Unmanned aerial vehicle part coating equipment with adjustable nozzle structure
By designing a coating equipment for drone parts with an adjustable nozzle structure, the problem of the nozzle structure being unable to adjust the atomization particle size has been solved, achieving fine and uniform atomized particles and efficient spraying effect, adapting to the spraying needs of different materials.
Patent Information
- Application Number
- CN202520357358.3
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-03-04
- Publication Date
- 2026-02-24
- Estimated Expiration
- 2035-03-04
AI Technical Summary
The nozzle structure of existing drone component coating equipment cannot easily adjust the atomization particle size, resulting in poor uniformity and low efficiency of the finished product, especially when spraying different materials.
A coating device for drone parts with an adjustable nozzle structure was designed, including a nozzle head, a rotating nozzle mechanism, a rotating mechanism, and an adjustment mechanism. The distance between the cone inside the nozzle and the pressure cap is adjusted through the linkage mechanism, and the atomization particle size is controlled by high-intensity air pressure and shear force to adapt to the coating needs of different materials.
It achieves fine and uniform atomized particles, improves spraying efficiency and finished product quality, reduces maintenance difficulty, and adapts to the spraying needs of different materials.
Smart Images
Figure CN223931641U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of nozzle technology, and more specifically, to a coating device for drone parts with an adjustable nozzle structure. Background Technology
[0002] In the field of metal products, the processing of drone parts requires coating equipment to evenly coat the surface with anti-corrosion paint and other coating materials. This can form a barrier between the metal and the external environment (such as humid air, acid rain, corrosive chemicals, etc.), preventing or delaying the erosion of the metal by corrosive media, thereby extending the service life of metal products.
[0003] To maintain coating uniformity, atomized spraying is generally required, where gas and liquid collide to form atomized particles. However, existing devices do not allow for convenient adjustment of the atomized particle size to meet specific requirements, resulting in poor uniformity of the finished product. When spraying different materials, smaller particles adhere better but have lower spraying efficiency, while larger particles easily cause uneven coating. Therefore, we propose a coating device for UAV components with an adjustable nozzle structure. Utility Model Content
[0004] The purpose of this invention is to overcome the shortcomings of the existing technology, adapt to practical needs, and provide a coating equipment for drone parts with an adjustable nozzle structure to solve the technical problem that the current nozzle structure is inconvenient to adjust the atomized particle size, which easily affects the processing efficiency and the quality of the finished product.
[0005] To solve the above-mentioned technical problems, this utility model provides the following technical solution: a coating equipment for drone parts with an adjustable nozzle structure, including a nozzle head, a rotary nozzle mechanism, a rotating mechanism, and an adjusting mechanism. Two nozzle heads are provided, and the two nozzle heads are respectively installed at both ends of an assembly frame. A positioning ring is sleeved on the outer side of each nozzle head. Feed pipes are installed through both sides of the upper end of each nozzle head. The rotating mechanism is rotatably installed inside the upper end of the nozzle head. The adjusting mechanism is installed inside the lower end of the nozzle head, and the adjusting mechanism and the rotating mechanism are connected by a linkage mechanism. The rotary nozzle mechanism is threadedly installed at the lower end of the nozzle head. The rotary nozzle mechanism consists of an assembly nozzle and an inner cone. The inner cone is located inside the assembly nozzle. A discharge hole is formed in a circular array on the outer side of the lower end of the assembly nozzle.
[0006] In use, the spraying liquid and airflow are introduced through two separate feed pipes. The spraying liquid enters the inner rotating cylinder, is guided through the insertion hole into the assembly nozzle, and then flows into the liquid collection ring of the inner cone. The airflow passes through the protrusion and enters the lifting cylinder through the air outlet, then is guided into the assembly nozzle through the inner side of the pressure cap. A narrow gap is formed between the lower end of the pressure cap and the inner cone. The airflow passes through this gap and blows towards the spraying liquid in the liquid collection ring. High-intensity air pressure atomizes the spraying liquid, causing the atomized particles to be sprayed outwards through the discharge hole. The rotating nozzle mechanism is assembled using a spiral method. The inner cone is inserted and positioned on the assembly hole. The convenient assembly and disassembly design facilitates maintenance and allows for easy analysis of the formation process. The inner cone structure of the atomizing particles is replaced to reduce maintenance difficulty. The motor on the upper side of the nozzle head is started to drive the drive teeth to rotate. The drive teeth mesh with the inner tooth groove of the inner rotating cylinder to drive it to rotate. The inner rotating cylinder drives the lifting cylinder to rotate through the linkage mechanism. During the rotation of the lifting cylinder, the upper end and the lower end of the upright rod are connected by the screw thread to achieve lifting and lowering. The distance between the pressure cap at the lower end of the lifting cylinder and the inner cone body becomes smaller, so that the liquid is subjected to stronger shearing force and abrupt breaking action when passing through the conical area, thereby making the atomized droplets smaller and more uniform. Through the above structural design, the atomized particle size can be adjusted by adjusting the distance between the pressure cap and the inner cone body, which can be adapted to the spraying operation of different materials and ensure the practicality of the device.
[0007] Preferably, an assembly hole is provided in the middle of the assembly nozzle, and the lower end of the inner cone is inserted into the assembly hole, and an annular liquid collection ring is provided at the lower outer end of the inner cone.
[0008] Preferably, the rotating mechanism is composed of an inner rotating cylinder, and a protrusion is provided in the middle of the inner rotating cylinder. Insertion holes are provided on both sides of the bottom of the inner rotating cylinder, and meshing grooves are provided in an annular array on the upper inner side of the inner rotating cylinder.
[0009] Preferably, the linkage mechanism consists of a feed tube and a connecting ring. The feed tube is installed through both upper ends of the connecting ring, and the upper end of the feed tube is inserted into the insertion hole. The inner side of the connecting ring is provided with a slider end.
[0010] Preferably, the adjusting mechanism consists of a pressure cap and a lifting cylinder, with the pressure cap fixed at the lower end of the lifting cylinder. An air vent and an adjusting groove are provided on the outer side of the upper end of the lifting cylinder, and the air vent and the adjusting groove are staggered. The slider end of the connecting ring is slidably installed in the adjusting groove.
[0011] Preferably, the lower end of the pressure cap has a conical notch, which is connected to the inner cone. The top of the nozzle head is fixed with a vertical rod, and the threaded end of the vertical rod is threadedly connected to the upper opening of the lifting cylinder.
[0012] Compared with the prior art, the beneficial effects of this utility model are:
[0013] 1. This utility model designs a rotary nozzle mechanism, in which the spraying liquid and airflow are introduced through two feed pipes respectively. After the spraying liquid enters the inner rotating cylinder, it is guided into the assembly nozzle through the insertion hole, and then flows into the liquid collection ring of the inner cone. The airflow enters the lifting cylinder through the air outlet after passing through the protrusion, and then is introduced into the assembly nozzle through the inner side of the pressure cap. A narrow gap is formed between the concave end of the pressure cap and the inner cone. The airflow blows the spraying liquid through the gap to the liquid collection ring, and the spraying liquid is atomized by high-intensity air pressure. Then, the atomized particles are sprayed outward through the discharge hole. The rotary nozzle mechanism is assembled by a spiral. The inner cone is inserted and positioned on the assembly hole. The convenient installation and removal design facilitates maintenance and makes it easy to replace the inner cone structure that forms the atomized particles, reducing the difficulty of maintenance.
[0014] 2. This utility model also incorporates a rotating mechanism. The motor on the upper side of the nozzle head drives the drive teeth to rotate. The drive teeth mesh with the inner tooth groove of the inner rotating cylinder, causing it to rotate. The inner rotating cylinder, through a linkage mechanism, drives the lifting cylinder to rotate. During the rotation of the lifting cylinder, the upper end and the lower end of the upright rod are connected by a threaded joint to achieve lifting and lowering. The distance between the lower end pressure cap and the inner cone of the lifting cylinder decreases, causing the liquid to experience stronger shearing and breaking forces when passing through the conical area. This results in finer and more uniform atomized droplets. Through the above structural design, the distance between the pressure cap and the inner cone can be adjusted to regulate the atomized particle size, adapting to the spraying operations of different materials and ensuring the practicality of the device. Attached Figure Description
[0015] Figure 1 This is a schematic diagram of the main structure of this utility model;
[0016] Figure 2 This is a schematic diagram of the nozzle head of this utility model;
[0017] Figure 3 This is a schematic diagram of the connection structure of this utility model;
[0018] Figure 4 This is a schematic cross-sectional view of the nozzle head of this utility model;
[0019] Figure 5 This is a schematic diagram of the rotating mechanism of this utility model;
[0020] Figure 6 This is a schematic diagram of the rotary nozzle mechanism of this utility model;
[0021] Figure 7 This is a schematic diagram of the unfolded structure of this utility model.
[0022] The following are the labels in the diagram: 1. Nozzle head; 101. Feed pipe; 102. Vertical rod; 103. Drive gear; 2. Assembly frame; 3. Positioning ring; 4. Rotating nozzle mechanism; 401. Assembly nozzle; 402. Inner cone; 403. Liquid collection ring; 404. Assembly hole; 405. Discharge hole; 5. Rotating mechanism; 501. Inner rotating cylinder; 502. Protrusion; 503. Insertion hole; 6. Adjusting mechanism; 601. Air outlet; 602. Pressure cap; 603. Lifting cylinder; 604. Adjusting groove; 7. Linkage mechanism; 701. Feed pipe; 702. Connecting ring. Detailed Implementation
[0023] like Figures 1 to 5 As shown, this utility model relates to a coating equipment for drone parts with an adjustable nozzle structure, including a nozzle head 1, a rotating nozzle mechanism 4, a rotating mechanism 5, and an adjusting mechanism 6. Two nozzle heads 1 are provided, and the two nozzle heads 1 are respectively installed at both ends of the assembly frame 2. A positioning ring 3 is sleeved on the outer side of the nozzle head 1. Feed pipes 101 are installed through both sides of the upper end of the nozzle head 1. The rotating mechanism 5 is rotatably installed inside the upper end of the nozzle head 1. The adjusting mechanism 6 is installed inside the lower end of the nozzle head 1, and the adjusting mechanism 6 and the rotating mechanism 5 are connected by a linkage mechanism 7. The rotating mechanism 5 is composed of an inner rotating cylinder 501, with a protrusion 502 in the middle of the inner rotating cylinder 501. Insertion holes 503 are opened on both sides of the bottom of the inner rotating cylinder 501. Engaging grooves are arranged in a ring array on the upper inner side of the inner rotating cylinder 501. The linkage mechanism 7 is composed of a feed pipe 701 and a connecting ring 702. Feed pipes 701 are installed through both upper ends of the connecting ring 702. The upper end of the feed tube 701 is inserted into the insertion hole 503. The inner side of the connecting ring 702 is provided with a slider end. The spraying liquid and airflow are introduced through two feed tubes 101 respectively. After the spraying liquid enters the inner rotating cylinder 501, it is guided into the assembly nozzle 401 through the insertion hole 503, and then flows into the liquid collection ring port 403 of the inner cone 402. The airflow enters the lifting cylinder 603 through the air outlet 601 after passing through the protrusion 502, and then enters the assembly nozzle 401 through the inner side of the pressure cap 602. The lower end of the pressure cap 602 has a notch. A narrow gap is formed between the inner cone 402 and the sprayed liquid. The airflow passes through the gap and blows the sprayed liquid into the liquid collection ring 403. The sprayed liquid is atomized by high-intensity air pressure, and then the atomized particles are sprayed outward through the discharge hole 405. The rotary nozzle mechanism 4 is assembled by a spiral. The inner cone 402 is inserted and positioned on the assembly hole 404. The convenient installation and removal design facilitates maintenance and makes it easy to replace the inner cone 402 structure that forms the atomized particles, reducing the difficulty of maintenance.
[0024] like Figures 2 to 7As shown, this utility model relates to a coating equipment for drone parts with an adjustable nozzle structure, including a nozzle head 1, a rotating nozzle mechanism 4, a rotating mechanism 5, and an adjusting mechanism 6. The rotating nozzle mechanism 4 is threadedly installed at the lower end of the nozzle head 1. The rotating nozzle mechanism 4 consists of an assembly nozzle 401 and an inner cone 402. An assembly hole 404 is provided in the middle of the assembly nozzle 401, and the lower end of the inner cone 402 is inserted into the assembly hole 404. An annular liquid collection ring 403 is provided at the lower outer end of the inner cone 402. The inner cone 402 is located inside the assembly nozzle 401. An annular array of discharge holes 405 is provided on the lower outer side of the assembly nozzle 401. The adjusting mechanism 6 consists of a pressure cap 602 and a lifting cylinder 603. The pressure cap 602 is fixed to the lower end of the lifting cylinder 603. An air vent 601 and an adjusting groove 604 are provided on the upper outer side of the lifting cylinder 603, and the air vent 601 and the adjusting groove 604 are staggered. The slider end of the connecting ring 702 is slidably installed on... Inside the adjusting groove 604, the lower end of the pressure cap 602 has a conical notch, which mates with the inner cone 402. A vertical rod 102 is fixed to the top of the nozzle head 1. The threaded end of the vertical rod 102 is threadedly connected to the upper opening of the lifting cylinder 603. Starting the motor on the upper side of the nozzle head 1 drives the drive gear 103 to rotate. The drive gear 103 meshes with the inner tooth groove of the inner rotating cylinder 501, causing it to rotate. The inner rotating cylinder 501 drives the lifting cylinder 603 to rotate via the linkage mechanism 7. During the rotation process, the upper end and the lower end of the vertical rod 102 are connected by a threaded joint to achieve lifting and lowering. The distance between the lower end of the lifting cylinder 603 pressure cap 602 and the inner cone 402 becomes smaller, so that the liquid is subjected to stronger shearing force and abrupt breaking action when passing through the conical area, thereby making the atomized droplets smaller and more uniform. Through the above structural design, the atomized particle size can be adjusted by adjusting the distance between the pressure cap 602 and the inner cone 402, which is suitable for spraying operations of different materials and ensures the practicality of the device.
[0025] Working Principle: This embodiment provides a coating device for drone parts with an adjustable nozzle structure. In use, the coating liquid and airflow are introduced through two feed pipes 101. After entering the inner rotating cylinder 501, the coating liquid is guided through the insertion hole 503 into the assembly nozzle 401, and then flows into the liquid collection ring 403 of the inner cone 402. The airflow passes through the protrusion 502 and enters the lifting cylinder 603 through the air outlet 601, then passes through the inner side of the pressure cap 602 into the assembly nozzle 401. A narrow gap is formed between the lower end recess of the pressure cap 602 and the inner cone 402. The airflow passes through this gap and blows towards the coating liquid in the liquid collection ring 403, atomizing the coating liquid through high-intensity air pressure. The particles are ejected outward through the discharge hole 405. The rotary nozzle mechanism 4 is assembled in a spiral manner. The inner cone 402 is inserted and positioned on the assembly hole 404. The motor on the upper side of the nozzle head 1 is started to drive the drive gear 103 to rotate. The drive gear 103 meshes with the inner tooth groove of the inner rotating cylinder 501 to drive it to rotate. The inner rotating cylinder 501 drives the lifting cylinder 603 to rotate through the linkage mechanism 7. During the rotation of the lifting cylinder 603, the upper end and the lower end of the vertical rod 102 are engaged to achieve lifting and lowering. The distance between the lower end pressure cap 602 of the lifting cylinder 603 and the inner cone 402 becomes smaller, so that the liquid is subjected to stronger shearing force and crushing effect when passing through the conical area, thereby making the atomized droplets finer and more uniform.
[0026] The embodiments disclosed herein are preferred embodiments, but are not limited thereto. Those skilled in the art can readily grasp the spirit of this utility model based on the above embodiments and make different extensions and variations. However, as long as they do not depart from the spirit of this utility model, they are all within the protection scope of this utility model.
Claims
1. A coating device for drone parts with an adjustable nozzle structure, comprising a nozzle head (1), a rotating nozzle mechanism (4), a rotating mechanism (5), and an adjusting mechanism (6), characterized in that: There are two nozzle heads (1), and the two nozzle heads (1) are respectively installed at both ends of the assembly frame (2). A positioning ring (3) is sleeved on the outside of the nozzle head (1). Feed pipes (101) are installed through both sides of the upper end of the nozzle head (1). The rotating mechanism (5) is rotatably installed inside the upper end of the nozzle head (1). The adjusting mechanism (6) is installed inside the lower end of the nozzle head (1). The adjusting mechanism (6) and the rotating mechanism (5) are connected by a linkage mechanism (7). The rotating nozzle mechanism (4) is threadedly installed at the lower end of the nozzle head (1). The rotating nozzle mechanism (4) consists of an assembly nozzle (401) and an inner cone (402). The inner cone (402) is located inside the assembly nozzle (401). The lower outer side of the assembly nozzle (401) is provided with a circular array of discharge holes (405).
2. The coating equipment for UAV parts with an adjustable nozzle structure according to claim 1, characterized in that: The assembly nozzle (401) has an assembly hole (404) in the middle, and the lower end of the inner cone (402) is inserted into the assembly hole (404). The lower outer end of the inner cone (402) has an annular liquid collection ring (403).
3. The coating equipment for UAV parts with an adjustable nozzle structure according to claim 2, characterized in that: The rotating mechanism (5) is composed of an inner rotating cylinder (501), and a protrusion (502) is provided in the middle of the inner rotating cylinder (501). Insertion holes (503) are provided on both sides of the bottom of the inner rotating cylinder (501), and meshing grooves are provided in an annular array on the upper inner side of the inner rotating cylinder (501).
4. The coating equipment for UAV parts with an adjustable nozzle structure according to claim 3, characterized in that: The linkage mechanism (7) consists of a feed tube (701) and a connecting ring (702). The feed tube (701) is installed through both upper ends of the connecting ring (702), and the upper end of the feed tube (701) is inserted into the insertion hole (503). The inner side of the connecting ring (702) is provided with a slider end.
5. The coating equipment for UAV parts with an adjustable nozzle structure according to claim 4, characterized in that: The adjustment mechanism (6) consists of a pressure cap (602) and a lifting cylinder (603), with the pressure cap (602) fixed at the lower end of the lifting cylinder (603). An air vent (601) and an adjustment groove (604) are provided on the outer side of the upper end of the lifting cylinder (603), and the air vent (601) and the adjustment groove (604) are staggered. The slider end of the connecting ring (702) is slidably installed in the adjustment groove (604).
6. The coating equipment for UAV parts with an adjustable nozzle structure according to claim 5, characterized in that: The lower end of the pressure cap (602) is provided with a conical notch, and the conical notch is connected to the inner cone (402). The top of the nozzle head (1) is fixed with a vertical rod (102), and the screw end of the lower end of the vertical rod (102) is threadedly connected to the upper opening of the lifting cylinder (603).