A drone hangar for parking drone fleets

By designing drone hangars with shutdown, collecting and lifting equipment, the problem of insufficient space utilization of drone hangars is solved, and the stable and efficient three-dimensional parking of drone groups is achieved to adapt to complex deployment environments.

CN120191546BActive Publication Date: 2025-08-15ZHANGZHOU SHIHUI ELECTRONIC TECH CO LTD
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Patent Information

Application Number
CN202510671213.5
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2025-05-23
Publication Date
2025-08-15
Estimated Expiration
2045-05-23

AI Technical Summary

Technical Problem

The existing drone hangars have shortcomings in space utilization, making it difficult to efficiently support the centralized parking of drone groups, especially in space-constrained environments, and the area of the land has increased significantly, and there is a lack of three-dimensional parking solutions.

Method used

A drone hangar including a shutdown mechanism, a closing mechanism and a lifting equipment is designed. The shutdown mechanism realizes stable parking and storage of the drone. The closing mechanism controls the motion state of the shutdown mechanism, and the lifting equipment changes the height position of the apron and uses three-dimensional space for multi-layer parking.

Benefits of technology

It has achieved stable and efficient space parking of drone groups, improved drone capacity within a unit area, and adapted to complex deployment environments.

✦ Generated by Eureka AI based on patent content.

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Abstract

The present invention discloses a drone hangar for parking a drone swarm. The present invention relates to the technical field of drones, and comprises a chassis, and a track groove fixedly connected to the inner wall of the chassis; a parking mechanism, which is used to place the drones. By setting the parking mechanism, the drone swarm can be parked, so that the drones after completing the flight mission can be parked on the upper surface of the parking mechanism, and then the drones can be stored in the inner cavity of the chassis by moving; a folding mechanism, which is used to store the parked drones. By setting the folding mechanism, the movement state of the parking mechanism can be controlled, so that the parking mechanism can be extended from the chassis so that the drones after completing the flight mission can be parked, and at the same time, the parked drones can be stored in the inner cavity of the chassis, so as to achieve the effect of parking the drone swarm by utilizing the three-dimensional vertical space.
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Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicles (UAVs), and in particular to a UAV hangar for parking a group of UAVs. Background Art

[0002] As an important component of the drone system, drone hangars are specialized facilities that provide parking, charging, maintenance, and mission management for drones. Their design must take into account functionality, safety, and environmental adaptability to ensure that drones are effectively protected and efficiently maintained during non-mission periods. Modern drone hangars are typically equipped with intelligent control systems that enable automatic opening and closing, environmental monitoring, energy management, and data transmission. Some high-end hangars also integrate autonomous charging devices to improve operational continuity through wireless charging or robotic arm battery replacement technology. Structurally, the hangars are made of lightweight alloys or composite materials, with windproof, rainproof, lightning-proof, and temperature-controlled properties, making them suitable for complex deployment environments such as outdoor, shipboard, and polar regions.

[0003] Currently, most drone hangars on the market adopt fixed or modular designs. Although they can meet the parking needs of a single drone or a small number of drones, there are still obvious deficiencies in space utilization, making it difficult to efficiently support the small-volume centralized parking of drone swarms. Traditional hangars usually plan parking space based on a single drone, resulting in a bulky overall structure. Especially when multiple drones need to be deployed, the floor area increases significantly, limiting its application in space-constrained environments (such as cities, ships, or field mobile deployments). In addition, the layout design of existing hangars often lacks a three-dimensional parking solution. Drones are mostly arranged in a flat manner, failing to fully utilize vertical space for multi-layer parking, further reducing the drone accommodation capacity per unit area. Summary of the Invention

[0004] To achieve the above objectives, the present invention is implemented through the following technical solutions: A drone hangar for parking a drone fleet, comprising a chassis, and a track groove fixedly connected to the inner wall of the chassis;

[0005] A parking mechanism is used to place drones. By setting up the parking mechanism, a group of drones can be parked so that after completing a flight mission, the drones can be parked on the upper surface of the parking mechanism and then moved to be stored in the inner cavity of the chassis;

[0006] A folding mechanism is used to store the parked drone. By setting up the folding mechanism, the movement state of the parking mechanism can be controlled so that the parking mechanism can be extended from the chassis to park the drone after completing the flight mission, and the parked drone can be stored in the inner cavity of the chassis.

[0007] A lifting device for raising and lowering a plurality of helipads, and a back plate fixedly connected to the outer surface of the lifting device. By setting up the lifting device, the height position of the plurality of helipads can be changed, thereby allowing the helipads with drones parked to be stored in the inner cavity of the chassis, and the helipads without drones parked to be raised and lowered to the outer surface of the chassis;

[0008] The folding mechanism is fixedly connected to the outer side of the chassis, the back plate is fixedly connected to the side of the track groove away from the inner wall of the chassis, and the lifting device is fixedly connected to the inner cavity of the chassis through the back plate;

[0009] The parking mechanism includes a positioning frame and a parking mechanism. The positioning frame is arranged on the outer surface of the chassis. There are several parking mechanisms, and several of the parking mechanisms are movably connected to the inner cavity of the chassis. By setting the positioning frame, the parking mechanism can be limited so that the parking mechanism will not leave the position of the positioning frame and cause the drone to leave the parking position. By setting multiple parking mechanisms, multiple drones can be parked, so that the drone group can be stably parked after completing the flight mission.

[0010] Preferably, the shutdown mechanism also includes a first support rod, which is symmetrically fixedly connected to the outer side of the chassis, and the end of the first support rod is slidably connected to a sliding tube, and the sliding tube is fixedly connected to the upper surface of the positioning frame, and the end of the first support rod away from the chassis is fixedly connected to a spring, and the end of the spring is fixedly connected to the inner wall of the sliding tube.

[0011] Preferably, the shutdown mechanism also includes a second support rod, which is fixedly connected to the outer side of the chassis, and the end of the second support rod away from the chassis is fixedly connected to a blocking plate, and the blocking plate passes through the positioning frame, and the sides of the lower surface of the positioning frame are symmetrically fixedly connected with racks.

[0012] Preferably, a first strong magnetic strip is fixedly connected to the inner wall of the positioning frame, and the parking mechanism includes an air-permeable plate, which is movably connected to the inner cavity of the positioning frame, and the upper surface of the barrier plate of the air-permeable plate is squeezed and adapted, and a second strong magnetic strip is fixedly connected to the lower surface of the air-permeable plate, and the second strong magnetic strip is in contact with the first strong magnetic strip, and a positioning tube is fixedly connected to the side of the air-permeable plate close to the track groove, and a gasket is fixedly connected to the outer surface of the positioning tube.

[0013] Preferably, the folding mechanism includes a first fixing frame, the first fixing frame is fixedly connected to the outer side surface of the chassis, a stepper motor is fixedly connected to the inner wall of the first fixing frame, the output end of the stepper motor is installed with a rotating rod through a coupling, the end of the rotating rod is fixedly connected to a reduction gear set, the outer surface of the rotating rod is fixedly connected to a stirring plate, the outer surface of the rotating rod is sleeved with a connecting box, and the outer shell of the reduction gear set is fixedly connected to the connecting box through a connecting rod.

[0014] Preferably, a first connecting tube passes through the outer surface of the connecting box, a second connecting tube is fixedly connected to the lower surface of the connecting box, an end of the second connecting tube is fixedly connected to a wrapping cover, the wrapping cover is fixedly connected to the outer surface of the chassis, a second fixing frame is fixedly connected to the side of the chassis away from the first fixing frame, a rolling bearing is fixedly connected to the inner wall of the second fixing frame, and a scraping mechanism is provided on the inner ring of the rolling bearing.

[0015] Preferably, the scraping mechanism includes a rotating column, there are two rotating columns, and the two rotating columns are fixedly connected to the inner ring of the rolling bearing and the output end of the reduction gear set respectively. The outer surface of the rotating column is sleeved with a circular gear, and the circular gear is meshed with the rack. The end of the rotating column is fixedly connected to a bent rod, and the outer surface of the bent rod is fixedly connected to a scraping strip, and the scraping strip is frictionally adapted to the lower surface of the air-permeable plate.

[0016] Preferably, the end of the first connecting tube away from the connecting box is fixedly connected to the air box, the lower surface of the air box is fixedly connected to the third fixing bracket, the end of the third fixing bracket is fixedly connected to the outer surface of the chassis, and the air box is penetrated by an air jet on the side close to the back plate, and the outer surface of the air jet is fixedly connected to a sealing ring.

[0017] Preferably, the lifting device includes an elevator, the elevator is fixedly connected to the outer surface of the back plate, a movable end of the elevator is provided with a movable plate, and the outer surface of the movable plate is fixedly connected to the movable plate.

[0018] Preferably, the outer surface of the movable plate passes through a limiting cylinder, the number of the limiting cylinders is several, and the limiting cylinders are distributed in two rows on the outer surface of the movable plate, the limiting cylinder is slidably connected to the inner cavity of the track groove, and the inner wall of the limiting cylinder is fixedly connected with a jet cylinder, the jet cylinder is aligned with the sealing ring, and the positioning cylinder is frictionally adapted to the inner wall of the limiting cylinder.

[0019] The present invention provides a drone hangar for parking drone fleets. It has the following beneficial effects:

[0020] 1. The drone hangar for parking drone swarms can park drone swarms by setting a parking mechanism, so that the drones can be parked on the upper surface of the parking mechanism after completing the flight mission, and then moved to be stored in the inner cavity of the chassis.

[0021] Second, the drone hangar for parking a fleet of drones can control the motion state of the parking mechanism by providing a folding mechanism, so that the parking mechanism can be extended from the chassis so that the drones that have completed their flight missions can be parked, and at the same time, the parked drones can be stored in the inner cavity of the chassis.

[0022] 3. The drone hangar used for parking drone clusters can change the height positions of several helipads by setting up lifting equipment, so that the helipads with parked drones can be stored in the inner cavity of the chassis, and the helipads without parked drones can be raised and lowered to the outer surface of the chassis.

[0023] 4. The drone hangar used for parking drone swarms can limit the parking mechanism by setting a positioning frame, so that the parking mechanism will not leave the position of the positioning frame and cause the drone to leave the parking position. By setting multiple parking mechanisms, multiple drones can be parked, so that the drone swarm can be stably parked after completing the flight mission.

[0024] 5. The drone hangar for parking drone fleets can cooperate with the output end of the reduction gear set by setting a rotating column, so that the rotational force after deceleration of the reduction gear set can drive the rotating column to rotate, and then the circular gear can rotate, and then the rack can drive the positioning frame to move laterally. By setting a bent rod and a scraper, when the rotating column rotates, the bent rod and the scraper can be brought into contact with the lower surface of the air permeable plate, so that the dust on the lower surface can be scraped off. BRIEF DESCRIPTION OF THE DRAWINGS

[0025] Figure 1 This is a schematic diagram of the external structure of a drone hangar for parking a drone fleet according to the present invention;

[0026] Figure 2 This is a rear view of the structure of a drone hangar for parking a drone fleet according to the present invention;

[0027] Figure 3 This is a partial structural schematic diagram of a drone hangar for parking a drone fleet according to the present invention;

[0028] Figure 4 This is a schematic structural diagram of the shutdown mechanism of the present invention;

[0029] Figure 5 Schematic diagram of the cross-sectional structure of the shutdown mechanism of the present invention;

[0030] Figure 6 This is a schematic diagram of the parking mechanism structure of the present invention;

[0031] Figure 7 This is a schematic diagram of the folding mechanism structure of the present invention;

[0032] Figure 8 For the present invention Figure 7 A magnified schematic diagram of the structure in the middle;

[0033] Figure 9 For the present invention Figure 7 A magnified schematic diagram of the structure B in the middle;

[0034] Figure 10 It is a schematic diagram of the partial structure of the folding mechanism of the present invention;

[0035] Figure 11 This is a structural diagram of the lifting device of the present invention;

[0036] Figure 12 It is a schematic diagram of the partial structure of the lifting device of the present invention;

[0037] Figure 13 It is a schematic diagram of the cross-sectional structure of the lifting equipment of the present invention.

[0038] In the figure: 1, chassis; 2, track groove; 3, back plate; 4, parking mechanism; 5, folding mechanism; 6, lifting device; 41, first support rod; 42, sliding tube; 43, spring; 44, positioning frame; 45, rack; 46, first strong magnetic strip; 47, parking mechanism; 48, second support rod; 49, blocking plate; 471, breathable plate; 472, second strong magnetic strip; 473, positioning tube; 474, washer; 51, first fixing frame; 52, stepping motor; 53, rotating rod; 54, connecting rod Connecting box; 55. First connecting pipe; 56. Stirring plate; 57. Second connecting pipe; 58. Wrapping cover; 59. Scraping mechanism; 510. Reduction gear set; 511. Second fixed frame; 512. Rolling bearing; 513. Third fixed frame; 514. Air box; 515. Jet port; 516. Sealing ring; 591. Rotating column; 592. Circular gear; 593. Bending rod; 594. Scraping strip; 61. Lifter; 62. Moving plate; 63. Movable plate; 64. Limiting cylinder; 65. Jet cylinder. DETAILED DESCRIPTION

[0039] The present invention will be described in further detail below with reference to the accompanying drawings and specific embodiments. The embodiments of the present invention are provided for purposes of illustration and description and are not intended to be exhaustive or to limit the invention to the disclosed forms. Many modifications and variations will be apparent to those skilled in the art. The embodiments are chosen and described to better illustrate the principles of the invention and its practical application, and to enable those skilled in the art to understand the invention and design various embodiments with various modifications suitable for specific applications.

[0040] like Figures 1-13 As shown, the present invention provides a technical solution: a drone hangar for parking a drone fleet, comprising a chassis 1, and a track groove 2 fixedly connected to the inner wall of the chassis 1;

[0041] A parking mechanism 4 is used to place drones. By setting up the parking mechanism 4, a group of drones can be parked, so that after completing a flight mission, the drones can be parked on the upper surface of the parking mechanism 4 and then moved to be stored in the inner cavity of the chassis 1;

[0042] A folding mechanism 5 is used to store the parked drone. The folding mechanism 5 can control the movement state of the parking mechanism 4, so that the parking mechanism 4 can be extended from the chassis 1 to park the drone after completing the flight mission, and the parked drone can be stored in the inner cavity of the chassis 1.

[0043] A lifting device 6 is used to lift and lower multiple landing pads, and a back panel 3 is fixedly connected to the outer surface of the lifting device 6. By setting up the lifting device 6, the height positions of multiple landing pads can be changed, thereby allowing the landing pads with drones parked to be stored in the inner cavity of the chassis 1, while the landing pads without drones parked can be raised and lowered to the outer surface of the chassis 1;

[0044] The folding mechanism 5 is fixedly connected to the outer side of the chassis 1, the back plate 3 is fixedly connected to the side of the track groove 2 away from the inner wall of the chassis 1, and the lifting device 6 is fixedly connected to the inner cavity of the chassis 1 through the back plate 3;

[0045] The parking mechanism 4 includes a positioning frame 44 and a parking mechanism 47. The positioning frame 44 is arranged on the outer surface of the chassis 1. The number of the parking mechanisms 47 is several, and several of the parking mechanisms 47 are movably connected to the inner cavity of the chassis 1. By setting the positioning frame 44, the parking mechanism 47 can be limited so that the parking mechanism 47 will not leave the position of the positioning frame 44 and cause the drone to leave the parking position. By setting multiple parking mechanisms 47, multiple drones can be parked, so that the drone group can be stably parked after completing the flight mission.

[0046] The shutdown mechanism 4 also includes a first support rod 41, which is symmetrically fixedly connected to the outer side of the chassis 1, and the end of the first support rod 41 is slidably connected to a sliding tube 42, and the sliding tube 42 is fixedly connected to the upper surface of the positioning frame 44. The end of the first support rod 41 away from the chassis 1 is fixedly connected to a spring 43, and the end of the spring 43 is fixedly connected to the inner wall of the sliding tube 42. By setting the first support rod 41, the sliding tube 42 can be limited so that the sliding tube 42 can produce stable movement on the outer surface of the first support rod 41, and then when the positioning frame 44 moves laterally, the sliding tube 42 can move laterally on the outer surface of the first support rod 41. By setting the spring 43, the spring 43 can store elastic potential energy after the sliding tube 42 moves laterally, and then rebound and return to its original position later.

[0047] The parking mechanism 4 also includes a second support rod 48, which is fixedly connected to the outer side of the chassis 1. The end of the second support rod 48 away from the chassis 1 is fixedly connected to a blocking plate 49, and the blocking plate 49 passes through the positioning frame 44. The sides of the lower surface of the positioning frame 44 are symmetrically fixedly connected with a rack 45. By arranging the blocking plate 49 and the second support rod 48, when the positioning frame 44 moves laterally and gradually approaches the chassis 1, the blocking plate 49 can gradually pass through the positioning frame 44, so that the blocking plate 49 no longer contacts the parking mechanism 47, and then when the positioning frame 44 is located in the inner cavity of the chassis 1, the parking mechanism 47 can slide into the inner cavity of the chassis 1. By arranging the rack 45, when the folding mechanism 5 is working, it can cooperate with the rack 45, so that the positioning frame 44 can produce lateral movement. The inner wall of the positioning frame 44 is fixedly connected with a first strong magnetic strip 46, and the parking mechanism 47 includes an air breathable plate 471, which is movably connected to the inner cavity of the positioning frame 44, and the upper surface of the barrier plate 49 of the air breathable plate 471 is squeezed and adapted, and the lower surface of the air breathable plate 471 is fixedly connected with a second strong magnetic strip 472, and the second strong magnetic strip 472 is in contact with the first strong magnetic strip 46, and the air breathable plate 471 is fixedly connected with a clamping tube 473 on the side close to the track groove 2, and the outer surface of the clamping tube 473 is fixedly connected with a gasket 474. By setting the first strong magnetic strip 46, it can cooperate with the second strong magnetic strip 472 on the lower surface of the air breathable plate 471, so that the air breathable plate 471 can be positioned together with the positioning frame 44, and by setting the air breathable plate 471, the drone that needs to be parked can be placed.

[0048] The folding mechanism 5 includes a first fixing frame 51, which is fixedly connected to the outer side of the chassis 1. A stepper motor 52 is fixedly connected to the inner wall of the first fixing frame 51. A rotating rod 53 is installed at the output end of the stepper motor 52 through a coupling. The end of the rotating rod 53 is fixedly connected to a reduction gear set 510. The outer surface of the rotating rod 53 is fixedly connected to a stirring plate 56. The outer surface of the rotating rod 53 is sleeved with a connecting box 54. The outer shell of the reduction gear set 510 is connected to the connecting box through the connecting rod. 54 is fixedly connected. By setting the first fixing frame 51, the stepping motor 52 can be supported and fixed, so that the stepping motor 52 can be fixed to the outer surface of the chassis 1. By setting the stepping motor 52, after the power is connected and the switch is turned on, the output end of the stepping motor 52 can rotate, thereby causing the rotating rod 53 to rotate rapidly. By setting the reduction gear set 510, the angular velocity of the rotation of the rotating rod 53 can be slowed down. By setting the stirring plate 56, the stirring plate 56 can be rotated under the action of the rotation of the rotating rod 53. The airflow is generated in the inner cavity of the connection box 54. The outer surface of the connection box 54 is penetrated by a first connection pipe 55. The lower surface of the connection box 54 is fixedly connected to a second connection pipe 57. The end of the second connection pipe 57 is fixedly connected to a wrapping cover 58. The wrapping cover 58 is fixedly connected to the outer surface of the chassis 1. The side of the chassis 1 away from the first fixing frame 51 is fixedly connected to the second fixing frame 511. The inner wall of the second fixing frame 511 is fixedly connected to a rolling bearing 512. The inner ring of the rolling bearing 512 is provided with a A scraping mechanism 59 is provided. By setting a second connecting pipe 57, the wrapping cover 58 can be connected to the connecting box 54, and then when the stirring plate 56 rotates, the air in the inner cavity of the wrapping cover 58 can enter the inner cavity of the connecting box 54 through the second connecting pipe 57. By setting a rolling bearing 512, the scraping mechanism 59 can rotate more stably. By setting the scraping mechanism 59, the dust attached to the lower surface of the air permeable plate 471 can be scraped off when the rotation and the air permeable plate 471 generate lateral movement.

[0049] The scraping mechanism 59 includes a rotating column 591, the number of the rotating columns 591 is two, and the two rotating columns 591 are fixedly connected to the inner ring of the rolling bearing 512 and the output end of the reduction gear set 510, respectively. The outer surface of the rotating column 591 is provided with a circular gear 592, and the circular gear 592 is engaged with the rack 45. The end of the rotating column 591 is fixedly connected to a bent rod 593, and the outer surface of the bent rod 593 is fixedly connected to a scraping strip 594, and the scraping strip 594 is fixedly connected to the lower surface of the air permeable plate 471. Friction adaptation, by setting up a rotating column 591, can cooperate with the output end of the reduction gear set 510, so that the rotational force after the reduction gear set 510 is decelerated can drive the rotating column 591 to rotate, and then the circular gear 592 is rotated, and then the rack 45 can drive the positioning frame 44 to move horizontally. By setting up a bent rod 593 and a scraper 594, when the rotating column 591 rotates, the bent rod 593 and the scraper 594 can be brought into contact with the lower surface of the air permeable plate 471, so that the dust on the lower surface can be scraped off.

[0050] The end of the first connecting pipe 55 away from the connecting box 54 is fixedly connected to the air box 514, and the lower surface of the air box 514 is fixedly connected to the third fixing frame 513, and the end of the third fixing frame 513 is fixedly connected to the outer surface of the chassis 1. The air box 514 is penetrated by an air jet 515 on the side close to the back plate 3, and the outer surface of the air jet 515 is fixedly connected to a sealing ring 516. By setting the air box 514, a plurality of adsorption sponges are provided in the inner cavity of the air box 514, which can adsorb dust in the air entering the inner cavity of the air box 514. By setting the air jet 515 and the sealing ring 516, the purified air in the inner cavity of the air box 514 can be ejected. The lifting device 6 includes a lift 61, and the lift 61 is fixedly connected to the outer surface of the back plate 3. The movable end of the lift 61 is provided with a movable plate 62, and the outer surface of the movable plate 62 is fixedly connected to the movable plate 63. By setting the lift 61, the air can be connected to the power supply and working. When the movable plate 62 at the output end can produce the effect of vertical up and down movement under control, thereby driving the movable plate 63 to produce vertical up and down movement, the outer surface of the movable plate 63 passes through the limiting cylinder 64, the number of the limiting cylinders 64 is several, and the limiting cylinders 64 are distributed in two rows on the outer surface of the movable plate 63, the limiting cylinder 64 is slidably connected to the inner cavity of the track groove 2, and the inner wall of the limiting cylinder 64 is fixedly connected with a jet cylinder 65, which is aligned with the sealing ring 516, and the positioning cylinder 473 is frictionally adapted with the inner wall of the limiting cylinder 64. By setting the limiting cylinder 64 and the jet cylinder 65, it can cooperate with the positioning cylinder 473, thereby enabling the parking mechanism 47 to be connected to the movable plate 63, and then when the movable plate 63 moves up and down, the parking mechanism 47 can produce the effect of vertical up and down movement, and when the sealing ring 516 and the jet port 515 spray gas, the gas can be sprayed through the jet cylinder 65.

[0051] Working principle: During use, when it is necessary to stop the drone group that has completed the flight mission, the operator controls the elevator 61, and makes the movable plate 62 drive the movable plate 63 to move vertically up and down, and aligns the parking mechanism 47 with the positioning frame 44, then stops the work of the elevator 61, and then connects the stepper motor 52 to the power supply and turns on the switch, so that the rotating rod 53 drives the stirring plate 56 to rotate rapidly, and makes the air enter the connecting box 54, and enter the inner cavity of the air box 514 through the first connecting pipe 55, and finally makes the jet port 515 and the sealing ring 516 generate airflow and make the airflow enter the inner cavity of the jet cylinder 65, and finally makes the positioning cylinder 473 leave the range of the limiting cylinder 64 and the jet cylinder 65, and then in the reduction gear Under the deceleration of group 510, the rotating column 591 drives the circular gear 592 to rotate slowly, thereby causing the rack 45 and the positioning frame 44 to move laterally. During the process, due to the attraction of the first strong magnetic strip 46 and the second strong magnetic strip 472, the breathable plate 471 is tightly connected to the positioning frame 44 until the positioning frame 44 and the breathable plate 471 extend out of the chassis 1. After that, the drone can be parked on the upper surface of the breathable plate 471. After parking, control the stepper motor 52 to run in the opposite direction, so that the positioning frame 44 and the breathable plate 471 can re-enter the inner cavity of the chassis 1. Then stop the stepper motor 52 and control the elevator 61, and then control the next parking mechanism 47 to contact the positioning frame 44. Then repeat the above operation to park several drones.

[0052] Obviously, the embodiments described are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field and related fields without making creative efforts should fall within the scope of protection of the present invention. Structures, devices, and operating methods not specifically described and explained in the present invention shall be implemented in accordance with conventional means in the field unless otherwise specified or limited.

Claims

1. A drone hangar for parking drone fleets, characterized in that: include: A chassis (1), and a track groove (2) fixedly connected to the inner wall of the chassis (1); A parking mechanism (4), the parking mechanism (4) is used to place the drone; A folding mechanism (5), the folding mechanism (5) is used to fold the parked drone; A lifting device (6) for lifting a plurality of parking mechanisms (4), and a back plate (3) fixedly connected to an outer surface of the lifting device (6); The folding mechanism (5) is fixedly connected to the outer side of the chassis (1), the back plate (3) is fixedly connected to the side of the track groove (2) away from the inner wall of the chassis (1), and the lifting device (6) is fixedly connected to the inner cavity of the chassis (1) through the back plate (3); The parking mechanism (4) includes a positioning frame (44) and a parking mechanism (47), wherein the positioning frame (44) is arranged on the outer surface of the chassis (1), and the number of the parking mechanisms (47) is several, and the several parking mechanisms (47) are movably connected to the inner cavity of the chassis (1); The folding mechanism (5) comprises a first fixing frame (51), the first fixing frame (51) is fixedly connected to the outer side of the chassis (1), a stepping motor (52) is fixedly connected to the inner wall of the first fixing frame (51), a rotating rod (53) is installed at the output end of the stepping motor (52) through a coupling, the end of the rotating rod (53) is fixedly connected to a reduction gear set (510), the outer surface of the rotating rod (53) is fixedly connected to a stirring plate (56), the outer surface of the rotating rod (53) is sleeved with a connecting box (54), the reduction gear set (510) is fixedly connected to the outer surface of the rotating rod (53), and the outer surface of the rotating rod (53) is sleeved with a connecting box (54). ) is fixedly connected to the connecting box (54) through a connecting rod, a first connecting tube (55) passes through the outer surface of the connecting box (54), a second connecting tube (57) is fixedly connected to the lower surface of the connecting box (54), an end of the second connecting tube (57) is fixedly connected to a wrapping cover (58), the wrapping cover (58) is fixedly connected to the outer surface of the chassis (1), a second fixing frame (511) is fixedly connected to the side of the chassis (1) away from the first fixing frame (51), and a rolling bearing (512) is fixedly connected to the inner wall of the second fixing frame (511).

2. The drone hangar for parking a drone fleet according to claim 1, characterized in that: The stopping mechanism (4) further comprises a first support rod (41), the first support rod (41) being symmetrically fixedly connected to the outer side surface of the chassis (1), the end of the first support rod (41) being slidably connected to a sliding tube (42), the sliding tube (42) being fixedly connected to the upper surface of the positioning frame (44), the end of the first support rod (41) away from the chassis (1) being fixedly connected to a spring (43), the end of the spring (43) being fixedly connected to the inner wall of the sliding tube (42).

3. The drone hangar for parking a drone fleet according to claim 2, characterized in that: The stopping mechanism (4) further comprises a second support rod (48), the second support rod (48) being fixedly connected to the outer side surface of the chassis (1), and a blocking plate (49) being fixedly connected to one end of the second support rod (48) away from the chassis (1), the blocking plate (49) passing through the positioning frame (44), and a rack (45) being symmetrically fixedly connected to the side of the lower surface of the positioning frame (44).

4. The drone hangar for parking a drone fleet according to claim 3, characterized in that: A first strong magnetic strip (46) is fixedly connected to the inner wall of the positioning frame (44), and the parking mechanism (47) includes a breathable plate (471), which is movably connected to the inner cavity of the positioning frame (44), and the upper surface of the blocking plate (49) of the breathable plate (471) is squeezed and adapted, and a second strong magnetic strip (472) is fixedly connected to the lower surface of the breathable plate (471), and the second strong magnetic strip (472) is in contact with the first strong magnetic strip (46), and a locking tube (473) is fixedly connected to the side of the breathable plate (471) close to the track groove (2), and a gasket (474) is fixedly connected to the outer surface of the locking tube (473).

5. The drone hangar for parking a drone fleet according to claim 4, characterized in that: A scraping mechanism (59) is provided at the inner ring of the rolling bearing (512), and the scraping mechanism (59) includes a rotating column (591). The number of the rotating columns (591) is two, and the two rotating columns (591) are fixedly connected to the inner ring of the rolling bearing (512) and the output end of the reduction gear set (510), respectively. The outer surface of the rotating column (591) is provided with a circular gear (592), and the circular gear (592) is engaged with the rack (45). The end of the rotating column (591) is fixedly connected to a bent rod (593), and the outer surface of the bent rod (593) is fixedly connected to a scraping strip (594), and the scraping strip (594) is frictionally adapted to the lower surface of the air permeable plate (471).

6. The drone hangar for parking a drone fleet according to claim 5, characterized in that: One end of the first connecting pipe (55) away from the connecting box (54) is fixedly connected to an air box (514), a lower surface of the air box (514) is fixedly connected to a third fixing frame (513), an end of the third fixing frame (513) is fixedly connected to the outer surface of the chassis (1), a jet port (515) is passed through a side of the air box (514) close to the back plate (3), and a sealing ring (516) is fixedly connected to the outer surface of the jet port (515).

7. The drone hangar for parking a drone fleet according to claim 6, characterized in that: The lifting device (6) comprises a lift (61), the lift (61) being fixedly connected to the outer surface of the back plate (3), a movable plate (62) being provided at the movable end of the lift (61), and a movable plate (63) being fixedly connected to the outer surface of the movable plate (62).

8. The drone hangar for parking a drone fleet according to claim 7, characterized in that: The outer surface of the movable plate (63) passes through a limiting cylinder (64), the number of the limiting cylinders (64) is several, and the limiting cylinders (64) are distributed in two rows on the outer surface of the movable plate (63), the limiting cylinder (64) is slidably connected to the inner cavity of the track groove (2), and the inner wall of the limiting cylinder (64) is fixedly connected with a jet cylinder (65), the jet cylinder (65) is aligned with the sealing ring (516), and the positioning cylinder (473) is frictionally adapted to the inner wall of the limiting cylinder (64).

Citation Information

Patent Citations

  • Unmanned aerial vehicle three-dimensional access equipment

    CN214463057U