hole, the partition is provided with a second positioning hole corresponding to the first positioning hole, and the positioning pin is inserted into the first positioning hole and the second positioning hole.

[0015] In one embodiment, the supporting assembly further includes a first connecting member and a second connecting member, the positioning pin is rotatably connected to the second connecting member at one end away from the second slide, and both ends of the first connecting member are rotatably connected to the support frame and the second connecting member respectively.

[0016] In one embodiment, the gliding UAV transfer warehouse further includes a warehouse door, which is rotatably connected to the warehouse body to cover the launch port.

[0017] In one embodiment, a limiting portion is provided inside the bin body, wherein the limiting portion is fixedly connected to the inner wall of the bin body and abuts against the supporting assembly to limit the rotation angle of the supporting assembly.

[0018] In one embodiment, the bin body is fixedly connected to a driving member, and an output end of the driving member is fixedly connected to the sliding member to drive the sliding member to slide along the first slideway.

[0019] The utility model discloses a technical scheme through being installed on the bearing assembly to the unmanned plane, and the bearing assembly rotation is connected the bin body, the sliding part is connected with the bin body slidingly, the sliding part is equipped with the abutment portion, and the abutment portion can be made with the bearing assembly abutted through the sliding sliding part, and the bearing assembly is driven to rotate relative to the bin body, and then the attitude of unmanned plane is adjusted, and the necessary inclination angle is provided for the takeoff of unmanned plane, and the unmanned plane can fly out from the launching port, and also can be adjusted to the level, the installation and stability of unmanned plane are convenient, and the task execution efficiency and security of unmanned plane are improved, and the additional launching device or inclination platform is not needed, the operation procedure is simplified, and the cost is reduced. BRIEF DESCRIPTION OF DRAWINGS

[0020] In order to more clearly illustrate the technical scheme in the embodiment of the utility model or prior art, below will be to the embodiment or prior art description needed to use the drawing briefly introduced, obviously, below description in the drawing only some embodiments of the utility model, for those skilled in the art, under the premise of not paying creative labor, can also obtain other drawings according to the structure shown in these drawings.

[0021] Figure 1 The structure schematic diagram of one embodiment of the gliding unmanned plane transfer bin provided by the utility model is shown in the figure.

[0022] Figure 2 The assembly structure diagram of bin body and sliding part is shown in the figure.

[0023] Figure 3 The structure schematic diagram of another embodiment of the gliding unmanned plane transfer bin provided by the utility model is shown in the figure.

[0024] Figure 4 The structure schematic diagram of the support frame is shown in the figure. Figure 3 The enlarged schematic diagram of A in the figure is shown in the figure.

[0025] Figure 5 The structure schematic diagram of another embodiment of the gliding unmanned plane transfer bin provided by the utility model is shown in the figure.

[0026] Figure 6 The structure schematic diagram of another embodiment of the gliding unmanned plane transfer bin provided by the utility model is shown in the figure.

[0027] Figure 7 The enlarged schematic diagram of B in the figure is shown in the figure. Figure 6 The enlarged schematic diagram of B in the figure is shown in the figure.

[0028] Figure 8 The structure relationship schematic diagram of bearing assembly and reinforcing rib is shown in the figure.

[0029] Explanation of reference numerals:

[0030] 100. Gliding UAV transfer warehouse; 1. Warehouse body; 11. Launch port; 12. First slide; 13. Connecting sleeve; 131. Limiting notch; 14. Warehouse door; 15. Limiting part; 151. First limiting member; 152. Second limiting member; 16. Reinforcing rib; 2. Load-bearing assembly; 21. Connecting column; 211. Mounting port; 22. Limiting pin; 23. Partition; 231. Second positioning hole; 24. Support frame; 241. Second slide; 242. Baffle; 2421. First connecting plate; 2422. Second connecting plate; 243. Support rail; 244. First positioning hole; 25. Positioning pin; 26. First connecting member; 27. Second connecting member; 3. Sliding member; 31. Abutment part; 4. Driving member.

[0031] The realization of the purpose, functional features and advantages of the present invention will be further explained in conjunction with embodiments and with reference to the accompanying drawings. DETAILED DESCRIPTION

[0032] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts shall fall within the scope of protection of the present invention.

[0033] It should be noted that if the embodiments of the present invention involve directional indications (such as up, down, left, right, front, back, etc.), the directional indications are only used to explain the relative position relationship, movement status, etc. between the components in a certain specific posture. If the specific posture changes, the directional indications will also change accordingly.

[0034] In addition, if there are descriptions involving "first", "second", etc. in the embodiments of the present invention, the descriptions of "first", "second", etc. are only for descriptive purposes and cannot be understood as indicating or implying their relative importance or implicitly indicating the number of the indicated technical features. Therefore, the features limited to "first" and "second" may explicitly or implicitly include at least one of such features. In addition, if "and / or" or "and / or" appears in the full text, its meaning includes three parallel schemes. Taking "A and / or B" as an example, it includes scheme A, or scheme B, or a scheme in which A and B are satisfied at the same time. In addition, the technical solutions between the various embodiments can be combined with each other, but it must be based on the ability of ordinary technicians in this field to implement. When the combination of technical solutions is mutually contradictory or cannot be implemented, it should be deemed that such a combination of technical solutions does not exist and is not within the scope of protection required by the present invention.

[0035] With the rapid development of drone technology, gliding drones (UAVs) have been widely used in various fields, including reconnaissance, monitoring, and search and rescue, due to their unique flight performance and flexibility. To achieve efficient deployment and rapid response of gliding drones, they are usually stored in dedicated transfer warehouses for rapid transportation to the mission area.

[0036] The design of traditional gliding drone transfer pods is relatively simple, primarily arranging drones at regular intervals within the pod to ensure safety and stability during transport. However, this design primarily focuses on the storage and transport functions of drones, neglecting their integration with launch missions. Specifically, traditional transfer pods often serve only as a simple storage and retrieval tool during takeoff, failing to effectively assist with the drone's takeoff. This is particularly true for gliding drones, which require a certain tilt angle and speed to generate sufficient lift during takeoff, and traditional transfer pods, due to design limitations, cannot meet these requirements.

[0037] The utility model provides a gliding type UAV transfer cabin 100.

[0038] See also Figures 1 to 8 In one embodiment of the present invention, the gliding drone transfer chamber 100 includes:

[0039] A silo 1 is provided with a launch port 11 on one side of the silo 1. The silo 1 is provided with a first slide 12, and the length direction of the first slide 12 is parallel to the plane where the launch port 11 is located;

[0040] A plurality of bearing components 2, the bearing components 2 are distributed at intervals in the warehouse body 1, and the bearing components 2 are rotatably connected to the inner wall of the warehouse body 1 on two adjacent sides of the launch port 11;

[0041] The sliding member 3 is slidably inserted into the first slideway 12 . The sliding member 3 is provided with a plurality of abutting portions 31 . The abutting portions 31 abut against the bearing assembly 2 to drive the bearing assembly 2 to rotate.

[0042] like Figure 1 As shown, both sides of the carrying assembly 2 are rotatably connected to the inner wall of the warehouse body 1. In some embodiments, the carrying assembly 2 includes a support frame 24, and the support frame 24 includes two support rails 243. The support rails 243 are rotatably connected to the warehouse body 1, wherein the support rails 243 correspond to the two support portions, and are used to control the support rails 243 to rotate in different directions;

[0043] Optionally, the number of the sliding members 3 can be one or more, in some embodiments, the two support portions are located on the same sliding member 3, and in other embodiments, the number of the sliding members 3 is more, and the number of the first sliding grooves 12 is correspondingly arranged, and the two support portions are located on different sliding members 3.

[0044] As shown in Figure 2 and Figure 3 In an embodiment, the two support portions are located on one side of the bearing assembly 2, and the two support portions are located on different sliding members 3, respectively, and the two support portions are located on both sides of the connection between the bearing assembly 2 and the cartridge body 1, respectively. It can be understood that when the support portion abuts against the bearing assembly 2, it can push the bearing assembly 2 to rotate around the rotating connection, and the two support portions can push the bearing assembly 2 to rotate in different directions, respectively. Moreover, when the two support portions abut against the bearing assembly 2, since they are located on the same side of the bearing assembly 2, the rotation angle of the bearing assembly 2 can be determined;

[0045] In another embodiment, the two support portions are located on the upper and lower sides of the bearing assembly 2, respectively, and the two support portions are located on the same sliding member 3. Through one sliding member 3, the rotation direction of the bearing assembly 2 in two directions can be controlled, and the production cost is reduced.

[0046] It should be noted that in some embodiments, one of the support rails 243 of the bearing assembly 2 is correspondingly provided with the sliding member 3, and in other embodiments, both of the support rails 243 of the bearing assembly 2 are correspondingly provided with the sliding assembly, so as to improve the pushing force of the bearing assembly 2 and ensure that the stress of the support assembly is uniform.

[0047] In some embodiments, the support rail 243 is provided with a third sliding groove on the side of the first sliding groove 12, the length direction of the third sliding groove is the same as the length direction of the support rail 243, the abutting portion 31 is located in the third sliding groove and is in sliding connection with the third sliding groove. By abutting and pushing different sides of the third sliding groove through the abutting portion 31, the rotation of the support rail 243 in different directions can be realized, and one abutting portion 31 can realize the control of the rotation and the rotation angle of the support rail 243, thereby reducing the production cost.

[0048] Moreover, a plurality of abutting portions 31 are arranged on one sliding member 3, and the rotation angle of a plurality of bearing assemblies 2 can be controlled simultaneously through the sliding member 3, and the rotation angles of the plurality of bearing assemblies 2 relative to the cartridge body 1 are ensured to be the same, thereby improving the control efficiency of the bearing assembly 2.

[0049] AsFigure 1 As shown, in order to enhance the strength of the silo body 1, the corners of the silo body 1 are generally provided with reinforcing ribs 16;

[0050] In some embodiments, as Figure 1 As shown, in order to ensure that the launch path of the UAV is not blocked by the reinforcing ribs 16 and the upper wall of the warehouse body 1 when the uppermost supporting assembly 2 is launched at an angle, a certain distance is left between the uppermost supporting assembly 2 and the upper wall of the warehouse body 1 to allow the UAV to take off normally.

[0051] like Figure 8 As shown, in other embodiments, an auxiliary firing port is provided on the upper side of the warehouse body 1. After the uppermost supporting component 2 is tilted, the UAV supported by the supporting component 2 can fly out through the auxiliary firing port. Moreover, after the uppermost supporting component 2 is tilted, the reinforcing rib 16 is located at the lower part of the plane where the supporting component 2 is located, so as to prevent the UAV from being blocked by the reinforcing rib 16 during the launch process.

[0052] The technical solution of the present invention is to install the UAV on the carrying component 2, and the carrying component 2 is rotatably connected to the warehouse body 1, and the sliding member 3 is slidably connected to the warehouse body 1. The sliding member 3 is provided with the abutting portion 31. By sliding the sliding member 3, the abutting portion 31 can be abutted against the carrying component 2, and the carrying component 2 can be driven to rotate relative to the warehouse body 1, thereby adjusting the posture of the UAV and providing the necessary tilt angle for the UAV to take off. The UAV can fly out of the launching port 11 and can also be adjusted to a horizontal position, which is convenient for the installation and stability of the UAV, improves the mission execution efficiency and safety of the UAV, and does not require an additional launching device or tilting platform, simplifies the operation process, and reduces costs.

[0053] Optionally, the carrying assembly 2 is provided with a connecting column 21, and the silo body 1 is provided with a connecting sleeve 13, the connecting sleeve 13 is sleeved on the connecting column 21, and the carrying assembly 2 is rotatably connected to the silo body 1 through the connecting column 21;

[0054] The bearing assembly 2 further includes a limit pin 22 , and the connecting column 21 and the connecting sleeve 13 both abut against the limit pin 22 to limit the connecting column 21 from being separated from the connecting sleeve 13 , and the limit pin 22 partially protrudes from the connecting sleeve 13 to be removed.

[0055] In some embodiments, the connecting column 21 is internally recessed in the circumferential direction to form a sliding groove, the limiting pin 22 is partially located inside the sliding groove and abuts against both sides of the sliding groove, the limiting pin 22 penetrates the side of the connecting sleeve 13 and is fixed relative to the connecting sleeve 13, and the length direction of the limiting pin 22 is consistent with the radial direction of the connecting sleeve 13, so as to limit the movement of the connecting column 21 in the axial direction of the connecting sleeve 13.

[0056] Optionally, in an embodiment, the limiting pin 22 is threadedly connected with the connecting sleeve 13, the threadedly connection makes the limiting pin 22 fixed relative to the connecting sleeve 13, and a gap is left between the end of the limiting pin 22 and the bottom wall of the sliding groove, so as to reduce the friction, and in another embodiment, the limiting pin 22 is directly inserted into the connecting sleeve 13, it should be noted that the limiting pin 22 abuts against the sliding groove by gravity, and the limiting pin 22 can be directly pulled out without rotation, which is suitable for occasions where the bearing assembly 2 needs to be frequently disassembled, and the present embodiment does not make specific limitation hereon.

[0057] In some other embodiments, the limiting pin 22 is threadedly connected with the connecting column 21, and the side of the connecting sleeve 13 is circumferentially provided with a notch corresponding to the limiting pin 22, so as to rotate the limiting pin 22 and limit the movement of the limiting pin 22 in the axial direction of the connecting sleeve 13, thereby limiting the movement of the connecting column 21.

[0058] It should be noted that the limiting pin 22 partially protrudes from the connecting sleeve 13, which facilitates the removal of the limiting pin 22 and the disassembly of the bearing assembly 2, facilitates replacement and maintenance, and can change the distance between two bearing assemblies 2 according to the size of the installed unmanned aerial vehicle, for example, when the unmanned aerial vehicle is too large, one or more bearing assemblies 2 can be disassembled, so that the distance between two adjacent bearing assemblies 2 is increased, and the versatility is improved.

[0059] Optionally, the side of the connecting sleeve 13 is circumferentially provided with a limiting notch 131 with an arc-shaped cross section, the connecting column 21 is provided with a mounting port 211 corresponding to the limiting notch 131, and the limiting pin 22 penetrates the limiting notch 131 and is inserted into the mounting port 211, so as to limit the rotation angle of the connecting column 21 relative to the connecting sleeve 13.

[0060] As Figure 7As shown, the limit pin 22 is relatively fixed to the connecting column 21. When the connecting column 21 is rotated to a certain angle relative to the connecting sleeve 13, the limit pin 22 will abut against the connecting sleeve 13, limiting the movement of the limit pin 22, thereby limiting the rotation of the connecting column 21. It can be understood that the rotation angle of the supporting component 2 is also limited, and according to the different lengths of the limiting notch 131, the angle at which the supporting component 2 can rotate is also different. The rotation angle of the supporting component 2 can be limited by adjusting the length of the limiting notch 131, and can be set according to needs to select the angle during launch.

[0061] Optionally, the supporting assembly 2 includes a partition 23 and a support frame 24, the connecting column 21 is fixedly connected to the side of the support frame 24 close to the first slide 12, and a second slide 241 is provided on the side of the support frame 24 opposite to the connecting column 21, and the partition 23 is inserted into the support frame 24 through the second slide 241.

[0062] It can be understood that the partition 23 is used to place the drone. The partition 23 is inserted into the support frame 24 through the second slide 241. The partition 23 is slidably connected to the support frame 24. When in use, the partition 23 can be taken out first, the drone is placed on the partition 23, and then the partition 23 is inserted into the support frame 24 to facilitate the installation and fixation of the drone.

[0063] Optionally, the support frame 24 includes a baffle 242 and two support rails 243, the second slide 241 is arranged in the support rail 243, and the connecting column 21 is fixedly connected to the side of the support rail 243 close to the first slide 12, and the two support rails 243 are fixedly connected to the baffle 242 on the side facing away from the launch port 11.

[0064] In some embodiments, no fixed connection structure is provided between the two support rails 243. It can be understood that when the partition 23 is inserted between the two support rails 243, the partition 23 can make the rotation angles between the two support rails 243 consistent; when the partition 23 is removed, the two support rails 243 lose the restriction of the partition 23, and the rotation angles of the two support rails 243 are different. Therefore, when inserting the partition 23, the two support rails 243 need to be rotated to be parallel to each other before the partition 23 can be inserted.

[0065] It should be noted that the baffle 242 can make the two support rails 243 rotate at the same angle and remain parallel, thereby facilitating the installation of the partition 23 .

[0066] Furthermore, when the supporting assembly 2 is tilted, the baffle 242 can abut against the partition 23 to limit the movement of the partition 23 .

[0067] It should be noted that, in some embodiments, there is a gap between one end of the connecting column 21 close to the connecting sleeve 13 and the connecting sleeve 13. During installation, one connecting column 21 is first inserted into the connecting sleeve 13 and pushed toward one side of the connecting sleeve 13. Then, the other connecting column 21 is aligned with the other connecting sleeve 13, and the other connecting column 21 is inserted. Finally, it is fixed by the limit pin 22 to facilitate the installation of the bearing assembly 2.

[0068] like Figure 5 As shown, in some embodiments, the baffle 242 includes a first connecting plate 2421 and a second connecting plate 2422, and the first connecting plate 2421 and the second connecting plate 2422 are plugged into each other, and the first connecting plate 2421 is fixedly connected to the support rail 243 at one end away from the second connecting plate 2422, and the second connecting plate 2422 is fixedly connected to the other support rail 243 at one end away from the first connecting plate 2421, and the first connecting plate 2421 and the second connecting plate 2422 can slide relative to each other along the length direction of the connecting portion. When installing the support frame 24, the first connecting plate 2421 and the second connecting plate 2422 can be pushed toward each other first, so that the distance between the two support rails 243 is reduced, and then the bearing assembly 2 is placed inside the warehouse body 1, so that the connecting column 21 and the connecting sleeve 13 correspond to each other, and then the first connecting plate 2421 and the second link portion are pulled away from each other, so that the connecting column 21 can be inserted into the connecting sleeve 13 for easy installation.

[0069] Optionally, the bearing assembly 2 further includes a positioning pin 25 , the support frame 24 defines a first positioning hole 244 , the partition 23 defines a second positioning hole 231 corresponding to the first positioning hole 244 , and the positioning pin 25 is inserted into the first positioning hole 244 and the second positioning hole 231 .

[0070] It is understood that the locating pins 25 can secure the partition 23 relative to the support frame 24, ensuring the stability of the partition 23 during transportation. The locating pins 25 make assembly and disassembly of the partition 23 and the support frame 24 easier and faster. The user only needs to insert the locating pins 25 into the corresponding first locating holes 244 and second locating holes 231 to complete the fixation, which not only improves assembly efficiency but also reduces maintenance costs.

[0071] In one embodiment, a clamping portion is provided at one end of the positioning pin 25 away from the second slideway 241 . The clamping portion is larger than the first positioning hole 244 and is used to clamp the positioning pin 25 .

[0072] Optionally, the bearing assembly 2 further includes a first connecting member 26 and a second connecting member 27 , the positioning pin 25 is rotatably connected to the second connecting member 27 at one end away from the second slide 241 , and the first connecting member 26 is rotatably connected to the support frame 24 and the second connecting member 27 at both ends.

[0073] like Figure 4 As shown, the user can lift the positioning pin 25 to release the restriction between the partition 23 and the support frame 24. Rotating the first connecting member 26 can drive the positioning pin 25 to move through the second connecting member 27. The positioning pin 25 can be pulled out through the first connecting member 26. Compared with directly pulling out the positioning pin 25, pulling it out through the first connecting member 26 is more labor-saving, thereby improving the convenience and comfort of operation.

[0074] Moreover, when limiting the partition 23 and the support frame 24, the first connecting member 26 and the second connecting member 27 will give the positioning pin 25 a force toward the second slide 241 due to their own weight, which can prevent the positioning pin 25 from falling out due to bumps during transportation, thereby ensuring the stability and safety of the transfer warehouse during transportation.

[0075] like Figure 6 As shown, optionally, the gliding UAV transfer warehouse 100 also includes a warehouse door 14, and the warehouse door 14 is rotatably connected to the warehouse body 1 to cover the launch port 11.

[0076] It can be understood that the door 14 effectively covers and protects the launch port 11 when not in use, preventing external objects or environmental factors (such as dust, rain, etc.) from entering the interior of the warehouse 1 and causing damage to the drone or the supporting component 2. It can also ensure the safety of the drone during transportation and prevent accidental falls or theft.

[0077] Optionally, a limiting portion 15 is provided inside the warehouse body 1 , and the limiting portion 15 is fixedly connected to the inner wall of the warehouse body 1 and abuts against the supporting component 2 to limit the rotation angle of the supporting component 2 .

[0078] It can be understood that the load-bearing component 2 abuts against the connecting sleeve 13 and the abutting portion 31, and the connecting sleeve 13 is subjected to greater pressure. The limiting portion 15 abuts against the load-bearing component 2 to disperse the pressure to prevent excessive local force, thereby ensuring the safety of equipment operation, and effectively preventing the load-bearing component 2 from excessive rotation or shaking, thereby enhancing structural stability.

[0079] like Figure 2 As shown, it should be noted that the limiting portion 15 includes a first limiting member 151 and a second limiting member 152, which respectively limit the maximum rotation angle of the supporting assembly 2 in different directions;

[0080] It should be noted that the limiting portion 15 may abut against the support rail 243 . When the baffle 242 is provided, the limiting portion 15 may also abut against the baffle 242 . This embodiment does not impose any specific limitation on this.

[0081] like Figure 2 As shown, optionally, the warehouse body 1 is fixedly connected to a driving member 4 , and an output end of the driving member 4 is fixedly connected to the sliding member 3 to drive the sliding member 3 to slide along the first slideway 12 .

[0082] The driving member 4 can realize the automatic movement of the sliding member 3. The user does not need to push or pull the sliding member 3 manually, which greatly reduces the physical burden, improves the convenience and efficiency of operation, and can significantly improve work efficiency.

[0083] It is understandable that the driving member 4 may be a hydraulic device or a starting device, and this embodiment does not impose any specific limitation on this.

[0084] In one embodiment, the driving member 4 is a motor, the output shaft of the motor is fixedly connected to the screw to drive the screw to rotate, and the sliding member 3 is threadedly connected to the screw, and the sliding member 3 can be raised and lowered by rotating it.

[0085] The above description is merely an exemplary embodiment of the present invention and does not limit the patent scope of the present invention. All equivalent structural transformations made using the contents of the present invention specification and drawings under the technical concept of the present invention, or direct / indirect application in other related technical fields are included in the patent protection scope of the present invention.

Claims

1. A gliding UAV transfer cabin, characterized in that: include: A silo, wherein a launch port is provided on one side of the silo, and a first slide is provided on the silo, wherein the length direction of the first slide is parallel to the plane where the launch port is located; A plurality of bearing components, the bearing components are spaced apart and distributed in the silo, and the bearing components are rotatably connected to the inner wall of the silo on two adjacent sides of the launch port; A sliding member is slidably inserted into the first slideway, and the sliding member is provided with a plurality of abutting portions, which abut against the bearing assembly to drive the bearing assembly to rotate.

2. The gliding UAV transfer cabin according to claim 1, characterized in that: The bearing assembly is provided with a connecting column, the silo body is provided with a connecting sleeve, the connecting sleeve is sleeved on the connecting column, and the bearing assembly is rotatably connected to the silo body through the connecting column; The bearing assembly further includes a limit pin, and the connecting column and the connecting sleeve both abut against the limit pin to limit the connecting column from being separated from the connecting sleeve, and the limit pin partially protrudes from the connecting sleeve to remove the limit pin.

3. The gliding UAV transfer cabin according to claim 2, characterized in that: The side surface of the connecting sleeve is provided with a limiting notch with an arc-shaped cross-section along the circumferential direction, and the connecting column is provided with an installation opening corresponding to the limiting notch. The limiting pin passes through the limiting notch and is inserted into the installation opening to limit the rotation angle of the connecting column relative to the connecting sleeve.

4. The gliding UAV transfer pod according to any one of claims 2 to 3, characterized in that: The bearing assembly includes a partition and a support frame. The connecting column is fixedly connected to the side of the support frame close to the first slide. A second slide is provided on the side of the support frame opposite to the connecting column. The partition is inserted into the support frame through the second slide.

5. The gliding UAV transfer cabin according to claim 4, characterized in that: The support frame includes a baffle and two support rails, the second slide is arranged in the support rail, and the connecting column is fixedly connected to the side of the support rail close to the first slide, and the two support rails are fixedly connected to the baffle on the side away from the launch port.

6. The gliding UAV transfer cabin according to claim 4, characterized in that: The bearing assembly further includes a positioning pin, the support frame is provided with a first positioning hole, the partition is provided with a second positioning hole corresponding to the first positioning hole, and the positioning pin is inserted into the first positioning hole and the second positioning hole.

7. The gliding UAV transfer cabin according to claim 6, characterized in that: The bearing assembly further includes a first connecting member and a second connecting member. The positioning pin is rotatably connected to the second connecting member at one end away from the second slideway, and the two ends of the first connecting member are rotatably connected to the support frame and the second connecting member respectively.

8. The gliding UAV transfer cabin according to claim 7, characterized in that: The gliding UAV transfer warehouse also includes a warehouse door, which is rotatably connected to the warehouse body to cover the launch port.

9. The gliding UAV transfer pod according to any one of claims 1 to 3, characterized in that: A limiting portion is provided inside the warehouse body, and the limiting portion is fixedly connected to the inner wall of the warehouse body and abuts against the bearing assembly to limit the rotation angle of the bearing assembly.

10. The gliding UAV transfer cabin according to any one of claims 1 to 3, characterized in that: The bin body is fixedly connected to a driving member, and an output end of the driving member is fixedly connected to the sliding member to drive the sliding member to slide along the first slideway.

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