A drone hangar that works normally under high temperature conditions

Abstract

The present invention relates to the field of drone technology, and more particularly to a drone hangar capable of operating normally under high-temperature conditions. The hangar comprises a hangar frame and a hangar controller disposed within the hangar frame. Heat insulation panels are fixedly mounted on the sides of the hangar frame. A hangar opening is formed at the upper end of the hangar frame, and a hangar door for opening or closing the hangar opening is disposed on the upper side of the hangar frame. An installation cavity is formed within the hangar frame, and a lifting mechanism is disposed within the installation cavity. A receiving platform is connected to the lifting end of the lifting mechanism. A ventilation device for ventilating the hangar frame and an air conditioner for cooling the installation cavity are disposed within the installation cavity. The hangar controller is capable of maintaining a certain low temperature environment within the drone hangar, ensuring normal operation of the drone hangar under high-temperature conditions.

Description

Technical Field

[0001] The present invention relates to the technical field of unmanned aerial vehicles (UAVs), and in particular to an UAV hangar that operates normally under high temperature conditions. Background Art

[0002] With the rapid development of the internet, drones are finding widespread application in numerous fields across modern society, including forestry, power grids, maritime security, and surveying and mapping. Drones can perform tasks such as reconnaissance, detection, and inspection. However, a single drone operation system still requires extensive personnel support, and these personnel must possess a high level of expertise. This means that a single drone operation system does not achieve true unmanned operation. Therefore, the need for a drone hangar system—a drone operation system that can operate without human intervention—has emerged.

[0003] In recent years, drone hangar systems have gradually gained popularity. These systems integrate automated drone homing, storage, maintenance, and charging functions. The entire drone operation process is controlled by the system itself, eliminating the need for human intervention. Currently, drone hangar systems are primarily used for multi-rotor drones, and most are consumer-grade.

[0004] Conventional drone hangars consist of a hangar frame, within which are located a landing platform, a lifting mechanism, and a power supply. An opening is located at the top of the hangar frame, where a hangar door mechanism is installed. This door controls the opening and closing of the hangar. When the hangar is opened, drones inside can fly out.

[0005] In the existing technology, drone hangars are used to place drones for regular surveys of specific geographical environments. When surveying specific geographical areas in the summer, especially in some desert environments, the maximum temperature in the summer can reach 70 degrees Celsius. At this temperature, some components inside the hangar will melt, making the drone hangar unable to work normally. Summary of the Invention

[0006] (1) Technical problems solved

[0007] In view of the deficiencies of the existing technology, the present invention provides a drone hangar that can operate normally under high temperature conditions, which can control the drone hangar to maintain a certain low temperature environment and ensure that the drone hangar operates normally under high temperature conditions.

[0008] (2) Technical solution

[0009] To achieve the above-mentioned objectives, an embodiment of the present application provides a drone hangar that can operate normally under high temperature conditions, including a hangar frame and a hangar controller arranged in the hangar frame, the sides of the hangar frame are respectively fixedly installed with heat insulation panels; a hangar opening is formed at the upper end of the hangar frame, and a hangar door for opening or closing the hangar opening is arranged on the upper side of the hangar frame; an installation cavity is formed in the hangar frame, a lifting mechanism is arranged in the installation cavity, and the lifting end of the lifting mechanism is connected to a receiving platform; a ventilation device for ventilating with the outside of the hangar frame and an air conditioner for cooling the installation cavity are arranged in the installation cavity.

[0010] Preferably, an annular support ring plate is formed in the middle of the hangar frame, a connecting port is formed in the middle of the support ring plate, and the receiving platform is located above the support ring plate; a drone parking compartment is formed on the side of the support ring plate close to the hangar opening, and an equipment installation compartment is formed on the side of the support ring plate away from the hangar opening; a middle partition plate is provided on the lower side of the receiving platform, and when the receiving platform extends out of the hangar opening, the middle partition plate covers the connecting port; the hangar controller, air conditioner and ventilation device are arranged in the equipment installation compartment.

[0011] Preferably, a plurality of connecting columns are provided on the lower side of the receiving platform, and the other end of the connecting column is fixed to the middle partition plate; the lifting mechanism includes a support sleeve fixedly connected to the lower side of the receiving platform, the lower end of the support sleeve passes through the middle partition plate, and a threaded hole is provided at the end of the support sleeve away from the receiving platform, and a bottom support seat is fixed at the bottom of the equipment installation bin, and a screw rod is rotatably connected to the bottom support seat, and the screw rod is threadedly connected to the threaded hole, and a first motor is provided on the bottom support seat to drive the screw rod to rotate; a vertical guide column is fixed to the side of the support ring plate away from the receiving platform, and a guide hole is provided on the middle partition plate, and the guide column passes through the guide hole.

[0012] Preferably, the hangar door includes a first hatch and a second hatch; sliding rods are provided in parallel on both sides of the hangar frame close to the hangar opening, a fixed seat is provided in the middle of the sliding rod, and the fixed seat is fixedly connected to the hangar frame; sliding seats are fixed on both sides of the first hatch and the second hatch respectively, and the sliding seats are sleeved on the sliding rods, and compression springs are sleeved on the sliding rods and on both sides of the fixed seats, one end of the compression spring abuts the fixed seat, and the other end abuts the sliding seat; a driving mechanism for controlling the closing of the first hatch and the second hatch respectively is provided in the equipment installation compartment.

[0013] Preferably, the driving mechanism includes a mounting plate fixed in the equipment mounting compartment, a second motor is fixed on the mounting plate, a winding drum is fixed on the output shaft of the second motor, and a rope is installed on the winding drum; a sliding hole is opened on the support ring plate, and a fixed pulley is provided on the side of the hangar frame close to the hangar opening; the end of the rope away from the winding drum passes through the sliding hole, and is fixedly connected to the first hatch or the second hatch after passing around the fixed pulley.

[0014] Preferably, an air outlet and an air inlet are provided on the hangar frame and in the equipment installation compartment, a control mechanism for controlling the opening or closing of the air inlet and the air outlet is provided in the equipment installation compartment, a first temperature sensor is provided on the outside of the hangar frame, and a second temperature sensor is provided on the inside of the hangar frame, and when the temperature value detected by the first temperature sensor is less than a set value, the control mechanism opens the air inlet and the air outlet.

[0015] Preferably, a first installation pipe for covering the air inlet and a second installation pipe for covering the air outlet are provided in the equipment installation compartment; the control mechanism opens or closes the first installation pipe and the second installation pipe, and the ventilation device is provided in the first installation pipe and the second installation pipe.

[0016] Preferably, the first mounting pipe and the second mounting pipe are formed with a closed opening at one end close to the equipment mounting bin, and the cross-section of the closed opening is an isosceles trapezoid; the control mechanism includes an electric push rod fixed in the equipment mounting bin, and the piston end of the electric push rod is connected to a closed block, and the closed block is in the shape of a prism, with a smaller area at the end away from the electric push rod and a larger area at the end close to the electric push rod, and a rubber layer is provided on the side wall of the closed block, and the electric push rod controls the closed block to close or open the closed opening.

[0017] Preferably, the ventilation device includes a first filter screen fixed in the first installation pipe, and a dehumidification layer is arranged on the inner side of the first filter screen; a second filter screen is arranged in the second installation pipe, and an exhaust fan is arranged on the side of the second filter screen close to the equipment installation compartment.

[0018] (3) Beneficial effects

[0019] The present invention provides a drone hangar that can operate normally under high temperature conditions. The hangar frame, receiving platform and lifting mechanism are provided, which can allow drones to take off and land during operation. At the same time, through the ventilation device and air conditioner provided on the inner side of the hangar frame, when the external ambient temperature of the hangar is low, the ventilation and heat exchange can be carried out to the inside of the hangar through the ventilation device. When the external ambient temperature is high, the air conditioner provided can cool the environment inside the hangar, so that the temperature inside the hangar is kept low. Through the support ring plate and the middle partition plate provided in the hangar, when the lifting mechanism controls the receiving platform to rise, the drone can take off. During the operation of the drone, the middle partition plate and the support ring plate abut against each other, so that the equipment installation compartment on the lower side of the support ring plate forms a closed environment. In this process, a low-temperature environment can be provided in the equipment installation compartment, so that each device in the drone hangar is always kept in a relatively low temperature environment. When the drone enters the drone hangar, the hangar door closes. After closing, the middle partition plate and the support ring plate separate, allowing the drone parking compartment and the equipment installation compartment to be connected, allowing the drone to remain in a lower temperature environment during storage. BRIEF DESCRIPTION OF THE DRAWINGS

[0020] Figure 1 This is a structural schematic diagram of a UAV hangar that works normally under high temperature conditions according to the present invention;

[0021] Figure 2 for Figure 1 A magnified view of the structure in the middle;

[0022] Figure 3 for Figure 1 A magnified view of the structure in middle B;

[0023] Figure 4 A schematic diagram of a protruding lifting mechanism in a UAV hangar operating normally under high temperature conditions according to the present invention;

[0024] Figure 5 This is a schematic diagram of a protruding ventilation device in a drone hangar operating normally under high temperature conditions according to the present invention.

[0025] In the accompanying drawings:

[0026] 100, hangar frame; 110, hangar opening; 120, support ring plate; 121, connecting port; 122, sliding hole; 130, air outlet; 140, air inlet; 150, first installation pipe; 160, second installation pipe; 161, closed port; 170, drone parking bay; 180, equipment installation bay; 200, hangar door; 210, first hatch; 220, second hatch; 221, sliding seat; 230, sliding rod; 231, fixing seat; 240, compression spring; 300, lifting mechanism; 310, support sleeve; 311, threaded hole; 3 20. Bottom support seat; 330. Screw rod; 340. First motor; 350. Guide column; 400. Receiving platform; 410. Middle partition plate; 420. Connecting column; 500. Ventilation device; 510. First filter; 520. Dehumidification layer; 530. Second filter; 540. Exhaust fan; 600. Air conditioner; 700. Driving mechanism; 710. Mounting plate; 720. Second motor; 730. Winding drum; 740. Rope; 750. Fixed pulley; 800. Control mechanism; 810. Electric push rod; 820. Closing block; 830. Rubber layer. DETAILED DESCRIPTION

[0027] The following will clearly and completely describe the technical solutions in the embodiments of the present invention in conjunction with the accompanying drawings. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0028] Example

[0029] The present invention provides a drone hangar that works normally under high temperature conditions. Figure 1-Figure 5 , including a hangar frame 100 and a hangar controller arranged in the hangar frame 100, and the sides of the hangar frame 100 are respectively fixedly installed with thermal insulation panels; the inside and outside of the hangar frame 100 are isolated by the thermal insulation panels to perform thermal insulation.

[0030] A hangar opening 110 is formed at the upper end of the hangar frame 100, and a hangar door 200 is provided on the upper side of the hangar frame 100 to open or close the hangar opening 110. An installation cavity is formed within the hangar frame 100, and a lifting mechanism 300 is provided within the installation cavity. The lifting end of the lifting mechanism 300 is connected to a receiving platform 400. A ventilation device 500 is provided within the installation cavity to ventilate the outside of the hangar frame 100, and an air conditioner 600 is provided to cool the installation cavity. When operating in a hot environment, the air conditioner 600 cools the installation cavity, maintaining a relatively low temperature environment within the installation cavity, thereby preventing damage to various components within the hangar. Furthermore, when the outside environment is relatively cold, the ventilation device 500 ventilates the installation cavity.

[0031] The hangar frame 100 has an annular support ring plate 120 formed in the middle, with a communication opening 121 formed in the middle. The receiving platform 400 is located above the support ring plate 120. A drone parking compartment 170 is formed on the side of the support ring plate 120 near the hangar entrance 110, and an equipment installation compartment 180 is formed on the side of the support ring plate 120 away from the hangar entrance 110. A central partition plate 410 is provided on the underside of the receiving platform 400. When the receiving platform 400 extends out of the hangar entrance 110, the central partition plate 410 covers the communication opening 121. The hangar controller, air conditioner 600, and ventilation system 500 are located within the equipment installation compartment 180. Through the support ring plate 120 and the suspended central partition plate 410, when a drone is needed, the lifting mechanism 300 controls the receiving platform 400 to rise, extend it out of the hangar entrance 110, and the drone takes off. When the receiving platform 400 extends out of the hangar opening 110, the lower middle partition plate 410 abuts the support ring plate 120, allowing the lower equipment installation compartment 180 to form a relatively closed chamber. Consequently, during use, the equipment installation compartment 180 can maintain a relatively low temperature. When the drone takes off or enters the drone parking compartment 170, the equipment installation compartment 180 can remain in a closed environment. When the drone enters the drone parking compartment 170, the hangar opening 110 is closed via the hangar door 200. At this point, the equipment installation compartment 180 and the drone parking compartment 170 are connected, allowing the drone to be stored at low temperatures.

[0032] A plurality of connecting columns 420 are provided on the lower side of the receiving platform 400 , and the other ends of the connecting columns 420 are fixed to the middle partition plate 410 .

[0033] The lifting mechanism 300 includes a support sleeve 310 fixedly connected to the lower side of the receiving platform 400, the lower end of the support sleeve 310 passes through the middle partition plate 410, and a threaded hole 311 is provided at the end of the support sleeve 310 away from the receiving platform 400. A bottom support seat 320 is fixed at the bottom of the installation bin, and a screw rod 330 is rotatably connected to the bottom support seat 320. The screw rod 330 is threadedly connected to the threaded hole 311, and a first motor 340 is provided on the bottom support seat 320 to drive the screw rod 330 to rotate; wherein the first motor 340 can drive the screw rod 330 to rotate by gear transmission, or can control the rotation of the screw rod 330 by chain or belt transmission, which is not limited here.

[0034] A vertical guide post 350 is fixed to a side of the support ring plate 120 away from the receiving platform 400 , and a guide hole is opened on the middle partition plate 410 , through which the guide post 350 passes.

[0035] The hangar door 200 includes a first hatch 210 and a second hatch 220; sliding rods 230 are arranged parallel to both sides of the hangar frame 100 near the hangar opening 110, and a fixing seat 231 is provided in the middle of the sliding rod 230, and the fixing seat 231 is fixedly connected to the hangar frame 100; sliding seats 221 are respectively fixed on both sides of the first hatch 210 and the second hatch 220, and the sliding seats 221 are sleeved on the sliding rods 230.

[0036] Compression springs 240 are respectively sleeved on the sliding rod 230 and located on both sides of the fixed seat 231. One end of the compression spring 240 abuts the fixed seat 231, and the other end abuts the sliding seat 221; a driving mechanism 700 is provided in the equipment installation compartment 180 to control the closing of the first hatch 210 and the second hatch 220 respectively.

[0037] The drive mechanism 700 includes a mounting plate 710 secured within the equipment installation compartment 180. A second motor 720 is secured to the mounting plate 710. A cable drum 730 is secured to the output shaft of the second motor 720, and a rope 740 is attached to the cable drum 730. A sliding hole 122 is defined in the support ring plate 120, and a fixed pulley 750 is provided on the side of the hangar frame 100 near the hangar entrance 110. The end of the rope 740, away from the cable drum 730, passes through the sliding hole 122, passes around the fixed pulley 750, and is then fixedly connected to the first or second door 210, 220. During operation, the second motor 720 controls the rotation of the cable drum 730, thereby controlling the closing of the first or second door 210, 220. Preferably, a pressure sensor is installed on one side of the first and second doors 210, 220 near the center of the hangar frame 100. When the first and second doors 210, 220 reach a set position and close the hangar opening 110, they abut against the pressure sensor. When they abut, the second motor 720 is controlled to stop. When the doors need to be opened again, the second motor 720 is controlled to rotate in the reverse direction. At this time, the first and second doors 210, 220 are opened under the action of the compression spring 240.

[0038] An air outlet 130 and an air inlet 140 are provided on the hangar frame 100 and within the equipment installation compartment 180. A control mechanism 800 is provided within the equipment installation compartment 180 to control the opening or closing of the air inlet 140 and the air outlet 130. A first temperature sensor is provided on the outside of the hangar frame 100, and a second temperature sensor is provided on the inside of the hangar frame 100. When the temperature detected by the first temperature sensor is less than a set value, the control mechanism 800 opens the air inlet 140 and the air outlet 130; otherwise, the air inlet 140 and the air outlet 130 are closed. The second temperature sensor is used to detect the temperature within the equipment installation compartment 180 and control the air conditioner 600 based on the temperature value.

[0039] A first installation pipe 150 for covering the air inlet 140 and a second installation pipe 160 for covering the air outlet 130 are provided in the equipment installation compartment 180; the control mechanism 800 opens or closes the first installation pipe 150 and the second installation pipe 160, and the ventilation device 500 is provided in the first installation pipe 150 and the second installation pipe 160.

[0040] The first installation pipe 150 and the second installation pipe 160 are formed with a closed opening 161 at one end close to the equipment installation chamber 180 . The cross section of the closed opening 161 is an isosceles trapezoid.

[0041] The control mechanism 800 includes an electric push rod 810 fixed within the equipment installation compartment 180. A sealing block 820 is connected to the piston end of the electric push rod 810. The sealing block 820 is prism-shaped, with a smaller area at the end away from the electric push rod 810 and a larger area at the end closer to the electric push rod 810. A rubber layer 830 is provided on the sidewall of the sealing block 820. The electric push rod 810 controls the sealing block 820 to close or open the sealing port 161. This arrangement ensures that the sealing port 161 is waterproof when closed.

[0042] The ventilation device 500 includes a first filter 510 secured within the first installation duct 150, with a dehumidification layer 520 positioned within the first filter 510. A second filter 530 is positioned within the second installation duct 160, and an exhaust fan 540 is positioned on the side of the second filter 530 proximal to the equipment installation compartment 180. In some special environments, when there is a significant temperature difference between day and night, the exhaust fan 540 can be used to ventilate the air within the equipment installation compartment 180 at night, maintaining a relatively low temperature within the compartment. When the outdoor temperature gradually rises, the control mechanism 800 closes the sealing opening 161. Simultaneously, the air conditioner 600 is used to cool the equipment installation compartment 180.

[0043] In the description of the present invention, it should be noted that the terms "center," "upper," "lower," "left," "right," "vertical," "horizontal," "inner," "outer," "front," and "back" and the like, indicating orientations or positional relationships, are based on the orientations or positional relationships shown in the accompanying drawings and are intended solely to facilitate and simplify the description of the present invention. They are not intended to indicate or imply that the devices or components referred to must have, be constructed, or operate in a specific orientation, and therefore should not be construed as limiting the present invention. Furthermore, the terms "first," "second," and "third" are used for descriptive purposes only and should not be construed as indicating or implying relative importance.

[0044] In the description of the present invention, it should be noted that, unless otherwise clearly specified or limited, the terms "installed", "connected", and "connected" should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integral connection, a mechanical connection, an electrical connection, a direct connection, an indirect connection through an intermediate medium, or internal communication between two components. For those of ordinary skill in the art, the specific meanings of the above terms in the present invention can be understood according to the specific circumstances. In the absence of conflict, the embodiments of the present invention and the features therein can be combined with each other.

[0045] The above-described embodiments merely illustrate the implementation methods of the present invention. While the descriptions are relatively specific and detailed, they should not be construed as limiting the scope of the present invention. It should be noted that a person skilled in the art would be able to make various modifications and improvements without departing from the spirit of the present invention, all of which fall within the scope of protection of the present invention. Therefore, the scope of protection of the present invention shall be determined by the appended claims.

Claims

1. A drone hangar capable of operating normally under high temperature conditions, comprising a hangar frame (100) and a hangar controller disposed within the hangar frame (100), characterized in that: The sides of the hangar frame (100) are respectively fixedly mounted with heat insulation panels; A hangar opening (110) is formed at the upper end of the hangar frame (100), and a hangar door (200) for opening or closing the hangar opening (110) is provided on the upper side of the hangar frame (100); an installation cavity is formed in the hangar frame (100), a lifting mechanism (300) is provided in the installation cavity, and a lifting end of the lifting mechanism (300) is connected to a receiving platform (400); a ventilation device (500) for ventilating the outside of the hangar frame (100) and an air conditioner (600) for cooling the installation cavity are provided in the installation cavity; An annular support ring plate (120) is formed in the middle of the hangar frame (100), a communication port (121) is formed in the middle of the support ring plate (120), and the receiving platform (400) is located above the support ring plate (120); A drone parking compartment (170) is formed on a side of the support ring plate (120) close to the hangar opening (110), and an equipment installation compartment (180) is formed on a side of the support ring plate (120) away from the hangar opening (110); a middle partition plate (410) is provided on the lower side of the receiving platform (400), and when the receiving platform (400) extends out of the hangar opening (110), the middle partition plate (410) covers the communication opening (121); The hangar controller, air conditioner (600) and ventilation device (500) are arranged in the equipment installation compartment (180).

2. The UAV hangar capable of operating normally under high temperature conditions according to claim 1, characterized in that: A plurality of connecting columns (420) are provided on the lower side of the receiving platform (400), and the other ends of the connecting columns (420) are fixed to the middle partition plate (410); The lifting mechanism (300) includes a support sleeve (310) fixedly connected to the lower side of the receiving platform (400), the lower end of the support sleeve (310) passes through the middle partition plate (410), and a threaded hole (311) is provided at one end of the support sleeve (310) away from the receiving platform (400). A bottom support seat (320) is fixed at the bottom of the equipment installation bin (180), and a screw rod (330) is rotatably connected to the bottom support seat (320). The screw rod (330) is threadedly connected to the threaded hole (311), and a first motor (340) is provided on the bottom support seat (320) to drive the screw rod (330) to rotate; A vertical guide column (350) is fixed on a side of the support ring plate (120) away from the receiving platform (400), and a guide hole is opened on the middle partition plate (410), and the guide column (350) passes through the guide hole.

3. The UAV hangar capable of operating normally under high temperature conditions according to claim 1, characterized in that: The hangar door (200) includes a first door (210) and a second door (220); Sliding rods (230) are arranged in parallel on both sides of the hangar frame (100) close to the hangar opening (110), and a fixing seat (231) is arranged in the middle of the sliding rod (230), and the fixing seat (231) is fixedly connected to the hangar frame (100); Sliding seats (221) are fixed on both sides of the first hatch (210) and the second hatch (220), respectively. The sliding seats (221) are sleeved on the sliding rod (230). Compression springs (240) are respectively sleeved on the sliding rod (230) and located on both sides of the fixed seat (231), one end of the compression spring (240) abuts against the fixed seat (231), and the other end abuts against the sliding seat (221); A driving mechanism (700) for controlling the closing of the first hatch (210) and the second hatch (220) is provided in the equipment installation compartment (180).

4. The UAV hangar capable of operating normally under high temperature conditions according to claim 3, characterized in that: The driving mechanism (700) includes a mounting plate (710) fixed in the equipment mounting compartment (180), a second motor (720) is fixed on the mounting plate (710), a winding drum (730) is fixed on the output shaft of the second motor (720), and a rope (740) is installed on the winding drum (730); A sliding hole (122) is provided on the support ring plate (120), and a fixed pulley (750) is provided on one side of the hangar frame (100) close to the hangar opening (110); One end of the rope (740) away from the winding drum (730) passes through the sliding hole (122), and after passing around the fixed pulley (750), is fixedly connected to the first cabin door (210) or the second cabin door (220).

5. The UAV hangar capable of operating normally under high temperature conditions according to claim 1, characterized in that: An air outlet (130) and an air inlet (140) are provided on the hangar frame (100) and located in the equipment installation compartment (180); A control mechanism (800) for controlling the opening or closing of the air inlet (140) and the air outlet (130) is provided in the equipment installation compartment (180), a first temperature sensor is provided on the outside of the hangar frame (100), and a second temperature sensor is provided on the inside of the hangar frame (100); when the temperature value detected by the first temperature sensor is less than a set value, the control mechanism (800) opens the air inlet (140) and the air outlet (130).

6. The drone hangar capable of operating normally under high temperature conditions according to claim 5, characterized in that: The equipment installation chamber (180) is provided with a first installation pipe (150) for covering the air inlet (140) and a second installation pipe (160) for covering the air outlet (130); The control mechanism (800) opens or closes the first installation duct (150) and the second installation duct (160), and the ventilation device (500) is arranged in the first installation duct (150) and the second installation duct (160).

7. The UAV hangar capable of operating normally under high temperature conditions according to claim 6, characterized in that: The first installation pipe (150) and the second installation pipe (160) are formed with a closed opening (161) at one end close to the equipment installation compartment (180), and the cross section of the closed opening (161) is an isosceles trapezoid; The control mechanism (800) includes an electric push rod (810) fixed in the equipment installation chamber (180), and the piston end of the electric push rod (810) is connected to a closing block (820). The closing block (820) is in the shape of a prism, with a smaller area at the end away from the electric push rod (810) and a larger area at the end close to the electric push rod (810). A rubber layer (830) is provided on the side wall of the closing block (820). The electric push rod (810) controls the closing block (820) to close or open the closing port (161).

8. The drone hangar capable of operating normally under high temperature conditions according to claim 6, characterized in that: The ventilation device (500) comprises a first filter (510) fixed in the first installation pipe (150), and a dehumidification layer (520) is arranged on the inner side of the first filter (510); a second filter (530) is arranged in the second installation pipe (160), and an exhaust fan (540) is arranged on the side of the second filter (530) close to the equipment installation compartment (180).

Images