Unmanned aerial vehicle hangar
By introducing the design of the structure and the drone-centered structure, the vertical stacking and collision problems in drone storage and management are solved, the automatic parking and charging of drones are realized, and the management efficiency and safety are improved.
Patent Information
- Application Number
- CN202423146715.6
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-19
- Publication Date
- 2025-10-28
- Estimated Expiration
- 2034-12-19
AI Technical Summary
How to efficiently store, maintain and manage drones, especially solving the problems of traditional hangars being unable to stack vertically and structural collisions of drones during launch, reduce manual operations and improve the degree of automation.
The system adopts a push-out structure and a drone-centered structure, and utilizes components such as slide rails, stepper motors, synchronous belt drives, and electric push rods to achieve automatic parking and charging of drones, and precise positioning through encoders and Hall switches.
It achieves safe and automated parking and charging of drones, reduces manual intervention, and improves the efficiency and safety of drone management.
Smart Images

Figure CN223479390U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, specifically to a UAV hangar. Background Technology
[0002] The rapid development of drone technology has led to its widespread application in various industries, including logistics, environmental monitoring, security patrols, and agricultural plant protection. However, in practical applications, the efficient storage, maintenance, charging, and management of drones has become a pressing issue. Drone hangars, as crucial infrastructure supporting drone operations, are receiving increasing attention from research and industry.
[0003] A drone hangar is an intelligent system that integrates drone storage, charging, and scheduling management functions. It provides 24 / 7 automated services for drones, reducing human intervention and improving operational efficiency. For example, in logistics and delivery scenarios, a drone hangar enables rapid battery replacement or charging, ensuring high-frequency operation; in environmental monitoring or security patrols, the hangar provides fixed parking points, facilitating continuous mission execution. Therefore, we have designed a drone hangar to provide a solid guarantee for the safe parking and efficient operation of drones. Utility Model Content
[0004] The purpose of this utility model is to provide a drone hangar that provides a space for charging and storing drones, storing drones, and monitoring and controlling the environment in which the drones are located, ensuring drone safety and charging functions.
[0005] The technical solution adopted in this utility model is as follows:
[0006] A drone hangar includes a hangar frame 1. A push-out structure 2 is provided at the bottom of the hangar frame 1. The push-out structure 2 includes slide rails 21 installed on the left and right sides of the hangar frame 1. A parking platform 4 is fixed between the inner rails of the left and right slide rails 21. A drone centering structure 3 is provided on the parking platform 4.
[0007] A platform frame 41 is fixedly installed at the lower edge of the parking platform 4. Mounting plates a37 are fixedly installed on the left and right sides of the parking platform 4. The inner rails of the two slide rails 21 are fixed on the outer sides of the two mounting plates a37 respectively. The outer rails of the two slide rails 21 are fixedly installed on the bottom left and right sides of the hangar frame 1 through corner brackets 28 and mounting plates b27.
[0008] The ejection structure 2 also includes a stepper motor 22 and a drive shaft 23 installed on the bottom rear side inside the hangar frame 1. Bearing seats are provided on both sides of the drive shaft 23. Synchronous pulleys 24 are fixedly installed in the middle and at both ends of the drive shaft 23. The synchronous pulley 24 in the middle of the drive shaft 23 is connected to the output shaft of the stepper motor 22 through a synchronous belt a. The synchronous pulleys 24 at both ends of the drive shaft 23 are connected to the mounting plates a37 on both sides of the parking platform 4 through a synchronous belt b241. A synchronous belt clamping plate 25 is provided at the rear end of the mounting plate a37.
[0009] The right side of the parking platform 4 has a mounting plate a37 with a proximity switch baffle 26 at its rear end, and the right side of the hangar frame 1 has a mounting plate b27 with proximity sensors 29 at both ends.
[0010] The UAV centering structure 3 includes two X-direction motion motors 31, two Y-direction motion motors 32, two X-direction stop bars 33, and two Y-direction stop bars 34. The two X-direction motion motors 31 are symmetrically installed at the left and right ends of the landing platform 4, and the two Y-direction motion motors 32 are symmetrically installed at the front and rear ends of the landing platform 4. Both X-direction motion motors 31 and Y-direction motion motors 32 are identical dual-output shaft motors. The output shafts at both ends of the two dual-output shaft motors are connected to ball screw sets 35 via couplings. The two X-direction stop bars 33 are symmetrically arranged on the front and rear sides of the landing platform 4, and the Y-direction stop bars 34 are symmetrically arranged on the left and right sides of the landing platform 4, with the Y-direction stop bars 34 located above the X-direction stop bars 33. The two ends of the X-direction stop bars 33 are respectively fixed to the nuts of the ball screw sets 35 on the left and right sides, and the two ends of the Y-direction stop bars 34 are respectively fixed to the nuts of the ball screw sets 35 on the front and rear sides.
[0011] The Y-direction stop lever 34 is provided with charging contacts.
[0012] The ball screw assembly 35 has an encoder 36 installed at the end of the screw.
[0013] The hangar frame 1 is hinged to the front end of the hangar door 5 via a hinge. The lower end of the hangar door 5 is hinged to the hangar frame 1. Electric push rods 6 are hinged to the top left and right ends inside the hangar frame 1. The push rod ends of the electric push rods 6 are hinged to the left and right ends of the hangar door 5.
[0014] The hangar frame 1 is equipped with casters at the four corners of its bottom.
[0015] In summary, due to the adoption of the above technical solution, the beneficial effects of this utility model are:
[0016] This invention solves the problem of traditional hangars' inability to vertically stack drones by incorporating a push-out structure. Simultaneously, by setting a drone-centered structure, it prevents the drone's structural components from colliding with the hangar frame during the push-out process, reducing manual operation, increasing automation, and ensuring drone safety. In summary, this invention features a novel structure, diverse functions, ensures drone safety, and is easy to promote and use. Attached Figure Description
[0017] Figure 1 This is a schematic diagram of the structure of this utility model;
[0018] Figure 2 This is a top view of the central structure and landing platform of the UAV of this utility model;
[0019] Figure 3 This is a schematic diagram of the launching structure and the central structure of the UAV in this utility model;
[0020] Figure 4 for Figure 3 A magnified view of a portion at point A;
[0021] Figure 5 This is a diagram showing the application state of this utility model;
[0022] The diagram shows: 1. Hangar frame; 2. Launch structure; 3. UAV centering structure; 4. Parking platform; 5. Hangar door; 6. Electric push rod; 21. Slide rail; 22. Stepper motor; 23. Drive shaft; 24. Synchronous pulley; 25. Synchronous belt clamping plate; 26. Proximity switch b; 27. Mounting plate b; 28. Angle mount; 29. Proximity sensor; 31. X-direction motion motor; 32. Y-direction motion motor; 33. X-direction stop bar; 34. Y-direction stop bar; 35. Ball screw assembly; 36. Encoder; 37. Mounting plate a; 38. Charging contact; 41. Platform frame. Detailed Implementation
[0023] To make the objectives, technical solutions, and advantages of the embodiments of this utility model clearer, the technical solutions of the embodiments of this utility model will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of this utility model, and not all embodiments. The components of the embodiments of this utility model described and shown in the accompanying drawings can generally be arranged and designed in various different configurations.
[0024] Therefore, the following detailed description of the embodiments of the present invention provided in the accompanying drawings is not intended to limit the scope of the claimed invention, but merely to illustrate selected embodiments of the invention. All other embodiments obtained by those skilled in the art based on the embodiments of the present invention without inventive effort are within the scope of protection of the present invention.
[0025] Example
[0026] like Figure 1-5 This embodiment provides a drone hangar, including a hangar frame 1. Universal wheels are installed at the four corners of the bottom of the hangar frame 1. An ejection structure 2 is provided at the bottom of the hangar frame 1. The ejection structure 2 includes slide rails 21 installed on the left and right sides inside the hangar frame 1. A parking platform 4 is fixed between the inner rails of the left and right slide rails 21. A drone centering structure 3 is provided on the parking platform 4.
[0027] The lower side edge of the parking platform 4 is fixed with a platform frame 41 by bolts. The left and right sides of the parking platform 4 are fixed with mounting plates a37 by bolts. The mounting plates a37 are fixed to the platform frame 41 by bolts. The inner rails of the two slide rails 21 are fixed to the outer sides of the two mounting plates a37 respectively. The outer rails of the two slide rails 21 are fixed to the bottom left and right sides of the hangar frame 1 by corner brackets 28 and mounting plates b27.
[0028] The ejection structure 2 also includes a stepper motor 22 and a drive shaft 23 installed at the bottom rear side inside the hangar frame 1. Bearing seats are provided on both sides of the drive shaft 23. Synchronous pulleys 24 are fixedly installed in the middle and at both ends of the drive shaft 23. The synchronous pulley 24 in the middle of the drive shaft 23 is connected to the output shaft of the stepper motor 22 via a synchronous belt a, thereby causing the stepper motor 22 to drive the drive shaft 23 to rotate. The synchronous pulleys 24 at both ends of the drive shaft 23 are connected to mounting plates a37 on both sides of the parking platform 4 via synchronous belts b241. A synchronous belt clamping plate 25 for connecting the synchronous belt b241 is provided at the rear end of the mounting plate a37. During the rotation of the synchronous pulleys at both ends of the drive shaft 23, the meshing synchronous belt b241 will drive the mounting plate a37 and the parking platform 4 fixed on the mounting plate a37 to move back and forth in the front-rear direction. A driven synchronous pulley of the synchronous belt b241 is provided on the lower side of the front end of the mounting plate b27.
[0029] A proximity switch baffle 26 is installed at the rear end of the mounting plate a37 on the right side of the parking platform 4, and proximity sensors 29 are installed at both ends of the mounting plate b27 on the right side of the hangar frame 1. When the proximity switch baffle 26 approaches the proximity sensor 29, it will control the stepper motor 22 to stop rotating.
[0030] The UAV centering structure 3 includes two X-direction motion motors 31, two Y-direction motion motors 32, two X-direction stop bars 33, and two Y-direction stop bars 34. The two X-direction motion motors 31 are symmetrically installed at the left and right ends of the landing platform 4, and the two Y-direction motion motors 32 are symmetrically installed at the front and rear ends of the landing platform 4. Both X-direction motion motors 31 and Y-direction motion motors 32 are identical dual-output shaft motors. The output shafts at both ends of the two dual-output shaft motors are connected to ball screw sets 35 via couplings. The two X-direction stop bars 33 are symmetrically arranged on the front and rear sides of the landing platform 4, and the Y-direction stop bars 34 are symmetrically arranged on the left and right sides of the landing platform 4, with the Y-direction stop bars 34 located above the X-direction stop bars 33. The two ends of the X-direction stop bars 33 are respectively fixed to the nuts of the ball screw sets 35 on the left and right sides, and the two ends of the Y-direction stop bars 34 are respectively fixed to the nuts of the ball screw sets 35 on the front and rear sides.
[0031] The Y-direction stop lever 34 is provided with a charging contact 38. The charging contact can make contact with the contact of a specific drone modification part to complete the charging of the drone.
[0032] The ball screw assembly 35 has an encoder 36 installed at the end of the screw. When the motor rotates, driving the screw to rotate, the encoder rotates synchronously to record the rotation position. When the set position is reached, the motor stops rotating.
[0033] The hangar frame 1 has a hangar door 5 hinged to its front end. The lower end of the hangar door 5 is hinged to the hangar frame 1. Electric push rods 6 are hinged to the top left and right ends of the hangar frame 1, with the push rod ends of the electric push rods 6 hinged to the left and right ends of the hangar door 5. When the extension structure 2 retracts the UAV from the parking platform 4 into the hangar frame 1, the electric push rods 6 rotate the hangar door 5, thereby closing the hangar door 5.
[0034] The working principle of this utility model is as follows: the hangar frame supports the entire system. The push-out structure is completed using linear slide rails, stepper motors, and synchronous belt drives. The stepper motor drives the drive shaft to rotate, and synchronous pulleys are installed at both ends of the drive shaft. Power is transmitted to the parking platform through the synchronous belt. The parking platform is fixed on the linear slide rails, allowing the parking platform to move back and forth in the horizontal direction. The drone centering structure consists of four centering motors, eight lead screws, four centering stops, and other fixing components. The lead screws, driven by the stepper motors, complete the movement in both the X and Y axes to achieve the centering operation of the drone. In addition, charging contacts are installed on the two centering stops on the X-axis, which can contact the contacts of specific drone modification parts to complete the charging of the drone. The drone centering structure ensures that the various structural components of the drone do not collide with the hangar frame when the push-out structure retracts the drone into the hangar. The hangar door is opened and closed by an electric push rod. The electric push rod can retract back and forth under the action of a controller, causing the door to rotate. Hall switches are installed before and after the ejection structure. When the ejection structure is extended to the set position, the Hall switch is triggered to stop it. Similarly, when the ejection structure is retracted to the designated position, the Hall switch is triggered to stop it in place. The UAV centering structure uses an encoder to determine the position of the centering push rod. When the motor rotates, the encoder rotates synchronously to record the rotation position. When the set position is reached, the motor stops rotating.
Claims
1. A hangar for unmanned aerial vehicles (UAVs), characterized in that, The system includes a hangar frame (1), and a push-out structure (2) is provided at the bottom of the hangar frame (1). The push-out structure (2) includes slide rails (21) installed on the left and right sides of the hangar frame (1). A parking platform (4) is fixed between the inner rails of the left and right slide rails (21). A UAV centering structure (3) is provided on the parking platform (4).
2. The unmanned aerial vehicle hangar according to claim 1, characterized in that: A platform frame (41) is fixedly installed at the lower edge of the parking platform (4). Mounting plates a (37) are fixedly installed on the left and right sides of the parking platform (4). The inner rails of the two slide rails (21) are fixed on the outer sides of the two mounting plates a (37). The outer rails of the two slide rails (21) are fixedly installed on the bottom left and right sides of the hangar frame (1) through corner brackets (28) and mounting plates b (27).
3. The unmanned aerial vehicle hangar according to claim 2, characterized in that: The ejection structure (2) also includes a stepper motor (22) and a drive shaft (23) installed on the bottom rear side of the hangar frame (1). Bearing seats are provided on both sides of the drive shaft (23). Synchronous pulleys (24) are fixedly installed in the middle and at both ends of the drive shaft (23). The synchronous pulley (24) in the middle of the drive shaft (23) is connected to the output shaft of the stepper motor (22) through a synchronous belt a. The synchronous pulleys (24) at both ends of the drive shaft (23) are connected to the mounting plates a (37) on both sides of the parking platform (4) through a synchronous belt b (241). A synchronous belt clamping plate (25) is provided at the rear end of the mounting plate a (37).
4. The unmanned aerial vehicle hangar according to claim 3, characterized in that: The mounting plate a (37) on the right side of the parking platform (4) is equipped with a proximity switch baffle (26) at the rear end, and the mounting plate b (27) on the right side of the hangar frame (1) is equipped with proximity sensors (29) at both ends.
5. A drone hangar according to claim 1, characterized in that: The UAV central structure (3) includes two X-direction motion motors (31), two Y-direction motion motors (32), two X-direction stop bars (33), and two Y-direction stop bars (34). The two X-direction motion motors (31) are symmetrically installed at the left and right ends of the landing platform (4), and the two Y-direction motion motors (32) are symmetrically installed at the front and rear ends of the landing platform (4). The X-direction motion motors (31) and Y-direction motion motors (32) are all the same dual-output shaft motors. The output shafts at both ends of the two dual-output shaft motors are... The output shaft is connected to the ball screw assembly (35) via a coupling. Two X-direction stop rods (33) are symmetrically arranged on the front and rear sides of the stopping platform (4), and Y-direction stop rods (34) are symmetrically arranged on the left and right sides of the stopping platform (4). The Y-direction stop rods (34) are located above the X-direction stop rods (33). The two ends of the X-direction stop rods (33) are respectively fixed to the nuts of the ball screw assemblies (35) on the left and right sides, and the two ends of the Y-direction stop rods (34) are respectively fixed to the nuts of the ball screw assemblies (35) on the front and rear sides.
6. A drone hangar according to claim 5, characterized in that: Charging contacts are provided on the Y-direction stop (34).
7. A drone hangar according to claim 5, characterized in that: The ball screw assembly (35) has an encoder (36) installed at the screw end.
8. A drone hangar according to claim 1, characterized in that: The front end of the hangar frame (1) is hinged to the hangar door (5), the lower end of the hangar door (5) is hinged to the hangar frame (1), and electric push rods (6) are hinged to the top left and right ends inside the hangar frame (1). The push rod ends of the electric push rods (6) are hinged to the left and right ends of the hangar door (5).
9. A drone hangar according to claim 1, characterized in that: The hangar frame (1) is equipped with casters at the four corners of its bottom.