CN216509166U - Vehicle-mounted unmanned aerial vehicle platform - Google Patents

Vehicle-mounted unmanned aerial vehicle platform Download PDF

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Publication number
CN216509166U
CN216509166U CN202220215546.9U CN202220215546U CN216509166U CN 216509166 U CN216509166 U CN 216509166U CN 202220215546 U CN202220215546 U CN 202220215546U CN 216509166 U CN216509166 U CN 216509166U
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guide rail
feathering
lead screw
vehicle
platform
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CN202220215546.9U
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董铂龙
印杰
任强
吴勇
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Chongqing Yufeite Technology Co ltd
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Chongqing Yufeite Technology Co ltd
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Abstract

The utility model belongs to the technical field of aircraft associated facilities, and particularly relates to a vehicle-mounted unmanned aerial vehicle platform which comprises a platform body for taking off and landing of an unmanned aerial vehicle, wherein the platform body comprises a taking-off and landing surface, a homing mechanism is installed on the taking-off and landing surface, a material passing port is formed in the middle of the taking-off and landing surface, a loading and unloading structure is arranged below the platform body and comprises a horizontal conveying roller and a vertical lifting device, the vertical lifting device is positioned below the material passing port, the tail end of the horizontal conveying roller faces the vertical lifting device, the feathering device comprises two feathering plates, the two feathering plates are respectively installed in the middle of two opposite sides of the taking-off and landing surface, the end parts of the feathering plates are connected with a first motor for driving the feathering plates to vertically rotate, and the width of the feathering plates is not less than the distance between two rotor wing tips when the two rotors on the same side are parallel. The utility model provides a highly integrated and vehicle-mounted unmanned aerial vehicle platform.

Description

Vehicle-mounted unmanned aerial vehicle platform
Technical Field
The utility model belongs to the technical field of aircraft associated facilities, and particularly relates to a vehicle-mounted unmanned aerial vehicle platform.
Background
An unmanned aerial vehicle is an unmanned aerial vehicle operated by utilizing radio remote control equipment and a self-contained program control device, and is widely applied to the fields of aerial photography, patrol, agriculture, plant protection, miniature self-timer, express transportation, disaster rescue, wild animal observation, mapping, news reporting, electric power inspection, disaster relief, movie shooting and the like due to the advantages of low cost, low risk, strong viability, good maneuvering performance and the like.
Based on present limited wireless charging and communication technology, unmanned aerial vehicle can't be for a long time outside independent work. In order to guarantee the long voyage and the good communication quality of unmanned aerial vehicle under scenes such as aerial photography, patrol, survey and drawing, still need be equipped with charging system for unmanned aerial vehicle usually, communication system and the platform that supplies unmanned aerial vehicle to take off and land, to the unmanned aerial vehicle that has the storehouse system, still need be equipped with handling device, in addition unmanned aerial vehicle's rotor still need occupy certain space usually, the space that leads to whole unmanned aerial vehicle platform to occupy is great, hardly with vehicle-mounted system integration in order to improve mobility.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a vehicle-mounted unmanned aerial vehicle platform, and provides a highly integrated unmanned aerial vehicle platform suitable for vehicles.
In order to achieve the purpose, the scheme of the utility model is as follows: on-vehicle unmanned aerial vehicle platform, including the platform body that is used for unmanned aerial vehicle to take off and land, the platform body is including the face of taking off and land, it constructs to install playback mechanism on the face of taking off and land, it has the drain hole to open at the face of taking off and land middle part, platform body below is equipped with handling structure, handling structure includes horizontal conveying roller and perpendicular lifting device, perpendicular lifting device is located the drain hole below, the end of horizontal conveying roller is towards perpendicular lifting device, feathering device includes two feathering boards, the middle part in the relative both sides of face of taking off and land is installed respectively to two feathering boards, the end connection in the same direction of feathering board has the first motor of the vertical pivoted of drive feathering board, the width in the same direction of feathering board is not less than the distance between two rotor tips when two rotors of homonymy are parallel.
The working principle and the beneficial effects of the scheme are as follows: after the unmanned aerial vehicle lands on the platform, the homing mechanism will park the unmanned aerial vehicle on the platform and homing to the central point of platform puts, both does benefit to the feathering, and the storehouse of the unmanned aerial vehicle of being convenient for again aims at the material passing mouth in the middle part of the lifting surface so that load and unload the storehouse. When loading the warehouse, on the delivery roller was put into to the warehouse that the loading and unloading workman will be equipped with the goods, the delivery roller transported the warehouse for perpendicular lifting device, perpendicular lifting device was listed as the warehouse from the punishment in advance mouth, unmanned aerial vehicle loads on the warehouse can. Otherwise, the cargo compartment can be disassembled. When needing the feathering, unmanned aerial vehicle lands back on the face of taking off and land, and the feathering board only need rotate to vertical position clockwise earlier, then rotates vertical position anticlockwise again, can let the rotor point of two rotors of homonymy support on the feathering board inboard surface to realize the feathering. The unmanned aerial vehicle after feathering occupies a small space (especially, the width). This scheme highly integrated to same platform body with each supporting system of unmanned aerial vehicle on, spatial layout is reasonable, compact structure, and it is integrated with various on-vehicle systems (especially have the on-vehicle system of container) to be applicable to very much.
Optionally, be equipped with vertical reciprocating motion's the fill of lifting on the perpendicular lifting devices, the end orientation of conveying roller lifts the fill, be equipped with storehouse push-and-pull device on the side of conveying roller, storehouse push-and-pull device includes first guide rail, first lead screw and first motor, first guide rail is on a parallel with the direction of delivery of conveying roller and installs the side of conveying roller, sliding connection has first slide on the first guide rail, install the pusher dog on the first slide, the pusher dog is connected with first slide, first lead screw nut installs on first slide, the first lead screw axle of first lead screw is by first motor drive.
First motor rotates and to pass through the reciprocal slip of first slide of first lead screw drive on first guide rail to on the storehouse of drive pusher dog push-and-pull conveying roller on the first slide lifted the fill, lifted the fill again and followed the punishment in advance mouth with the storehouse from unmanned aerial vehicle loading and unloading.
Optionally, the pusher dog is in a [ -shape formed by butt joint of two L-shaped auxiliary pawls, one of which is rotatably connected to the first sliding seat and the end of which is connected to a second motor for driving the pusher dog to rotate in the horizontal direction.
The [ -shaped pusher dog can form a bending force application end at two ends, and after the warehouse is placed between the two force application ends of the pusher dog, the pusher dog can conveniently push and pull the warehouse. When the second motor rotates the two force application ends of the pusher dog to the horizontal direction, the pusher dog can be used for pushing and pulling the cargo compartment, and when the two force application ends rotate to the vertical direction, the force application ends can be prevented from touching the cargo compartment.
Optionally, the vertical lifting device includes a second guide rail vertically arranged, the second guide rail is slidably connected to a second sliding base, the second sliding base is driven by a second lead screw, and the lifting bucket is horizontally fixed on the second sliding base; the device also comprises a third guide rail which is horizontally arranged, a third sliding seat driven by a third lead screw is arranged on the third guide rail, and the second guide rail is vertically fixed on the third sliding seat.
Utilize the second lead screw drive to lift the fill and at the vertical reciprocating motion of second guide rail in vertical direction, operate steadily, bearing capacity is strong.
Optionally, the device further comprises a horizontally arranged third guide rail, a third sliding base driven by a third lead screw is arranged on the third guide rail, and the second guide rail is vertically fixed on the third sliding base.
Through third guide rail and third slide, the whole perpendicular lifting device of horizontal translation in the horizontal direction, be convenient for adjust perpendicular lifting device and cross the relative position between material mouth, the conveying roller.
Optionally, the homing mechanism includes two sets of homing rods, each set of homing rods is parallel to each other, the feathering plate is located between one set of homing rods, two ends of the homing rods are slidably connected with the side of the platform, the two sets of homing rods are vertically distributed in a staggered manner, and two ends of the homing rods are connected with the fourth lead screw.
Optionally, four locking arm openings are formed in the lifting surface, and a locking arm mechanism which can be vertically stretched is arranged below each locking opening; the locking arm mechanism comprises a vertically arranged fourth guide rail, a fifth lead screw and a locking rod, the fifth lead screw is arranged on the fourth guide rail in parallel, a fourth sliding seat is connected onto the fourth guide rail in a sliding mode, a lead screw nut of the fifth lead screw is fixed onto the fourth sliding seat, the locking rod is arranged on the fourth sliding seat, and a lock head is arranged on one upward end of the locking rod.
Unmanned aerial vehicle all has four rotors usually, and locking arm mechanism stretches out from the locking arm mouth, and the fifth lead screw rotates and can drive the tapered end and reciprocate in vertical direction, and the tapered end stretches out in the locking arm mouth, and the tapered end stretches out the locking arm mouth and can lock the rotor arm on the locking lever to with the unmanned aerial vehicle locking on the platform, reduce the vibration of unmanned aerial vehicle when the transportation, further reduce the friction between rotor tip and the feathering board.
Optionally, the lock head comprises a lock groove and a connecting rod, the lock groove of the lock head penetrates through and is slidably connected with a lock pin, a through hole is formed in the lock head in parallel with the lock pin, a power rod is slidably connected in the through hole, the power rod and the lock pin are fixedly connected with the connecting rod, and the power rod is connected with a linear driving device.
The linear driving device drives the power rod to drive the lock pin to move, the rotor arm can be locked in the lock groove when the lock pin penetrates through the lock groove, and the linear driving device moves in the reverse direction to withdraw the lock pin from the lock groove when the rotor arm needs to be taken out. The linear driving device is preferably one of an electric cylinder, a linear motor, a gear rack mechanism, a hydraulic cylinder and a pneumatic cylinder.
Optionally, the lock head is further provided with a guide hole, the guide hole is parallel to the lock pin, a guide rod is connected in the guide hole in a sliding manner, and the guide rod is fixed with the connecting rod.
The power rod and the lock pin can further keep parallel and stably move by the guiding action of the guide rod.
Optionally, a wear-resistant layer is arranged on one surface of the feathering plate facing the platform, and the roughness of the wear-resistant layer is less than 3.2.
Unmanned aerial vehicle is when the vehicle-mounted transportation, can take place relative motion because of the vehicle vibration between unmanned aerial vehicle rotor and the feathering, and relative motion can produce certain sliding friction, through adopting more smooth wearing layer, can reduce the wearing and tearing between rotor and the feathering mechanism.
Drawings
Fig. 1 is a schematic mechanism diagram of a vehicle-mounted unmanned aerial vehicle platform according to an embodiment of the utility model;
FIG. 2 is a schematic structural diagram of a loading/unloading structure according to an embodiment of the present invention;
FIG. 3 is a schematic view of the push-pull device of the warehouse according to the embodiment of the present invention;
FIG. 4 is a schematic diagram of a locking arm mechanism according to an embodiment of the present invention.
The reference numbers in the drawings of the specification include: the device comprises a platform body 1, a lifting surface 2, a material passing port 3, a vertical lifting device 4, a conveying roller 5, a conveying frame 6, a first motor 7, a first lead screw 8, a first sliding seat 9, a first lead screw nut 10, a pusher dog 11, an auxiliary pawl 12, a first guide rail 13, a second guide rail 14, a third guide rail 15, a second sliding seat 16, a lifting hopper 17, a third sliding seat 18, a second motor 19, a feathering plate 20, a cover plate 21, a fourth motor 22, a fifth motor 23, a fourth lead screw 24, a fifth lead screw 25, a fourth guide rail 26, a fourth sliding seat 27, a lock rod 28, a lock groove 29, a lock pin 30, a power rod 31, a connecting rod 32 and a return rod 33.
Detailed Description
The following is further detailed by way of specific embodiments:
examples
The embodiment is basically as shown in the attached figures 1, 2, 3 and 4: on-vehicle unmanned aerial vehicle platform, including handling structure and the platform body 1 that is used for unmanned aerial vehicle to take off and land, platform body 1 is including the face 2 that takes off and land, it has material through hole 3 to open on the face 2 that takes off and land, handling structure includes horizontal conveying roller 5 and perpendicular lifting device 4, perpendicular lifting device 4 is located material through hole 3 below, be equipped with vertical reciprocating motion's lifting fill 17 on the perpendicular lifting device 4, be equipped with storehouse push-and-pull device on the side of conveying roller 5, conveying roller 5 is installed on carriage 6, the gyro wheel is installed to carriage 6 below. It has four locking arm mouths to open on the face 2 that takes off and land, and locking arm mouth upper cover has closed apron 21, and one side of apron 21 is articulated through a pivot and a side of punishment in advance mouth 3, is connected with the gate motor that is used for opening and close apron 21 in the pivot, and when apron 21 was closed, apron 21 top surface and 2 parallel and level of face that takes off and land.
The warehouse push-pull device comprises a first guide rail 13, a first lead screw 8 and a first motor 7, wherein the first guide rail 13 is arranged on the side edge of the conveying roller 5 in a direction parallel to the conveying direction of the conveying roller 5, a first sliding seat 9 is connected onto the first guide rail 13 in a sliding manner, a pusher dog 11 is arranged on the first sliding seat 9, the pusher dog 11 is in a [ "shape formed by butting two L-shaped auxiliary claws 12, one auxiliary claw 12 is connected onto the first sliding seat 9 in a rotating manner, the end part of the auxiliary claw is connected with a second motor 19 for driving the pusher dog 11 to rotate in the horizontal direction, a first lead screw nut 10 is arranged on the first sliding seat 9, and a first lead screw shaft of the first lead screw 8 is driven by the first motor 7.
The vertical lifting device 4 comprises a second guide rail 14 which is vertically arranged, the second guide rail 14 is slidably connected with a second sliding base 16, the second sliding base 16 is driven by a second lead screw, and a lifting bucket 17 is horizontally fixed on the second sliding base 16. The device also comprises a third guide rail 15 which is horizontally arranged, a third sliding seat 18 driven by a third lead screw is arranged on the third guide rail 15, and the second guide rail 14 is vertically fixed on the third sliding seat 18.
Still install feathering device on the platform body 1, feathering device includes two feathering boards 20, and two feathering boards 20 are installed respectively in the middle part in the relative both sides of the face of rising and falling 2, and the end connection of feathering board 20 has the drive in the same direction as the vertical pivoted third motor of oar board 20, and the third motor is servo motor, and the width of feathering board 20 is not less than the distance between two rotor wing tips when two rotors of homonymy are parallel. The feathering board 20 is coated with copper foil on the surface facing the rising and falling surface 2.
Still include the playback mechanism, the playback mechanism includes two sets of pole 33 that return, and the quantity of every group pole 33 that returns is two and parallel to each other, and feathering plate 20 is located between one of them set of pole 33 that returns, and the both ends and the platform body 1 side sliding connection of pole 33 that return, two sets of pole 33 that return distribute crisscross perpendicularly, and the pole 33 both ends that return all are connected with fourth lead screw 24, connect fourth motor 22 on the fourth lead screw 24.
A locking arm mechanism is arranged below each locking arm opening and comprises a fourth guide rail 26, a fifth lead screw 25 and a locking rod 28 which are vertically arranged, the fourth guide rail 26 is fixed below the platform body 1, the fifth lead screw 25 is parallelly arranged on the fourth guide rail 26, and the fifth lead screw is connected with a fifth motor 23. The fourth slide carriage 27 is connected to the fourth guide rail 26 in a sliding manner, a screw nut of the fifth screw 25 is fixed to the fourth slide carriage 27, the lock rod 28 is installed on the fourth slide carriage 27, and a lock head is arranged at one upward end of the lock rod 28. The lock head comprises a lock groove 29 and a connecting rod 32, the lock groove 29 of the lock head is penetrated and slidably connected with a lock pin 30, a through hole is formed in the lock head in parallel with the lock pin 30, a power rod 31 is slidably connected in the through hole, the power rod 31 and the lock pin 30 are fixedly connected with the connecting rod 32, the power rod 31 is connected with an electric cylinder, and the electric cylinder is fixed below the platform body 1. The lock head is also provided with a guide hole which is parallel to the lock pin 30, a guide rod is connected in the guide hole in a sliding way, and the guide rod is fixed with a connecting rod 32.
The specific implementation process comprises the following steps:
when unmanned aerial vehicle stopped on the plane of taking off and landing 2, the gate motor drove apron 21 and rotates as for 2 parallel and level of plane of taking off and landing, and unmanned aerial vehicle can freely translate on plane of taking off and landing 2 and apron 21.
After the unmanned aerial vehicle lands on the plane of taking off and landing 2, fourth motor 22 drive fourth lead screw 24 rotates, drives each pole 33 that resets and presss from both sides to the inboard, with the unmanned aerial vehicle center of the plane of taking off and landing 2 that resets.
Through the rotation of third lead screw, the perpendicular lifting mechanism translation of drive is under the material passing port 3, lets lift fill 17 be located the material passing port 3 under, promotes conveying roller 5 adjustment position, adjusts the upper and lower position of lifting fill 17, until lifting fill 17 and conveying roller 5 parallel and level. Meanwhile, the door control motor drives the cover plate 21 to rotate, and the material passing port 3 is opened.
When loading the warehouse, unmanned aerial vehicle berths the punishment in mouth 3 departments of crossing of the face of taking off and land 2, and the loading and unloading workman only need put into the conveying roller 5 with the warehouse that is equipped with the goods on, and second motor 19 rotates, lets pusher dog 11 erect, and first lead screw 8 of first motor 7 drive lets pusher dog 11 remove near the warehouse, then second motor 19 reversal, lets the both ends level of pusher dog 11 place and let the warehouse arrange in between 11 both ends of pusher dog. The first motor 7 then drives the first threaded spindle 8 again, the first carriage 9 moves in the direction of the lifting hopper 17 until the loading bay is pushed onto the lifting hopper 17, and the second motor 19 rotates again, so that the pusher 11 is set up again. Then through the rotation of second lead screw, let second slide 16 drive lift fill 17 and the perpendicular rising of storehouse, until the storehouse is installed the unmanned aerial vehicle below can.
When unloading the storehouse of carrying cargo, unmanned aerial vehicle unloads the storehouse from punishment in advance mouth 3, and the storehouse falls to lifting on fighting 17, and second lead screw antiport lifts fighting 17 and descends to behind the parallel and level with conveying roller 5, and second motor 19 rotates, lets the both ends level of pusher dog 11 place and let the storehouse place in between 11 both ends of pusher dog. The first motor 7 then drives the first threaded spindle 8 again, and the first carriage 9 is moved away from the lifting hopper 17 until the loading bay is pushed onto one end of the conveyor roller 5, and the loading and unloading worker can remove the loading bay.
The cylinder is extended to withdraw the pin 30 from the lock and expose the slot 29. Then four fifth motors 23 start simultaneously, let locking lever 28 rise, back in the lock slot 29 is entered into completely to the lock head back of pushing up apron 21 and unmanned aerial vehicle's rotor arm, and the electric jar shrink, and lockpin 30 inserts once more back on the lock head to lock whole unmanned aerial vehicle to the platform. The third motor drives the feathering plate 20 to rotate clockwise to the vertical position first, and then rotate anticlockwise to the vertical position, so that the rotor tips of the two rotors on the same side are supported on the inner side surface of the feathering plate 20, and thereby feathering is realized.
When the unmanned plane wants to take off, the feathering plates 20 are rotated to be in a horizontal state and are collected at two sides of the lifting surface 2, then the lock pin 30 is pulled out, the fifth motor 23 rotates reversely, and the lock rod 28 is collected below the lifting surface 2. The fourth motor 22 rotates in the reverse direction, and the fifth screw drives all the return rods 33 to return. After the actions are completed, the unmanned aerial vehicle can take off.
The foregoing is merely an example of the present invention and common general knowledge of known specific structures and features of the embodiments is not described herein in any greater detail. It should be noted that, for those skilled in the art, without departing from the structure of the present invention, several changes and modifications can be made, which should also be regarded as the protection scope of the present invention, and these will not affect the effect of the implementation of the present invention and the practicability of the present invention. The descriptions in the embodiments and the like in the specification can be used to explain the contents of the claims.

Claims (10)

1. On-vehicle unmanned aerial vehicle platform, its characterized in that: including the platform body that is used for unmanned aerial vehicle to take off and land, the platform body is including the face of taking off and land, install playback mechanism on the face of taking off and land, it has the material crossing port to open at the face of taking off and land middle part, platform body below is equipped with handling structure, handling structure includes horizontal conveying roller and perpendicular lifting device, perpendicular lifting device is located the material crossing port below, the end of horizontal conveying roller is towards perpendicular lifting device, feathering device includes two feathering plates, the middle part in the relative both sides of the face of taking off and land is installed respectively to two feathering plates, the end connection in the same direction of feathering plate has the first motor of the vertical pivoted of drive feathering plate, the width in the same direction of feathering plate is not less than the distance between two rotor tips when two rotors of homonymy are parallel.
2. The vehicle-mounted drone platform of claim 1, wherein: be equipped with vertical reciprocating motion's lifting bucket on the perpendicular lifting device, the end orientation lifting bucket of conveying roller, be equipped with storehouse push-and-pull device on the side of conveying roller, storehouse push-and-pull device includes first guide rail, first lead screw and first motor, first guide rail is on a parallel with the direction of delivery of conveying roller and installs the side of conveying roller, sliding connection has first slide on the first guide rail, install the pusher dog on the first slide, the pusher dog is connected with first slide, first lead screw nut installs on first slide, the first lead screw axle of first lead screw is by first motor drive.
3. The vehicle-mounted drone platform of claim 2, wherein: the pusher dog is in a [ -shape by butt joint of two L-shaped auxiliary claws, wherein one auxiliary claw is rotatably connected to the first sliding seat, and the end part of the auxiliary claw is connected with a second motor for driving the pusher dog to rotate in the horizontal direction.
4. The vehicle-mounted drone platform of claim 3, wherein: the vertical lifting device comprises a second guide rail which is vertically arranged, a second sliding seat is connected to the second guide rail in a sliding manner, the second sliding seat is driven by a second lead screw, and the lifting hopper is horizontally fixed on the second sliding seat; the device also comprises a third guide rail which is horizontally arranged, a third sliding seat driven by a third lead screw is arranged on the third guide rail, and the second guide rail is vertically fixed on the third sliding seat.
5. The vehicle-mounted drone platform of claim 4, wherein: the device also comprises a third guide rail which is horizontally arranged, a third sliding seat driven by a third lead screw is arranged on the third guide rail, and the second guide rail is vertically fixed on the third sliding seat.
6. The vehicle-mounted drone platform of claim 5, wherein: the homing mechanism comprises two groups of homing rods, the number of each group of homing rods is two, the homing rods are parallel to each other, the feathering plates are positioned between one group of homing rods, the two ends of the homing rods are slidably connected with the side edges of the platform, the two groups of homing rods are vertically distributed in a staggered manner, and the two ends of each homing rod are connected with a fourth lead screw.
7. The vehicle-mounted drone platform of claim 6, wherein: four locking arm openings are formed in the lifting surface, and a locking arm mechanism which can be vertically stretched is arranged below each locking opening; the locking arm mechanism comprises a vertically arranged fourth guide rail, a fifth lead screw and a locking rod, the fifth lead screw is arranged on the fourth guide rail in parallel, a fourth sliding seat is connected onto the fourth guide rail in a sliding mode, a lead screw nut of the fifth lead screw is fixed onto the fourth sliding seat, the locking rod is arranged on the fourth sliding seat, and a lock head is arranged on one upward end of the locking rod.
8. The vehicle-mounted drone platform of claim 7, wherein: the lock head comprises a lock groove and a connecting rod, the lock groove part of the lock head is penetrated and slidably connected with a lock pin, a through hole is formed in the lock head in parallel with the lock pin, a power rod is slidably connected in the through hole, the power rod and the lock pin are fixedly connected with the connecting rod, and the power rod is connected with a linear driving device.
9. The vehicle-mounted drone platform of claim 8, wherein: the lock head is also provided with a guide hole, the guide hole is parallel to the lock pin, a guide rod is connected in the guide hole in a sliding manner, and the guide rod is fixed with the connecting rod.
10. The vehicle-mounted drone platform of claim 9, wherein: and a wear-resistant layer is arranged on one surface of the feathering plate facing the platform, and the roughness of the wear-resistant layer is less than 3.2.
CN202220215546.9U 2022-01-26 2022-01-26 Vehicle-mounted unmanned aerial vehicle platform Active CN216509166U (en)

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Application Number Priority Date Filing Date Title
CN202220215546.9U CN216509166U (en) 2022-01-26 2022-01-26 Vehicle-mounted unmanned aerial vehicle platform

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Application Number Priority Date Filing Date Title
CN202220215546.9U CN216509166U (en) 2022-01-26 2022-01-26 Vehicle-mounted unmanned aerial vehicle platform

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117918125A (en) * 2024-01-22 2024-04-26 华南农业大学 Unmanned aerial vehicle carrying device and operation method

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117918125A (en) * 2024-01-22 2024-04-26 华南农业大学 Unmanned aerial vehicle carrying device and operation method
CN117918125B (en) * 2024-01-22 2026-01-30 华南农业大学 A drone transport device and operating method

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