Take-off and landing foot support suitable for surveying and mapping of unmanned aerial vehicle on rugged road section
By combining the design of limit blocks, clamping mechanisms and telescopic mechanisms, the stability problem of drone footplates on rough terrain is solved, enabling drones to take off and land smoothly and safely on rough terrain.
Patent Information
- Application Number
- CN202520206408.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-02-10
- Publication Date
- 2026-02-27
- Estimated Expiration
- 2035-02-10
AI Technical Summary
Existing drone footplate designs are cumbersome and have low adaptability, making it difficult to maintain stability on uneven ground and increasing the risks during takeoff and landing.
A landing foot bracket including a limiting mechanism, a clamping mechanism, and a telescopic mechanism was designed. The combination of limiting blocks and arc-shaped feet ensures the stability of the drone on rough roads. Rubber sheets and rubber rings are used to increase friction and anti-slip effect, and the telescopic mechanism is adapted to different drone models.
It enables drones to take off and land smoothly on rough terrain, reducing tilting and swaying, enhancing the stability and safety of takeoff and landing, and has strong adaptability.
Smart Images

Figure CN223949400U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to unmanned aerial vehicle foot support technical field, concretely is a kind of take-off and landing foot support suitable for unmanned aerial vehicle surveying and mapping in rugged section. BACKGROUND
[0002] With the continuous progress of unmanned aerial vehicle technology, its surveying and mapping application in rugged terrain is more and more concerned, and unmanned aerial vehicle shows excellent flexibility and efficiency in the fields of environmental monitoring, topographic mapping, post-disaster assessment and the like. However, the take-off and landing operation in rugged section faces a series of challenges, especially for the design and application of unmanned aerial vehicle foot support.
[0003] The existing unmanned aerial vehicle foot support is generally accompanied by cumbersome design, low degree of adaptation, and difficult to maintain stability on uneven ground, which may cause the unmanned aerial vehicle to tilt during take-off or landing, increasing the risk of accidents. UTILITY MODEL CONTENT
[0004] In view of the deficiencies of the prior art, the utility model provides a take-off and landing foot support suitable for unmanned aerial vehicle surveying and mapping in rugged section, which solves the problems of cumbersome design, low degree of adaptation and difficulty in maintaining stability on uneven ground of unmanned aerial vehicle foot support.
[0005] To achieve the above purpose, the utility model provides the following technical scheme: a take-off and landing foot support suitable for unmanned aerial vehicle surveying and mapping in rugged section, comprising an unmanned aerial vehicle body, two unmanned aerial vehicle body foot supports are fixedly installed at the bottom of the unmanned aerial vehicle body, a limiting mechanism is fixedly installed at the bottom of each of the two unmanned aerial vehicle body foot supports, a pressing mechanism is fixedly installed at the top of each of the two limiting mechanisms, an extension mechanism is fixedly connected to the side of each of the two limiting mechanisms, two supporting legs are fixedly installed at the bottom of each of the two limiting mechanisms, and an arc-shaped foot support is connected to the bottom of each of the four supporting legs.
[0006] Preferably, side holes are formed in the side surfaces of the two limiting mechanisms, and top holes are formed in the top surfaces of the two limiting mechanisms, and the limiting mechanisms are made of carbon steel.
[0007] Preferably, a wave-shaped limiting block is arranged on the other side of each of the two limiting mechanisms, and a rubber sheet is attached to the limiting block to limit the vertical movement of the unmanned aerial vehicle body support.
[0008] Preferably, each of the two pressing mechanisms comprises a pressing bolt, a pressing piece is fixedly installed at the bottom of the pressing bolt, the limiting bolt passes through the top hole of the limiting mechanism, and the limiting bolt will not fall off.
[0009] Preferably, a nut and a rubber ring are sleeved on the pressing bolt, and the nut and the rubber ring are concentrically matched between the pressing bolt and the limiting mechanism.
[0010] Preferably, the limiting mechanism bottom is fixedly connected with two support legs, and the bottom of each support leg is fixedly connected with an arc-shaped foot support.
[0011] Preferably, the two limiting mechanisms are connected with a telescopic mechanism in the middle, and the telescopic mechanism is formed by two second connecting rods and a first connecting rod concentrically and superimposedly matched.
[0012] The utility model provides a kind of landing foot support suitable for unmanned aerial vehicle surveying and mapping in rugged section, compared with prior art, it has the following beneficial effects:
[0013] 1、the unmanned aerial vehicle landing foot support, by the compression bolt downward movement, so that unmanned aerial vehicle body foot support is fixed between gasket and arc-shaped slot, and reach fixed effect by lock nut, rubber ring and rubber sheet make fixed more firmly, telescopic mechanism is realized by the contact between internal thread and external thread to expand the type of foot support, operation is simple, reaches the effect of adaptation different model unmanned aerial vehicle.
[0014] 2、the unmanned aerial vehicle landing foot support, by a pair of support leg below connecting two arc-shaped foot supports with 40 °, guarantee unmanned aerial vehicle when taking off on rugged road surface, make unmanned aerial vehicle can normally take off and not by unequal unmanned aerial vehicle blade output caused by inclination, simultaneously make unmanned aerial vehicle when landing even if it shakes, can be by the same frequency shaking of two ends symmetrical arc-shaped foot support to offset shaking, make last successful landing, arc-shaped foot support below has rubber gasket, increase landing contact area, make line contact become surface contact, and play the effect of shock absorption and buffering. BRIEF DESCRIPTION OF DRAWINGS
[0015] Figure 1 It is the whole structure schematic diagram of the utility model;
[0016] Figure 2 It is the front view structure schematic diagram of the utility model;
[0017] Figure 3 It is the foot support structure schematic diagram of the utility model;
[0018] Figure 4 It is the foot support front view structure schematic diagram of the utility model;
[0019] Figure 5 It is the split schematic diagram of telescopic mechanism of the utility model;
[0020] Figure 6 It is the telescopic mechanism connection schematic diagram of the utility model.
[0021] In the figure: 1, unmanned aerial vehicle body; 2, unmanned aerial vehicle body foot support; 3, limiting mechanism; 301, limiting block; 302, side hole; 303, arc-shaped clamping groove; 304, support leg; 305, rubber sheet; 4, compression mechanism; 401, compression bolt; 402, nut; 403, rubber ring; 404, pressing piece; 5, arc-shaped foot support; 501, rubber gasket; 6, telescopic mechanism; 601, first connecting rod; 602, second connecting rod; 603, internal thread; 604, external thread. DETAILED DESCRIPTION
[0022] The technical solutions in the embodiments of the utility model will be clearly and completely described below with reference to the drawings in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, rather than all the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by those skilled in the art without creative labor fall within the scope of protection of the utility model.
[0023] Please refer to Figures 1-6 The utility model provides a technical scheme:
[0024] As shown in Figure 1 , 2 , a take-off and landing foot support suitable for unmanned aerial vehicle surveying and mapping in rugged road sections, comprising unmanned aerial vehicle body 1, characterized in that the bottom of unmanned aerial vehicle body 1 is fixedly installed with two unmanned aerial vehicle body foot supports 2, the bottom of each of the two unmanned aerial vehicle body foot supports 2 is fixedly installed with a limiting mechanism 3, the top of each of the two limiting mechanisms 3 is provided with a compression mechanism 4, the side of each of the two limiting mechanisms 3 is fixedly connected with a telescopic mechanism 6, and the bottom of each of the two limiting mechanisms 3 is fixedly connected with two arc-shaped foot supports 5.
[0025] Specifically, as shown in Figure 3 , the limiting mechanism 3 comprises a limiting block 301, when the unmanned aerial vehicle body foot support 2 is placed into the limiting mechanism 3 and fixed, the limiting block 301 can effectively prevent the unmanned aerial vehicle body foot support 2 from being fixed unstably on the side and causing problems such as falling off, the limiting block 301 is additionally provided with a rubber sheet 305, the rubber sheet 305 is arranged in a wave-shaped arc, thereby increasing the friction between the unmanned aerial vehicle body foot support 2 and the limiting block 301 and reducing the damage caused by the unmanned aerial vehicle body foot support 2 to the inner wall, the limiting mechanism 3 is additionally provided with a side hole 302 on the side, thereby facilitating the installation and adjustment of the entire limiting mechanism, and the bottom end of the limiting mechanism 3 is fixedly connected with two support legs 304.
[0026] Specifically, as shown in Figure 1 , 3As shown, the bottom of each support leg 304 is fixedly connected with an arc-shaped foot 5, and the connecting point of the support leg 304 and the arc-shaped foot 5 is located at the middle of the length direction of the arc-shaped foot 5. This design can ensure uniform weight distribution and enhance the stability of the support on rugged ground. The opening angle between each pair of arc-shaped feet 5 is 40°, which effectively reduces the shaking of the UAV body during take-off and landing. The bottom of the arc-shaped foot 5 is attached with a rubber pad 501, which increases the contact area during take-off and landing, changes the linear contact to surface contact, and has a damping effect.
[0027] As shown in Figure 4 , the pressing mechanism 4 includes a pressing bolt 401, the bottom of which is fixedly installed with a pressing plate 404. The surface of the pressing plate 404 can be bonded with a layer of foam adhesive and has a hemispherical structure, which helps to increase the contact area with the UAV body foot 2 and is beneficial for fixation. A nut 402 is sleeved on the pressing bolt 401, and the bottom of the nut 402 has a rubber ring 403. The rubber ring 403 and the nut 402 are concentrically fitted on the pressing bolt 401. By tightening the nut 402, the UAV body foot 2 is successfully fixed on the arc-shaped slot 303. At the same time, the rubber ring 403 can increase the friction between the nut and the upper plate of the limiting mechanism 3, which can effectively improve the anti-skid effect.
[0028] As shown in Figure 2 , 5 , 6, the telescopic mechanism 6 is composed of two second connecting rods 602 with a length of 100 mm and a first connecting rod 601 with a length of 120 mm in the middle. A section of the first connecting rod 601 is internally threaded 603, and the second connecting rod 602 is externally threaded 604.
[0029] Specifically, the first connecting rod 601 has a smooth section inside. When the external thread 604 of the second connecting rod 602 partially overlaps with the smooth section inside the first connecting rod 601, the telescopic mechanism 6 can be telescoped. When the external thread 604 contacts the internal thread 603, the telescopic mechanism 6 is fixed, thereby realizing the telescopic adjustment of the device. The adjustment range is 140 mm-320 mm, which makes the device suitable for multiple models of UAVs.
[0030] Working principle: in use, first according to the model of unmanned aerial vehicle body 1 determine the spacing between the unmanned aerial vehicle body support 2, adjust telescopic mechanism 6, the distance between the two ends of the symmetrical limiting mechanism 3 is slightly larger than the spacing between the unmanned aerial vehicle body support 2, two ends of the unmanned aerial vehicle body support 2 are assembled in the limiting mechanism 3, fixed by tightening the nut 402 on the pressing mechanism 4, and fixed more firmly by the rubber sheet 305 and the rubber ring 403, when the unmanned aerial vehicle is landing on the rugged road, the opening angle between each pair of the arc-shaped support 5 is 40°, effectively reducing the problem of body shaking when the unmanned aerial vehicle takes off and lands, and the symmetrical arrangement of the four arc-shaped supports 5 can effectively ensure the stability of the unmanned aerial vehicle, and the arc-shaped support 5 is provided with a rubber pad 501 below, which increases the contact area of landing and plays a damping and buffering effect.
[0031] Although the embodiments of the utility model have been shown and described, it can be understood by those skilled in the art that various changes, modifications, replacements and variations can be made to these embodiments without departing from the principles and spirits of the utility model, and the scope of the utility model is defined by the appended claims and their equivalents.
Claims
1. A take-off and landing foot support suitable for use with an unmanned aerial vehicle for surveying rough terrain, comprising a body (1) of the unmanned aerial vehicle, characterised in that The bottom of the unmanned aerial vehicle body (1) is fixedly provided with two unmanned aerial vehicle body supports (2), the bottom of each of the two unmanned aerial vehicle body supports (2) is fixedly provided with a limiting mechanism (3), the top of each of the two limiting mechanisms (3) is provided with a pressing mechanism (4), the side of each of the two limiting mechanisms (3) is fixedly connected with an extension mechanism (6), and the bottom of each of the two limiting mechanisms (3) is fixedly connected with two arc-shaped supports (5).
2. The take-off and landing foot support for rugged terrain mapping by a drone according to claim 1, wherein: The two limiting mechanisms (3) comprise a limiting block (301), the limiting block (301) is attached with a rubber sheet (305), the side of the limiting mechanism (3) is provided with a side hole (302), the middle of the limiting mechanism (3) is provided with an arc-shaped clamping groove (303), the bottom of the limiting mechanism (3) is fixedly connected with two supporting legs (304), and the limiting mechanism (3) is made of carbon steel.
3. The take-off and landing foot support for use in mapping rough terrain by a drone according to claim 1, characterized in that: The two pressing mechanisms (4) comprise a pressing bolt (401), the bottom of the pressing bolt (401) is fixedly provided with a pressing sheet (404), the pressing bolt (401) is sleeved with a nut (402), the bottom of the nut (402) is provided with a rubber ring (403), and the rubber ring (403) and the nut (402) are concentrically arranged on the pressing bolt (401).
4. The take-off and landing foot support for use in mapping rough terrain with a drone according to claim 1, characterized in that: The bottom surface of the four arc-shaped supports (5) is attached with rubber pads (501), and the supporting legs (304) and the arc-shaped supports (5) are fixedly connected at the middle positions of the arc-shaped supports in the length direction of the arc-shaped supports.
5. The take-off and landing foot support for use in mapping rough terrain with a drone according to claim 1, characterized in that: The extension mechanism (6) is composed of two second connecting rods (602) and a first connecting rod (601) in the middle, one section of the inside of the first connecting rod (601) is provided with an internal thread (603), and the outside of the second connecting rod (602) is provided with an external thread (604).