Load preassembling device for unmanned aerial vehicle
By using the automated design of pre-installed devices on drone payloads, the problem of wasted time due to manual operation in drone rescue systems is solved, enabling rapid response and low-cost automated delivery of rescue supplies.
Patent Information
- Application Number
- CN202511847597.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-12-09
- Publication Date
- 2026-01-16
AI Technical Summary
Existing drone rescue systems rely on manual operation, resulting in long delivery times for rescue supplies and an inability to respond quickly in emergencies.
Design a payload pre-loading device for UAVs, including a mounting component, a locking component, and a gripping component for fixed connection to the drone nest, to realize the automated pre-loading and mounting of the throwing component. Through the electrical connection and locking connection between the gripping component and the throwing component, the entire process is automated.
It shortens the time for delivering relief supplies from tens of minutes in traditional manual operations to minutes, reduces the reliance on professional drone pilots, supports unattended operations, and reduces maintenance costs.
Smart Images

Figure CN121341418A_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The present application relates to the technical field of unmanned aerial vehicle emergency rescue, in particular to a load preloading device for unmanned aerial vehicle. BACKGROUND
[0002] When an emergency event occurs, such as lifesaving or a terrorist event, different urgent needs will be faced, and emergency relief materials need to be delivered to rescuers or people in distress in a split second. It is difficult to achieve instant point-to-point rescue through personnel and ground transportation vehicles. At this time, the corresponding materials can be delivered to the scene by unmanned aerial vehicles. When an emergency event occurs, the traffic around the event often becomes congested, and delivering emergency materials through the air is the best way.
[0003] The prior art mainly relies on the manual mounting of rescue materials by the operator of the unmanned aerial vehicle, and the unmanned aerial vehicle is flown to the scene for delivery. Decision-making and reaction time are required. From receiving the call to the arrival of the operator at the scene to mount the materials, to take off and rescue, the whole process is time-consuming and long, and the valuable golden rescue time is easily missed. In the case of unmanned operation, the mounting of materials cannot be performed. SUMMARY
[0004] The purpose of the present application is to provide a load preloading device for unmanned aerial vehicle, which can effectively shorten the delivery time of rescue.
[0005] In order to achieve the above purpose, the present application adopts the following technical scheme: The load preloading device for unmanned aerial vehicle comprises a mounting assembly fixedly connected with a nest, and a locking assembly fixedly connected with the unmanned aerial vehicle, and the locking assembly is electrically connected with the unmanned aerial vehicle. The mounting assembly is drivingly connected with a grabbing assembly, the grabbing assembly is installed in the mounting assembly, the grabbing assembly is snapingly connected with a delivery assembly for loading emergency rescue materials, the delivery assembly is releasably connected with the locking assembly, and the locking assembly is electrically connected with the delivery assembly.
[0006] Further, the mounting assembly comprises an installation plate fixedly connected with the nest, the installation plate is fixedly connected with a surrounding plate, the installation plate and the surrounding plate form an installation chamber, the installation plate is fixedly connected with a grabbing driving motor, the grabbing driving motor is arranged in the installation chamber, the grabbing driving motor is drivingly connected with a lead screw, the lead screw is threadedly connected with the grabbing assembly, the installation plate is fixedly connected with a guide rail for moving, guiding and limiting the grabbing assembly, the guide rail is arranged parallel to the lead screw, and the grabbing assembly is slidingly connected with the guide rail.
[0007] Further, the installation plate is fixedly connected with a plurality of limiting columns for the alignment and preloading of the delivery assembly, and the free end of the limiting column is plug-in connected with the delivery assembly.
[0008] Further, a clamping operation sensor is installed on the driving motor to detect the running stroke of the lead screw, the top of the enclosure is fixedly connected with an initial position sensor for detecting the initial position of the clamping assembly, a mounting position sensor for detecting the movement of the clamping assembly to the mounting position, the initial position sensor and the mounting position sensor are respectively arranged at both ends of the lead screw, and the initial position sensor is arranged close to one end of the mounting plate.
[0009] Further, the shape of the end of the enclosure away from the mounting plate matches the included angle of the adjacent two wing supports of the unmanned aerial vehicle connected to one end of the locking assembly, and two correction levers for correcting the position of the unmanned aerial vehicle are fixedly connected to the lower side of the end of the enclosure away from the mounting plate.
[0010] Further, the clamping assembly comprises a clamping bracket threadedly connected with the lead screw, the clamping bracket is provided with a sliding groove matched with the guide rail, the clamping bracket is slidably connected with the guide rail through the sliding groove, the clamping bracket is provided with two magnetic members matched with the initial position sensor and the mounting position sensor in position and function respectively, the clamping bracket is fixedly provided with two parallel arranged steering gears, the steering gears are drivingly connected with grippers for clamping the throwing assembly, and the two grippers are oppositely arranged.
[0011] Further, the gripper is in "L" shape, the vertical part of the gripper is fixedly connected with the steering gear, the horizontal part of the gripper is a plurality of evenly spaced gripping fingers, the gripping fingers are opposite and close to each other on one side in arc shape, an upper pressing plate for limiting the throwing assembly is arranged between the gripper and the clamping bracket, and the upper pressing plate is fixedly connected with the bottom of the clamping bracket.
[0012] Further, the throwing assembly comprises a containing cabin for containing rescue supplies, the containing cabin is fixedly connected with a slot for plug-in connection with the clamping assembly, the shape of the slot matches the gripper and the upper pressing plate, the containing cabin is fixedly connected with a positioning hole matched with the shape and position of the limiting column, the containing cabin is fixedly connected with a locking device matched with the locking assembly, the containing cabin is fixedly connected with a first locking positioning magnet for assisting the locking device in locking positioning, and the first locking positioning magnet is magnetically connected with the corresponding position of the locking assembly. The locking device comprises a lock tongue for locking connection with the locking assembly, and a locking driving motor for driving the lock tongue to rotate, the locking driving motor is electrically connected with an electrical connection port, the electrical connection port is electrically connected with the locking assembly, and the locking driving motor is provided with power supply by the unmanned aerial vehicle.
[0013] Further, the accommodating cabin comprises a cabin body and a cabin cover matched with the cabin body, the cabin cover is threadedly connected with the cabin body, the cabin body is fixedly connected with an inflation bottle for inflating a rescue air bag, one side of the cabin body is connected with a side cover through a rotating shaft, the other side of the side cover is buckled with the cabin body, and the cabin body, the cabin cover and the side cover are all provided with a plurality of through holes.
[0014] Further, the locking assembly comprises a locking plate fixedly connected with the unmanned aerial vehicle, the locking plate is provided with a locking hole matched with the lock tongue, the locking plate is respectively fixedly connected with an insertion sensor for detecting that the lock tongue is inserted in place, a locking sensor for detecting that the lock tongue is rotationally locked in place, and a power supply plate for supplying power to the locking device, the power supply plate is connected with the electric connection port, the power supply plate, the insertion sensor and the locking sensor are all electrically connected with the unmanned aerial vehicle, and the locking plate is fixedly connected with a second locking alignment magnet matched with the position of the first locking alignment magnet.
[0015] Compared with the prior art, the present application has the following advantages: Rapid response: the present application shortens the task response time from dozens of minutes of traditional manual operation to minutes through the processes of preloading and automatic mounting, thereby gaining valuable time for emergency rescue.
[0016] High degree of automation: the present application realizes the full-process automation from mounting to releasing, greatly reduces the technical dependence on professional pilots, and supports unattended operation.
[0017] Integration and low cost: the present application is designed for the DJI ecosystem, can fully utilize the unattended capability of the DJI airport and the remote management capability of the DJI Sky platform, and the device itself has load storage and mounting functions, so that no additional machine volume needs to be designed for the unmanned aerial vehicle, the unmanned aerial vehicle modification is simplified, and the overall operation and maintenance cost is effectively reduced. BRIEF DESCRIPTION OF DRAWINGS
[0018] In order to more clearly illustrate the technical solutions of the embodiments of the present application, the following will briefly introduce the drawings needed to be used in the embodiments. It should be understood that the following drawings only show some embodiments of the present application, and therefore should not be regarded as a limitation on the scope. For those skilled in the art, other related drawings can also be obtained without creative labor on the basis of these drawings.
[0019] Figure 1 is a schematic diagram of the overall structure of the present application; Figure 2 is a schematic diagram of the internal structure of the overall structure of the present application; Figure 3 is a schematic diagram of the overall structure of the mounting assembly of the present application; Figure 4is the overall structure schematic diagram of the grabbing assembly of the present application; Figure 5 is the top view of the grabbing assembly of the present application; Figure 6 is the overall structure schematic diagram of the throwing assembly of the present application; Figure 7 is the rear view of the throwing assembly of the present application; Figure 8 is the internal structure schematic diagram of the throwing assembly of the present application; Figure 9 is the overall structure schematic diagram of the locking assembly of the present application.
[0020] Reference signs: mounting assembly 10; mounting plate 11; surrounding plate 12; grabbing drive motor 13; screw rod 14; guide rail 15; limiting column 16; initial position sensor 171; mounting position sensor 172; grabbing operation sensor 18; correction lever 19; grabbing assembly 20; grabbing support 21; sliding groove 22; steering wheel 23; grabbing finger 241; upper pressing plate 25; magnetic element 26; throwing assembly 30; accommodating cabin 31; cabin body 311; cabin cover 312; gas cylinder 313; side cover 314; insertion slot 32; alignment hole 33; locking tongue 34; electrical connection port 35; first locking alignment magnet 36; locking assembly 40; locking plate 41; locking hole 42; insertion sensor 43; power supply plate 44; locking alignment sensor 45; second locking alignment magnet 46. DETAILED DESCRIPTION
[0021] The present application is further explained in the following examples, which are intended to be purely exemplary of the application and should not be considered as limiting the scope of the application. The examples can be combined and / or interchanged, in parts or in whole, in accordance with the principles of the application.
[0022] It should be noted that the drawings provided in the following examples are only schematic and are intended to provide a general understanding of the present application. In particular, the shape, relative position and number of layers are not intended to be limiting and can vary in actual implementation.
[0023] In the following description, numerous specific details are discussed in order to provide a thorough understanding of the embodiments of the present application. However, those skilled in the art will recognize that the embodiments of the present application can be practiced without these specific details.
[0024] Please see Figure 1 and Figure 2 A payload preloading device for a drone includes a mounting assembly 10 fixedly connected to a drone nest and a locking assembly 40 fixedly connected to the drone, with the locking assembly 40 electrically connected to the drone. The mounting assembly 10 is driven to connect a gripping assembly 20, which is installed within the mounting assembly 10. The gripping assembly 20 grips and connects to a throwing assembly 30 for loading emergency rescue supplies. The throwing assembly 30 is releasably locked to the locking assembly 40, and the locking assembly 40 is electrically connected to the throwing assembly 30.
[0025] In use, the mounting component 10 is fixedly connected to the top cover of the drone's nest, and the locking component 40 is fixedly connected to one end of the drone and electrically connected to the drone via a wire. The operator pre-installs the throwing component 30 into the mounting component 10. When the drone needs to perform a rescue mission, the operator controls the gripping component 20 to grab the throwing component 30 containing rescue supplies, and the mounting component 10 drives the gripping component 20 to move. The gripping component 20 moves the throwing component 30 to the drone's end, aligning and engaging with the locking component 40, achieving electrical connection and a releaseable locking connection. At this point, the operator controls the gripping component 20 to release its connection to the throwing component 30 and return to its initial position.
[0026] After the drone carrying the throwing component 30 takes off and delivers relief supplies to the designated rescue location, the drone control locking component 40 releases the locking between itself and the throwing component 30, and the throwing component 30 is completely detached from the drone body and dropped to the target.
[0027] Compared to the previous method of loading supplies onto a drone before it could fly, this invention effectively shortens rescue deployment time. After the delivery component 30 is pre-installed into the mounting component 10, the mounting component 10 and the gripping component 20 handle the installation and removal of the delivery component 30. The entire process is automated, effectively reducing the technical requirements for the personnel handling the delivery. Furthermore, when not in use, the delivery component 30 remains on the gripping component 20 and the mounting component 10, serving as internal storage. This allows for external loading of rescue supplies, eliminating the need for internal storage and replacement, minimizing drone modifications, and reducing maintenance costs.
[0028] Please see Figures 1 to 3The mounting assembly 10 comprises a mounting plate 11 fixedly connected with the nest, a surrounding plate 12 fixedly connected with the mounting plate 11, the mounting plate 11 and the surrounding plate 12 surrounding a mounting bin, a grabbing driving motor 13 fixedly connected with the mounting plate 11, the grabbing driving motor 13 arranged in the mounting bin, a lead screw 14 drivingly connected with the grabbing driving motor 13, the lead screw 14 threadedly connected with the grabbing assembly 20, a guide rail 15 fixedly connected with the mounting plate 11 and used for guiding and limiting the movement of the grabbing assembly 20, the guide rail 15 arranged parallel to the lead screw 14, and the grabbing assembly 20 slidingly connected with the guide rail 15.
[0029] The mounting bin surrounded by the mounting plate 11 and the surrounding plate 12 is used for temporarily storing the throwing assembly 30 and other components, the lead screw 14 is driven to rotate by the driving motor 13, and the grabbing assembly 20 is driven to move stably and directionally under the guidance and limitation of the guide rail 15.
[0030] Please refer to Figures 1 to 3 The mounting plate 11 is fixedly connected with a plurality of limiting columns 16 used for pre-assembly alignment of the throwing assembly 30, and the free ends of the limiting columns 16 are insertedly connected with the throwing assembly 30.
[0031] The positioning component is arranged below the lead screw 14 and fixedly connected with the mounting plate 11, the free ends of the two limiting columns 16 are insertedly connected with the throwing assembly 30, and the two limiting columns 16 are arranged at two ends of the throwing assembly 30 respectively, so as to realize pre-assembly positioning of the throwing assembly 30 and facilitate alignment and grabbing of the grabbing assembly 20.
[0032] Please refer to Figures 1 to 3 The driving motor 13 is provided with a grabbing running sensor 18 used for detecting the running stroke of the lead screw 14, an initial position sensor 171 fixedly connected with the top of the surrounding plate and used for detecting the initial position of the grabbing assembly 20, and a mounting position sensor 172 used for detecting the mounting position of the grabbing assembly 20, the initial position sensor 171 and the mounting position sensor 172 are arranged at two ends of the lead screw 14 respectively, and the initial position sensor 171 is arranged close to one end of the mounting plate.
[0033] The running stroke and rotating speed of the lead screw 14 are detected by the grabbing running sensor 18, so as to detect the real-time distance of the movement of the grabbing assembly 20 and feed back to the control mainboard. The initial position sensor 171 and the mounting position sensor 172 can both be Hall sensors. Whether the grabbing assembly 20 moves to the initial position or the mounting position is detected by the initial position sensor 171 and the mounting position sensor 172 respectively and fed back to the control mainboard.
[0034] Please refer to Figures 1 to 3The shape of the surrounding plate 12 away from one end of the mounting plate 11 matches the angle between the adjacent two wing supports of the unmanned aerial vehicle connected to one end of the locking assembly 40, and the lower side of the surrounding plate 12 away from one end of the mounting plate 11 is fixedly connected with two correction levers 19 for correcting the position of the unmanned aerial vehicle.
[0035] When the unmanned aerial vehicle returns to the nest and the nest cover is closed, the position of the unmanned aerial vehicle is corrected by the correction lever 19, and the connection and locking of the throwing assembly 30 and the locking assembly 40 connected to the unmanned aerial vehicle are facilitated. The surrounding plate 12 is placed between the adjacent two wing supports of the unmanned aerial vehicle, and the shape of the surrounding plate 12 close to one end of the unmanned aerial vehicle matches the angle between the adjacent two wing supports of the unmanned aerial vehicle, which further facilitates the connection and locking of one end of the unmanned aerial vehicle installation locking assembly 40 and the throwing assembly 30.
[0036] Please refer to Figures 1 to 5 The grabbing assembly 20 includes a grabbing support 21 threadedly connected with the lead screw 14, the grabbing support 21 is provided with a sliding groove 22 matched with the guide rail 15, the grabbing support 21 is slidably connected with the guide rail 15 through the sliding groove 22, the grabbing support 21 is provided with two magnetic members 26 matched with the initial position sensor 171 and the mounting position sensor 172 in position and function, respectively, the grabbing support 21 is fixedly provided with two parallelly arranged steering gears 23, the steering gears 23 are drivingly connected with two grippers 24 for grabbing the throwing assembly 30, and the two grippers 24 are oppositely arranged.
[0037] The grabbing support 21 is provided with an internal thread hole matched with the lead screw 14, the grabbing support 21 is threadedly connected with the lead screw 14 through the internal thread hole, and the grabbing support 21 is slidably connected with the guide rail 15 through the sliding groove 22, so as to ensure the stable movement of the grabbing assembly 20. The two magnetic members 26 can be magnets. During the movement of the grabbing support 21, the initial position sensor 171 and the mounting position sensor 172 correspondingly detect the two magnetic members 26, so as to detect whether the grabbing assembly 20 is moved to the position. The two steering gears 23 respectively control the rotation of the two grippers 24, so that the two grippers 24 are opened or closed, and the rotation directions of the two steering gears 23 are controlled, so as to realize the disconnection and grabbing of the throwing assembly 30.
[0038] Please refer to Figure 1 , Figure 2 and Figure 4The grabber 24 is in "L" shape, the vertical part of the grabber 24 is fixedly connected with the steering gear 23, the horizontal part of the grabber 24 is a plurality of evenly spaced grab fingers 241, the opposite and mutually close side of the grab fingers 241 is in arc shape, the grabber 24 is provided with an upper pressing plate 25 for limiting the throwing assembly 30 between the grabber 24 and the grabbing support 21, and the upper pressing plate 25 is fixedly connected with the bottom of the grabbing support 21.
[0039] The grabber 24 is rotated by the steering gear 23, so that the grab fingers 241 of the grabber 24 are rotatably inserted with the throwing assembly 30, and the throwing assembly 30 is limited in the front and back directions. The opposite and mutually close side of the grab fingers 241 is in arc shape, which facilitates the rotation and insertion of the throwing assembly 30 and enhances the stability of grabbing and unfastening. The cross section of the upper pressing plate 25 is a rectangular slot with an open bottom. When grabbing, after the grabber 24 is rotatably inserted into the throwing assembly 30, the grab fingers 241 remain horizontal, and at the same time, the two vertical parts of the rectangular slot limit the throwing assembly 30 in the left and right directions, and in cooperation with the two grabbers 24, the throwing assembly 30 is limited in the up and down directions. Through the all-directional limiting and fixing of the throwing assembly 30, the stable grabbing of the throwing assembly 30 by the grabbing assembly 20 is realized.
[0040] Please refer to Figure 1 、 Figure 2 、 Figures 4 to 6 The throwing assembly 30 includes a containing cabin 31 for containing rescue supplies, the containing cabin 31 is fixedly connected with an insertion slot 32 for being inserted and connected with the grabbing assembly 20, the shape of the insertion slot 32 matches the grabber 24 and the upper pressing plate 25, the containing cabin 31 is fixedly connected with a positioning hole 33 matching the shape and position of the limiting column 16, the containing cabin 31 is fixedly connected with a locking device matching the locking assembly 40, the containing cabin 31 is fixedly connected with a first locking and positioning magnet 36 for assisting the locking and positioning of the locking device, and the first locking and positioning magnet 36 is magnetically connected with the corresponding position of the locking assembly 40. The locking device includes a lock tongue 34 for being locked and connected with the locking assembly 40, and a locking drive motor for driving the rotation of the lock tongue 34, the locking drive motor is electrically connected with an electrical connection port 35, the electrical connection port 35 is electrically connected with the locking assembly 40, and the locking drive motor is powered by the unmanned aerial vehicle.
[0041] When installing the throwing assembly 30, the two limiting columns 16 are inserted and connected with the positioning hole 33, the pre-positioning of the throwing assembly 30 is completed, so that the grabbing assembly 20 is positioned and grabbed.
[0042] When grabbing, the gripper 24 of the gripping assembly 20 is inserted into the slot 32, the grabbing fingers 241 are kept horizontal, and the slot 32 is limited between the two vertical parts of the upper pressing plate 25, so as to realize stable grabbing.
[0043] When mounting, the first locking and positioning magnet 36 is magnetically connected with the corresponding position of the locking assembly 40, so as to avoid the influence of shaking on the positioning of the locking tongue 34 or the electric connection port 35 and the locking assembly 40, and assist the locking device to be locked and connected with the locking assembly 40. After the locking tongue 34 and the locking assembly 40 are positioned, the electric connection port 35 is electrically connected with the locking assembly 40, so as to realize power supply for the locking driving motor by the unmanned aerial vehicle. When the locking assembly 40 detects that the locking tongue is inserted into position, the locking driving motor is controlled to drive the locking tongue 34 to rotate, so as to realize the locking connection between the throwing assembly 30 and the locking assembly 40, and then realize the mounting of the containing cabin 31 to the unmanned aerial vehicle.
[0044] Please refer to Figure 1 、 Figure 2 、 Figure 4 、 Figure 7 and Figure 8 , the containing cabin 31 includes a cabin body 311 and a cabin cover 312 matched with the cabin body 311, the cabin cover 312 is threadedly connected with the cabin body 311, the cabin body 311 is fixedly connected with an inflation bottle 313 for inflating a rescue airbag, one side of the cabin body 311 is connected with a side cover 314 through a rotating shaft, the other side of the side cover 314 is buckling connected with the cabin body 311, and the cabin body 311, the cabin cover 312 and the side cover 314 are all provided with a plurality of through holes.
[0045] The cabin cover 312 is rotated to open, the rescue materials are loaded into the containing cabin 31, and then the cabin cover 312 is rotated to be reset and closed with the cabin body 311, so as to realize the loading of the rescue materials. The inflation bottle 313 is connected with the rescue airbag through a water-soluble inflation valve. When water rescue is performed, after the throwing assembly is thrown to a water target, the cabin body 311 is quickly filled with water through the through hole, the water-soluble inflation valve is dissolved by water, so that the inflation bottle 313 is communicated with the rescue airbag, and the inflation bottle 313 is triggered to quickly inflate the airbag. After the airbag volume is quickly expanded, the side cover 314 is broken to form a life buoy, and the water target is rescued.
[0046] Please refer to Figure 1 、 Figure 2 、 Figures 6 to 9The locking assembly 40 includes a locking plate 41 fixedly connected with the unmanned aerial vehicle, the locking plate 41 is provided with a locking hole 42 matched with the lock tongue 34, the locking plate 41 is fixedly connected with an insertion sensor 43 for detecting whether the lock tongue 34 is inserted in place, a locking sensor 45 for detecting whether the lock tongue 34 is rotated and locked in place, and a power supply plate 44 for supplying power to the locking device, the power supply plate 44 is connected with the electrical connection port 35, and the power supply plate 44, the insertion sensor 43 and the locking sensor 45 are electrically connected with the unmanned aerial vehicle, and the locking plate 41 is fixedly connected with a second locking alignment magnet 46 matched with the position of the first locking alignment magnet 36.
[0047] The insertion sensor 43, the locking sensor 45 and the power supply plate 44 are electrically connected with the port of the unmanned aerial vehicle through communication wires to realize information interaction and power supply. The power supply plate 44 is connected with the electrical connection port 35 to realize power supply of the locking drive motor of the locking device. When the lock tongue 34 passes through the locking hole 42, the insertion sensor 43 detects whether the lock tongue 34 is successfully aligned. When it is detected that the lock tongue 34 is successfully aligned, the mainboard controls the locking drive motor to drive the lock tongue 34 to rotate, and at the same time, the locking sensor 45 detects whether the lock tongue 34 is rotated in place, so as to realize the locking connection of the throwing assembly 30 and the locking assembly 40, and then realize the mounting of the containing cabin 31 to the unmanned aerial vehicle. The first locking alignment magnet 36 and the second locking alignment magnet 46 are magnetically connected in the corresponding positions to avoid the influence of shaking on the alignment of the lock tongue 34 or the electrical connection port 35 and the locking assembly 40, and assist the locking device to be aligned and connected with the locking assembly 40.
[0048] After the unmanned aerial vehicle automatically mounts the throwing assembly 30, the unmanned aerial vehicle has the condition of taking off with the load and flying to the destination to implement rescue. If the task needs to be switched or cancelled on the way, the unmanned aerial vehicle flies back to the nest with the throwing assembly 30, and is unloaded from the unmanned aerial vehicle by the clamping assembly 20 and the mounting assembly. The execution step is that after receiving the unloading instruction, the gripper 24 of the clamping assembly 20 is opened, and under the driving action of the mounting assembly 10, the gripper 24 moves towards the throwing assembly 30. When the gripper 24 clamps the throwing assembly 30 and feeds back, the locking device on the throwing assembly 30 is unlocked, the gripper 24 clamping the throwing assembly 30 retreats to the initial position, and the whole movement of the mechanism is closed-loop control.
[0049] Compared with the method that the unmanned aerial vehicle is loaded after personnel take out the materials and then flies out, the present application effectively shortens the rescue and delivery time. After the throwing assembly is aligned and pre-installed in the mounting assembly, the mounting and dismounting of the throwing assembly are realized by the mounting assembly and the clamping assembly. The whole process is automatic operation, which effectively reduces the technical requirements for the mounting personnel. When the mounting assembly is not installed, the throwing assembly is kept in the clamping assembly and the mounting assembly, which also plays the role of in-machine storage, and the rescue materials are externally mounted, so that the scene of in-machine storage and replacement does not need to be considered, the modification of the unmanned aerial vehicle is less, and the operation and maintenance cost is reduced.
[0050] Fast response: The present application shortens the task response time from dozens of minutes of traditional manual operation to minutes through the process of loading preloading and automatic mounting, which saves valuable time for emergency rescue.
[0051] High degree of automation: The present application realizes the full process automation from mounting to releasing, greatly reduces the technical dependence on professional pilots, and supports unattended operation.
[0052] Integration and low cost: The present application is designed for DJI ecosystem, which can fully utilize the unattended ability of DJI airport and the remote management ability of the platform, and the device itself has load storage and mounting functions, without the need to design additional machine volume for unmanned aerial vehicles, simplifying the modification of unmanned aerial vehicles and effectively reducing the overall operation and maintenance cost.
[0053] In the above embodiments, although the present application has been described in conjunction with specific embodiments thereof, many alternatives, modifications and variations will be apparent to those skilled in the art in light of the foregoing description. Embodiments of the present application are intended to embrace all such alternatives, modifications and variations as fall within the scope of the appended claims.
[0054] The above embodiments only exemplarily illustrate the principles and effects of the present application, and are not used to limit the present application. Any person skilled in the art can modify or change the above embodiments without departing from the spirit and scope of the present application. Therefore, all equivalent modifications or changes completed by those skilled in the art without departing from the spirit and technical thought disclosed by the present application should be covered by the claims of the present application.
Claims
1. A load pre-loading device for a drone, characterized in that: The installation assembly (10) is fixedly connected with the nest, and the locking assembly (40) is fixedly connected with the unmanned aerial vehicle and electrically connected with the unmanned aerial vehicle, the installation assembly (10) is drivingly connected with the grabbing assembly (20), the grabbing assembly (20) is installed in the installation assembly (10), the grabbing assembly (20) is clamped with the throwing assembly (30) for loading emergency rescue materials, the throwing assembly (30) is releasably locked with the locking assembly (40), and the locking assembly (40) is electrically connected with the throwing assembly (30).
2. The load pre-loading device for UAV according to claim 1, wherein, The installation assembly (10) includes an installation plate (11) fixedly connected with the nest, the installation plate (11) is fixedly connected with a surrounding plate (12), the installation plate (11) and the surrounding plate (12) form an installation bin, the installation plate (11) is fixedly connected with a grabbing driving motor (13), the grabbing driving motor (13) is arranged in the installation bin, the grabbing driving motor (13) is drivingly connected with a lead screw (14), the lead screw (14) is threadedly connected with the grabbing assembly (20), the installation plate (11) is fixedly connected with a guide rail (15) for guiding and limiting the movement of the grabbing assembly (20), the guide rail (15) is arranged parallel to the lead screw (14), and the grabbing assembly (20) is slidingly connected with the guide rail (15).
3. The load pre-loading device for UAV according to claim 2, wherein, The installation plate (11) is fixedly connected with a plurality of limiting columns (16) for aligning and preassembling the throwing assembly (30), and the free ends of the limiting columns (16) are insertedly connected with the throwing assembly (30).
4. The load pre-loading device for UAV according to claim 2, wherein, The driving motor (13) is provided with a grabbing running sensor (18) for detecting the running stroke of the lead screw (14), the top of the surrounding plate is fixedly connected with an initial position sensor (171) for detecting the initial position of the grabbing assembly (20), and a mounting position sensor (172) for detecting the movement of the grabbing assembly (20) to the mounting position, the initial position sensor (171) and the mounting position sensor (172) are respectively arranged at both ends of the lead screw (14), and the initial position sensor (171) is arranged close to one end of the installation plate.
5. The load pre-loading device for UAV according to claim 2, wherein, The shape of the end of the surrounding plate (12) away from the installation plate (11) matches the included angle of the adjacent two wing supports of the locking assembly (40) of the unmanned aerial vehicle, and the lower side of the end of the surrounding plate (12) away from the installation plate (11) is fixedly connected with two correction levers (19) for correcting the position of the unmanned aerial vehicle.
6. The load pre-loading device for UAV according to claim 3, wherein, The grab assembly (20) comprises a grab support (21) threadedly connected with the lead screw (14), the grab support (21) is provided with a sliding groove (22) matched with the guide rail (15), the grab support (21) is slidably connected with the guide rail (15) through the sliding groove (22), the grab support (21) is provided with two magnetic members (26) matched with the initial position sensor (171) and the mounting position sensor (172) in position and function respectively, the grab support (21) is fixedly provided with two parallel arranged steering gears (23), the steering gears (23) are drivingly connected with two grippers (24) for connecting the throwing assembly (30), and the two grippers (24) are oppositely arranged.
7. The load pre-loading device for UAV according to claim 6, wherein, The gripper (24) is in "L" shape, the vertical part of the gripper (24) is fixedly connected with the steering gear (23), the horizontal part of the gripper (24) is a plurality of evenly spaced gripping fingers (241), the gripping fingers (241) are in arc shape on the opposite and mutually close side, the gripper (24) and the grab support (21) are provided with an upper pressing plate (25) for limiting the throwing assembly (30), and the upper pressing plate (25) is fixedly connected with the bottom of the grab support (21).
8. The load pre-loading device for UAV according to claim 7, wherein, The throwing assembly (30) comprises a containing cabin (31) for containing rescue materials, the containing cabin (31) is fixedly connected with a slot (32) for plug-in connection with the grab assembly (20), the shape of the slot (32) is matched with the gripper (24) and the upper pressing plate (25), the containing cabin (31) is fixedly connected with a positioning hole (33) matched with the shape and position of the limiting column (16), the containing cabin (31) is fixedly connected with a locking device matched with the locking assembly (40), the containing cabin (31) is fixedly connected with a first locking and positioning magnet (36) for assisting the locking device in locking and positioning, and the first locking and positioning magnet (36) is magnetically connected with the corresponding position of the locking assembly (40). The locking device comprises a lock tongue (34) for locking connection with the locking assembly (40), and a locking drive motor for driving the lock tongue (34) to rotate, the locking drive motor is electrically connected with an electric connection port (35), the electric connection port (35) is electrically connected with the locking assembly (40), and the locking drive motor is powered by the unmanned aerial vehicle.
9. The load pre-loading device for UAV according to claim 8, wherein, The containing cabin (31) comprises a cabin body (311) and a cabin cover (312) matched with the cabin body (311), the cabin cover (312) is threadedly connected with the cabin body (311), the cabin body (311) is fixedly connected with an inflation bottle (313) for inflating a rescue air bag, one side of the cabin body (311) is connected with a side cover (314) through a rotating shaft, the other side of the side cover (314) is bucklingly connected with the cabin body (311), and the cabin body (311), the cabin cover (312) and the side cover (314) are all provided with a plurality of through holes.
10. The load pre-loading device for UAV according to claim 8, wherein, The locking assembly (40) comprises a locking plate (41) fixedly connected with the unmanned aerial vehicle, the locking plate (41) is provided with a lock hole (42) matched with the lock tongue (34), the locking plate (41) is respectively fixedly connected with an inserting sensor (43) for detecting that the lock tongue (34) is inserted in place, a locking sensor (45) for detecting that the lock tongue (34) is rotated and locked in place, and a power supply plate (44) for supplying power for the locking device, the power supply plate (44) is connected with the electric connection port (35), and the power supply plate (44), the inserting sensor (43) and the locking sensor (45) are electrically connected with the unmanned aerial vehicle, and the locking plate (41) is fixedly connected with a second locking alignment magnet (46) matched with the position of the first locking alignment magnet (36).