Spherical unmanned aerial vehicle positioning structure

Abstract

The invention belongs to the technical field of unmanned aerial vehicle equipment, and discloses a spherical unmanned aerial vehicle positioning structure which is technically characterized in that the spherical unmanned aerial vehicle positioning structure comprises an unmanned aerial vehicle body, a protection mechanism is arranged on the outer side of the unmanned aerial vehicle body and comprises an arc-shaped rod, a positioning assembly and a dismounting assembly, and an anti-rolling mechanism is arranged on the surface of the arc-shaped rod; the anti-rolling mechanism comprises multiple groups of stop levers, a storage assembly and an adjusting assembly, and the adjusting assembly comprises a clamping part and a transmission part, so that the problems that the spherical shell of the unmanned aerial vehicle cannot be conveniently mounted and dismounted at present, the stability of the spherical unmanned aerial vehicle is poor during landing, and the stability of the spherical unmanned aerial vehicle is poor are solved. And the spherical unmanned aerial vehicle is easy to roll at will, so that the unmanned aerial vehicle is damaged.

Description

Technical Field

[0001] The invention relates to the technical field of unmanned aerial vehicle equipment, in particular to a spherical unmanned aerial vehicle positioning structure. Background Art

[0002] As the application of drones continues to expand, drones with different structures and functions have also emerged. Current drones are usually composed of a body and a propeller, which uses the rotation of the propeller to provide lifting force to drive the entire drone to fly. When a drone is in use, the propeller and the body are prone to contact and collide with surrounding objects, which poses certain safety hazards. Therefore, spherical drones with spherical frames have become more and more popular with users.

[0003] When the existing spherical drone is in use, the spherical shell of the drone cannot be easily installed and disassembled, which makes it inconvenient to store the spherical drone. In addition, the spherical drone has poor stability when landing, and the spherical drone is easy to roll randomly, which may cause damage to the drone. Summary of the invention

[0004] The purpose of the present invention is to provide a spherical UAV positioning structure to solve the problems raised in the above background technology.

[0005] To achieve the above object, the present invention provides the following technical solutions:

[0006] A spherical UAV positioning structure comprises a UAV body, a protective mechanism is arranged on the outside of the UAV body, the protective mechanism comprises an arc-shaped rod, a positioning assembly and a disassembly assembly, the arc-shaped rod is provided with multiple groups, the positioning assembly is located on the upper and lower sides of the UAV body and is connected to the arc-shaped rod, the positioning assembly is used to control multiple groups of arc-shaped rods to surround the outside of the UAV body at equal intervals, the disassembly assembly is connected to the positioning assembly, the disassembly assembly installs and disassembles the arc-shaped rod on the outside of the UAV body by cooperating with the positioning assembly, the surface of the arc-shaped rod is provided with an anti-roll mechanism, and the anti-roll mechanism The structure includes a baffle rod, a storage assembly and an adjustment assembly. The baffle rod is provided with multiple groups. The storage assembly is located on the surface of the arc-shaped rod and connected to the baffle rod. The storage assembly is used to control the multiple groups of baffle rods to be located at equal intervals on the surface of the arc-shaped rod. The adjustment assembly includes a clamping part and a transmission part. The clamping part is located in the arc-shaped rod and cooperates with the storage assembly. The clamping part controls the baffle rod as a whole to be in the arc-shaped rod by cooperating with the storage assembly. The transmission part is connected to the clamping part. The transmission part controls the baffle rod to rotate to the outside of the arc-shaped rod by cooperating with the clamping part and controls the baffle rod to maintain a vertical state with the arc-shaped rod.

[0007] As a further solution of the present invention: the positioning assembly includes a top rod detachably mounted on the top wall of the drone body, an end cover detachably mounted on the top end of the top rod, and a side wall of the end cover is provided with a plurality of top holes that cooperate with the top end of the arc-shaped rod; a bottom rod detachably mounted on the bottom wall of the drone body, a bottom cover detachably mounted on the bottom end of the bottom rod, and a side wall of the bottom cover is provided with a plurality of bottom holes that cooperate with the bottom end of the arc-shaped rod.

[0008] As a further solution of the present invention: the disassembly and assembly component includes a top plate and a bottom ring, an upper connecting hole connected to the top hole is opened downwardly on the surface of the end cover, an upper positioning hole is arranged on the top end of the arc-shaped rod, an upper positioning rod matching with the upper positioning hole is fixedly installed on the bottom wall of the top plate, two groups of first magnetic sheets matching with each other are fixedly installed on the two side walls opposite to the top plate and the end cover, a lower connecting hole connected to the bottom hole is opened downwardly on the surface of the bottom cover, a lower positioning hole is opened at the bottom end of the arc-shaped rod, a lower positioning rod matching with the lower positioning hole is fixedly installed on the bottom wall of the bottom ring, and two groups of second magnetic sheets matching with each other are fixedly installed on the two side walls opposite to the bottom cover and the bottom ring.

[0009] As a further solution of the present invention: the storage assembly includes a plurality of storage grooves with equal spacing arranged on the surface of the arc-shaped rod, a carrying plate is rotatably installed in the storage groove, and the blocking rod is fixedly installed on the surface of the carrying plate.

[0010] As a further solution of the present invention: the clamping part includes telescopic grooves respectively opened on the two side walls opposite to the storage groove, an extrusion spring is fixedly installed in the telescopic groove, a limiting column is fixedly installed on the telescopic end of the extrusion spring, and two groups of limiting grooves cooperating with the limiting column are opened on the side wall of the supporting plate.

[0011] As a further solution of the present invention: the transmission part includes a side plate slidably mounted on the side wall of the arc-shaped rod, the side wall of the arc-shaped rod is provided with a sliding part connected to the side plate, the side wall of the arc-shaped rod is provided with a guide hole connected to the telescopic groove inwardly, a pulling rope is fixedly mounted on the end of the limit column, the pulling rope extends through the guide hole to the outside of the arc-shaped rod and is connected to the side plate, and a control spring cooperating with the gear lever is fixedly mounted on the side wall of the storage groove.

[0012] As a further solution of the present invention: the sliding part includes a sliding groove opened on the side wall of the arc-shaped rod, a sliding block is slidably installed in the sliding groove, the sliding block extends to the outside of the sliding groove and is connected to the side plate, and a return spring connected to the sliding block is fixedly installed in the sliding groove.

[0013] As a further solution of the present invention: both ends of the top rod and the bottom rod are respectively provided with external threads, the bottom wall of the end cover and the surface of the drone body are respectively provided with upper threaded holes that cooperate with the top rod, and the surface of the bottom cover and the bottom wall of the drone body are respectively provided with lower threaded holes that cooperate with the bottom rod.

[0014] Compared with the prior art, the beneficial effects of the present invention are as follows: by setting the positioning assembly and the disassembly assembly to cooperate with each other, multiple groups of arc-shaped rods can be conveniently installed and disassembled on the outside of the drone body; by setting the adjustment assembly composed of the clamping part and the transmission part to cooperate with the storage assembly, the relative position of the blocking rod and the arc-shaped rod can be conveniently adjusted on the outside of the arc-shaped rod, thereby effectively preventing the arc-shaped rod and the drone body from rolling on the ground when landing, and effectively improving the safety performance of the drone body. The problem that the spherical shell of the drone cannot be conveniently installed and disassembled at present, the spherical drone has poor stability when landing, and the spherical drone is easy to roll at will, thereby causing damage to the drone, is solved. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 A schematic diagram of a spherical drone positioning structure provided in an embodiment of the present invention Figure 1 .

[0016] Figure 2 A schematic diagram of a spherical drone positioning structure provided in an embodiment of the present invention Figure 2 .

[0017] Figure 3 for Figure 1 Schematic diagram of the enlarged structure of A.

[0018] Figure 4 The present invention is a schematic structural diagram of a top plate and a bottom ring in a spherical UAV positioning structure provided in an embodiment of the present invention.

[0019] Figure 5 It is a schematic diagram of the main structure of a spherical UAV positioning structure provided in an embodiment of the present invention.

[0020] Figure 6 for Figure 5 Schematic diagram of the enlarged structure of B.

[0021] Figure 7 for Figure 5 Schematic diagram of the enlarged structure of C in the figure.

[0022] Figure 8 The present invention provides a schematic diagram of a supporting plate and its connection structure in a spherical UAV positioning structure.

[0023] Among them: 1-UAV body, 2-protection mechanism, 21-arc-shaped rod, 22-positioning assembly, 221-top rod, 222-end cover, 223-top hole, 224-bottom rod, 225-bottom cover, 226-bottom hole, 23-disassembly assembly, 231-top plate, 232-bottom ring, 233-upper positioning rod, 234-lower positioning rod, 235-upper connecting hole, 236-upper positioning hole, 237-lower connecting hole, 238-lower positioning hole, 239-first magnetic sheet, 230-second magnetic sheet, 3 -Anti-roll mechanism, 31-bumper rod, 32-storage assembly, 321-storage slot, 322-carrying plate, 33-adjustment assembly, 331-clamping part, 3311-telescopic slot, 3312-limiting column, 3313-limiting slot, 3314-extrusion spring, 332-transmission part, 3321-side plate, 3322-guide hole, 3323-pull rope, 3324-control spring, 4-sliding part, 41-sliding slot, 42-sliding block, 43-reset spring, 5-upper threaded hole, 6-lower threaded hole. DETAILED DESCRIPTION

[0024] It should be noted that, in the absence of conflict, the embodiments of the present invention and the features in the embodiments may be combined with each other.

[0025] The specific implementation of the present invention is described in detail below in conjunction with specific embodiments.

[0026] like Figure 1 , Figure 8As shown, it is a structural diagram of a spherical UAV positioning structure provided by an embodiment of the present invention, including a UAV body 1, a protective mechanism 2 is arranged on the outside of the UAV body 1, and the protective mechanism 2 includes an arc-shaped rod 21, a positioning component 22 and a disassembly component 23. The arc-shaped rod 21 is provided with multiple groups, and the positioning component 22 is located on the upper and lower sides of the UAV body 1 and is connected to the arc-shaped rod 21. The positioning component 22 is used to control multiple groups of arc-shaped rods 21 to be equally spaced around the outside of the UAV body 1. The disassembly component 23 is connected to the positioning component 22. The disassembly component 23 installs and disassembles the arc-shaped rod 21 on the outside of the UAV body 1 by cooperating with the positioning component 22. The surface of the arc-shaped rod 21 is provided with an anti-rolling mechanism 3, and the anti-rolling mechanism 3 includes There are a baffle rod 31, a storage assembly 32 and an adjustment assembly 33. The baffle rod 31 is provided with multiple groups. The storage assembly 32 is located on the surface of the arc-shaped rod 21 and is connected to the baffle rod 31. The storage assembly 32 is used to control multiple groups of baffle rods 31 to be located at equal intervals on the surface of the arc-shaped rod 21. The adjustment assembly 33 includes a clamping portion 331 and a transmission portion 332. The clamping portion 331 is located in the arc-shaped rod 21 and cooperates with the storage assembly 32. The clamping portion 331 controls the baffle rod 31 as a whole to be in the arc-shaped rod 21 by cooperating with the storage assembly 32. The transmission portion 332 is connected to the clamping portion 331. The transmission portion 332 controls the baffle rod 31 to rotate to the outside of the arc-shaped rod 21 by cooperating with the clamping portion 331 and controls the baffle rod 31 to maintain a vertical state with the arc-shaped rod 21.

[0027] Initially, the multiple groups of arc-shaped rods 21 and the drone body 1 are in a state of being separated from each other. When the drone body 1 needs to be used for flight, the positioning component 22 and the disassembly and assembly component 23 cooperate with each other, and the multiple groups of arc-shaped rods 21 can be easily installed at equal intervals on the outside of the drone body 1. At this time, the multiple groups of arc-shaped rods 21 are in the shape of hollow balls and wrap the drone body 1 inside. When the drone body 1 is flying, the multiple groups of arc-shaped rods 21 can safely protect the drone body 1, and can effectively prevent the wings on the outside of the drone body 1 from colliding with the external environment and causing damage. Initially, the clamping portion 331 cooperates with the storage assembly 32 to control the multiple groups of baffles 31 to be located inside the arc-shaped rod 21 as a whole. When the drone body 1 is landing, when the drone body 1 is tilted at an angle during landing, the arc-shaped rod 21 on the surface of the drone body 1 can further protect the drone body 1. The arc-shaped rod 21 can prevent the wings on the outside of the drone body 1 from directly contacting the ground. When the existing spherical drone is tilted at an angle during landing, the spherical drone will continue to roll on the ground. In the technical solution of the present application, when the arc-shaped rod 21 on the surface of the drone body 1 contacts the ground and rolls, the transmission portion 332 cooperates with the clamping portion 331 to control the baffle 31 on the surface of the arc-shaped rod 21 to automatically rotate to the outside of the arc-shaped rod 21, and the baffle 31 remains perpendicular to the arc-shaped rod 21. At this time, the baffle 31 can limit the arc-shaped rod 21, effectively preventing the arc-shaped rod 21 and the drone body 1 from continuously rolling on the ground.

[0028] like Figure 1 , Figure 2 , Figure 5 , Figure 6 , Figure 7 As shown, as a preferred embodiment of the present invention, the positioning component 22 includes a top rod 221 detachably mounted on the top wall of the drone body 1, an end cover 222 detachably mounted on the top end of the top rod 221, and a side wall of the end cover 222 is provided with a plurality of top holes 223 that cooperate with the top end of the arc-shaped rod 21; a bottom rod 224 detachably mounted on the bottom wall of the drone body 1, a bottom cover 225 detachably mounted on the bottom end of the bottom rod 224, and a side wall of the bottom cover 225 is provided with a plurality of bottom holes 226 that cooperate with the bottom end of the arc-shaped rod 21.

[0029] When the arc-shaped rod 21 needs to be installed, firstly, the top rod 221 and the bottom rod 224 are installed on the upper and lower sides of the drone body 1, and then the end cover 222 is installed on the top of the top rod 221, and the bottom cover 225 is installed on the bottom of the bottom rod 224. The top of the arc-shaped rod 21 is inserted into the top hole 223 on the side of the end cover 222, and the bottom of the arc-shaped rod 21 is inserted into the bottom hole 226 on the side of the bottom cover 225. The disassembly assembly 23 can conveniently fix the position of the arc-shaped rod 21 in the top hole 223 and the bottom hole 226. When the arc-shaped rod 21 needs to be disassembled outside the drone body 1, the disassembly assembly 23 releases the restriction on the arc-shaped rod 21 in the top hole 223 and the bottom hole 226, and the arc-shaped rod 21 can be conveniently removed from between the end cover 222 and the bottom cover 225.

[0030] like Figure 1 , Figure 2 , Figure 4 , Figure 5 , Figure 6 , Figure 7 As shown, as a preferred embodiment of the present invention, the disassembly and assembly component 23 includes a top plate 231 and a bottom ring 232, an upper connecting hole 235 connected to the top hole 223 is opened downward on the surface of the end cover 222, an upper positioning hole 236 is set at the top of the arc-shaped rod 21, an upper positioning rod 233 that cooperates with the upper positioning hole 236 is fixedly installed on the bottom wall of the top plate 231, two groups of first magnetic sheets 239 that cooperate with each other are fixedly installed on the two side walls opposite to the top plate 231 and the end cover 222, a lower connecting hole 237 connected to the bottom hole 226 is opened downward on the surface of the bottom cover 225, a lower positioning hole 238 is opened at the bottom end of the arc-shaped rod 21, a lower positioning rod 234 that cooperates with the lower positioning hole 238 is fixedly installed on the bottom wall of the bottom ring 232, and two groups of second magnetic sheets 230 that cooperate with each other are fixedly installed on the two side walls opposite to the bottom cover 225 and the bottom ring 232.

[0031] After the arc rod 21 is inserted into the top hole 223 and the bottom hole 226, the upper positioning hole 236 at the top of the arc rod 21 is aligned with the upper connecting hole 235, and the lower positioning hole 238 at the bottom end of the arc rod 21 is aligned with the lower connecting hole 237, and the top plate 231 is placed on the surface of the end cover 222. Two groups of first magnetic sheets 239 fix the position of the top plate 231 on the surface of the end cover 222 by magnetic attraction. At this time, the upper positioning rod 233 on the bottom wall of the top plate 231 is inserted into the upper positioning hole 236, and the bottom ring 232 is placed on the surface of the bottom cover 225. Two groups of second magnetic sheets 230 fix the bottom ring 232 on the surface of the bottom cover 225 by magnetic attraction, and the lower positioning rod 234 on the surface of the bottom ring 232 is inserted into the lower positioning hole 238, so that the arc rod 21 can be conveniently fixed and installed between the end cover 222 and the bottom cover 225.

[0032] like Figure 1 , Figure 3 , Figure 5 , Figure 6 , Figure 8 As shown, as a preferred embodiment of the present invention, the storage assembly 32 includes a plurality of equally spaced storage grooves 321 opened on the surface of the arc-shaped rod 21, a carrying plate 322 is rotatably installed in the storage groove 321, and the blocking rod 31 is fixedly installed on the surface of the carrying plate 322.

[0033] Initially, the clamping part 331 fixes the position of the carrier plate 322 in the receiving groove 321 on the surface of the arc-shaped rod 21. At this time, the arc-shaped rod 21 on the surface of the carrier plate 322 is entirely in the receiving groove 321. When the drone body 1 is landed, it tilts so that the arc-shaped rod 21 rolls on the ground. The transmission part 332 cooperates with the clamping part 331 to control the blocking rod 31 to rotate toward the outside of the receiving groove 321. After the blocking rod 31 rotates 90 degrees toward the outside of the receiving groove 321, the clamping part 331 fixes the position of the carrier plate 322 again in the receiving groove 321. At this time, the blocking rod 31 is outside the arc-shaped rod 21, which can effectively prevent the arc-shaped rod 21 and the drone body 1 from rolling continuously.

[0034] like Figure 1 , Figure 2 , Figure 3 , Figure 5 , Figure 8 As shown, as a preferred embodiment of the present invention, the clamping portion 331 includes telescopic grooves 3311 respectively opened on the two side walls opposite to the receiving groove 321, and a compression spring 3314 is fixedly installed in the telescopic groove 3311, and a limiting column 3312 is fixedly installed on the telescopic end of the compression spring 3314, and two groups of limiting grooves 3313 cooperating with the limiting column 3312 are opened on the side wall of the supporting plate 322.

[0035] When the locking cam 3312 is in the unlock state, the locking cam 3312 is in the unlock state, and the locking cam 3312 is locked.

[0036] like Figure 1 , Figure 2 , Figure 3 , Figure 5 , Figure 6 , Figure 8 As shown, as a preferred embodiment of the present invention, the transmission part 332 includes a side plate 3321 slidably installed on the side wall of the arc-shaped rod 21, the side wall of the arc-shaped rod 21 is provided with a sliding part 4 connected to the side plate 3321, the side wall of the arc-shaped rod 21 is provided with a guide hole 3322 connected to the telescopic groove 3311, the end of the limiting column 3312 is fixedly installed with a pulling rope 3323, the pulling rope 3323 passes through the guide hole 3322 and extends to the outside of the arc-shaped rod 21 and is connected to the side plate 3321, and the side wall of the storage groove 321 is fixedly installed with a control spring 3324 that cooperates with the gear lever 31.

[0037] When the arc-shaped rod 21 rolls on the ground, the pressure of the drone body 1 and the arc-shaped rod 21 will push the side plate 3321 to slide on the surface of the arc-shaped rod 21. At this time, the side plate 3321 and the pulling rope 3323 cooperate with each other to automatically pull the limiting column 3312 into the telescopic slot 3311. At this time, the limiting column 3312 and the limiting slot 3313 are separated from each other.

[0038] like Figure 1 , Figure 2 , Figure 3 , Figure 6 , Figure 8 As shown, as a preferred embodiment of the present invention, the sliding portion 4 includes a sliding groove 41 opened on the side wall of the arc-shaped rod 21, a sliding block 42 is slidably installed in the sliding groove 41, the sliding block 42 extends to the outside of the sliding groove 41 and is connected to the side plate 3321, and a return spring 43 connected to the sliding block 42 is fixedly installed in the sliding groove 41.

[0039] The sliding block 42 cooperates with the slide groove 41 to support and position the side plate 3321, so that the side plate 3321 is stably located outside the arc-shaped rod 21. When the arc-shaped rod 21 rolls on the ground, the sliding block 42 slides in the slide groove 41, thereby conveniently adjusting the position of the side plate 3321.

[0040] like Figure 1 , Figure 2 , Figure 5 , Figure 6 , Figure 7 As shown, as a preferred embodiment of the present invention, both ends of the top rod 221 and the bottom rod 224 are respectively provided with external threads, the bottom wall of the end cover 222 and the surface of the drone body 1 are respectively provided with upper threaded holes 5 that cooperate with the top rod 221, and the surface of the bottom cover 225 and the bottom wall of the drone body 1 are respectively provided with lower threaded holes 6 that cooperate with the bottom rod 224.

[0041] By providing the upper threaded hole 5 and the lower threaded hole 6 to cooperate with the external thread, the top rod 221 and the bottom rod 224 can be easily installed and removed on the surface of the drone body 1.

[0042] The working principle of the present invention is as follows: initially, the multiple groups of arc-shaped rods 21 are in a mutually separated state from the drone body 1. When the drone body 1 needs to be used for flight, the top rod 221 and the bottom rod 224 are first installed on the upper and lower sides of the drone body 1, respectively. Then, the end cover 222 is installed on the top of the top rod 221, and the bottom cover 225 is installed on the bottom of the bottom rod 224. The top of the arc-shaped rod 21 is inserted into the top hole 223 on the side of the end cover 222, and the bottom end of the arc-shaped rod 21 is inserted into the bottom hole 226 on the side of the bottom cover 225. After the arc-shaped rod 21 is inserted into the top hole 223 and the bottom hole 226, the upper positioning hole 236 at the top of the arc-shaped rod 21 is connected to the upper connecting hole 235. Align, the lower positioning hole 238 at the bottom end of the arc-shaped rod 21 is aligned with the lower connecting hole 237, the top plate 231 is placed on the surface of the end cover 222, and the two groups of first magnetic sheets 239 fix the position of the top plate 231 on the surface of the end cover 222 by magnetic attraction. At this time, the upper positioning rod 233 on the bottom wall of the top plate 231 is inserted into the upper positioning hole 236, and the bottom ring 232 is placed on the surface of the bottom cover 225. The two groups of second magnetic sheets 230 fix the bottom ring 232 on the surface of the bottom cover 225 by magnetic attraction, and the lower positioning rod 234 on the surface of the bottom ring 232 is inserted into the lower positioning hole 238, so that the arc-shaped rod 21 can be conveniently fixed and installed between the end cover 222 and the bottom cover 225. At this time, the multiple groups of arc-shaped rods 21 are in the shape of a hollow ball to wrap the drone body 1 inside. When the drone body 1 is flying, the multiple groups of arc-shaped rods 21 can provide safety protection for the drone body 1, and can effectively prevent the wings outside the drone body 1 from colliding with the external environment and causing damage.

[0043] When the drone body 1 is landing, when the angle of the drone body 1 is tilted during landing, the arc-shaped rod 21 on the surface of the drone body 1 can further protect the drone body 1. The arc-shaped rod 21 can prevent the wings on the outside of the drone body 1 from directly contacting the ground. When the existing spherical drone is tilted during landing, the spherical drone will continue to roll on the ground. In the technical solution of the present application, when the arc-shaped rod 21 on the surface of the drone body 1 contacts the ground and rolls, the pressure of the drone body 1 and the arc-shaped rod 21 will push the side plate 3321 to slide on the surface of the arc-shaped rod 21. At this time, the side plate 3321 cooperates with the pulling rope 3323 to automatically pull the limit column 3312 into the telescopic slot 3311. At this time, the limit column 3312 and the limit slot 3313 are separated from each other. The limiting column 3312 releases the limit on the carrier plate 322, and the transmission part 332 applies a thrust to the blocking rod 31, so that the blocking rod 31 rotates to the outside of the storage groove 321. After the blocking rod 31 rotates 90 degrees, the limiting column 3312 is inserted into another set of limiting grooves 3313 on the surface of the carrier plate 322. The limiting column 3312 can conveniently fix the position of the carrier plate 322 and the blocking rod 31. At this time, the blocking rod 31 can limit the arc rod 21, effectively preventing the arc rod 21 and the drone body 1 from continuously rolling on the ground.

[0044] The preferred embodiments of the present invention are described in detail above, but the present invention is not limited to the above embodiments. Various changes can be made within the knowledge scope of ordinary technicians in this field without departing from the purpose of the present invention.

Claims

1. A spherical drone positioning structure, comprising a drone body, characterized in that: A protective mechanism is arranged on the outside of the drone body, and the protective mechanism includes an arc-shaped rod, a positioning assembly and a disassembly assembly. The arc-shaped rod is provided with multiple groups. The positioning assembly is located on the upper and lower sides of the drone body and is connected to the arc-shaped rod. The positioning assembly is used to control multiple groups of arc-shaped rods to surround the outside of the drone body at equal intervals. The disassembly assembly is connected to the positioning assembly. The disassembly assembly installs and disassembles the arc-shaped rod on the outside of the drone body by cooperating with the positioning assembly. An anti-roll mechanism is arranged on the surface of the arc-shaped rod, and the anti-roll mechanism includes a stopper, a storage assembly, and a plurality of arc-shaped rods. Parts and adjustment components, the baffle rods are provided with multiple groups, the storage component is located on the surface of the arc-shaped rod and connected to the baffle rod, the storage component is used to control the multiple groups of baffle rods to be located on the surface of the arc-shaped rod at equal intervals, the adjustment component includes a clamping part and a transmission part, the clamping part is located in the arc-shaped rod and cooperates with the storage component, the clamping part controls the baffle rod as a whole to be in the arc-shaped rod by cooperating with the storage component, the transmission part is connected to the clamping part, the transmission part controls the baffle rod to rotate to the outside of the arc-shaped rod by cooperating with the clamping part and controls the baffle rod to maintain a vertical state with the arc-shaped rod.

2. A spherical UAV positioning structure according to claim 1, characterized in that: The positioning assembly includes a top rod detachably mounted on the top wall of the drone body, an end cover detachably mounted on the top end of the top rod, and a side wall of the end cover is provided with a plurality of top holes that cooperate with the top end of the arc-shaped rod; a bottom rod detachably mounted on the bottom wall of the drone body, a bottom cover detachably mounted on the bottom end of the bottom rod, and a side wall of the bottom cover is provided with a plurality of bottom holes that cooperate with the bottom end of the arc-shaped rod.

3. A spherical UAV positioning structure according to claim 2, characterized in that: The disassembly and assembly component includes a top plate and a bottom ring, an upper connecting hole connected to the top hole is opened downwardly on the surface of the end cover, an upper positioning hole is arranged on the top end of the arc-shaped rod, an upper positioning rod matching with the upper positioning hole is fixedly installed on the bottom wall of the top plate, two groups of first magnetic sheets matching with each other are fixedly installed on the two side walls opposite to the top plate and the end cover, a lower connecting hole connected to the bottom hole is opened downwardly on the surface of the bottom cover, a lower positioning hole is opened at the bottom end of the arc-shaped rod, a lower positioning rod matching with the lower positioning hole is fixedly installed on the bottom wall of the bottom ring, and two groups of second magnetic sheets matching with each other are fixedly installed on the two side walls opposite to the bottom cover and the bottom ring.

4. The spherical UAV positioning structure according to claim 1, characterized in that: The storage assembly comprises a plurality of storage grooves which are arranged on the surface of an arc-shaped rod and are distributed at equal intervals. A carrying plate is rotatably installed in the storage groove, and the blocking rod is fixedly installed on the surface of the carrying plate.

5. A spherical UAV positioning structure according to claim 4, characterized in that: The clamping part includes telescopic grooves respectively opened on the two side walls opposite to the storage groove, an extrusion spring is fixedly installed in the telescopic groove, a limiting column is fixedly installed on the telescopic end of the extrusion spring, and two groups of limiting grooves cooperating with the limiting column are opened on the side wall of the supporting plate.

6. A spherical UAV positioning structure according to claim 5, characterized in that: The transmission part includes a side plate slidably mounted on the side wall of the arc-shaped rod, the side wall of the arc-shaped rod is provided with a sliding part connected to the side plate, the side wall of the arc-shaped rod is provided with a guide hole connected to the telescopic groove inwardly, a pulling rope is fixedly mounted on the end of the limit column, the pulling rope extends through the guide hole to the outside of the arc-shaped rod and is connected to the side plate, and a control spring cooperating with the gear lever is fixedly mounted on the side wall of the storage groove.

7. A spherical UAV positioning structure according to claim 6, characterized in that: The sliding part includes a sliding groove opened on the side wall of the arc-shaped rod, a sliding block is slidably installed in the sliding groove, the sliding block extends to the outside of the sliding groove and is connected to the side plate, and a return spring connected to the sliding block is fixedly installed in the sliding groove.

8. The spherical UAV positioning structure according to claim 2, characterized in that: External threads are respectively provided at both ends of the top rod and the bottom rod, upper threaded holes cooperating with the top rod are respectively provided on the bottom wall of the end cover and the surface of the drone body, and lower threaded holes cooperating with the bottom rod are respectively provided on the surface of the bottom cover and the bottom wall of the drone body.

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