Magnetic separation structure for unmanned aerial vehicle

Abstract

The utility model provides a kind of unmanned plane magnetic attraction type material separation structure, it is related to unmanned plane technical field, the utility model includes controller, the side of controller is equipped with fuselage, the side of controller is equipped with electromagnet, the both sides of controller are equipped with limiting device, the limiting device is limited to material by first limiting plate and second limiting plate, the both sides of controller are equipped with mounting assembly, the limiting device is mounted to the both sides of controller by mounting assembly, the utility model can be separated when unmanned plane is to the material of magnetic attraction, the both sides of material are blocked and limited clamping, avoid the situation that part is longer material, cannot be placed stably, to improve the use effect of unmanned plane magnetic attraction type material separation structure. By using mounting assembly, the limiting device can be quickly installed, then subsequent limiting device is conveniently used on unmanned plane, to improve the use effect of limiting device.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicles (UAVs), and in particular to a magnetic material separation structure for UAVs. Background Technology

[0002] The magnetic cargo separation structure for drones is mainly used for tasks such as cargo transportation, delivery, or retrieval by drones in specific environments. It connects and separates from cargo through a magnetic system, and is characterized by high efficiency, simplicity, and safety.

[0003] When using the magnetic cargo separation structure on a drone, the drone contacts the cargo with an electromagnet on the controller side. The electromagnet's magnetic field then connects the cargo to the drone. By controlling the strength of the magnetic field, the cargo can be separated or connected to the drone as needed. However, during separation, some longer cargo items cannot be placed stably, leading to problems that affect the effectiveness of the magnetic cargo separation structure. Utility Model Content

[0004] The technical problem this invention aims to solve is that when materials are being separated, some longer materials cannot be placed stably, which affects the effectiveness of the drone's magnetic material separation structure.

[0005] The technical solution adopted by this utility model to solve its technical problem is: a magnetic material separation structure for unmanned aerial vehicles, including a controller, a fuselage on one side of the controller, an electromagnet on one side of the controller, and limiting devices on both sides of the controller. The limiting devices limit the material through a first limiting plate and a second limiting plate.

[0006] The effect achieved by the above components is as follows: When using the drone's magnetic material separation structure, the drone's fuselage makes the electromagnet on one side of the controller contact the material, and then the magnetic field of the electromagnet is used to connect the material to the drone. By controlling the strength of the magnetic field, the material can be separated from or connected to the drone when needed. When separating, a limiting device can be used to block and limit the material on both sides during separation, so that the material can be separated smoothly.

[0007] Preferably, the controller is provided with mounting components on both sides. The mounting components install the limiting device on both sides of the controller. The limiting device includes a placement plate, a motor, a round rod, a first limiting plate, an electric telescopic rod, and a second limiting plate. The motor is located on one side of the placement plate to drive the round rod to rotate on one side of the placement plate. The round rod drives the first limiting plate to rotate. The electric telescopic rod is located on one side of the first limiting plate to drive the second limiting plate to move.

[0008] The aforementioned components achieve the following effect: When the electromagnet separates the magnetically attracted materials, the motors fixed to one side of the two placement plates are activated. These motors drive a round rod fixed via a coupling to rotate inside the placement plate. The round rod then drives a first limiting plate fixed to one side to rotate, and one side of each of the two first limiting plates approaches the magnetically attracted materials. Then, the electric telescopic rod fixed to the first limiting plate is activated, causing a second limiting plate fixed to the output end of the electric telescopic rod to contact and press against the materials. The two second limiting plates then clamp and limit the materials, preventing them from shaking and ensuring they are stably placed on the ground. The materials are then separated from the electromagnet, and the motors and electric telescopic rods are reset. The materials are then separated and placed on the ground. By using the limiting device, when the drone separates magnetically attracted materials, it can block and limit the materials from both sides, preventing longer materials from being placed stably, thereby improving the effectiveness of the drone's magnetic material separation structure.

[0009] Preferably, the round rod is provided with a bearing on the side near the placement plate, and the bearing reduces the frictional force between the round rod and the placement plate.

[0010] The effect achieved by the above components is that by fixing the round rod and the placement plate with bearings, the friction between the two is reduced, and the round rod can rotate more easily on one side of the placement plate.

[0011] Preferably, a rubber pad is provided on one side of the second limiting plate, and the rubber pad increases the friction on one side of the second limiting plate.

[0012] The effect achieved by the above components is as follows: by fixing the rubber pad to one side of the second limiting plate, the friction of one side of the second limiting plate is increased. Then, when the second limiting plate is used as a support leg to park and support the drone, the friction between the second limiting plate and the ground is increased, thereby improving the performance of the second limiting plate.

[0013] Preferably, a stabilizing plate is provided on the side of the first limiting plate near the second limiting plate, and the stabilizing plate limits one side of the second limiting plate.

[0014] The effect achieved by the above components is as follows: by fixing the stabilizing plate to the side of the first limiting plate near the second fiberboard, the stabilizing plate restricts the movement trajectory of the second limiting plate, thereby improving the movement stability of the second limiting plate.

[0015] Preferably, the mounting assembly includes two square tubes, bolts, and a mounting plate. The two square tubes are located on both sides of the controller. The bolts are inserted into the square tubes to fix the mounting plate inside the square tubes. One side of the mounting plate is connected to the placement plate.

[0016] The effect achieved by the above components is as follows: by moving the two placement plates, the mounting plate fixed on one side of the two placement plates is inserted into the square tube fixed on one side of the controller. Then, the bolt is rotated so that the bolt passes through the square tube and is threadedly fixed to the mounting plate. Then, the placement plates are fixed in position on both sides of the controller. By using the installation components, the limit device can be quickly installed, which facilitates its subsequent use on the drone, thereby improving the effectiveness of the limit device.

[0017] Preferably, the mounting plate has a trapezoidal block on the side away from the placement plate, and the trapezoidal block reduces the size of one side of the mounting plate.

[0018] The effect achieved by the above components is to reduce the size of one side of the mounting plate by fixing it to one side with a trapezoidal block, thereby making it easier to insert the square tube into the mounting plate.

[0019] Preferably, an operating block is provided on one side of the bolt to increase the size of one side of the bolt.

[0020] The effect achieved by the above components is that the operating block is fixed on one side of the bolt, and then the size of one side of the bolt is raised, making it easier for the operator to turn the bolt.

[0021] In summary, the beneficial effects of this utility model are as follows:

[0022] By using a limiting device, when a drone separates magnetically attached materials, it can block and limit the materials on both sides, preventing longer materials from being placed stably, thereby improving the effectiveness of the drone's magnetic material separation structure.

[0023] By using the installation components, the limit device can be quickly installed, making it convenient to use on drones and thus improving its effectiveness. Attached Figure Description

[0024] The present invention will be further described below with reference to the accompanying drawings and embodiments.

[0025] Figure 1 This is a three-dimensional structural diagram of the present invention;

[0026] Figure 2 This is a three-dimensional structural diagram of the limiting device of this utility model;

[0027] Figure 3 This utility model Figure 2 A schematic diagram of a partial three-dimensional structure;

[0028] Figure 4 This utility model Figure 2 Enlarged view of point A.

[0029] Legend: 1. Controller; 2. Electromagnet; 3. Body; 4. Limiting device; 41. Placement plate; 42. Motor; 43. Round rod; 44. First limiting plate; 45. Electric telescopic rod; 46. Second limiting plate; 47. Bearing; 48. Rubber pad; 49. Stabilizing plate; 5. Mounting assembly; 51. Square tube; 52. Bolt; 53. Mounting plate; 54. Trapezoidal block; 55. Operating block. Detailed Implementation

[0030] The present invention will now be described in further detail with reference to the accompanying drawings. These drawings are simplified schematic diagrams, illustrating only the basic structure of the present invention, and therefore only show the components relevant to the present invention.

[0031] In the description of this utility model, it should be noted that, unless otherwise explicitly specified and limited, the terms "connected" or "linked" should be interpreted broadly. For example, it can refer to a fixed connection, a detachable connection, or an integral connection; it can refer to a mechanical connection or an electrical connection; it can refer to a direct connection or an indirect connection through an intermediate medium. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.

[0032] Figures 1 to 4 The illustrated drone magnetic material separation structure includes a controller 1, a fuselage 3 on one side of the controller 1, an electromagnet 2 on another side of the controller 1, and limiting devices 4 on both sides of the controller 1. The limiting devices 4 use a first limiting plate 44 and a second limiting plate 46 to limit the material. When using the drone magnetic material separation structure, the drone fuselage 3 brings the electromagnet 2 on one side of the controller 1 into contact with the material. The magnetic field of the electromagnet 2 then connects the material to the drone. By controlling the strength of the magnetic field, the material can be separated from or connected to the drone as needed. During separation, the limiting devices 4 can be used to block and clamp the material on both sides, ensuring smooth separation.

[0033] Figures 1 to 4The controller 1 shown has mounting components 5 on both sides. The mounting components 5 install the limiting device 4 on both sides of the controller 1. The limiting device 4 includes a placement plate 41, a motor 42, a round rod 43, a first limiting plate 44, an electric telescopic rod 45, and a second limiting plate 46. The motor 42 is located on one side of the placement plate 41 to drive the round rod 43 to rotate on one side of the placement plate 41. The round rod 43 drives the first limiting plate 44 to rotate. The electric telescopic rod 45 is located on one side of the first limiting plate 44 to drive the second limiting plate 46 to move. When the electromagnet 2 separates the magnetically attracted materials, the motors 42 fixed on one side of the two placement plates 41 can be activated. The motors 42 drive the round rods 43 fixed through the coupling to rotate inside the placement plates 41. Then, the round rods 43 drive the first limiting plates 44 fixed on one side to rotate, and the two first limiting plates 44 move closer to the magnetically attracted materials. Then, the electric telescopic rods 45 fixed on the first limiting plates 44 are activated, so that the second limiting plates 46 fixed at the output end of the electric telescopic rods 45 come into contact with and squeeze the materials. Then, the two second limiting plates 46 clamp and limit the materials, preventing the materials from shaking and placing them stably on the ground. Then, the materials are separated from the electromagnet 2. Then, the motors 42 and the electric telescopic rods 45 are reset, and the materials are separated and placed on the ground. By using the limiting device 4, when the UAV separates the magnetically attracted materials, it can block and limit the materials on both sides, preventing some longer materials from being placed stably, thereby improving the use effect of the UAV magnetic material separation structure. The motor is a self-locking motor, model number 5840-31ZY, and the electric telescopic pole model number is JC35FA17.

[0034] Figures 1 to 4 The circular rod 43 shown is equipped with a bearing 47 on the side near the placement plate 41. The bearing 47 reduces the friction between the circular rod 43 and the placement plate 41. By fixing the circular rod 43 and the placement plate 41 with the bearing 47, the friction between them is reduced, making it easier for the circular rod 43 to rotate on one side of the placement plate 41. A rubber pad 48 is provided on one side of the second limiting plate 46. The rubber pad 48 increases the friction on one side of the second limiting plate 46. By fixing the rubber pad 48 to one side of the second limiting plate 46, the friction on one side of the second limiting plate 46 is increased. When the second limiting plate 46 is used as a support leg to park and support the drone, the friction between the second limiting plate 46 and the ground is increased, thereby improving the performance of the second limiting plate 46. A stabilizing plate 49 is provided on the side of the first limiting plate 44 near the second limiting plate 46. The stabilizing plate 49 limits one side of the second limiting plate 46. The stabilizing plate 49 is fixed to the side of the first limiting plate 44 near the second fiberboard, and then the stabilizing plate 49 restricts the movement trajectory of the second limiting plate 46, thereby improving the movement stability of the second limiting plate 46.

[0035] Figures 1 to 4The mounting assembly 5 shown includes two square tubes 51, bolts 52, and mounting plates 53. The two square tubes 51 are located on both sides of the controller 1. The bolts 52 are inserted into the square tubes 51 to fix the mounting plates 53 inside the square tubes 51. One side of the mounting plates 53 is connected to the placement plates 41. By moving the two placement plates 41, the mounting plates 53 fixed on one side of the two placement plates 41 are inserted into the square tubes 51 fixed on one side of the controller 1. Then, the bolts 52 are rotated so that the bolts 52 pass through the square tubes 51 and are threadedly fixed to the mounting plates 53. This completes the fixing of the placement plates 41 on both sides of the controller 1. By using the mounting assembly 5, the limiting device 4 can be quickly installed, which facilitates its subsequent use on the drone, thereby improving the effectiveness of the limiting device 4.

[0036] Figures 1 to 4 The mounting plate 53 shown has a trapezoidal block 54 on the side away from the placement plate 41, which lowers the dimension of one side of the mounting plate 53. By fixing the trapezoidal block 54 to one side of the mounting plate 53, the dimension of one side of the mounting plate 53 is lowered, making it easier to insert the mounting plate 53 into the square tube 51. An operating block 55 is provided on the bolt 52 side to raise the dimension of one side of the bolt 52. By fixing the operating block 55 to the bolt 52 side, the dimension of one side of the bolt 52 is raised, making it easier for the operator to rotate the bolt 52.

[0037] Working principle: When using the drone's magnetic material separation structure, the drone's fuselage 3 makes the electromagnet 2 on one side of the controller 1 come into contact with the material. Then, the magnetic field of the electromagnet 2 is used to connect the material to the drone. By controlling the strength of the magnetic field, the material can be separated from or connected to the drone when needed. When separating, the limiting device 4 can be used to block and limit the material on both sides during separation, so that the material can be separated smoothly. When the electromagnet 2 separates the magnetically attracted materials, the motors 42 fixed on one side of the two placement plates 41 can be activated. The motors 42 drive the round rods 43 fixed through the coupling to rotate inside the placement plates 41. Then, the round rods 43 drive the first limiting plates 44 fixed on one side to rotate, and the two first limiting plates 44 move closer to the magnetically attracted materials. Then, the electric telescopic rods 45 fixed on the first limiting plates 44 are activated, so that the second limiting plates 46 fixed at the output end of the electric telescopic rods 45 come into contact with and squeeze the materials. Then, the two second limiting plates 46 clamp and limit the materials, preventing the materials from shaking and placing them stably on the ground. Then, the materials are separated from the electromagnet 2. Then, the motors 42 and the electric telescopic rods 45 are reset, and the materials are separated and placed on the ground. By using the limiting device 4, when the UAV separates the magnetically attracted materials, it can block and limit the materials on both sides, preventing some longer materials from being placed stably, thereby improving the use effect of the UAV magnetic material separation structure.

[0038] By moving the two placement plates 41, the mounting plate 53 fixed on one side of the two placement plates 41 is inserted into the square tube 51 fixed on one side of the controller 1. Then, the bolt 52 is rotated so that the bolt 52 passes through the square tube 51 and is threadedly fixed to the mounting plate 53. Then, the placement plates 41 are fixed in position on both sides of the controller 1. By using the installation component 5, the limit device 4 can be quickly installed, which facilitates its subsequent use on the drone, thereby improving the performance of the limit device 4.

[0039] The above are merely preferred embodiments of this utility model and are not intended to limit the utility model in any other way. Any person skilled in the art may make changes or equivalent variations to the disclosed technical content and apply them to other fields. However, any simple modifications, equivalent changes, and alterations made to the above embodiments based on the technical essence of this utility model, without departing from the scope of the utility model's technical solution, shall still fall within the protection scope of this utility model's technical solution. In the description of this utility model, it should be noted that, unless otherwise explicitly specified and limited, the terms "installation" and "connection" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium; and they can refer to the internal connection of two components. For those skilled in the art, the specific meaning of the above terms in this utility model can be understood through specific circumstances.

Claims

1. A magnetic material separation structure for unmanned aerial vehicles, comprising a controller (1), characterized in that: The controller (1) has a body (3) on one side, an electromagnet (2) on one side, and a limiting device (4) on both sides. The limiting device (4) limits the material through a first limiting plate (44) and a second limiting plate (46).

2. The unmanned aerial vehicle magnetic material separation structure of claim 1, wherein: The controller (1) is provided with mounting components (5) on both sides. The mounting components (5) install the limiting device (4) on both sides of the controller (1). The limiting device (4) includes a placement plate (41), a motor (42), a round rod (43), a first limiting plate (44), an electric telescopic rod (45), and a second limiting plate (46). The motor (42) is located on one side of the placement plate (41) to drive the round rod (43) to rotate on one side of the placement plate (41). The round rod (43) drives the first limiting plate (44) to rotate. The electric telescopic rod (45) is located on one side of the first limiting plate (44) to drive the second limiting plate (46) to move.

3. The unmanned aerial vehicle magnetic material separation structure of claim 2, wherein: The round rod (43) is provided with a bearing (47) on the side near the placement plate (41), and the bearing (47) reduces the friction between the round rod (43) and the placement plate (41).

4. The unmanned aerial vehicle magnetic material separation structure of claim 3, wherein: A rubber pad (48) is provided on one side of the second limiting plate (46), and the rubber pad (48) increases the friction on one side of the second limiting plate (46).

5. The unmanned aerial vehicle magnetic material separation structure of claim 4, wherein: The first limiting plate (44) has a stabilizing plate (49) on the side near the second limiting plate (46), and the stabilizing plate (49) limits one side of the second limiting plate (46).

6. The unmanned aerial vehicle magnetic material separation structure of claim 5, wherein: The mounting assembly (5) includes two square tubes (51), bolts (52) and mounting plate (53). The two square tubes (51) are located on both sides of the controller (1). The bolts (52) are inserted into the square tubes (51) to fix the mounting plate (53) inside the square tubes (51). One side of the mounting plate (53) is connected to the placement plate (41).

7. The unmanned aerial vehicle magnetic material separation structure of claim 6, wherein: The mounting plate (53) has a trapezoidal block (54) on the side away from the placement plate (41), and the trapezoidal block (54) reduces the size of one side of the mounting plate (53). 8.The magnetic material separating structure of unmanned aerial vehicle according to claim 7, wherein: An operating block (55) is provided on one side of the bolt (52) to increase the size of one side of the bolt (52).

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