Unmanned aerial vehicle routing inspection landing platform
By designing a drone inspection landing platform and utilizing a servo motor-driven clamping block and rubber rod airbag buffer structure, the problem of drone tilting and sliding on unpaved ground was solved, achieving stable landing and improved safety for the drone.
Patent Information
- Application Number
- CN202520377816.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-03-05
- Publication Date
- 2025-12-26
- Estimated Expiration
- 2035-03-05
AI Technical Summary
When a drone lands on unpaved ground, the fuselage tilts and slides, causing the blades to collide with the ground and resulting in damage to the drone.
A drone inspection landing platform was designed, comprising a landing platform, a servo motor, a lead screw, a clamping block, a support assembly, and a dust removal assembly. The servo motor drives the clamping block to hold the drone, and the combination of a rubber rod and an airbag buffer and shock absorption structure ensures stable landing of the drone.
It improves the stability and safety of drone landing, reduces blade damage, and extends the service life of drones.
Smart Images

Figure CN223721197U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model belongs to unmanned plane technical field, specifically a kind of unmanned plane inspection landing platform. BACKGROUND
[0002] Unmanned plane inspection is to detect and maintain equipment, facilities or building environment using unmanned plane technology, commonly used in electric power, oil and gas, wind, bridge, agriculture and environmental detection and other fields.
[0003] The advantage of unmanned plane inspection has fast coverage of large area, shortens the inspection time, reduces the risk of high-altitude or dangerous environment operation, adapts to complex terrain, carries high-precision sensor, can provide detailed data, and generally includes task planning, flight execution, data transmission and analysis and maintenance plan making in unmanned plane inspection process, after inspection, unmanned plane needs to land in flat area.
[0004] In the existing unmanned plane technology, when unmanned plane lands on non-paved ground, the body will tilt and slide, causing the blade to knock the ground, causing the unmanned plane to be damaged.
[0005] Therefore, the utility model provides a kind of unmanned plane inspection landing platform. UTILITY MODEL CONTENT
[0006] In order to make up for the deficiency of prior art, at least one technical problem proposed in the background art is solved.
[0007] The utility model solves the technical scheme that the utility model discloses a kind of unmanned plane inspection landing platform, including landing platform;The servo motor is fixedly connected in the middle part of the landing platform;The screw rod is fixedly connected in the transmission end of the servo motor;The screw rod is rotatably connected in the middle part of the landing platform;The clamping block is matched with the screw rod screw nut pair;The clamping block slides in the middle part of the landing platform;A pair of clamping blocks are symmetrically arranged in the middle part of the landing platform;The clamping block is mutually inclined;The landing platform bottom is equipped with damping assembly;The fixed assembly is equipped on the inner wall of the clamping block;The landing platform is equipped with dust removal assembly through damping assembly;The landing platform is equipped with support assembly through damping assembly;This step is equipped with unmanned plane landing platform structure by the setting of landing platform, servo motor, screw rod, clamping block, support assembly and dust removal assembly, realizes the function that unmanned plane is fixed after landing on the top of landing platform, solves the situation that unmanned plane tilts and falls from the top of landing platform after landing, improves the stability after unmanned plane landing, reduces the situation that unmanned plane blade is damaged due to the tilt of unmanned plane after landing, improves the safety of unmanned plane landing.
[0008] Preferably, the damping assembly comprises rubber rods, a base box and air bags; the rubber rods are arranged in multiple groups; the multiple groups of the rubber rods are fixedly connected to the bottom and the side wall of the landing platform; the ends of the multiple groups of the rubber rods away from the landing platform are fixedly connected to the inner side wall of the base box; the air bags are fixedly connected to the inner side wall of the base box; the air bags are arranged in multiple groups on the inner side wall of the base box and are uniformly distributed at the four corners of the inner side wall of the base box; this step, by arranging the rubber rods, the base box and the air bags, forms a landing platform buffering and damping structure, achieves the function of buffering the impact generated when the unmanned aerial vehicle lands, solves the problem that the unmanned aerial vehicle is damaged due to impact with the landing platform when the unmanned aerial vehicle lands, improves the stability of the unmanned aerial vehicle when it lands, reduces the damage to the internal parts of the unmanned aerial vehicle caused by impact, and improves the service life of the unmanned aerial vehicle.
[0009] Preferably, the fixing assembly comprises springs, a pressing plate and protrusions; the pressing plate is slidingly connected to the inner side wall of the clamping block; one end of the spring is fixedly connected to the inside of the clamping block; the spring is arranged in multiple groups on the inner side wall of the clamping block and is symmetrically arranged; the other end of the spring is fixedly connected to the side wall of the pressing plate; the protrusions are fixedly connected to the inner side wall of the clamping block near the bottom of the pressing plate; this step, by arranging the spring, the pressing plate and the protrusion, forms a support frame fixing structure, achieves the function of fixing the support frame in the middle of the clamping block, solves the problem of shaking of the support frame in the middle of the clamping block, and improves the stability of the clamping block when clamping and fixing the support frame.
[0010] Preferably, the dust cleaning assembly comprises a fixed plate and air nozzles; the fixed plate is fixedly connected to the top of the base box; the air nozzles are fixedly connected to the middle of the fixed plate; the air nozzles are arranged in multiple groups in the middle of the fixed plate and are uniformly distributed in the middle of the fixed plate; this step, by arranging the fixed plate and the air nozzles, forms a dust cleaning structure on the top of the landing platform, achieves the function of cleaning the top of the landing platform, solves the problem that dust or foreign matter adheres to the top of the landing platform, causing abnormal wear of the support frame, and improves the cleanliness of the top of the landing platform.
[0011] Preferably, the support assembly comprises legs, foot plates and ground nails; the legs are hingedly connected to the outer side wall of the base box; the legs are arranged in multiple groups on the outer side wall of the base box and are symmetrically arranged; the foot plates are hingedly connected to the ends of the legs away from the base box; the ground nails are fixedly connected to the bottom of the foot plates; the ground nails are arranged in multiple groups on the bottom of the foot plates and are uniformly distributed on the bottom of the foot plates; this step, by arranging the legs, the foot plates and the ground nails, forms a base box support and fixing structure, achieves the function of supporting and fixing the device, solves the problem of sliding or deviation of the base box when placed, and improves the stability of the device when placed.
[0012] Preferably, the outer side wall of the landing platform is fixedly connected with elastic cloth; the outer side wall of the elastic cloth is fixedly connected with the inner side wall of the base box; through the setting of the elastic cloth, a sealing structure is formed, dust or foreign matters are reduced from entering the inside of the landing platform and the base box, and the cleanliness of the inside of the base box is improved.
[0013] Preferably, the supporting leg is made of stainless steel; the supporting leg is made of stainless steel, the structural strength of the supporting leg is improved, the corrosion of the supporting leg by the ground is reduced, and the service life of the supporting leg is improved.
[0014] The beneficial effects of the utility model are as follows:
[0015] 1. The unmanned aerial vehicle inspection landing platform, through the setting of the landing platform, the servo motor, the lead screw, the clamping block, the supporting assembly and the dust removal assembly, a landing platform structure of the unmanned aerial vehicle is formed, the function of fixing the unmanned aerial vehicle after the unmanned aerial vehicle lands on the top of the landing platform is realized, the situation that the unmanned aerial vehicle tilts and falls from the top of the landing platform after landing is solved, the stability of the unmanned aerial vehicle after landing is improved, the situation that the unmanned aerial vehicle blade is damaged due to the tilt of the unmanned aerial vehicle after landing is reduced, and the safety of the unmanned aerial vehicle during landing is improved.
[0016] 2. The unmanned aerial vehicle inspection landing platform, through the setting of the rubber rod, the base box and the air bag, a landing platform buffer damping structure is formed, the function of buffering the impact generated when the unmanned aerial vehicle lands is realized, the situation that the unmanned aerial vehicle is damaged due to the impact between the unmanned aerial vehicle and the landing platform during landing is solved, the stability of the unmanned aerial vehicle during landing is improved, the situation that the internal parts of the unmanned aerial vehicle are damaged due to the impact of the unmanned aerial vehicle is reduced, and the service life of the unmanned aerial vehicle is improved. BRIEF DESCRIPTION OF DRAWINGS
[0017] The utility model will be further described in connection with the drawings.
[0018] Figure 1 It is the perspective view of the utility model;
[0019] Figure 2 It is the structure schematic view of the air bag and the landing platform cooperation in the utility model;
[0020] Figure 3 It is the structure schematic view of the clamping block and the landing platform cooperation in the utility model;
[0021] Figure 4 It is the structure schematic view of the pressing plate and the clamping block cooperation in the utility model.
[0022] In the diagram: 1. Landing platform; 11. Servo motor; 12. Lead screw; 13. Clamping block; 2. Rubber rod; 21. Base box; 22. Airbag; 3. Spring; 31. Pressure plate; 32. Protruding strip; 4. Fixing plate; 41. Air nozzle; 5. Support leg; 51. Foot plate; 52. Ground stake; 6. Elastic cloth. Detailed Implementation
[0023] To make the technical means, creative features, objectives and effects of this utility model easier to understand, the present utility model will be further described below in conjunction with specific embodiments.
[0024] like Figures 1 to 4 As shown, an embodiment of this utility model provides a drone inspection landing platform, including a landing platform 1; a servo motor 11 is fixedly connected to the middle of the landing platform 1; a lead screw 12 is fixedly connected to the transmission end of the servo motor 11; the lead screw 12 is rotatably connected to the middle of the landing platform 1; a clamping block 13 is fitted to the lead screw 12 and nut pair; the clamping block 13 slides in the middle of the landing platform 1; a pair of clamping blocks 13 are arranged symmetrically in the middle of the landing platform 1; the clamping blocks 13 are inclined to each other; a shock-absorbing component is provided at the bottom of the landing platform 1; a fixing component is provided on the inner side wall of the clamping block 13; a dust-cleaning component is provided on the landing platform 1 through the shock-absorbing component; a support component is provided on the landing platform 1 through the shock-absorbing component; during operation, the device is placed on the ground and fixed by the support component; the dust-cleaning component blows off the dust or foreign objects on the top of the landing platform 1; after the drone inspection is completed, the drone lands on the landing platform 1. At the top of landing platform 1, the drone's support frame contacts the top of landing platform 1. The servo motor 11 is activated, driving the lead screw 12 to rotate. The lead screw 12 then drives the clamping blocks 13 to move closer together, contacting and clamping the drone's support frame. After the drone stops, the servo motor 11 is reversed, the clamping blocks 13 open, and the fixed drone is released. This step, through the arrangement of landing platform 1, servo motor 11, lead screw 12, clamping blocks 13, support components, and dust removal components, forms a drone landing platform structure. This achieves the function of fixing the drone after it lands on the top of landing platform 1, solving the problem of the drone tilting and falling from the top of landing platform 1 after landing, improving the stability of the drone after landing, reducing the possibility of drone blade damage due to tilting after landing, and improving the safety of drone landing.
[0025] like Figure 2As shown, the damping assembly includes rubber rods 2, a base box 21 and air bags 22; the rubber rods 2 are provided in multiple groups; the multiple groups of rubber rods 2 are fixedly connected to the bottom and the side wall of the landing platform 1; the ends of the multiple groups of rubber rods 2 away from the landing platform 1 are fixedly connected to the inner side wall of the base box 21; the air bags 22 are fixedly connected to the inner side wall of the base box 21; the air bags 22 are provided in multiple groups on the inner side wall of the base box 21 and are uniformly distributed at the four corners of the inner side wall of the base box 21; in work, when the unmanned aerial vehicle lands on the top of the landing platform 1, the unmanned aerial vehicle impacts the landing platform 1, the rubber rods 2 slow down the impact of the landing platform 1, the landing platform 1 shakes after being impacted, and the air bags 22 protect the corners of the landing platform 1; through the arrangement of the rubber rods 2, the base box 21 and the air bags 22, a landing platform 1 buffer damping structure is formed, the function of buffering the impact generated when the unmanned aerial vehicle lands is realized, the situation that the unmanned aerial vehicle is damaged due to the impact between the unmanned aerial vehicle and the landing platform 1 when the unmanned aerial vehicle lands is solved, the stability of the unmanned aerial vehicle when landing is improved, the situation that the internal parts of the unmanned aerial vehicle are damaged due to the impact of the unmanned aerial vehicle is reduced, and the service life of the unmanned aerial vehicle is improved.
[0026] As shown in Figure 4 , the fixing assembly includes springs 3, a pressing plate 31 and protrusions 32; the pressing plate 31 is slidingly connected to the inner side wall of the clamping block 13; one end of the spring 3 is fixedly connected to the inside of the clamping block 13; multiple groups of springs 3 are arranged on the inner side wall of the clamping block 13 and are symmetrically arranged; the other end of the spring 3 is fixedly connected to the side wall of the pressing plate 31; the protrusions 32 are fixedly connected to the inner side wall of the clamping block 13 near the bottom of the pressing plate 31; in work, when the clamping block 13 clamps and fixes the support frame of the unmanned aerial vehicle, the pressing plate 31 contacts the support frame, the pressing plate 31 is extruded when the clamping blocks 13 are close to each other, the springs 3 are compressed, and the protrusions 32 and the pressing plate 31 cooperate to fix the support frame in the middle of the clamping block 13; through the arrangement of the springs 3, the pressing plate 31 and the protrusions 32, a support frame fixing structure is formed, the function of fixing the support frame in the middle of the clamping block 13 is realized, the situation that the support frame shakes in the middle of the clamping block 13 is solved, and the stability of the clamping block 13 when clamping and fixing the support frame is improved.
[0027] As shown in Figure 1 , the dust cleaning assembly includes a fixed plate 4 and air nozzles 41; the fixed plate 4 is fixedly connected to the top of the base box 21; the air nozzles 41 are fixedly connected to the middle of the fixed plate 4; multiple groups of air nozzles 41 are arranged in the middle of the fixed plate 4 and are uniformly distributed in the middle of the fixed plate 4; in work, the air nozzles 41 are connected to compressed air, when dust or foreign matter adheres to the top of the landing platform 1, the air nozzles 41 in the middle of the fixed plate 4 blow air to the top of the landing platform 1, and blow off the dust or foreign matter adhering to the top of the landing platform 1; through the arrangement of the fixed plate 4 and the air nozzles 41, a landing platform 1 top dust cleaning structure is formed, the function of cleaning the top of the landing platform 1 is realized, the situation that dust or foreign matter adheres to the top of the landing platform 1, causing the support frame to abnormally wear, is solved, and the cleanliness of the top of the landing platform 1 is improved.
[0028] As Figure 1 shown, the support assembly comprises a support leg 5, a foot disc 51 and a ground nail 52; the support leg 5 is hinged to the outer side wall of the base box 21; a plurality of groups of support legs 5 are arranged on the outer side wall of the base box 21 and are symmetrically arranged; the foot disc 51 is hinged to the end of the support leg 5 away from the base box 21; the ground nail 52 is fixedly connected to the bottom of the foot disc 51; a plurality of groups of ground nails 52 are arranged on the bottom of the foot disc 51 and are uniformly distributed on the bottom of the foot disc 51; in work, after the base box 21 is placed on the ground, the support leg 5 is rotated, the foot disc 51 is in contact with the ground, the ground nail 52 is inserted into the ground, and the base box 21 is supported and fixed; through the arrangement of the support leg 5, the foot disc 51 and the ground nail 52, a support and fixing structure of the base box 21 is formed, the function of supporting and fixing the device is realized, the situation that the base box 21 slips or deviates when placed is solved, and the stability of the device when placed is improved.
[0029] As Figure 1 shown, the elastic cloth 6 is fixedly connected to the outer side wall of the landing platform 1; the outer side wall of the elastic cloth 6 is fixedly connected to the inner side wall of the base box 21; in work, the elastic cloth 6 seals between the landing platform 1 and the base box 21, and blocks dust or foreign matter outside; through the arrangement of the elastic cloth 6, a sealing structure is formed, dust or foreign matter entering the inside of the landing platform 1 and the base box 21 is reduced, and the cleanliness of the inside of the base box 21 is improved.
[0030] As Figure 1 shown, the support leg 5 is made of stainless steel; in work, the support leg 5 is made of stainless steel, the structural strength of the support leg 5 is improved, the situation that the support leg 5 is corroded by the ground is reduced, and the service life of the support leg 5 is improved.
[0031] In work, the device is placed on the ground, the device is fixed through the support assembly, the dust or foreign matter on the top of the landing platform 1 is blown off by the dust removal assembly, after the unmanned aerial vehicle completes the inspection, the unmanned aerial vehicle lands on the top of the landing platform 1, the support frame of the unmanned aerial vehicle contacts the top of the landing platform 1, the servo motor 11 is started, the servo motor 11 drives the screw rod 12 to rotate, the screw rod 12 drives the clamping blocks 13 to approach each other, the clamping blocks 13 contact the support frame of the unmanned aerial vehicle and clamp and fix the support frame, after the unmanned aerial vehicle stops, the servo motor 11 is reversed, the clamping blocks 13 are opened, and the fixed unmanned aerial vehicle is loosened; when the unmanned aerial vehicle lands on the top of the landing platform 1, the unmanned aerial vehicle impacts the landing platform 1, the rubber rod 2 alleviates the impact of the landing platform 1, the landing platform 1 shakes after being impacted, and the air bag 22 protects the corners of the landing platform 1; when the clamping blocks 13 clamp and fix the support frame of the unmanned aerial vehicle, the pressing plate 31 contacts the support frame, the pressing plate 31 is extruded when the clamping blocks 13 approach each other, the spring 3 is compressed, and the convex strip 32 and the pressing plate 31 cooperate to fix the support frame in the middle of the clamping blocks 13; the air nozzle 41 is connected with compressed air, when dust or foreign matter adheres to the top of the landing platform 1, the air nozzle 41 in the middle of the fixed plate 4 blows air to the top of the landing platform 1, and blows off the dust or foreign matter adhering to the top of the landing platform 1; after the base box 21 is placed on the ground, the support leg 5 is rotated, the foot disc 51 contacts the ground, and the ground nail 52 is inserted into the ground to support and fix the base box 21; the elastic cloth 6 seals between the landing platform 1 and the base box 21, and blocks dust or foreign matter outside; the support leg 5 is made of stainless steel, the structural strength of the support leg 5 is improved, the corrosion of the support leg 5 by the ground is reduced, and the service life of the support leg 5 is improved.
[0032] The basic principle, main features and advantages of the utility model are shown and described above. It should be understood by those skilled in the art that the utility model is not limited by the above examples, and the above examples and descriptions in the specification are only to illustrate the principle of the utility model, and various changes and improvements can be made to the utility model without departing from the spirit and scope of the utility model, and these changes and improvements all fall within the scope of the utility model claimed. The protection scope of the utility model is defined by the appended claims and their equivalents.
Claims
1. A drone inspection landing platform, comprising a landing platform (1); characterized in that: A servo motor (11) is fixedly connected to the middle of the landing platform (1); a lead screw (12) is fixedly connected to the transmission end of the servo motor (11); the lead screw (12) is rotatably connected to the middle of the landing platform (1); a clamping block (13) is fitted to the lead screw nut pair of the lead screw (12); the clamping block (13) slides in the middle of the landing platform (1); a pair of clamping blocks (13) are provided in the middle of the landing platform (1) and are symmetrically arranged; the clamping blocks (13) are inclined to each other; a shock-absorbing component is provided at the bottom of the landing platform (1); a fixing component is provided on the inner side wall of the clamping block (13); a dust removal component is provided on the landing platform (1) through the shock-absorbing component; a support component is provided on the landing platform (1) through the shock-absorbing component.
2. The UAV inspection and landing platform according to claim 1, characterized in that: The shock absorption assembly includes a rubber rod (2), a base box (21), and an airbag (22); multiple sets of the rubber rod (2) are provided; multiple sets of the rubber rod (2) are fixedly connected to the bottom and side wall of the landing platform (1); the ends of the multiple sets of the rubber rod (2) away from the landing platform (1) are jointly fixedly connected to the inner side wall of the base box (21); the airbag (22) is fixedly connected to the inner side wall of the base box (21); multiple sets of the airbag (22) are provided on the inner side wall of the base box (21), and are evenly distributed at the four corners of the inner side wall of the base box (21).
3. The UAV inspection and landing platform according to claim 1, characterized in that: The fixing assembly includes a spring (3), a pressure plate (31), and a protrusion (32); the pressure plate (31) is slidably connected to the inner wall of the clamping block (13); one end of the spring (3) is fixedly connected to the inside of the clamping block (13); multiple sets of springs (3) are provided on the inner wall of the clamping block (13) and are arranged symmetrically; the other end of the spring (3) is fixedly connected to the side wall of the pressure plate (31); the protrusion (32) is fixedly connected to the bottom of the inner wall of the clamping block (13) near the pressure plate (31).
4. The UAV inspection and landing platform according to claim 2, characterized in that: The dust removal assembly includes a fixed plate (4) and an air nozzle (41); the fixed plate (4) is fixedly connected to the top of the base box (21); the air nozzle (41) is fixedly connected to the middle of the fixed plate (4); multiple sets of air nozzles (41) are provided in the middle of the fixed plate (4) and are evenly distributed in the middle of the fixed plate (4).
5. The UAV inspection landing platform according to claim 2, characterized in that: The support assembly includes a support leg (5), a foot plate (51), and a ground nail (52); the support leg (5) is hinged to the outer wall of the base box (21); multiple sets of the support leg (5) are provided on the outer wall of the base box (21) and are arranged symmetrically; the foot plate (51) is hinged to the end of the support leg (5) away from the base box (21); the ground nail (52) is fixedly connected to the bottom of the foot plate (51); multiple sets of the ground nail (52) are provided on the bottom of the foot plate (51) and are evenly distributed on the bottom of the foot plate (51).
6. The UAV inspection landing platform according to claim 2, characterized in that: An elastic cloth (6) is fixedly connected to the outer wall of the landing platform (1); the outer wall of the elastic cloth (6) is fixedly connected to the inner wall of the base box (21).
7. The UAV inspection landing platform according to claim 5, characterized in that: The support leg (5) is made of stainless steel.