A portable unmanned aerial vehicle landing base

Abstract

The utility model relates to the technical field of unmanned plane landing seat, especially portable unmanned plane landing base, the utility model provides such a portable unmanned plane landing base, including support frame, strip type lamp, waterproof membrane, buffer block and hinge etc, the inboard fixed connection of support frame has buffer block, support frame and buffer block symmetry formula are provided with two, two buffer blocks are through the hinge symmetry formula rotation connection, and the hinge symmetry formula is installed on the side of two buffer block bottom each other close, two buffer block top all fixedly connected with waterproof membrane, two waterproof membranes are all fixedly connected with strip type lamp between the similar support frame. The utility model discloses through handle and hinge cooperation to realize the unfolding and folding of equipment, and it is convenient to carry and quickly deploy, through the cooperation of telescopic link and limiting block, realize the stable support of equipment on uneven ground, and can adjust height according to the terrain, improve applicability.

Description

Technical Field

[0001] This utility model relates to the field of drone landing pad technology, and in particular to a portable drone landing pad. Background Technology

[0002] The landing gear, or drone landing pad, primarily supports the drone for safe takeoff and landing. It bears and distributes the drone's weight during takeoff and landing, reducing damage to equipment from ground collisions. Through effective shock absorption design, it absorbs landing impact forces, protecting onboard instruments from vibration. Furthermore, its adaptability to different terrains allows the drone to operate in various complex environments, ensuring stability and preventing tilting or tipping, thus guaranteeing the safe and successful completion of flight missions.

[0003] Traditional landing gear often uses fixed brackets or sled-type structures. Although they can provide basic support, they generally have problems such as poor shock absorption and weak ability to adapt to complex terrain. Especially in outdoor operations, drones often face challenges such as uneven ground, strong wind interference, and nighttime operations, which can increase take-off and landing risks or interrupt missions.

[0004] Therefore, a portable drone landing pad needs to be designed to solve the above-mentioned technical problems. Utility Model Content

[0005] To overcome the shortcomings of being unable to cope with strong winds and varied terrain, this utility model provides a portable drone landing pad.

[0006] The technical solution of this utility model is as follows: a portable drone landing pad, comprising a support frame, strip lights, a waterproof membrane, reflective pads, a handle, protrusions, buffer blocks, hinges, a telescopic rod, limiting blocks, and anti-slip pads. Buffer blocks are fixedly connected to the inner side of the support frame. Two buffer blocks are symmetrically arranged, and the two buffer blocks are symmetrically connected by hinges. The hinges are symmetrically installed on the bottom sides of the two buffer blocks that are close to each other. A waterproof membrane is fixedly connected to the top of each of the two buffer blocks. Strip lights are fixedly connected between each waterproof membrane and the adjacent support frame. Multiple reflective stickers are symmetrically fixedly connected to one side of the part. Handles are fixedly connected to one side of each of the two support frames. Multiple protrusions are fixedly connected to the bottom of the handle on the left in a linear array. Multiple grooves for the protrusions to be engaged are opened at the bottom of the handle on the right. Multiple square slots are symmetrically opened in a rectangular array at the bottom of the buffer block. Telescopic rods are symmetrically rotatably connected to one side of each square slot. Several through holes are arranged in a linear array on each telescopic rod. Anti-slip pads are fixedly connected to the side of each telescopic rod near the hinge. Limiting blocks are installed on the through holes near the anti-slip pads.

[0007] As a preferred technical solution of this utility model, it also includes a storage battery and a locator. Multiple rectangular slots are symmetrically opened on one side of the bottom of the two buffer blocks. Multiple storage batteries are symmetrically fixedly connected in all rectangular slots. A locator is fixedly connected on one side of the bottom of each storage battery. The two strip lights and all the locators are electrically connected to the storage battery.

[0008] As a preferred technical solution of this utility model, it also includes a placement box, a sealing cover, a connecting block, and a hook. Multiple placement boxes for placing weights are symmetrically fixedly connected to the sides of the two support frames that are close to each other. A sealing cover is rotatably connected to the sides of all placement boxes that are far apart from each other. Multiple placement slots are symmetrically opened at the bottom of the two buffer blocks on the sides that are far apart from each other. A connecting block is fixedly connected to one side inside each placement slot. A hook is rotatably connected to the side of each connecting block that is close to the hinge. All hooks can be stored in the placement slots.

[0009] As a preferred technical solution of this utility model, it also includes a solar panel, a slide rail and a stop block. Multiple solar panels are arranged symmetrically on the left and right sides. Multiple slide rails are symmetrically fixedly connected to both sides of each solar panel. A stop block is fixedly connected to the end of each slide rail that is close to each other. All solar panels are slidably connected to the middle of two buffer blocks on the side that is far apart from each other. All solar panels are electrically connected to all batteries.

[0010] As a preferred technical solution of this utility model, it also includes magnets, with magnets symmetrically embedded and fixedly connected to one side of the bottom of the two buffer blocks.

[0011] As a preferred technical solution of this utility model, the buffer block is made of rubber.

[0012] Beneficial effects: 1. This utility model uses a handle and hinge to unfold and fold the equipment, making it easy to carry and deploy quickly. The telescopic rod and limit block work together to provide stable support for the equipment on uneven ground, and the height can be adjusted according to the terrain to improve its applicability.

[0013] 2. This utility model provides visual and signal guidance for drones by working in conjunction with reflective stickers and locators, thereby improving landing accuracy. It also provides flashing guidance at night through strip lights, making it easier for drones to land at night.

[0014] 3. This utility model collects solar energy through solar panels to charge the battery, extending the equipment's range and adapting to outdoor environments. It also protects circuit components with a waterproof membrane to prevent short circuits caused by rain, thus improving equipment reliability. Attached Figure Description

[0015] Figure 1 This is a three-dimensional structural diagram of the present invention.

[0016] Figure 2 This is a three-dimensional structural diagram of the components of this utility model, including the strip light, waterproof membrane, and reflective sticker.

[0017] Figure 3 This is a three-dimensional structural diagram of the buffer block, hinge, and telescopic rod components of this utility model.

[0018] Figure 4 for Figure 3 Enlarged diagram of point A in the middle.

[0019] Figure 5 This is a three-dimensional structural diagram of the telescopic rod, limiting block, and anti-slip pad of this utility model.

[0020] Figure 6 This is a partial cross-sectional view of the reflective sticker, handle, and solar panel components of this utility model.

[0021] Figure 7 This is a three-dimensional structural diagram of the solar panel, slide rail, and stop block components of this utility model.

[0022] The components in the attached diagram are labeled as follows: 1-Support frame, 2-Strip light, 3-Waterproof membrane, 4-Reflective sticker, 5-Handle, 6-Protrusion, 7-Buffer block, 8-Hinge, 9-Telescopic rod, 10-Limit block, 11-Anti-slip pad, 12-Battery, 13-Positioner, 14-Placement box, 15-Sealing cover, 16-Connecting block, 17-Hook, 18-Solar panel, 19-Slide rail, 20-Stop block, 21-Magnet. Detailed Implementation

[0023] Example: A portable drone landing pad, such as Figure 1-6As shown, the system includes a support frame 1, strip lights 2, a waterproof membrane 3, reflective pads 4, a handle 5, a protrusion 6, a buffer block 7, a hinge 8, a telescopic rod 9, a limiting block 10, and an anti-slip pad 11. Buffer blocks 7, made of rubber, are glued to the inner side of the support frame 1. Two buffer blocks 7 are symmetrically arranged on the left and right sides, connected by hinges 8 in a symmetrical rotational manner. The hinges 8 are symmetrically installed on the bottom sides of the two buffer blocks 7, close to each other. A waterproof membrane 3 is glued to the top of each buffer block 7. Strip lights 2 are glued between the two waterproof membranes 3 and the sides of the support frame 1 that are close to each other. Two reflective stickers 4 are glued together in a symmetrical arrangement on the left and right sides. Handles 5 are bolted to the two support frames 1 on the opposite sides. Three protrusions 6 are welded in a linear array on the bottom right side of the left handle 5. Three grooves are provided on the bottom left side of the right handle 5 so that the protrusions 6 can be locked in place. The bottom of the buffer block 7 has four square slots symmetrically arranged in a rectangular array on the bottom. Telescopic rods 9 are symmetrically connected to the opposite sides of the four square slots. Several through holes are arranged in a linear array on each of the four telescopic rods 9. Anti-slip pads 11 are glued to the end of each of the four telescopic rods 9 near the hinge 8. Limiting blocks 10 are installed on the through holes near the anti-slip pads 11.

[0024] like Figure 3 As shown, it also includes a battery 12 and a locator 13. Two rectangular slots are symmetrically opened on the side of the bottom of the two buffer blocks 7 that are close to each other. Two batteries 12 are symmetrically glued in the two rectangular slots. A locator 13 is glued to the side of the bottom of the two batteries 12 that are far from each other. The two strip lights 2 and the two locators 13 are electrically connected to the two batteries 12.

[0025] like Figure 1 , Figure 3 and Figure 4 As shown, it also includes a placement box 14, a sealing cover 15, a connecting block 16, and a hook 17. Four placement boxes 14 for placing weights are symmetrically installed on the side of the two support frames 1 that are close to each other, and are bolted on the side of the four placement boxes 14 that are far apart from each other. The sealing cover 15 is rotatably connected to the side of the four placement boxes 14 that are far apart from each other. Four placement slots are symmetrically opened on the bottom side of the two buffer blocks 7 that are far apart from each other. The connecting block 16 is glued to the side of the four placement slots that are far apart from each other. The hook 17 is rotatably connected to the side of the four connecting blocks 16 that is close to the hinge 8, and the hook 17 can be stored in the placement slot.

[0026] When using this device to park a drone for takeoff, the operator must first pull handle 5 to rotate around hinge 8 to the side away from each other and open it. At this time, the two buffer blocks 7 form a platform structure. Then, the operator must pull the four telescopic rods 9 to rotate away from hinge 8 to form a four-legged support structure. When the ground where this device is placed is uneven, the limit block 10 can be pulled out and the telescopic rods 9 adjusted. After the telescopic rods 9 are adjusted to make the platform structure level, the limit block 10 is inserted into the through hole on the telescopic rod 9 to lock it. When the wind is too strong at the location of this device, the sealing cover 15 can be opened, the weights can be taken out from the placement box 14, and all the hooks 17 can be rotated to a horizontal and vertical state. Then, the weights are hung on the hooks 17 to add weight and prevent them from being blown over by the wind. When the drone needs to land on the platform structure, sunlight can be reflected to the drone through the reflective sticker 4 so that the drone can confirm the position of the platform structure. When the drone lands, the two locators 13 can provide the drone with position information so that the drone can land accurately on the platform structure.

[0027] like Figure 6 and Figure 7 As shown, it also includes solar panels 18, slide rails 19, and stops 20. There are two solar panels 18 arranged symmetrically on the left and right sides. Two slide rails 19 are symmetrically installed on the front and rear sides of the two solar panels 18 by bolts. Stops 20 are welded to the ends of the four slide rails 19 that are close to each other. The two solar panels 18 are slidably connected to the middle of the two buffer blocks 7 on the opposite sides. The two solar panels 18 are electrically connected to the two batteries 12.

[0028] like Figure 3 As shown, it also includes magnets 21. Magnets 21 are symmetrically embedded in the bottom of the two buffer blocks 7 on opposite sides and glued together.

[0029] When the device's power supply is insufficient and the weather is sunny, the operator needs to pull the two solar panels 18 to the side furthest apart. When the stop block 20 contacts the support frame 1, the two solar panels 18 are unfolded. At this time, the solar panels 18 convert the collected solar energy into electrical energy and store it in the battery 12. When the device is in a rainy area, the waterproof membrane 3 can effectively protect the circuit components to prevent water ingress and leakage. When the device is at night, the operator can turn on the strip light 2, which will flash to illuminate the drone in the dark. The instructions are as follows: When it is time to put away this device, the operator must first remove all weights from the hook 17 and put them back into the corresponding placement box 14. Then, rotate the hook 17 to the side closer to the hinge 8 to reset it. Next, remove all the limit blocks 10 in sequence, then retract the telescopic rod 9. Then, rotate all the telescopic rods 9 to the side closer to the hinge 8 and reset them. At this time, the operator needs to pull the two handles 5 to the side closer to each other to retract them. When the two handles 5 are close together, the four magnets 21 can attract the two handles 5 tightly, making it convenient for the operator to lift and take away.

Claims

1. A portable drone landing pad, characterized by: The system includes a support frame (1), strip lights (2), waterproof membrane (3), reflective stickers (4), handles (5), protrusions (6), buffer blocks (7), hinges (8), telescopic rods (9), limiting blocks (10), and anti-slip pads (11). A buffer block (7) is fixedly connected to the inner side of the support frame (1). There are two symmetrically arranged support frames (1) and buffer blocks (7). The two buffer blocks (7) are symmetrically connected by hinges (8), which are installed symmetrically on the bottom sides of the two buffer blocks (7). A waterproof membrane (3) is fixedly connected to the top of each buffer block (7). Strip lights (2) are fixedly connected between each of the two waterproof membranes (3) and the adjacent support frame (1). The top side is symmetrically fixed with multiple reflective stickers (4), and the two support frames (1) are fixedly fixed with handles (5) on one side. The bottom of the left handle (5) is fixedly fixed with multiple protrusions (6) in a straight array. The bottom of the right handle (5) is provided with multiple grooves that can be locked by the protrusions (6). The bottom of the buffer block (7) is provided with multiple square slots in a rectangular array. The inside of all the square slots is symmetrically rotatably connected with telescopic rods (9) on one side. All the telescopic rods (9) are provided with several through holes arranged in a straight array. All the telescopic rods (9) are fixedly connected with anti-slip pads (11) on the side near the hinge (8). Limiting blocks (10) are installed on the through holes near the anti-slip pads (11).

2. The portable drone landing pad as described in claim 1, characterized in that: It also includes a battery (12) and a locator (13). Multiple rectangular slots are symmetrically opened on one side of the bottom of the two buffer blocks (7). Multiple batteries (12) are symmetrically fixedly connected in all rectangular slots. A locator (13) is fixedly connected on one side of the bottom of all batteries (12). The two strip lights (2) and all the locators (13) are electrically connected to the battery (12).

3. The portable drone landing pad as described in claim 2, characterized in that: It also includes a placement box (14), a sealing cover (15), a connecting block (16) and a hook (17). Multiple placement boxes (14) for placing weights are symmetrically fixedly connected on the side of the two support frames (1) that are close to each other. A sealing cover (15) is rotatably connected on the side of all placement boxes (14) that are far apart from each other. Multiple placement slots are symmetrically opened on the bottom side of the two buffer blocks (7) that are far apart from each other. A connecting block (16) is fixedly connected on one side inside all placement slots. A hook (17) is rotatably connected on the side of all connecting blocks (16) that is close to the hinge (8). All hooks (17) can be stored in the placement slot.

4. A portable drone landing pad as described in claim 3, characterized in that: It also includes solar panels (18), slide rails (19) and stops (20). Multiple solar panels (18) are symmetrically arranged on the left and right sides. Multiple slide rails (19) are symmetrically fixedly connected to both sides of all solar panels (18). Stops (20) are fixedly connected to the ends of all slide rails (19) that are close to each other. All solar panels (18) are slidably connected to the middle of two buffer blocks (7) on the side that are far apart from each other. All solar panels (18) are electrically connected to all batteries (12).

5. A portable drone landing pad as described in claim 4, characterized in that: It also includes magnets (21), and magnets (21) are symmetrically embedded and fixedly connected to one side of the bottom of the two buffer blocks (7).

6. A portable drone landing pad as described in claim 5, characterized in that: The buffer block (7) is made of rubber.

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