Unmanned aerial vehicle nest of low-altitude unmanned aerial vehicle remote sensing network
By designing a low-altitude drone remote sensing network drone nest with an outward tilt and a foldable solar cover, the existing drone nest has solved the problem of large structure and large area of occupied space, and the flexible lifting and charging of drones is realized, and the layout needs of the drone remote sensing network is met.
Patent Information
- Application Number
- CN202421406651.6
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-06-19
- Publication Date
- 2025-06-27
- Estimated Expiration
- 2034-06-19
AI Technical Summary
The existing drone nest structure is large, the area occupied by a large area, and the layout site requirements are high, making it difficult to flexibly adjust the distribution of drones in the drone remote sensing network.
A drone nest with a low-altitude drone remote sensing network is designed, including an open-up shell, a base, energy storage device, charging device, apron and solar cover. Through the outward tilt opening and foldable solar cover design, the drone is flexible to lift and charge, and the distribution of the drone can be flexibly adjusted.
It improves the lifting space and charging efficiency of the drone, flexibly adjusts the distribution of the drone, meets the layout needs of the low-altitude drone remote sensing network, and improves the drone remote sensing network detection system.
Smart Images

Figure CN223031317U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to a drone nest of a low-altitude drone remote sensing network, belonging to the field of drone nest tools. Background Technique
[0002] Since the birth of the first unmanned aircraft in 1914, drones (UAVs) have a history of exactly 100 years. A drone is a powered, controllable, and multi-task-performable unmanned aerial vehicle. Since its birth, it has been mainly applied in the military field. As an intelligent and information-based weapon, drones have played an important role in reconnaissance, surveillance, communication, long-distance attack, etc. Compared with manned aircraft, drones are favored by the armies of various countries because of their advantages such as small size, low cost, convenient use, and strong adaptability. Drones will surely become the "sharp-winged soldiers" in the air and space field of the century.
[0003] In recent years, the application of drones in the civilian field has also been increasing, and various countries have gradually opened up the civilian use of drones. Drones have been widely applied in multiple fields such as public security, emergency search and rescue, agriculture and forestry, environmental protection, transportation, communication, meteorology, and film and television aerial photography. For example, a low-altitude drone remote sensing network arranged in cities can conduct intermittent patrols by drones carrying relevant detection equipment to achieve the purpose of detection. At the same time, with the development of low-altitude flying cars, the role of the drone remote sensing network will become more obvious. For example, drones in the remote sensing network can detect the path in advance and then plan a safe path for the flying car.
[0004] As the place where drones dock, charge, and store, the drone nest plays a crucial role in the remote sensing network. The existing drone nests have large structures and large occupied areas, or have high requirements for the layout places. For example, the tower-mounted drone nests used in the power grid can facilitate the supply of power. That is, there are high requirements for the distribution positions of drones in the remote sensing network.
[0005] There is a need for a drone nest that is easy to arrange, conducive to parking and power supply, and can flexibly adjust the distribution of drones in the drone remote sensing network. Content of the Utility Model
[0006] In view of this, the purpose of the utility model is to provide a drone nest of a low-altitude drone remote sensing network, which is easy to arrange, conducive to parking and power supply, and can flexibly adjust the distribution of drones in the drone remote sensing network; it can overcome the deficiencies of the prior art.
[0007] The purpose of the utility model is achieved through the following technical solutions:
[0008] The utility model discloses a drone nest for a low-altitude drone remote sensing network, which comprises a housing with an upward opening. A base is arranged inside the housing, and an energy storage device and a charging device for the drone are arranged on the base. A landing pad is arranged on the base. The upper middle part of the housing is an outwardly inclined opening, and a solar cover plate and an unfolding and closing device for the solar cover plate are arranged at the upper end of the housing.
[0009] The upper end of the above-mentioned housing is an inclined surface with one high and one low, and the solar cover plate is inclinedly installed at the upper end of the housing.
[0010] In the above, the solar cover plate is composed of an upper cover plate and a lower cover plate that can be superposed on each other. Guide rods are arranged on the lower cover plate, a first guide rail that cooperates with the guide rods is arranged at the high end of the housing, a second guide rail that cooperates with the guide rods is arranged on the upper cover plate, and limiting grooves for the upper cover plate and the lower cover plate are arranged on the left and right sides of the housing. The lower cover plate can move upward along the first guide rail and simultaneously push the upper cover plate upward to vacate the upper space of the housing, and the limiting grooves limit the closed state of the upper cover plate and the lower cover plate.
[0011] In the above, guide grooves are arranged on the upper and lower sides of the guide rods and the lower cover plate, and clamping blocks that cooperate with the guide grooves are respectively arranged on the first guide rail and the second guide rail.
[0012] In the above, the unfolding and closing device comprises a rack arranged at the lower end of the lower cover plate, a gear that cooperates with the rack is arranged at the high end of the housing, the gear is connected to a driving motor, and the controller of the driving motor is connected to a central computer through a signal transmission device.
[0013] In the above, a gap is arranged between the base and the side of the housing, and through holes are arranged at the bottom of the gap.
[0014] In the above, a maintenance sealing door communicating with the base is arranged at the lower end of the housing.
[0015] Compared with the prior art, the beneficial effects of the utility model are as follows:
[0016] 1. Through the outwardly inclined opening of the utility model, firstly, it can provide more lifting space for the drone, which is beneficial to the lifting of the drone. Secondly, power can be generated through the solar cover plate, and then energy can be stored through the energy storage device, and then energy can be provided for the drone for charging. In this way, the layout of the drone station can be flexibly carried out, which is beneficial to improving the drone remote sensing network detection system. The solar cover plate can be opened or closed through the unfolding and closing device, so as to realize the lifting and storage and rain protection of the drone.
[0017] 2. The upper end of the housing is an inclined surface with one high and one low, and the solar cover plate is inclinedly installed at the upper end of the housing. With such a structure, by inclinedly installing the solar cover plate, it is beneficial for the solar cover plate to receive light over a larger area for power generation.
[0018] 3. The lower cover plate can move upward along the first guide rail while pushing the upper cover plate upward to vacate the upper space of the housing, maximizing the surrounding space above the helipad, thus facilitating the lifting and lowering of the drone. By dividing the solar cover plate into the upper cover plate and the lower cover plate, moreover, in the later stage of unfolding, the lower cover plate can move upward along the first guide rail while pushing the upper cover plate upward. The upper cover plate and the lower cover plate in the folded state can move the overall center of gravity of the solar function cover plate closer to the base, minimizing the lever force on the base caused by the unfolding of the solar cover plate and facilitating the maintenance of the stability of the base.
[0019] 4. Guide grooves are provided on both the upper and lower sides of the guide rod and the lower cover plate. On the first guide rail and the second guide rail, there are respectively catch blocks that cooperate and engage with the guide grooves. In this way, the first guide rail and the second guide rail can share the guide rod, thus ensuring the guiding movement.
[0020] 5. The unfolding and closing device includes a rack provided at the lower end of the lower cover plate, a gear provided at the high end of the housing that cooperates with the rack, the gear is connected to a driving motor, and the controller of the driving motor is connected to the central computer through a signal transmission device. In this way, the unfolding or closing of the lower cover plate can be achieved through the cooperation of the rack, the gear, and the driving motor.
[0021] 6. A gap is provided between the base and the side of the housing, and through holes are provided at the bottom of the gap. In this way, through the through holes, firstly, a ventilation effect can be achieved inside the housing; secondly, when water seeps into the housing, it can be drained through the through holes; thirdly, through some of the through holes, screws can be installed to facilitate the fixing of the housing.
[0022] Other advantages, objectives, and features of the present utility model will be described to some extent in the subsequent specification, and to some extent, will be obvious to those skilled in the art based on the study of the following text, or can be learned from the practice of the present utility model. The objectives and other advantages of the present utility model can be achieved and obtained through the following specification. BRIEF DESCRIPTION OF THE DRAWINGS
[0023] In order to make the objectives, technical solutions, and advantages of the present utility model clearer, the present utility model will be further described in detail below in conjunction with the drawings, where:
[0024] Figure 1 It is a schematic connection structure diagram of the closed state of the solar cover plate of the present utility model.
[0025] Figure 2 It is a schematic connection structure diagram of the open state of the lower cover plate of the present utility model.
[0026] Figure 3 It is a schematic connection structure diagram of the open state where the lower cover plate moves upward to push the upper cover plate of the present utility model.
[0027] Figure 4 is Figure 3 the split structure schematic diagram of
[0028] Figure 5 is Figure 4 the enlarged structure schematic diagram of part A in
[0029] Figure 6 is the enlarged structure schematic diagram of part B in 4.
[0030] Figure 7 is Figure 4 the connection structure schematic diagram from another angle of
[0031] Figure 8 is Figure 7 the enlarged structure schematic diagram of part C in
[0032] Figure 9 is Figure 7 the enlarged structure schematic diagram of part D in
[0033] Figure 10 is the structure schematic diagram from another angle of the state where the lower cover plate moves upward to push the upper cover plate open.
[0034] Among them, the housing 1; the base 2; the helipad 3; the solar cover plate 4; the upper cover plate 4-1; the lower cover plate 4-2; the guide rod 4-3; the first guide rail 4-4; the second guide rail 4-5; the guide groove 4-6; the chuck 4-7; the limit groove 5; the rack 6; the gear 7; the drive motor 8; the gap 9; the through hole 10; the maintenance sealing door 11. Specific embodiments
[0035] Hereinafter, with reference to the accompanying drawings, the preferred embodiments of the present invention will be described in detail. It should be understood that the preferred embodiments are only for explaining the present invention, rather than limiting the protection scope of the present invention.
[0036] Such as Figures 1 - 10As shown in the figure, the utility model discloses a drone nest of a low-altitude drone remote sensing network, which includes a housing 1 with an upward opening. A base 2 is provided inside the housing 1. An energy storage device and a charging device for the drone are provided on the base 2. A maintenance sealing door 11 communicating with the base 2 is provided at the lower end of the housing 1. A landing pad 3 is provided on the base 2. The middle and upper part of the housing 1 is an outwardly inclined opening. A solar cover 4 and an unfolding and closing device for the solar cover 4 are provided at the upper end of the housing 1. The solar cover 4 is connected to the energy storage device. With such a structure, through the outwardly inclined opening, firstly, more lifting space can be provided for the drone, which is beneficial to the lifting and lowering of the drone. Secondly, electricity can be generated through the solar cover 4, and then stored through the energy storage device, and then used to charge the drone. In this way, the layout of the drone station can be flexibly carried out, which is beneficial to improving the drone remote sensing network detection system. The solar cover 4 can be opened or closed through the unfolding and closing device, so as to realize the lifting and lowering and storage and rain protection of the drone.
[0037] Furthermore, the upper end of the housing 1 is an inclined surface with one high and one low. The solar cover 4 is inclinedly installed at the upper end of the housing 1. With such a structure, by inclinedly installing the solar cover 4, it is beneficial for the solar cover 4 to receive light over a larger area for power generation.
[0038] Further, the solar cover plate 4 is composed of an upper cover plate 4-1 and a lower cover plate 4-2 that can be superposed on each other. A guide rod 4-3 is provided on the lower cover plate 4-2. A first guide rail 4-4 that cooperates with the guide rod 4-3 is provided at the high end of the housing 1. A second guide rail 4-5 that cooperates with the guide rod 4-3 is provided on the upper cover plate 4-1. Limit slots 5 for the upper cover plate 4-1 and the lower cover plate 4-2 are provided on both the left and right sides of the housing 1. The lower cover plate 4-2 can move upward along the first guide rail 4-4 and simultaneously push the upper cover plate 4-1 upward to vacate the upper space of the housing 1. The limit slots 5 limit the closed state of the upper cover plate 4-1 and the lower cover plate 4-2. In detail, a limit block for the upper cover plate 4-1 is provided on the free section of the guide rod 4-3. In this way, when closing, the upper cover plate 4-1 can be pulled down for closing through the limit block. Although when closing, the upper cover plate 4-1 can slide downward under the action of gravity to achieve closing, however, the limit block can further ensure the stability of the closing of the upper cover plate 4-1. Moreover, a rain shield for covering the housing 1 is provided on the upper side edge of the upper cover plate 4-1. With such a structure, the lower cover plate 4-2 can move upward along the first guide rail 4-4 and simultaneously push the upper cover plate 4-1 upward to vacate the upper space of the housing 1, which can maximize the surrounding space above the apron 3, thus facilitating the lifting and lowering of the unmanned aerial vehicle. By dividing the solar cover plate 4 into the upper cover plate 4-1 and the lower cover plate 4-2, and moreover, in the later stage of unfolding, the lower cover plate 4-2 can move upward along the first guide rail 4-4 and simultaneously push the upper cover plate 4-1 upward. The upper cover plate 4-1 and the lower cover plate 4-2 in the folded state can move the overall center of gravity of the solar function cover plate 4 closer to the base 2, minimizing the lever force on the base 2 due to the unfolding of the solar cover plate 4 as much as possible, which is beneficial to maintaining the stability of the base 2.
[0039] Specifically, guide grooves 4-6 are provided on both the upper and lower sides of the guide rod 4-3 and the lower cover plate 4-2. Clamping blocks 4-7 that cooperate and are clamped with the guide grooves 4-6 are respectively provided on the first guide rail 4-4 and the second guide rail 4-5. In this way, the first guide rail 4-4 and the second guide rail 4-5 can share the guide rod 4-3, thus ensuring the guiding movement.
[0040] Further, the unfolding and closing device includes a rack 6 provided at the lower end of the lower cover plate 4-2. A gear 7 that cooperates with the rack 6 is provided at the high end of the housing 1. The gear 7 is connected to a driving motor 8. The controller of the driving motor 8 is connected to the central computer through a signal transmission device. In this way, the unfolding or closing of the lower cover plate 4-2 can be realized through the cooperation of the rack 6, the gear 7, and the driving motor 8.
[0041] Further, a gap 9 is provided between the base 2 and the side of the housing 1, and a through hole 10 is provided at the bottom of the gap 9. In this way, through the through hole 10, firstly, the ventilation effect can be achieved inside the housing 1; secondly, when water seeps into the housing 1, the water can be drained through the through hole 10; thirdly, through some of the through holes 10, screws can be installed to facilitate the fixation of the housing 1.
[0042] When such a device is in use, when the drone needs to ascend or descend, the central computer issues an instruction to the drive motor 8, and then the drive motor 8 opens the upper cover plate 4-1 and the lower cover plate 4-2 of the solar cover plate 4, so as to create a space for the drone to ascend and descend, facilitating the drone to cruise along the established route.
[0043] The above are only the preferred embodiments of the present invention, and there is no restriction on the present invention in any form of confidentiality. Any simple modification, equivalent change and modification made to the above embodiments based on the technical content of the present invention and according to the technical essence of the present invention still fall within the scope of the technical solution of the present invention.
Claims
1. A drone nest for a low-altitude drone remote sensing network, comprising a housing (1) with an opening facing upward, a base (2) provided inside the housing (1), an energy storage device and a drone charging device provided on the base (2), and a helipad (3) provided on the base (2), characterized in that: The upper middle portion of the shell (1) is an opening inclined outwards, and a solar cover (4) and an unfolding and closing device for the solar cover (4) are provided at the upper end of the shell (1).
2. The drone nest of the low-altitude drone remote sensing network according to claim 1 is characterized in that: The upper end of the shell (1) is an inclined surface with one high and one low, and the solar cover (4) is installed at an angle on the upper end of the shell (1).
3. The drone nest of the low-altitude drone remote sensing network according to claim 2 is characterized in that: The solar cover plate (4) is composed of an upper cover plate (4-1) and a lower cover plate (4-2) that can be overlapped with each other, a guide rod (4-3) is provided on the lower cover plate (4-2), a first guide rail (4-4) that cooperates with the guide rod (4-3) is provided at the high end of the shell (1), a second guide rail (4-5) that cooperates with the guide rod (4-3) is provided on the upper cover plate (4-1), and limiting grooves (5) for the upper cover plate (4-1) and the lower cover plate (4-2) are provided on the left and right sides of the shell (1), the lower cover plate (4-2) can move upward along the first guide rail (4-4) and simultaneously push the upper cover plate (4-1) to move upward to free up space above the shell (1), and the limiting grooves (5) limit the closed state of the upper cover plate (4-1) and the lower cover plate (4-2).
4. The drone nest of the low-altitude drone remote sensing network according to claim 3 is characterized in that: The guide rod (4-3) and the lower cover plate (4-2) are both provided with guide grooves (4-6) on the upper and lower sides, and the first guide rail (4-4) and the second guide rail (4-5) are respectively provided with clamping blocks (4-7) that cooperate with the guide grooves (4-6) and are clamped together.
5. The drone nest of the low-altitude drone remote sensing network according to claim 3 is characterized in that: The unfolding and closing device comprises a rack (6) provided at the lower end of the lower cover plate (4-2), a gear (7) cooperating with the rack (6) provided at the upper end of the housing (1), the gear (7) being connected to a drive motor (8), and a controller of the drive motor (8) being connected to a central computer via a signal transmission device.
6. The drone nest of the low-altitude drone remote sensing network according to claim 1, characterized in that: A gap (9) is provided between the base (2) and the side of the shell (1), and a through hole (10) is provided at the bottom of the gap (9).
7. The drone nest of the low-altitude drone remote sensing network according to any one of claims 1 to 6, characterized in that: A maintenance sealing door (11) which is in communication with the base (2) is provided at the lower end of the shell (1).