Portable unmanned aerial vehicle take-off and landing guiding platform

By designing a retractable support rod structure, the problem of the large size and inconvenience of carrying the drone take-off and landing platform was solved, realizing the portability and rapid deployment of the take-off and landing platform.

CN223721196UActive Publication Date: 2025-12-26THE 54TH RESEARCH INSTITUTE OF CHINA ELECTRONICS TECHNOLOGY GROUP CORPORATION
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Patent Information

Application Number
CN202520374575.3
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

Technical Problem

Existing drone take-off and landing platforms are irregularly shaped due to their legs, occupy a large volume, and are inconvenient for users to carry around.

Method used

A portable UAV-guided take-off and landing platform was designed, which adopts a retractable support rod structure. The support rod can be retracted and extended through limiting components and spring mechanism. With the cooperation of sleeve and locking hole, the support rod can slide in the sleeve and achieve rapid deployment and retraction through the restoring deformation of the spring.

Benefits of technology

The take-off and landing platform is compact and portable when not in use, and can be quickly deployed and easy to operate, thus meeting the portability requirements.

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Abstract

The utility model belongs to the field of unmanned aerial vehicles, and particularly relates to a portable unmanned aerial vehicle guide take-off and landing platform which comprises a take-off and landing platform body, storage grooves which are evenly distributed are formed in the bottom of the take-off and landing platform body, sleeves are hinged to the interiors of the storage grooves, and supporting rods are slidably connected to the interiors of the sleeves. Two clamping holes which are distributed up and down are formed in one side of the sleeve; after the device is used, the clamping rod is pressed out of the interior of the clamping hole close to the lower position, then the first spring is compressed, the supporting rod is not limited, the supporting rod can move in the sleeve, the supporting rod can be retracted into the sleeve, and when the clamping rod meets the clamping hole close to the upper position, the clamping rod can be clamped in the clamping hole close to the lower position. And under the action of deformation recovery of a first spring, a clamping rod is pushed to be clamped for limiting, and then a sleeve is rotated, so that the sleeve can be retracted into a storage groove, the size of the device is just as large as that of the lifting platform body at the moment, and the device is very convenient to carry.
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Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned plane field, concretely is a portable unmanned plane guiding take -off and landing platform. BACKGROUND

[0002] Unmanned aircraft is called "unmanned plane" for short, and the English abbreviation is "UAV", which is a no -person aircraft controlled by radio remote control equipment and self -provided program control device, or by on -board computer completely or intermittently autonomously, when the unmanned plane takes off, because the outdoor condition is poor, so the take -off and landing platform is configured to take off and land.

[0003] In the actual use of the personnel in the field, the existing take -off and landing platform is not convenient to carry because the take -off and landing platform has supporting legs, the shape is irregular and occupies a large volume, so that the user can not carry it, which affects the use of the user, therefore, aiming at the above -mentioned problem, a portable unmanned plane guiding take -off and landing platform is provided. UTILITY MODEL CONTENT

[0004] In order to make up for the deficiency of the prior art, the problem that the existing take -off and landing platform is not convenient to carry because the take -off and landing platform has supporting legs, the shape is irregular and occupies a large volume, so that the user can not carry it, which affects the use of the user, is solved, and the utility model provides a portable unmanned plane guiding take -off and landing platform.

[0005] The utility model solves the technical scheme that the utility model discloses a portable unmanned plane guiding take -off and landing platform, including take -off and landing platform body, the bottom of take -off and landing platform body is set up and is received groove that is evenly distributed, the inside hinged of received groove has sleeve, the inside sliding connection of sleeve has support rod, the one side of sleeve is set up and is two card hole that is distributed above and below, the one side of support rod sets up limit component.

[0006] Preferably, the limit component includes a movable slot, a first spring, and a clamping rod. The movable slot is provided on one side of the support rod. The first spring is fixedly connected inside the movable slot. The clamping rod is movably connected inside the movable slot. The first spring is fixedly connected to the bottom of the clamping rod.

[0007] Preferably, a second spring is fixedly connected inside the sleeve. One side of the second spring is fixedly connected with a connecting plate. The connecting plate is fixedly connected with the support rod.

[0008] Preferably, an adjusting bolt is threadedly connected to the bottom of the support rod.

[0009] Preferably, a damping shaft is arranged outside the sleeve. The sleeve is hingedly connected with the receiving groove through the damping shaft.

[0010] Preferably, the inner part of the movable slot is communicated with a sliding groove, and the outer part of the clamping rod is fixedly connected with a sliding plate which is slidingly connected in the inner part of the sliding groove.

[0011] Preferably, the top of the clamping rod is fixedly connected with a soft pad made of rubber.

[0012] The utility model discloses the beneficial effect that:

[0013] 1. The utility model discloses after using, press clamping rod, and the clamping rod is pressed to the inside of the lower position card hole, then first spring is compressed at this time, and the support rod loses the restriction, and the support rod can move in the inside of the sleeve like this, and the support rod can be retracted in the inside of the sleeve like this, and when the clamping rod meets the upper position card hole, under the action of the first spring recovery deformation, push the clamping rod and enter the limit, then rotate the sleeve, and the sleeve can be retracted in the inside of the storage slot like this, and the device volume just has the landing platform body so big at this time, very convenient to carry.

[0014] 2. The utility model discloses through the setting of second spring, and the support rod is pushed back in the inside of the sleeve by the support of connecting plate when, and will compress second spring, and when the support rod is stretched, it is not necessary to be tired, when pressing the clamping rod, the support rod loses the restriction, and second spring restores deformation, and the support rod is pushed out through the connecting plate, and thus reaches the use quick effect. BRIEF DESCRIPTION OF DRAWINGS

[0015] In order to more clearly illustrate the technical scheme in the embodiments of the utility model or the prior art, the following will briefly introduce the drawings needed to be used in the embodiment or the prior art description, and obviously, the drawings in the following description are only some embodiments of the utility model, and for those skilled in the art, other drawings can also be obtained without paying creative labor under the premise.

[0016] Figure 1 It is the structure three -dimensional schematic view of the whole of the utility model;

[0017] Figure 2 It is another direction three -dimensional schematic view of the whole of the utility model structure;

[0018] Figure 3 It is the structure cross -sectional view schematic view of the sleeve of the utility model;

[0019] Figure 4 It is the structure cross -sectional view schematic view of the support rod of the utility model.

[0020] In the figure: 1, landing platform body; 2, storage groove; 3, sleeve; 4, support rod; 5, clamping hole; 6, limiting assembly; 601, movable slot; 602, first spring; 603, clamping rod; 7, second spring; 8, connecting plate; 9, adjusting bolt; 10, damping shaft; 11, sliding groove; 12, sliding plate. DETAILED DESCRIPTION

[0021] 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.

[0022] Please refer to Figures 1-4 As shown in the figure, a portable unmanned aerial vehicle guiding landing platform, including landing platform body 1, the bottom of landing platform body 1 is provided with storage groove 2 that is evenly distributed, the inside of storage groove 2 is hinged with sleeve 3, the inside of sleeve 3 is slidably connected with support rod 4, one side of sleeve 3 is provided with two clamping holes 5 that are distributed in upper and lower positions, one side of support rod 4 is provided with limiting assembly 6;

[0023] When working, landing platform body 1 is used for the take-off and landing of unmanned aerial vehicle, sleeve 3 and support rod 4 are matched with limiting assembly 6 and can be folded down, so that it is convenient to carry and use.

[0024] Further, limiting assembly 6 includes movable slot 601, first spring 602 and clamping rod 603, movable slot 601 is arranged on one side of support rod 4, first spring 602 is fixedly connected to the inside of movable slot 601, clamping rod 603 is movably connected to the inside of movable slot 601, and first spring 602 is fixedly connected to the bottom of clamping rod 603;

[0025] When working, after the device is used, clamping rod 603 is pressed, clamping rod 603 is pressed into the inside of clamping hole 5 in the lower position, then first spring 602 is compressed, and support rod 4 loses the limitation, so that support rod 4 can move in the inside of sleeve 3, so that support rod 4 can be retracted into the inside of sleeve 3, and when clamping rod 603 meets clamping hole 5 in the upper position, clamping rod 603 is clamped into the limit under the action of the deformation recovery of first spring 602, then sleeve 3 is rotated, so that sleeve 3 can be retracted into the inside of storage groove 2, then the volume of the device is only as large as landing platform body 1.

[0026] Further, second spring 7 is fixedly connected to the inside of sleeve 3, one side of second spring 7 is fixedly connected with connecting plate 8, and connecting plate 8 is fixedly connected with support rod 4;

[0027] When working, the second spring 7 is compressed when the supporting rod 4 is pushed back into the sleeve 3 and is supported by the connecting plate 8, so that the supporting rod 4 does not need to be forced when being extended, and the second spring 7 restores the deformation when the supporting rod 4 is no longer limited, so that the supporting rod 4 is pushed out by the connecting plate 8.

[0028] Further, the bottom of the supporting rod 4 is threadedly connected with an adjusting bolt 9.

[0029] When working, the height of the adjusting bolt 9 can be adjusted by rotating the adjusting bolt 9, so that the device can be balanced.

[0030] Further, the outside of the sleeve 3 is provided with a damping shaft 10, and the sleeve 3 is hingedly connected with the receiving groove 2 through the damping shaft 10.

[0031] When working, the sleeve 3 has resistance when rotating, and cannot be moved at will, through the damping shaft 10.

[0032] Further, the inside of the movable groove 601 is communicated with a sliding groove 11, and the outside of the clamping rod 603 is fixedly connected with a sliding plate 12 which is slidingly connected in the inside of the sliding groove 11.

[0033] When working, the sliding plate 12 which is slidingly connected in the sliding groove 11 makes the clamping rod 603 move more stably and prevents the clamping rod 603 from rotating.

[0034] Further, the top of the clamping rod 603 is fixedly connected with a soft pad, and the soft pad is made of rubber.

[0035] When working, the soft pad makes the clamping rod 603 more comfortable to press.

[0036] Working principle: after the device is used, the clamping rod 603 is pressed to be pressed into the inside of the lower clamping hole 5, so that the first spring 602 is compressed, and the supporting rod 4 is no longer limited, so that the supporting rod 4 can move in the inside of the sleeve 3, so that the supporting rod 4 can be retracted into the inside of the sleeve 3, and when the clamping rod 603 meets the upper clamping hole 5, the clamping rod 603 is clamped into the limiting position under the action of the restoring deformation of the first spring 602, and then the sleeve 3 is rotated, so that the sleeve 3 is retracted into the inside of the receiving groove 2, so that the device has a size only as large as the landing platform body 1, which is very convenient to carry, and the second spring 7 is compressed when the supporting rod 4 is pushed back into the inside of the sleeve 3 and is supported by the connecting plate 8, so that the supporting rod 4 does not need to be forced when being extended, and the second spring 7 restores the deformation when the supporting rod 4 is no longer limited, so that the supporting rod 4 is pushed out by the connecting plate 8, thereby achieving the effect of quick use.

[0037] The basic principle, main features and advantages of the present application are shown and described above. Those skilled in the art should understand that the present application is not limited by the above embodiments, and the above embodiments and descriptions in the specification are only to illustrate the principles of the present application. Without departing from the spirit and scope of the present application, various changes and improvements can be made to the present application, and these changes and improvements all fall within the scope of the claimed present application.

Claims

1. A portable drone guiding landing platform comprising a landing platform body (1), characterized in that: The bottom of the take-off and landing platform body (1) is provided with evenly distributed receiving grooves (2), the inside of the receiving groove (2) is hingedly connected with a sleeve (3), the inside of the sleeve (3) is slidably connected with a supporting rod (4), one side of the sleeve (3) is provided with two upper and lower clamping holes (5), and one side of the supporting rod (4) is provided with a limiting assembly (6).

2. The portable unmanned aerial vehicle guidance and recovery platform of claim 1, wherein: The limiting assembly (6) comprises a movable slot (601), a first spring (602) and a clamping rod (603), the movable slot (601) is formed on one side of the supporting rod (4), the first spring (602) is fixedly connected inside the movable slot (601), the clamping rod (603) is movably connected inside the movable slot (601), and the first spring (602) is fixedly connected to the bottom of the clamping rod (603).

3. The portable unmanned aerial vehicle guidance and recovery platform of claim 1, wherein: The inside of the sleeve (3) is fixedly connected with a second spring (7), one side of the second spring (7) is fixedly connected with a connecting plate (8), and the connecting plate (8) is fixedly connected with the supporting rod (4).

4. The portable unmanned aerial vehicle guidance and recovery platform of claim 1, wherein: The bottom of the supporting rod (4) is threadedly connected with an adjusting bolt (9).

5. The portable unmanned aerial vehicle guidance and recovery platform of claim 1, wherein: The outside of the sleeve (3) is provided with a damping shaft (10), and the sleeve (3) is hingedly connected with the receiving groove (2) through the damping shaft (10).

6. The portable unmanned aerial vehicle guidance and recovery platform of claim 2, wherein: The inside of the movable slot (601) is communicated with a sliding groove (11), and the outside of the clamping rod (603) is fixedly connected with a sliding plate (12) which is slidably connected inside the sliding groove (11).

7. The portable unmanned aerial vehicle guidance and recovery platform of claim 6, wherein: The top of the clamping rod (603) is fixedly connected with a soft pad, and the soft pad is made of rubber.