Safe take-off and landing equipment for flight of unmanned aerial vehicle

Abstract

The utility model belongs to the technical field of unmanned aerial vehicles, and particularly relates to unmanned aerial vehicle flight safety take-off and landing equipment which comprises a box body and a storage assembly arranged on the outer side of the end of the box body. The storage assembly comprises motors, a mounting plate and a first rotating arm, and the two motors are mounted on the outer side of one end of the box body; the cover plate of the storage assembly extends outwards and is unfolded, so that a more stable and wider take-off space can be provided for the unmanned aerial vehicle, particularly on an uneven or soft surface, bumping or rollover during take-off can be prevented, meanwhile, the box body can serve as a buffer area, impact force during landing of the unmanned aerial vehicle is absorbed, the damage risk is reduced, and the service life of the unmanned aerial vehicle is prolonged. And a stable landing platform is provided.

Description

Technical Field

[0001] The utility model belongs to the technical field of unmanned aerial vehicles (UAVs), and in particular relates to a UAV flight safety take-off and landing device. Background Art

[0002] A surveying and mapping drone is a type of drone equipment specifically used for collecting geographic information. It combines aerial photography, remote sensing technology, and drone technology, and can capture detailed images of the earth's surface at high altitudes, thereby generating high-precision geographic information data. Surveying and mapping drones have high-precision terrain reconstruction and three-dimensional modeling capabilities, and can meet the precise measurement needs of land area, shape, boundaries, and other information in the second round of rural land extensions. The high-definition images obtained through drone aerial photography can accurately measure the area of ​​the land, providing accurate data support for the second round of rural land extensions.

[0003] However, traditional surveying and mapping drones lack cover protection. During takeoff and landing, the drone may be affected by uneven ground, debris or severe weather conditions, resulting in bumps, rollover or damage. The impact force during landing may act directly on the drone body, increasing the risk of damage. Without a cover, the drone's precision components are more susceptible to erosion and damage from the external environment, such as dust, rain, etc.

[0004] Therefore, a UAV flight safety take-off and landing equipment is designed to solve the above problems. Utility Model Content

[0005] To solve the problems raised in the above background technology. The utility model provides a drone flight safety take-off and landing device, which can provide a smoother and more spacious take-off space for the drone by extending and unfolding the storage component cover, especially on uneven or soft ground, which helps to prevent bumps or rollovers during take-off. Similarly, the box can serve as a buffer area to absorb the impact force when the drone lands, reduce the risk of damage, and provide a stable landing platform. During take-off and landing, the cover can block severe weather conditions such as wind, rain, dust, etc., protect the drone's precision components from damage, and ensure that the drone can perform tasks stably and continuously. The cover can be stored in the box when not in use, making the entire device compact and easy to carry, suitable for rapid deployment in a variety of environments. In the stored state, the device has a simpler appearance and is less likely to attract attention, which helps to use it in situations where concealed operations are required.

[0006] To achieve the above-mentioned object, the present invention provides the following technical solution: a drone flight safety take-off and landing device, comprising a box body, and a storage assembly arranged on the outer side of the end portion of the box body;

[0007] The storage assembly includes a motor, a mounting plate and a first rotating arm, two motors are installed on the outside of one end of the box, two mounting plates are fixedly connected to the inside of both ends of the box, the outside of the main shaft of the motor is fixedly connected to the first rotating arm, the first rotating arm is arranged inside the box, one side of the first rotating arm is rotatably connected to the second rotating arm, the outside of one end of the second rotating arm is rotatably connected to the third rotating arm, one side of the third rotating arm is fixedly connected to the first limit block and the second limit block, and the outside of the end of the third rotating arm is fixedly connected to the cover plate.

[0008] As a preferred embodiment of the safe take-off and landing equipment for unmanned aerial vehicle flight of the present invention, a connecting rod is fixedly connected to the outer side of one end of each of the two second rotating arms.

[0009] As a preferred embodiment of the safe take-off and landing equipment for unmanned aerial vehicle flight of the present invention, the first limit block and the second limit block are in contact with the inner side of the through groove formed in the mounting plate.

[0010] As a preferred embodiment of the safe take-off and landing equipment for unmanned aerial vehicle flight of the present invention, a display is installed on the outer side of one end of the cover plate.

[0011] As a preferred embodiment of the safe take-off and landing equipment for unmanned aerial vehicle flight of the present invention, ventilation slots are provided on the inner sides of both ends of the box.

[0012] As a preferred embodiment of the safe take-off and landing equipment for unmanned aerial vehicle flight of the present invention, the lower surface of the box is rotatably connected to support legs.

[0013] As a preferred embodiment of the safe take-off and landing equipment for unmanned aerial vehicle flight of the present invention, a charging base is fixedly connected to the inner side of the bottom end of the box.

[0014] Compared with the prior art, the beneficial effects of the present invention are: a storage component is added to the present application, and the storage component cover is extended outward and unfolded to provide a smoother and more spacious take-off space for the UAV, especially on uneven or soft ground, which helps to prevent bumps or rollovers during take-off. Similarly, the box can serve as a buffer area to absorb the impact force when the UAV lands, reduce the risk of damage, and provide a stable landing platform. During take-off and landing, the cover can block severe weather conditions such as wind, rain, dust, etc., protect the precision components of the UAV from damage, and ensure that the UAV can perform its mission stably and continuously. The cover can be stored in the box when not in use, making the entire device compact and easy to carry, suitable for rapid deployment in a variety of environments. In the stored state, the appearance of the device is simpler and less likely to attract attention, which is helpful for use in situations where covert operation is required. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] The accompanying drawings are used to provide a further understanding of the present invention and constitute a part of the specification. Together with the embodiments of the present invention, they are used to explain the present invention and do not constitute a limitation of the present invention. In the accompanying drawings:

[0016] Figure 1 It is a schematic diagram of the overall structure of the utility model;

[0017] Figure 2 This is a schematic diagram of the structure of the support legs and handle in the utility model;

[0018] Figure 3 It is a cross-sectional view of the box body in the utility model;

[0019] Figure 4 This is a schematic structural diagram of the cover plate and connecting rod in the utility model;

[0020] Figure 5 It is a schematic structural diagram of the second rotating arm and the third rotating arm in the present utility model;

[0021] Figure 6 It is a structural schematic diagram of the first limiting block and the second limiting block in the utility model.

[0022] In the picture:

[0023] 1. Box body;

[0024] 2. Storage assembly; 21. Motor; 22. Mounting plate; 23. First rotating arm; 24. Second rotating arm; 25. Third rotating arm; 26. First limit block; 27. Second limit block; 28. Cover; 29. ​​Connecting rod; 210. Charging base; 211. Display; 212. Ventilation slot; 213. Support leg; 214. Handle. DETAILED DESCRIPTION

[0025] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0026] like Figure 1 As shown;

[0027] A device for safe take-off and landing of a UAV comprises a box 1.

[0028] In this embodiment: Traditional surveying and mapping drones lack cover protection. During takeoff and landing, the drone may be affected by uneven ground, debris or adverse weather conditions, resulting in bumps, rollover or damage. The impact force during landing may directly act on the drone body, increasing the risk of damage. Without a cover, the drone's precision components are more susceptible to erosion and damage from the external environment, such as dust, rain, etc. In order to solve this technical problem, a storage component 2 is added on this basis.

[0029] More specifically:

[0030] like Figures 1 to 6 As shown:

[0031] Combined with the above content: the storage assembly 2 includes a motor 21, a mounting plate 22 and a first rotating arm 23. Two motors 21 are installed on the outside of one end of the box body 1. Two mounting plates 22 are fixedly connected to the inside of the two ends of the box body 1. The outside of the main shaft of the motor 21 is fixedly connected to the first rotating arm 23. The first rotating arm 23 is arranged inside the box body 1. One side of the first rotating arm 23 is rotatably connected to the second rotating arm 24. The outside of one end of the second rotating arm 24 is rotatably connected to the third rotating arm 25. One side of the third rotating arm 25 is fixedly connected to the It is connected to a first limit block 26 and a second limit block 27, which are in contact with the inner side of the through groove opened in the mounting plate 22. The outer side of the end of the third rotating arm 25 is fixedly connected to a cover plate 28, and the outer side of one end of the two second rotating arms 24 is fixedly connected to a connecting rod 29. The inner side of the bottom end of the box body 1 is fixedly connected to a charging base 210, and ventilation grooves 212 are opened on the inner sides of both ends of the box body 1. The lower surface of the box body 1 is rotatably connected to a support leg 213, and the outer sides of both ends of the box body 1 are fixedly connected to a handle 214.

[0032] In this embodiment, when the user uses the device, he can move the device to a specified position. At this time, the user can start the motor 21, and the motor 21 drives the first rotating arm 23 outside the main shaft to rotate. When the first rotating arm 23 rotates, it will press against the second rotating arm 24 outside the first rotating arm 23 to rotate and rise. Then, the second rotating arm 24 pushes the third rotating arm 25 to rise on one side of the mounting plate 22 until the cover plate 28 is extended from the inside of the box body 1. At this time, the first limit block 26 moves to the end of the through groove of the mounting plate 22. At this time, Under the action of the rotating arm 23 and the second rotating arm 24, the second limit block 27 is pushed into the arc-shaped part of the through groove of the mounting plate 22, which can drive the third rotating arm 25 to rotate, and can drive the cover 28 outside the end of the third rotating arm 25 to rotate, and unfold the two cover plates 28 to the outside. At this time, the drone inside the box 1 can take off. When it is necessary to retract the drone, start the motor 21 again, and pull the cover plate 28 back and close it through the second rotating arm 24 and the third rotating arm 25. At the same time, the rubber charging base 210 can buffer the drone and charging, the ventilation slots 212 can ensure the circulation of air inside the box 1, and the multiple support legs 213 can be deployed outward to support the box 1. The cover 28 of the storage component 2 is extended outward and deployed to provide a smoother and more spacious take-off space for the drone, especially on uneven or soft ground, which helps to prevent bumps or rollovers during take-off. Similarly, the box 1 can serve as a buffer area to absorb the impact force when the drone lands, reduce the risk of damage, and provide a stable landing platform. During take-off and landing, the cover 28 can block adverse weather conditions such as wind, rain, dust, etc., protect the precision components of the drone from damage, and ensure that the drone can perform its mission stably and continuously. The cover 28 can be stored in the box 1 when not in use, making the entire device compact and easy to carry, suitable for rapid deployment in various environments. In the stored state, the device has a simpler appearance and is less noticeable, which helps to use it in situations where covert operation is required. The handle 214 allows the operator to easily lift and move the entire device, especially when frequent location changes or movement between different sites, which can significantly reduce the physical burden.

[0033] Going further:

[0034] In an optional embodiment, a display 211 is mounted on the outer side of one end of the cover 28 .

[0035] In this embodiment: the model of the display 211 can be CEM-12PS-VDH0. The display 211 can be remotely connected to the drone via Bluetooth or other means. The display 211 can display the status information of the drone in real time, such as battery level, flight altitude, speed, direction, etc., so that the operator can quickly understand the current status of the drone and make corresponding adjustments. During takeoff and landing, the display 211 can display information such as whether the drone is fully charged to ensure correct operation.

[0036] Working principle: When the user uses the device, he can move the device to the specified position. At this time, the user can start the motor 21, and the motor 21 drives the first rotating arm 23 on the outer side of its main shaft to rotate. When the first rotating arm 23 rotates, it will press against the second rotating arm 24 on the outer side of the first rotating arm 23 to rotate and rise. Then, the third rotating arm 25 is pushed up on one side of the mounting plate 22 by the second rotating arm 24 until the cover plate 28 is extended from the inside of the box body 1. At this time, the first limit block 26 moves to the end of the through slot provided on the mounting plate 22. At this time, under the action of the first rotating arm 23 and the second rotating arm 24, the second limit block 27 is Push the arc-shaped part of the through groove opened in the mounting plate 22, and then the third rotating arm 25 can be driven to rotate, which can drive the cover 28 on the outer side of the end of the third rotating arm 25 to rotate, and the two cover plates 28 are unfolded outward. At this time, the drone inside the box 1 can take off. When the drone needs to be retracted, the motor 21 is started again, and the cover plate 28 is pulled back and closed by the second rotating arm 24 and the third rotating arm 25. At the same time, the rubber charging base 210 can buffer and charge the drone, and the ventilation slots 212 can ensure the circulation of air inside the box 1. At the same time, the multiple support legs 213 are unfolded outward to retract the box 1. Support, by extending and unfolding the cover 28 of the storage component 2, a smoother and more spacious take-off space can be provided for the UAV, especially on uneven or soft ground, which helps to prevent bumps or rollovers during take-off. Similarly, the box 1 can serve as a buffer area to absorb the impact force when the UAV lands, reduce the risk of damage, and provide a stable landing platform. During take-off and landing, the cover 28 can block adverse weather conditions such as wind, rain, dust, etc., protect the precision components of the UAV from damage, and ensure that the UAV can perform its mission stably and continuously. The cover 28 can be stored in the box 1 when not in use, making the entire device compact. , easy to carry, suitable for rapid deployment in a variety of environments. In the stored state, the appearance of the device is simpler and less likely to attract attention, which helps to use it in situations where covert operation is required. The display 211 can display the status information of the drone in real time, such as battery level, flight altitude, speed, direction, etc., so that the operator can quickly understand the current status of the drone and make corresponding adjustments. During takeoff and landing, the display 211 can display information such as whether the drone is fully charged to ensure correct operation. The handle 214 allows the operator to easily lift and move the entire device, especially when it is necessary to frequently transfer locations or move between different venues.

[0037] Finally, it should be noted that the above description is merely a preferred embodiment of the present invention and is not intended to limit the present invention. Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art will be able to modify the technical solutions described in the aforementioned embodiments or replace some of the technical features therein with equivalents. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present invention shall be included within the scope of protection of the present invention.

Claims

1. A drone flight safety take-off and landing device, comprising a box (1), characterized in that: It also includes a storage assembly (2) arranged on the outside of the end of the box (1); The storage assembly (2) comprises a motor (21), a mounting plate (22) and a first rotating arm (23); two motors (21) are mounted on the outer side of one end of the box (1); two mounting plates (22) are fixedly connected to the inner sides of both ends of the box (1); a first rotating arm (23) is fixedly connected to the outer side of the main shaft of the motor (21); the first rotating arm (23) is arranged inside the box (1); one side of the first rotating arm (23) is rotatably connected to the second rotating arm (24); one end of the second rotating arm (24) is rotatably connected to the outer side of a third rotating arm (25); one side of the third rotating arm (25) is fixedly connected to a first limit block (26) and a second limit block (27); and the outer side of the end of the third rotating arm (25) is fixedly connected to a cover plate (28).

2. The UAV flight safety take-off and landing equipment according to claim 1, characterized in that: A connecting rod (29) is fixedly connected to the outer sides of one end of the two second rotating arms (24).

3. The UAV flight safety take-off and landing equipment according to claim 1, characterized in that: The first limiting block (26) and the second limiting block (27) are in contact with the inner side of the through slot formed in the mounting plate (22).

4. The UAV flight safety take-off and landing equipment according to claim 1, characterized in that: A display (211) is mounted on the outer side of one end of the cover plate (28).

5. The UAV flight safety take-off and landing equipment according to claim 1, characterized in that: Ventilation slots (212) are provided on the inner sides of both ends of the box body (1).

6. The UAV flight safety take-off and landing equipment according to claim 1, characterized in that: The lower surface of the box body (1) is rotatably connected to a support leg (213).

7. The UAV flight safety take-off and landing equipment according to claim 1, characterized in that: A charging base (210) is fixedly connected to the inner side of the bottom end of the box (1).

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