An unmanned aerial vehicle hangar with automatic induction opening function

Abstract

The utility model belongs to the technical field of unmanned plane hangar, disclose an unmanned plane hangar of automatic response opening function, including hangar main part and a pair of top cap, the bottom both sides of hangar main part are installed with a pair of deceleration double shaft motor, and the both sides of hangar main part are installed with the shaft of two output ends of deceleration double shaft motor, and the one end of shaft penetrates and is installed with transmission rod in one side of hangar main part, and the other end of transmission rod is fixedly connected with the one side of top cap, and the opposite side of a pair of top cap is equipped with through groove, and the one side of one of through groove is installed with fan, and the position of one side outer wall of a pair of top cap is installed with a pair of mounting blocks near through groove, and the both sides of through groove are rotatably connected with a pair of electric telescopic rod in the one side outer wall of top cap, and the other end of a pair of electric telescopic rod is rotatably connected with the one side lower end of cover plate. The device simple and reasonable in structure, novel in design, easy to operate, has higher practicality, is convenient for extensive use.

Description

Technical Field

[0001] This utility model belongs to the field of drone hangar technology, and more specifically, it relates to a drone hangar with automatic sensing and opening function. Background Technology

[0002] Drone hangars are facilities specifically designed for storing and protecting drones. They are typically equipped with automated systems such as automatic sensor-activated opening, intelligent management, and environmental control. Drone hangars improve drone operating efficiency, facilitate maintenance and management, and are widely used in fields such as delivery, agricultural monitoring, and inspection.

[0003] Currently, when some drone hangars encounter rainy weather, after the drones return to the hangar and the top cover is retracted, moisture remains inside the hangar. Because the top cover is retracted, this residual moisture cannot evaporate to the outside, leading to corrosion and rust on the drones and internal hangar parts, which seriously affects the service life of the drones and hangars.

[0004] Therefore, in view of this, we will study and improve the existing structure and its shortcomings, and provide a drone hangar with automatic sensing and opening function, in order to achieve a more practical purpose. Utility Model Content

[0005] To solve the above-mentioned technical problems, this utility model provides a drone hangar with an automatic sensing and opening function, which is achieved by the following specific technical means:

[0006] An automatic sensor-activated drone hangar includes a hangar body and a pair of top covers. A pair of geared dual-axis motors are installed on both sides of the bottom of the hangar body. Each of the two output ends of the geared dual-axis motors has a rotating shaft. One end of each rotating shaft passes through one side of the hangar body and is fitted with a transmission rod. The other end of the transmission rod is fixedly connected to one side of the top cover. Each pair of top covers has a through-slot on opposite sides. A fan is installed on one side of one of the through-slots. A pair of mounting blocks are installed on the outer wall of one side of each pair of top covers near the through-slot. A cover plate is rotatably connected between the mounting blocks via a shaft. A pair of electric telescopic rods are rotatably connected to the outer wall of one side of each top cover on both sides of the through-slot. The other end of each pair of electric telescopic rods is rotatably connected to the lower end of one side of the cover plate.

[0007] Furthermore, a vision sensor is mounted on the upper surface of one of the top covers.

[0008] Furthermore, a temperature and humidity sensor is installed on the inner wall of one of the top covers.

[0009] Furthermore, a controller is installed on the inner wall of the top cover near the temperature and humidity sensor. The controller is electrically connected to the geared dual-axis motor, fan, electric telescopic rod, vision sensor, and temperature and humidity sensor.

[0010] Furthermore, the size of the cover plate is larger than the size of the through groove.

[0011] Furthermore, an isolation net is installed on one side of each of the two through slots.

[0012] Compared with the prior art, the present invention has the following beneficial effects:

[0013] By using temperature and humidity sensors in conjunction with fans, the humidity inside the hangar increases during rainy weather, and the internal heat is also high after the drone has just finished flying. If the temperature and humidity sensors detect that the temperature and humidity inside the hangar are too high, the controller will activate the fans to blow air into the hangar, accelerating airflow. This not only effectively cools the hangar but also dries it out, preventing residual rainwater from causing corrosion and rust on the internal parts and the inner wall of the roof, thus extending its service life.

[0014] By using the electric telescopic rod and the cover plate together, when the fan stops working, the controller will operate the electric telescopic rod to retract. During the extension and retraction of the electric telescopic rod, the cover plate will move towards the through slot, thereby covering the through slot and effectively preventing rainwater or dust from entering the main body of the hangar during idle periods. Attached Figure Description

[0015] Figure 1 This is a three-dimensional schematic diagram of the present invention.

[0016] Figure 2 This is a bottom-view sectional perspective view of the main body of the hangar in this utility model.

[0017] Figure 3 This is a three-dimensional diagram of the unfolded present invention.

[0018] Figure 4 This is a three-dimensional diagram of the unfolded present invention.

[0019] Figure 5 This is a utility model Figure 2 An enlarged diagram of A in the diagram.

[0020] In the diagram, the correspondence between component names and drawing numbers is as follows:

[0021] 1. Hanger main body; 2. Top cover; 201. Through slot; 202. Mounting block; 203. Isolation net; 3. Geared dual-axis motor; 301. Rotating shaft; 302. Transmission rod; 4. Fan; 5. Cover plate; 6. Electric telescopic rod; 7. Vision sensor; 8. Temperature and humidity sensor; 9. Controller. Detailed Implementation

[0022] The embodiments of this utility model will be described in further detail below with reference to the accompanying drawings and examples. The following examples are used to illustrate this utility model, but should not be used to limit the scope of this utility model.

[0023] In the description of this utility model, unless otherwise stated, "a plurality of" means two or more; the terms "upper," "lower," "left," "right," "inner," "outer," "front end," "rear end," "head," "tail," etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings, and are only for the convenience of describing this utility model and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation, and therefore should not be construed as a limitation of this utility model. In addition, the terms "first," "second," "third," etc., are used for descriptive purposes only and should not be construed as indicating or implying relative importance.

[0024] In the description of this utility model, it should be noted that, unless otherwise explicitly specified and limited, the terms "connected" and "linked" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.

[0025] Example:

[0026] As attached Figure 1 To be continued Figure 5 As shown:

[0027] This utility model provides an unmanned aerial vehicle (UAV) hangar with an automatic sensing and opening function, including a hangar body 1 and a pair of top covers 2. The hangar body 1 is prior art, and its internal structure will not be described in detail in this application. A pair of geared dual-axis motors 3 are installed on both sides of the bottom of the hangar body 1. A rotating shaft 301 is installed on each of the two output ends of the geared dual-axis motors 3. One end of the rotating shaft 301 passes through one side of the hangar body 1 and is installed with a transmission rod 302. The other end of the transmission rod 302 is fixedly connected to one side of the top cover 2. Each of the two top covers 2 has a through groove 201 on opposite sides. A fan 4 is installed on one side of one through groove 201, and the other through groove 201 is used for ventilation. A pair of mounting blocks 202 are installed on the outer wall of one side of the two top covers 2 near the through groove 201. A cover plate 5 is rotatably connected between the two mounting blocks 202 via a shaft. A pair of electric telescopic rods 6 are rotatably connected on both sides of the outer wall of one side of the top cover 2 located in the through groove 201. The other end of the pair of electric telescopic rods 6 is rotatably connected to the lower end of one side of the cover plate 5.

[0028] One of the top covers 2 has a vision sensor 7 installed on its upper surface.

[0029] One of the top covers 2 has a temperature and humidity sensor 8 installed on its inner wall.

[0030] Among them, a controller 9 is installed on the inner wall of the top cover 2 near the temperature and humidity sensor 8. The controller 9 is electrically connected to the geared dual-axis motor 3, fan 4, electric telescopic rod 6, vision sensor 7 and temperature and humidity sensor 8. The controller 9, geared dual-axis motor 3, fan 4, electric telescopic rod 6, vision sensor 7 and temperature and humidity sensor 8 are all common models on the market. The controller 9 can not only independently control the opening and closing of these devices, but also coordinate their operation to ensure the efficient operation of the system as a whole.

[0031] The cover plate 5 is larger than the through groove 201. When the fan 4 stops working, the controller 9 will operate the electric telescopic rod 6 to retract. During the extension and retraction of the electric telescopic rod 6, the cover plate 5 will move towards the through groove 201 to cover the through groove 201, effectively preventing rainwater or dust from entering the hangar body 1 during idle periods.

[0032] One side of each pair of through channels 201 is equipped with an isolation net 203, which can effectively prevent insects and leaves from entering the interior of the hangar body 1.

[0033] It should be noted that the device structure and accompanying drawings of this utility model mainly describe the principle of this utility model. In terms of the technical aspects of this design principle, the setting of the power mechanism, power supply system and control system of the device is not fully described. However, under the premise that those skilled in the art understand the principle of the above utility model, the specific details of its power mechanism, power supply system and control system can be clearly understood. The control method in the application document is automatic control through controller 9. The control circuit of controller 9 can be implemented by those skilled in the art through simple programming.

[0034] All standard parts used in this application can be purchased from the market, and can be customized according to the description and drawings. The specific connection methods of each part adopt conventional methods such as bolts, rivets, and welding that are mature in the prior art. The machinery, parts and equipment adopt conventional models in the prior art, and the structure and principle of the components known to those skilled in the art can be known by those skilled in the art through technical manuals or conventional experimental methods.

[0035] The working principle of this embodiment:

[0036] When the drone approaches the hangar body 1, once the vision sensor 7 detects the drone, the controller 9 will activate the geared dual-axis motor 3. The geared dual-axis motor 3 drives the transmission rod 302 to rotate via the rotating shaft 301, thereby causing the top cover 2 to rotate to one side of the hangar body 1. After the drone lands smoothly inside the hangar body 1, the controller will then control the top cover 2 to retract. If it is rainy, the humidity inside the hangar body 1 will increase. At the same time, the internal heat of the drone after its flight will also be high. If the temperature and humidity sensor 8 detects that the temperature and humidity inside the hangar body 1 are too high, the controller 9 will activate the fan 4 to blow air into the hangar body 1, accelerating airflow. This not only effectively cools down the hangar body 1 but also dries it, preventing residual rainwater from causing corrosion and rust on the internal parts of the hangar body 1 and the inner wall of the top cover 2, thus extending its service life.

[0037] The embodiments of this utility model are given for illustrative and descriptive purposes only, and are not intended to be exhaustive or to limit the utility model to the forms disclosed. Many modifications and variations will be apparent to those skilled in the art. The embodiments were chosen and described in order to better illustrate the principles and practical applications of this utility model, and to enable those skilled in the art to understand this utility model and design various embodiments with various modifications suitable for a particular purpose.

Claims

1. An unmanned aerial vehicle (UAV) hangar with an automatic sensing and opening function, comprising a hangar body (1) and a pair of top covers (2), wherein a pair of geared dual-axis motors (3) are installed on both sides of the bottom of the hangar body (1), and each of the two output ends of the geared dual-axis motors (3) is equipped with a rotating shaft (301), one end of the rotating shaft (301) penetrates one side of the hangar body (1) and is equipped with a transmission rod (302), and the other end of the transmission rod (302) is fixedly connected to one side of the top cover (2), characterized in that: Each of the two top covers (2) has a through groove (201) on one side. A fan (4) is installed on one side of one of the through grooves (201). A pair of mounting blocks (202) are installed on the outer wall of one side of the two top covers (2) near the through groove (201). A cover plate (5) is rotatably connected between the two mounting blocks (202) via a shaft. A pair of electric telescopic rods (6) are rotatably connected on both sides of the outer wall of one side of the top cover (2) located in the through groove (201). The other end of the pair of electric telescopic rods (6) is rotatably connected to the lower end of one side of the cover plate (5).

2. The drone hangar with automatic sensor-activated opening function as described in claim 1, characterized in that: A vision sensor (7) is mounted on the upper surface of one of the top covers (2).

3. The drone hangar with automatic sensor-activated opening function as described in claim 2, characterized in that: A temperature and humidity sensor (8) is installed on the inner wall of one of the top covers (2).

4. The drone hangar with automatic sensor-activated opening function as described in claim 3, characterized in that: A controller (9) is installed on the inner wall of the top cover (2) near the temperature and humidity sensor (8). The controller (9) is electrically connected to the geared dual-axis motor (3), fan (4), electric telescopic rod (6), vision sensor (7) and temperature and humidity sensor (8).

5. The drone hangar with automatic sensor-activated opening function as described in claim 1, characterized in that: The size of the cover plate (5) is larger than the size of the through groove (201).

6. The drone hangar with automatic sensor-activated opening function as described in claim 1, characterized in that: An isolation net (203) is installed on one side of each of the two through channels (201).

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