A hangar applicable to drones

Abstract

The present invention discloses a hangar applicable to drones. The hangar includes a hangar body, and the hangar body includes a base, a takeoff and landing platform, a lifting drive, a lifting linkage component, and an opening and closing component. The lifting drive is arranged in the base; the lower end and the upper end of the lifting linkage component are respectively connected to the lifting drive and the takeoff and landing platform. The opening and closing component includes an opening and closing linkage component and at least two opening and closing covers. The opening and closing covers are hinged to the opening and closing linkage component. The opening and closing linkage component is provided with a first through hole for the lifting linkage component to pass through. A pressing structure is arranged on the side surface of the lifting linkage component. When the lifting linkage component descends, the pressing structure is used to abut against the upper side surface of the opening and closing linkage component or the upper end of the first through hole, so that the opening and closing covers rotate and close to form a closed cavity for accommodating the takeoff and landing platform, and the pressing structure keeps pressing on the opening and closing linkage component to keep the opening and closing covers closed; when the opening and closing covers are opened, the takeoff and landing platform rises and is exposed. The present invention can be widely applied to the field of drone technology.

Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicles, and in particular to a hangar suitable for unmanned aerial vehicles. Background Art

[0002] With the rapid development of drone technology, drones have quickly become popular in many industries, providing convenience and improving efficiency for many industries. After completing the work and returning, the drone usually lands on the ground and is brought back by the operator. The drone is relatively heavy and inconvenient for the operator to carry. Especially in the case of autonomous operation of specific tasks such as regular park inspections, traffic road inspections, river inspections, protected area inspections, and atmospheric monitoring, if the operator brings the drone back every day, it will undoubtedly increase the workload. Therefore, a hangar can be set up on site to store drones. At present, there is no reliable hangar available, and it is impossible to guarantee the safe storage of drones after landing.

[0003] In addition, due to the limitation of battery technology, the endurance problem has become a shortcoming of drones. When the drone is low on power, it needs to return to the base in time, and manually charge or replace the battery, which makes the drone only able to complete tasks in a small range and a short time. Therefore, how to extend the endurance of drones and increase their autonomous working ability without human intervention is also a problem that should be solved at present. Summary of the invention

[0004] In order to solve at least one of the above technical problems, the present invention provides a hangar suitable for unmanned aerial vehicles, and the technical solution adopted is as follows.

[0005] The hangar suitable for unmanned aerial vehicles provided by the present invention comprises a hangar body, the hangar body comprises a base, a take-off and landing platform, a lifting drive, a lifting linkage component and an opening and closing assembly, the base is hollow, and the top of the base is open; the unmanned aerial vehicle can take off and land on the take-off and landing platform; the lifting drive is arranged in the base; the lower end of the lifting linkage component is connected to the lifting drive, and the upper end of the lifting linkage component is connected to the take-off and landing platform, and under the drive of the lifting drive, the lifting linkage component and the take-off and landing platform can be lifted and lowered; the opening and closing assembly comprises an opening and closing linkage component and at least two opening and closing covers, and the opening and closing covers are connected to the opening and closing The linkage parts are hinged, and each of the opening and closing cover bodies is closed to form a closed cavity for accommodating the lifting and lowering platform, and the lifting and lowering platform is exposed when each of the opening and closing cover bodies is opened; wherein, the opening and closing linkage parts are provided with a first through hole, and the lifting linkage parts pass through the first through hole, and the side of the lifting linkage parts is provided with a downward pressing structure, and during the process of the lifting linkage parts descending, the downward pressing structure is used to abut against the upper side of the opening and closing linkage parts or the downward pressing structure is used to abut against the upper end edge of the first through hole, and with the contact position between the outer side surface of the opening and closing cover body and the open part of the base as the fulcrum, the opening and closing cover body can be rotated inward to achieve closure.

[0006] In certain embodiments of the present invention, a jacking structure is provided on the side of the lifting linkage member. During the upward movement of the lifting linkage member, the jacking structure is configured to abut against the lower side of the opening and closing linkage member or the jacking structure is configured to abut against the lower edge of the first through hole, so as to cause the opening and closing linkage member to rise.

[0007] In certain embodiments of the present invention, the lifting linkage member includes an inverted first conical structure. The large-diameter end of the first conical structure is connected to the takeoff and landing platform. During the downward movement of the lifting linkage member, the side surface of the first conical structure is configured to abut against the upper edge of the first through hole.

[0008] In certain embodiments of the present invention, the lifting linkage member includes a second conical structure. The small-diameter end of the first conical structure is connected to the small-diameter end of the second conical structure. The large-diameter end of the second conical structure is connected to the lifting driver. During the upward movement of the lifting linkage member, the side surface of the second conical structure is configured to abut against the lower edge of the first through hole.

[0009] In certain embodiments of the present invention, the takeoff and landing platform is provided with a wireless charging component.

[0010] In certain embodiments of the present invention, the opening and closing cover body includes a cover body support structure, a light-emitting component and a transparent cover. The cover body support structure is hinged to the opening and closing linkage member; and / or, the opening and closing cover body includes a cover body support structure and a solar cover.

[0011] In certain embodiments of the present invention, the cover body support structure is made of piezoelectric ceramic material, and the cover body support structure can convert thermal energy into electrical energy for standby.

[0012] In certain embodiments of the present invention, the outer side surface of the opening and closing cover body has a arched curved surface.

[0013] In certain embodiments of the present invention, the opening and closing cover body is provided as a petal-shaped structure.

[0014] In certain embodiments of the present invention, the hangar body includes a support member. One end of the support member is connected to the base, and the other end is used to connect to the bearing foundation.

[0015] In certain embodiments of the present invention, the hangar includes columns, and at least one hangar body is installed on the columns.

[0016] The embodiments of the present invention have at least the following beneficial effects: When the hangar body is in the open state, the takeoff and landing platform is exposed, and the unmanned aerial vehicle can take off and land on the takeoff and landing platform; during the process of the lifting drive driving the lifting linkage component and the takeoff and landing platform to descend, the pressing structure of the lifting linkage component can press the opening and closing linkage component, and the opening and closing linkage component descends, and the outer side surface of the opening and closing cover body can abut against the base and rotate inward, and each opening and closing cover body is closed; when the hangar body is in the closed state, the takeoff and landing platform is in the closed cavity formed by the opening and closing cover bodies, and the pressing structure keeps pressing the opening and closing linkage component to keep each opening and closing cover body closed. The present invention can be widely applied to the field of unmanned aerial vehicle technology. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] The aspects and advantages described and / or appended in the embodiments of the present invention will become apparent and be readily understood in conjunction with the following drawings. It should be noted that the embodiments shown in the following drawings are exemplary and are only used to explain the present invention and should not be construed as a limitation to the present invention.

[0018] Figure 1 It is a structural diagram of the hangar, and the figure shows that there are four hangar bodies provided on the column, and each hangar body is closed.

[0019] Figure 2 is Figure 1 the structural diagram after the hangar body in [FIGURE NUMBER] is opened.

[0020] Figure 3 It is a structural diagram of the hangar body, and the figure shows a support component and a mounting component.

[0021] Figure 4 It is a structural diagram of the takeoff and landing platform, the lifting drive, the lifting linkage component, the opening and closing assembly and the base.

[0022] Figure 5 It is an exploded view of the opening and closing cover body, and the figure shows that the opening and closing cover body has a cover body support structure, a light-emitting component, a transparent cover and a sealing structure.

[0023] Reference numerals:

[0024] 1100, base;

[0025] 1200, takeoff and landing platform; 1201, wireless charging component; 1202, bottom plate; 1203, cover plate;

[0026] 1300, lifting drive;

[0027] 1401, opening and closing linkage component; 1402, opening and closing cover body; 1403, first through hole; 1404, cover body support structure; 1405, light-emitting component; 1406, transparent cover; 1407, sector plug; 1408, sealing structure;

[0028] 1501. First conical structure; 1502. Second conical structure;

[0029] 1600. Support member;

[0030] 1701. GPS antenna; 1702. Data transmission antenna;

[0031] 2001. Column; 2002. Mounting member. Detailed implementation mode

[0032] The following combines Figures 1 to 5 Embodiments of the present invention are described in detail. Examples of the embodiments are shown in the drawings, where the same or similar reference numerals throughout denote the same or similar elements or elements having the same or similar functions. The embodiments described by referring to the drawings below are exemplary and are only used to explain the present invention and should not be construed as a limitation of the present invention.

[0033] In the description of the present invention, it should be understood that if terms such as "center", "middle part", "longitudinal", "transverse", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "axial", "radial", "circumferential", etc. are used to indicate the orientation or positional relationship, it is based on the orientation or positional relationship shown in the drawings. It is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, so it should not be construed as a limitation of the present invention. Features defined with "first" and "second" are used to distinguish feature names and do not have special meanings. In addition, features defined with "first" and "second" may explicitly or implicitly include one or more of such features. In the description of the present invention, unless otherwise specified, the meaning of "a plurality" is two or more.

[0034] In the description of the present invention, it should be noted that unless otherwise clearly specified and defined, the terms "mount", "connect", "connection" should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be directly connected or indirectly connected through an intermediate medium, and it can be the communication inside two elements. For those of ordinary skill in the art, the specific meanings of the above terms in the present invention can be understood according to specific situations.

[0035] The present invention relates to a hangar suitable for an unmanned aerial vehicle (UAV). The hangar includes a hangar body, which comprises a base 1100, a lifting drive 1300, a lifting linkage member, and a takeoff and landing platform 1200. The base 1100 is hollow and has an open top. The inner cavity of the base 1100 is arranged as a cylindrical cavity. The lifting drive 1300 is disposed in the base 1100. The lower end of the lifting linkage member is connected to the lifting drive 1300, and the upper end of the lifting linkage member is connected to the takeoff and landing platform 1200. The UAV can take off and land on the takeoff and landing platform 1200. It can be understood that under the drive of the lifting drive 1300, the lifting linkage member and the takeoff and landing platform 1200 rise so that the UAV can land on the takeoff and landing platform 1200. After the UAV takes off, the lifting drive 1300 drives the lifting linkage member and the takeoff and landing platform 1200 to descend.

[0036] Furthermore, the hangar body includes an opening and closing assembly, which comprises an opening and closing linkage member 1401 and at least two opening and closing covers 1402. The opening and closing covers 1402 are hinged to the opening and closing linkage member 1401. Specifically, the lower end of the opening and closing cover 1402 is hinged to the opening and closing linkage member 1401, and each opening and closing cover 1402 can rotate and open / close on the opening and closing linkage member 1401. It can be understood that when the opening and closing covers 1402 are closed, they form a closed cavity for accommodating the takeoff and landing platform 1200, and when the opening and closing covers 1402 are opened, the takeoff and landing platform 1200 is exposed. After the UAV lands, the opening and closing covers 1402 can be used to enclose and store the UAV parked on the takeoff and landing platform 1200, ensuring safety and anti-theft, and can also protect the UAV and the takeoff and landing platform 1200 from wind and rain, avoiding damage to the UAV and the takeoff and landing platform 1200 and reducing maintenance costs.

[0037] Specifically, during the descending process of the lifting linkage member, it can press down the opening and closing linkage member 1401. Taking the contact position between the opening and closing cover 1402 and the open edge of the base 1100 as the fulcrum, the opening and closing cover 1402 can rotate inward to achieve closing. Correspondingly, when the lifting linkage member rises, the pressing on the opening and closing linkage member 1401 is released, and the opening and closing cover 1402 can open outward under the action of its own gravity. It can be understood that during the lifting process of the takeoff and landing platform 1200, the opening and closing of the opening and closing cover 1402 is realized by using the lifting linkage member and the opening and closing linkage member 1401, avoiding the need to separately provide a power mechanism for opening and closing the opening and closing cover 1402, reducing equipment costs, and improving operating efficiency.

[0038] In conjunction with the accompanying drawings, the opening and closing linkage component 1401 is provided with a first through hole 1403, the first through hole 1403 is located in the middle of the opening and closing linkage component 1401, the first through hole 1403 passes through the opening and closing linkage component 1401 in the vertical direction, and the lifting linkage component passes through the first through hole 1403. Further, a downward pressing structure is provided on the side of the lifting linkage component, the downward pressing structure is located above the opening and closing linkage component 1401, and in the process of the lifting linkage component descending, the downward pressing structure is used to press against the upper side of the opening and closing linkage component 1401 or the downward pressing structure is used to press against the upper end edge of the first through hole 1403, so that the opening and closing cover body 1402 is closed.

[0039] As an embodiment, the lifting linkage component includes an inverted first conical structure 1501, the large diameter end of the first conical structure 1501 is connected to the lifting platform 1200, and the diameter of the large diameter end of the first conical structure 1501 is greater than the diameter of the first through hole 1403. It can be understood that during the descent of the lifting linkage component, the side of the first conical structure 1501 is used to abut against the upper edge of the first through hole 1403. In this case, the side of the first conical structure 1501 plays the role of a downward pressing structure.

[0040] Of course, as an alternative, it can also be designed as follows: in some examples, the pressing structure is set as a protruding structure on the side of the lifting linkage component, and the pressing structure is used to resist the upper side of the opening and closing linkage component 1401. In some examples, the pressing structure is set as a shoulder on the side of the lifting linkage component.

[0041] As an embodiment, an upper top structure is provided on the side of the lifting linkage component, and the upper top structure is located below the opening and closing linkage component 1401. During the rising process of the lifting linkage component, the upper top structure is used to abut against the lower side of the opening and closing linkage component 1401 or the upper top structure is used to abut against the lower end edge of the first through hole 1403, so that the opening and closing linkage component 1401 rises, so that the opening and closing cover body 1402 after opening is further opened, so that the lifting and lowering platform 1200 is further exposed.

[0042] Specifically, when the lifting linkage component presses down the opening and closing linkage component 1401 and the opening and closing cover 1402 remains closed, the lifting linkage component rises, and the pressing structure gradually releases the pressing restriction on the opening and closing linkage component 1401, and the opening and closing cover 1402 gradually opens outward under the action of its own gravity. As the lifting linkage component further rises, the upper structure presses against the opening and closing linkage component 1401 from below, and the opening and closing linkage component 1401 rises with the lifting linkage component. At this time, the opening and closing cover 1402 can be further opened, expanding the opening range, so that the landing platform 1200 is fully exposed.

[0043] In some examples, the lifting linkage member includes a second conical structure 1502. The small-diameter end of the first conical structure 1501 is connected to the small-diameter end of the second conical structure 1502. Specifically, the small-diameter ends of the first conical structure 1501 and the second conical structure 1502 are connected and fixed by a threaded structure. Further, the large-diameter end of the second conical structure 1502 is connected to the lifting driver 1300, and the diameter of the large-diameter end of the second conical structure 1502 is larger than the diameter of the first through-hole 1403. It can be understood that during the rising process of the lifting linkage member, the side surface of the second conical structure 1502 is used to abut against the lower edge of the first through-hole 1403. In this case, the side surface of the second conical structure 1502 functions as an upward pushing structure.

[0044] Of course, as an alternative solution, it can also be designed as follows: In some examples, the upward pushing structure is provided as a protruding structure on the side surface of the lifting linkage member, and the upward pushing structure is used to abut against the lower side surface of the opening and closing linkage member 1401. In some examples, the upward pushing structure is provided as a shoulder on the side surface of the lifting linkage member.

[0045] As an implementation manner, it is designed that the outer side surface of the opening and closing cover 1402 has a convex curved surface, and the curved surface contacts the inner wall of the base 1100 or the curved surface contacts the edge of the open end of the base 1100, which can reduce the contact area between the opening and closing cover 1402 and the base 1100, thereby reducing the frictional force between the outer side surface of the opening and closing cover 1402 and the base 1100. And it can make the center of gravity of the opening and closing cover 1402 shift outward, making it more convenient for the opening and closing cover 1402 to open outward.

[0046] Specifically, the opening and closing cover 1402 bulges outward. On the one hand, it can form a curved surface on the outer side surface, and on the other hand, it can expand the volume of the closed cavity formed by the closing of the hangar body.

[0047] In some examples, the opening and closing cover 1402 is provided as a petal-shaped structure. Combining with the attached drawings, the opening and closing cover 1402 is small at the top and large at the bottom and bulges outward. Therefore, the center of gravity of the opening and closing cover 1402 is at a position below and outside. After the downward pressing structure releases the downward pressure on the opening and closing linkage member 1401, the opening and closing cover 1402 can be easily rotated and opened outward.

[0048] Further, to avoid the corner of the opening and closing linkage member 1401 from interfering with the rotation of the opening and closing cover 1402, the corner of the opening and closing linkage member 1401 is provided as a rounded corner or a chamfer. In some examples, a sector plug 1407 is provided at the corner of the opening and closing linkage member 1401. The sector plug 1407 is fixedly installed on the opening and closing linkage member 1401 by screws to form a rounded corner or a chamfer.

[0049] It can be understood that the hangar body includes a controller for manipulating the operation of the hangar body. Specifically, the controller is communicatively connected to the lifting drive 1300, and the controller sends a signal to the lifting drive 1300 to start or stop it. In some examples, the controller is connected to the base 1100. Specifically, the controller is connected to the inner side surface of the base 1100. Further, a gasket is provided between the controller and the inner side surface of the base 1100, and the gasket is made of a thermally conductive silicone grease material to facilitate heat conduction and dissipation.

[0050] In some examples, the controller is connected to a GPS antenna 1701. With reference to the drawings, the GPS antenna 1701 is provided on the outer side surface of the base 1100.

[0051] As an implementation manner, the hangar body includes a data transmission component communicatively connected to the controller. The data transmission component can receive and send signals. Specifically, the operator sends a signal to the data transmission component through a terminal. After the data transmission component learns the instruction, it sends a signal to the controller. In some examples, the data transmission component is connected to the base 1100. Specifically, the data transmission component is connected to the inner side surface of the base 1100. Further, a gasket is provided between the data transmission component and the inner side surface of the base 1100, and the gasket is made of a thermally conductive silicone grease material to facilitate heat conduction and dissipation.

[0052] In some examples, the data transmission component is provided with a data transmission antenna 1702. With reference to the drawings, the data transmission antenna 1702 is provided on the outer side surface of the base 1100.

[0053] When the UAV needs to land, the operator sends a signal to open the hangar body to the data transmission component through the terminal. After the data transmission component learns the instruction, it sends a signal to start the lifting drive 1300 to the controller. The lifting drive 1300 drives the landing platform 1200 to rise, and the opening and closing cover 1402 opens. After the UAV takes off or when the UAV needs to be stored enclosed, the operator sends a signal to close the hangar body through the terminal. After the signal is processed by the data transmission component and the controller, the lifting drive 1300 drives the landing platform 1200 to descend, and the opening and closing cover 1402 closes.

[0054] As an implementation manner, the landing platform 1200 is provided with a wireless charging component 1201 so that the UAV can be charged after landing. Specifically, the wireless charging component 1201 is provided inside the landing platform 1200, and the wireless charging component 1201 is set as a wireless charging coil.

[0055] With reference to the drawings, the landing platform 1200 includes a bottom plate 1202 and a cover plate 1203. The wireless charging component 1201 is provided on the bottom plate 1202, and the cover plate 1203 is provided on the upper side of the bottom plate 1202. In some examples, the cover plate 1203 is made of a plastic material.

[0056] It can be understood that the lower side of the bottom plate 1202 is connected to the upper end of the lifting linkage component. Specifically, a flange is provided at the upper end of the first conical structure 1501, and the bottom plate 1202 is installed with the flange of the first conical structure 1501 through a plurality of bolts or screws.

[0057] As an implementation manner, identification marks are provided on the surface of the landing platform 1200. In combination with the attached drawings, identification marks are provided on the upper side of the cover plate 1203. It can be understood that before the drone lands, the identification marks are read to accurately land on the landing platform 1200.

[0058] Specifically, the identification mark is set as an identification code, and the identification code is printed on the upper side of the cover plate 1203. The identification code is a barcode or a two-dimensional code. As an alternative solution, the identification mark can also be designed as an indicative graphic. It can be understood that the drone is provided with a camera, and the drone realizes autonomous landing by reading the identification code or image recognition.

[0059] As an implementation manner, the opening and closing cover 1402 includes a cover support structure 1404, a lighting component 1405, and a transparent cover 1406. The cover support structure 1404 is hinged to the opening and closing linkage component 1401, and the transparent cover 1406 covers the lighting component 1405 and is connected to the cover support structure 1404. It can be understood that after the hangar body is closed, it can be used for lighting.

[0060] In combination with the attached drawings, both the cover support structure 1404 and the transparent cover 1406 arch outwards. The cover support structure 1404 and the transparent cover 1406 are respectively set as structures similar to petals. The lighting component 1405 includes at least one light strip. Specifically, the light strip is set as an LED light strip, and the lighting component 1405 is attached to the outer side of the cover support structure 1404.

[0061] Furthermore, the cover support structure 1404 is made of piezoelectric ceramic material, and the cover support structure 1404 can convert thermal energy into electrical energy for standby. Specifically, the hangar includes a storage battery, and the storage battery is connected to the cover support structure 1404 through a wire. The heat generated by lighting up the lighting component 1405 can cause the piezoelectric ceramic to generate electrical energy, and the electrical energy is stored in the storage battery.

[0062] In some examples, it can also be alternatively designed as: the opening and closing cover 1402 includes a cover support structure 1404 and a solar cover. The cover support structure 1404 is hinged to the opening and closing linkage component 1401, and the solar cover is arranged on the outer side of the cover support structure 1404. It can be understood that the solar cover can store electricity for the storage battery and generate electricity using solar energy.

[0063] Of course, as an alternative solution, in some examples, it can also be designed that: the partial opening and closing cover 1402 includes a cover support structure 1404, a light-emitting component 1405, and a transparent cover 1406. The partial opening and closing cover 1402 includes a cover support structure 1404 and a solar cover, realizing multiple functions such as night lighting and daytime power generation.

[0064] As an implementation manner, the opening and closing cover 1402 includes a sealing structure 1408. The sealing structure 1408 is set as a sealing strip. Specifically, the sealing structure 1408 is arranged along the edge of the cover support structure 1404. It can be understood that when the hangar body is closed, the gap between two adjacent opening and closing covers 1402 is filled by the sealing structure 1408 to ensure the airtightness of the hangar body.

[0065] As an implementation manner, the hangar body includes a support member 1600. One end of the support member 1600 is connected to the base 1100, and the other end is used to connect to the bearing foundation. With reference to the attached drawings, the support member 1600 includes a support rod. The support rod is bent into an L shape so that one end of the support rod supports the base 1100 of the hangar body upward, and a connecting flange for installing the base 1100 is arranged at the end of the support rod.

[0066] Furthermore, the hangar includes columns 2001 as the bearing foundation. The support member 1600 is connected to the columns 2001 through installation members 2002 to set the hangar body at a high place. It can be understood that multiple hangar bodies can be arranged on the columns 2001 to increase the capacity of the hangar and facilitate the takeoff and landing of multiple unmanned aerial vehicles. Furthermore, the installation member 2002 and the column 2001 are detachable. In some examples, the installation member 2002 includes a hoop, which is convenient for installation and disassembly.

[0067] Regarding the bearing foundation, as an alternative solution, a wall can also be used as the bearing foundation. In this case, the support member 1600 can be fixedly installed on the wall using screws or expansion bolts.

[0068] In some examples, a wire routing channel is provided in the column 2001 and the support member 1600, and the storage battery is arranged at the bottom of the column 2001. Of course, as an alternative solution, the storage battery can also be arranged in the base 1100.

[0069] The content of the present invention will be described in detail below with specific embodiments. It should be noted that the following description is only an exemplary illustration and not a specific limitation to the present invention.

[0070] The hangar includes columns 2001 and at least one hangar body. The hangar body is installed on the columns 2001. The hangar body includes a base 1100, a takeoff and landing platform 1200, a lifting drive 1300, a lifting linkage component, and an opening and closing component. The base 1100 is set as an inverted conical barrel, and the base 1100 is connected to the columns 2001 through a support component 1600 and a hoop. The lifting drive 1300 includes an electric telescopic rod, and the top of the electric telescopic rod is connected to the lifting linkage component. A wireless charging component 1201 is provided in the takeoff and landing platform 1200, and the drone can be charged after landing.

[0071] The lifting linkage component includes a first conical structure 1501 and a second conical structure 1502. The first conical structure 1501 is inverted. For the convenience of wiring, the first conical structure 1501 and the second conical structure 1502 are set as hollow conical structures, and the connection between the first conical structure 1501 and the second conical structure 1502 is connected through a hollow threaded part.

[0072] Combined with the attached drawings, the opening and closing component includes an opening and closing linkage component 1401 and four opening and closing covers 1402. The opening and closing linkage component 1401 is set as a rectangular plate, and the lower end of the opening and closing cover 1402 is hinged to the straight edge of the opening and closing linkage component 1401 through a rotating shaft. The opening and closing cover 1402 is set as a petal-shaped structure, simulating the action of petal opening and closing, and the hangar body is used as a bionic intelligent hangar.

[0073] After the hangar body is closed, it can be used as a street lamp, and it can provide lighting at night and generate electricity during the day, realizing multiple functions. Specifically, some of the opening and closing covers 1402 include a cover support structure 1404, a lighting component 1405, a transparent cover 1406, and a sealing structure 1408. Some of the opening and closing covers 1402 include a cover support structure 1404, a solar cover, and a sealing structure 1408.

[0074] In the description of this specification, if there are descriptions of reference terms such as "one embodiment", "some examples", "some embodiments", "schematic embodiments", "examples", "specific examples", or "some examples", it means that the specific features, structures, materials, or characteristics described in connection with the embodiment or example are included in at least one embodiment or example of the present invention. In this specification, the schematic expressions of the above terms do not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials, or characteristics described can be combined in a suitable manner in any one or more embodiments or examples.

[0075] The above has described the embodiments of the present invention in detail in conjunction with the attached drawings, but the present invention is not limited to the above embodiments. Within the scope of knowledge possessed by those of ordinary skill in the art in the technical field, various changes can be made without departing from the gist of the present invention.

[0076] In the description of the present invention, if a comma (,) appears in the patent name, it indicates a "and" relationship, rather than an "or" relationship. For example, if the patent name is "A, B", it means that the content claimed by the present invention is: the technical solution with the subject name A and the technical solution with the subject name B.

Claims

1. A hangar suitable for UAVs, Features: It includes a hangar body, the hangar body includes A hollow base (1100), wherein the top of the base (1100) is open; A take-off and landing platform (1200), on which the drone can take off and land; A lifting drive (1300), wherein the lifting drive (1300) is arranged in the base (1100); a lifting linkage component, wherein the lower end of the lifting linkage component is connected to the lifting drive (1300), and the upper end of the lifting linkage component is connected to the lifting platform (1200), and under the drive of the lifting drive (1300), the lifting linkage component and the lifting platform (1200) can be lifted and lowered; An opening and closing assembly, the opening and closing assembly comprising an opening and closing linkage component (1401) and at least two opening and closing covers (1402), the opening and closing covers (1402) being hinged to the opening and closing linkage component (1401), each of the opening and closing covers (1402) being closed to form a closed cavity for accommodating the landing platform (1200), and each of the opening and closing covers (1402) being opened to expose the landing platform (1200); The opening and closing linkage component (1401) is provided with a first through hole (1403), the lifting linkage component passes through the first through hole (1403), and a side surface of the lifting linkage component is provided with a downward pressing structure. During the process of the lifting linkage component descending, the downward pressing structure is used to press against the upper side surface of the opening and closing linkage component (1401) or the downward pressing structure is used to press against the upper edge of the first through hole (1403). With the contact position between the outer side surface of the opening and closing cover body (1402) and the open portion of the base (1100) as a fulcrum, the opening and closing cover body (1402) can be rotated inwards to achieve closure; The lifting linkage component comprises an inverted first conical structure (1501), the large diameter end of the first conical structure (1501) is connected to the lifting and lowering platform (1200), and when the lifting linkage component is descending, the side surface of the first conical structure (1501) is used to abut against the upper edge of the first through hole (1403); The lifting linkage component comprises a second conical structure (1502), the small diameter end of the first conical structure (1501) is connected to the small diameter end of the second conical structure (1502), the large diameter end of the second conical structure (1502) is connected to the lifting drive (1300), and when the lifting linkage component is lifted, the side surface of the second conical structure (1502) is used to abut against the lower end edge of the first through hole (1403); The opening and closing cover body (1402) comprises a cover body support structure (1404), a light-emitting component (1405) and a transparent cover (1406), wherein the cover body support structure (1404) is hingedly connected to the opening and closing linkage component (1401); and / or the opening and closing cover body (1402) comprises a cover body support structure (1404) and a solar cover.

2. The hangar suitable for unmanned aerial vehicles according to claim 1, Features: The side of the lifting linkage member is provided with an upward pushing structure. During the upward movement of the lifting linkage member, the upward pushing structure is used to abut against the lower side of the opening and closing linkage member (1401) or the upward pushing structure is used to abut against the lower end edge of the first through hole (1403) so as to lift the opening and closing linkage member (1401).

3. The hangar applicable to a drone according to claim 1 or 2, characterized in that: The landing platform (1200) is provided with a wireless charging component (1201).

4. The hangar applicable to a drone according to claim 1, characterized in that: The cover support structure (1404) is made of piezoelectric ceramic material, and the cover support structure (1404) can convert thermal energy into electrical energy for standby.

5. The hangar applicable to a drone according to claim 1 or 2 or 4, characterized in that: The outer side of the opening and closing cover (1402) has a arched curved surface.

6. The hangar applicable to a drone according to claim 5, characterized in that: The opening and closing cover (1402) is arranged in a petal-shaped structure.

7. The hangar applicable to a drone according to claim 1, characterized in that: The hangar includes a column (2001), and at least one hangar body is installed on the column (2001).

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