Device facilitating landing and transferring of unmanned aerial vehicle
By introducing damping shock absorbers and adjustable fixtures into the drone landing and transfer devices, the impact problems and specification adaptability problems during drone landing are solved, and more efficient drone fixing and protection are achieved.
Patent Information
- Application Number
- CN202421074947.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-05-16
- Publication Date
- 2024-12-17
- Estimated Expiration
- 2034-05-16
AI Technical Summary
The existing drone landing and transfer devices lack shock-absorbing structures, which makes the drone easily damaged when landing and is difficult to adapt to the fixation of a variety of drone landing gears of different specifications and shapes.
Designed a device including a base plate, tie rod, self-locking universal wheel, shock absorber platform and adjustable fixtures, using damping shock absorbers and elastic metal plates to reduce impact, and through adjustable slide rails and lock bolts Flexible fixation of drone landing gears of different specifications and shapes.
It effectively reduces impact damage of drones during landing, improves the fixing flexibility of drone landing gears of various specifications and shapes, and enhances the adaptability and stability of the device.
Smart Images

Figure CN222179901U_ABST
Abstract
Description
Technical Field
[0001] The present application relates to the field of drone landing and transportation, and more specifically, to a device for facilitating drone landing and transportation. Background Art
[0002] The drone landing and transfer device is used to provide a landing platform for the auxiliary plant protection drone and assist in transferring it to a short-distance transfer vehicle on a truck.
[0003] The device for landing and transferring the drone in the related technology usually includes a base plate and a pull rod pulled out from one side thereof, and universal wheels are installed at the bottom of the base plate and the pull rod. When the drone landing gear stops on the base plate, a fixing buckle for fixing the drone landing gear is usually provided at a designated position on the base plate. When the drone needs to be transferred to the back seat of a truck, the pull rod is pulled out from the base plate, and one end of the pull rod is lifted up with the universal wheel at the bottom of the base plate as a fulcrum, so that the universal wheel at its bottom is limited and blocked by a preset baffle on the rear end of the truck's back seat, and then the side of the base plate away from the pull rod is lifted up to transfer the heavier drone to the back seat of the truck with ease.
[0004] However, in the process of implementing the technical solutions in the embodiments of the present application, the inventors of the present application found that the above technology has at least the following technical problems:
[0005] (1) In the above solution, the drone landing gear directly lands on the bottom plate, and the bottom plate lacks a shock-absorbing structure, which will cause the drone to have a large impact with the landing site when landing, which may easily cause damage to the drone;
[0006] (2) In the above scheme, the UAV landing gear is fixed by a fixed buckle, and the position of the fixed buckle is fixed. Figure 6-Figure 8 There are many different specifications and shapes of UAV landing racks, but the above solution is difficult to adapt to the shape to complete the fixation. Utility Model Content
[0007] In order to make up for the above shortcomings, the present application provides a device that facilitates the landing and transportation of drones, which helps to reduce the damage caused to the drone itself during landing of the drone landing gear, thereby indirectly protecting the drone; at the same time, it facilitates the adaptive fixation of drone landing gear of various different specifications and shapes.
[0008] The present application provides a device for facilitating the landing and transportation of a drone, comprising a bottom plate and a pull rod connected thereto, wherein the bottom ends of the bottom plate and the pull rod are both provided with self-locking universal wheels, and further comprising a shock absorbing platform and a drone mounting component:
[0009] The shock absorbing platform comprises a damping shock absorber arranged on the top surface of the bottom plate and a landing platform arranged on the damping shock absorber;
[0010] The drone installation component includes slide rails arranged on both sides of the landing platform, and the two slide rails are commonly and adjustably fixed with fixing parts, and the fixing parts are used to install and fix drone landing racks of various specifications and shapes.
[0011] Preferably, pull-out cavities are provided on both sides of one side of the base plate, the pull rod is pull-connected to the two pull-out cavities, locking bolts A are connected to both sides of the base plate, and screw holes matching the locking bolts A are provided in pairs on both sides of the pull rod.
[0012] Preferably, through holes matching the locking bolts A are provided on both side edges of the bottom plate.
[0013] Preferably, four damping shock absorbers are provided, and are respectively connected to four corners of the top of the base plate, and the tops are respectively fixed to the bottom end surfaces of the landing platform.
[0014] Preferably, there are two fixing parts, each comprising an elastic metal plate for clamping the UAV landing gear, slideways are provided on both sides of the elastic metal plate, locking bolts B are provided in the slideways, and the locking bolts B can pass through the slide rails and are screwed with locking nuts that are clamped on the bottom end surface of the slide rails.
[0015] Beneficial effect: The present application provides a device for convenient landing and transportation of drones. The landing platform and the damping shock absorber are used to cooperate with each other to reduce the probability of a large impact between the drone and the landing site when the landing gear of the drone lands on it; after landing, the adjustable fixing parts are used to facilitate the transfer of the drone. Figure 6-Figure 8 The UAV landing racks of various specifications and shapes shown are fixed, and the fixing flexibility is relatively improved. BRIEF DESCRIPTION OF THE DRAWINGS
[0016] In order to more clearly illustrate the technical solutions of the implementation methods of the present application, the drawings required for use in the implementation methods will be briefly introduced below. It should be understood that the following drawings only show certain embodiments of the present application and therefore should not be regarded as limiting the scope. For ordinary technicians in this field, other related drawings can be obtained based on these drawings without paying creative work.
[0017] Figure 1 Schematic diagram of the structure state after the device is retracted to facilitate the landing and transportation of the drone;
[0018] Figure 2 Schematic diagram of the structural state of the device after it is deployed to facilitate the landing and transportation of drones;
[0019] Figure 3 A structural diagram showing the connection relationship between the landing platform and the fixing member, view 1;
[0020] Figure 4 A second perspective diagram of the structural diagram of the connection relationship between the landing platform and the fixing member;
[0021] Figure 5 is a schematic diagram of the structure of the base plate;
[0022] Figure 6 A schematic diagram of the structure of the drone landing rack after the first shape is installed on the device to facilitate the landing and transportation of the drone;
[0023] Figure 7 A schematic diagram of the structure of the drone landing rack after the second shape is installed on the device to facilitate the landing and transportation of the drone;
[0024] Figure 8 Schematic diagram of the structure of the drone landing rack after the third shape is installed to facilitate the landing and transportation of the drone.
[0025] In the figure: 1-bottom plate; 11-pull-out cavity; 12-through hole; 2-pull rod; 21-screw hole; 3-self-locking universal wheel; 4-shock absorbing platform; 41-landing platform; 42-damping shock absorber; 5-UAV mounting component; 51-slide rail; 52-fixing piece; 521-elastic metal plate; 5211-slideway; 522-locking bolt B; 523-locking nut; 6-locking bolt A. DETAILED DESCRIPTION
[0026] The technical solutions in the embodiments of the present application will be clearly and completely described below in conjunction with the drawings in the embodiments of the present application. Obviously, the described embodiments are only part of the embodiments of the present application, rather than all of the embodiments.
[0027] See also Figure 1-Figure 2 , Figure 6-Figure 8 As shown, the present application provides a device for facilitating the landing and transportation of a drone, comprising a base plate 1 and a pull rod 2 connected thereto by pulling and pulling, the bottom ends of the base plate 1 and the pull rod 2 are both provided with self-locking universal wheels 3, and also comprising a shock absorbing platform 4 and a drone mounting component 5:
[0028] The shock absorbing platform 4 includes a damping shock absorber 42 disposed on the top surface of the bottom plate 1 and a landing platform 41 disposed on the damping shock absorber 42;
[0029] The drone mounting component 5 includes slide rails 51 disposed on both sides of the landing platform 41 . The two slide rails 51 are commonly and adjustably fixed with a fixing member 52 , and the fixing member 52 is used to install and fix drone landing gears of various specifications and shapes.
[0030] In this embodiment, the landing platform 41 and the damping shock absorber 42 are used to cooperate with each other to reduce the probability of a large impact between the drone and the landing site when the landing gear of the drone lands on it; after landing, the adjustable fixing member 52 is used to facilitate the Figure 6-Figure 8 The UAV landing racks of various specifications and shapes shown are fixed, and the fixing flexibility is relatively improved.
[0031] See also Figure 1-Figure 2 , Figure 5 As shown, both sides of one side of the bottom plate 1 are provided with a pull-out cavity 11, the pull rod 2 is connected to the two pull-out cavities 11 by pulling, both sides of the bottom plate 1 are connected with locking bolts A6, and both sides of the pull rod 2 are provided with pairs of screw holes 21 adapted to the locking bolts A6. Specifically, by using the cooperation between the locking bolts A6 on each side and the two screw holes 21 corresponding thereto, the pull rod 2 can be fixed after being pulled out and retracted from the bottom plate 1.
[0032] Through holes 12 adapted to the locking bolts A6 are provided on both sides of the bottom plate 1. Specifically, the locking bolts A6 and the through holes 12 cooperate to facilitate the locking bolts A6 to extend into the drawer cavity 11 and be tightened and fixed with the screw holes 21, indirectly assisting the fixing of the locking bolts A6 and the pull rod 2.
[0033] See also Figure 1 As shown, there are four damping shock absorbers 42, which are respectively connected to the four corners of the top of the bottom plate 1, and the tops are respectively fixed to the bottom end surface of the landing platform 41. Specifically, when the landing gear of the drone lands on the landing platform 41, the design of the damping spring shock absorber 42 can play a buffering role, reducing the possibility of a large impact between the drone and the landing site when landing.
[0034] See also Figure 1-Figure 4 As shown, there are two fixing members 52, each of which includes an elastic metal plate 521 for pressing the landing gear of the UAV, and slideways 5211 are provided on both sides of the elastic metal plate 521. Locking bolts B522 are provided in the slideways 5211. The locking bolts B522 can pass through the slide rails 51 and are screwed with locking nuts 523 pressed against the bottom end surfaces of the slide rails 51. Specifically, the elastic metal plate 521 is conveniently fixed to the two slide rails 51 by the cooperation of the locking bolts B522 and the locking nuts 523, and the sliding cooperation of the locking bolts B522 and the slide rails 51 and the slideway 5211 is convenient for adaptive fixing to adapt to the position of the landing gear of the UAV, which is more practical.
[0035] It should also be noted that a non-slip rubber pad (not shown) is adhered to the lower surface of the head of the locking bolt B522 and is tightly attached to the upper surface of the elastic metal plate 521, thereby reducing the probability of the elastic metal plate 521 slipping after the locking bolt B522 is fixed, and indirectly increasing the stability of the fixed installation of the drone.
[0036] When using this application:
[0037] The external remote controller will control the drone to land on the upper surface of the landing platform 41. The landing platform 41 and the damping shock absorber 42 are used to reduce the probability of a large impact between the drone and the landing site when the landing gear of the drone lands on it. After landing, the adjustable fixing member 52 is used to facilitate the Figure 6-Figure 8 The UAV landing gear of various different specifications and shapes shown in the figure can be fixed, and the fixing flexibility is relatively improved. Specifically, according to the shape specifications of the UAV landing gear, when the two elastic metal plates 521 are pressed on both sides of the bottom of the UAV landing gear, the elastic metal plates 521 can be easily fixed to the two slide rails 51 by using the locking bolts B522 and the locking nuts 523, so that the UAV landing gear can be easily fixed.
[0038] It is obvious to those skilled in the art that the present application is not limited to the details of the exemplary embodiments described above, and that the present application can be implemented in other specific forms without departing from the spirit or essential features of the present application. Therefore, the embodiments should be regarded as exemplary and non-limiting in all respects, and the scope of the present application is defined by the appended claims rather than the above description, and it is intended that all changes falling within the meaning and scope of the equivalent elements of the claims be included in the present application. Any reference numeral in a claim should not be regarded as limiting the claim to which it relates.
Claims
1. A device for facilitating the landing and transportation of a drone, comprising a base plate (1) and a pull rod (2) connected thereto by pulling and pulling, wherein the bottom ends of the base plate (1) and the pull rod (2) are both provided with self-locking universal wheels (3), characterized in that: Also includes: A shock absorbing platform (4), comprising a damping shock absorber (42) arranged on the top surface of the bottom plate (1) and a landing platform (41) arranged on the damping shock absorber (42); The drone mounting component (5) comprises slide rails (51) arranged on both sides of the landing platform (41), the two slide rails (51) being commonly and adjustably fixed with a fixing member (52), and the fixing member (52) is used to install and fix drone landing gears of various specifications and shapes.
2. The device for facilitating the landing and transportation of a drone according to claim 1 is characterized in that: Both sides of one side of the base plate (1) are provided with pull-out cavities (11), the pull rod (2) is pull-connected to the two pull-out cavities (11), both sides of the base plate (1) are connected with locking bolts A (6), and both sides of the pull rod (2) are provided with pairs of screw holes (21) that are compatible with the locking bolts A (6).
3. The device for facilitating the landing and transportation of a drone according to claim 2 is characterized in that: Through holes (12) adapted to the locking bolts A (6) are provided on both sides of the bottom plate (1).
4. The device for facilitating the landing and transportation of a drone according to claim 1, characterized in that: The damping shock absorbers (42) are provided in four parts and are respectively connected to the four corners of the top of the bottom plate (1), and the tops are respectively fixed to the bottom end surfaces of the landing platform (41).
5. The device for facilitating the landing and transportation of a drone according to claim 1, characterized in that: There are two fixing members (52), each comprising an elastic metal plate (521) for pressing the landing gear of the UAV, slideways (5211) are provided on both sides of the elastic metal plate (521), and locking bolts B (522) are provided in the slideways (5211). The locking bolts B (522) can pass through the slide rail (51) and are screwed with locking nuts (523) pressed against the bottom end surface of the slide rail (51).
