Unmanned aerial vehicle hangar heat dissipation combined equipment

Abstract

The utility model discloses heat dissipation combined equipment for an unmanned aerial vehicle hangar, belongs to the technical field of unmanned aerial vehicle hangars, and aims to solve the problems that an intelligent heat dissipation system is lacked, the heat dissipation efficiency cannot be automatically adjusted according to the actual temperature in the hangar, and the heat dissipation effect is reduced. Comprising a hangar shell, an electric control sliding cover, electric push rods, a parking platform, a refrigerating device, a heat dissipation mechanism, an adjusting mechanism and a temperature sensor, the electric push rods are symmetrically and fixedly connected to the lower portion of the interior of the hangar shell, the parking platform is fixedly connected to the upper portions of the electric push rods, and the refrigerating device is arranged below the electric push rods; the heat dissipation mechanism is arranged between the parking platform and the refrigerating device, and the adjusting mechanisms are symmetrically arranged on the left side and the right side of the hangar shell. According to the unmanned aerial vehicle hangar, by arranging the refrigerating device and the heat dissipation mechanism, all positions of the unmanned aerial vehicle above the parking platform can be subjected to air cooling heat dissipation, so that heat resistance and heat accumulation are reduced, heat dissipation uniformity is improved, and normal operation of the unmanned aerial vehicle hangar is ensured.

Description

TECHNICAL FIELD

[0001] The utility model belongs to the unmanned aerial vehicle hangar technical field, concretely relates to a kind of unmanned aerial vehicle hangar heat dissipation combination equipment. BACKGROUND

[0002] Unmanned aircraft is called "unmanned aerial vehicle" for short, English abbreviation "UAV", is the use of radio remote control equipment and self-provided program control device manipulates the aircraft without people, with the rapid development of multicopter unmanned aerial vehicle, and the continuous expansion of application range, people's pursuit of multicopter unmanned aerial vehicle technology, unmanned aerial vehicle hangar is one of the infrastructure of unmanned aerial vehicle operation. Unmanned aerial vehicle hangar is a special parking place specially designed for unmanned aerial vehicle, and is also an important ground infrastructure for realizing unmanned aerial vehicle automation and intelligent operation.

[0003] The prior art patent announcement number CN221214671U is a kind of unmanned aerial vehicle hangar, the above-mentioned patent structure is reasonable and simple, production cost is low, installation is convenient, and complete function can be adjusted to the height of lifting plate, so that the lifting plate is lifted to the highest and then the unmanned aerial vehicle is launched and landed, so that the collision between unmanned aerial vehicle propeller and unmanned aerial vehicle hangar can be avoided;The hangar roof of the utility model can be opened and closed under the driving of motor, so that the problem of effectively preventing the hangar from being exposed to outdoor environment for a long time, especially in rainy season, the hangar surface is easily corroded by rainwater, reduces the service life of hangar, but there are still the following deficiencies in actual use: starting from reality, after the hangar is stored, many high-power components, such as motor, electronic speed controller, battery, etc., are usually integrated in the unmanned aerial vehicle hangar, a large amount of heat will be generated when these components work, and the heat in the hangar is difficult to discharge quickly, the temperature continues to rise, the hangar cannot operate normally, and the intelligent heat dissipation system is lacked, the heat dissipation efficiency cannot be automatically adjusted according to the actual temperature in the hangar, and the heat dissipation effect is reduced.

[0004] Therefore, an unmanned aerial vehicle hangar heat dissipation combination equipment is needed to solve the problem of lacking intelligent heat dissipation system, unable to automatically adjust heat dissipation efficiency according to actual temperature in the hangar and reduce heat dissipation effect in the prior art. UTILITY MODEL CONTENTS

[0005] The utility model aims at providing a kind of unmanned aerial vehicle hangar heat dissipation combination equipment to solve the problems raised in the above background.

[0006] To achieve the above object, the utility model provides following technical scheme: a unmanned plane hangar heat radiation combination equipment, including hangar shell, electric control sliding cover, electric push rod, parking platform, refrigerating plant, heat radiation mechanism, adjusting mechanism and temperature sensor, the electric control sliding cover is connected in the upper left and right sides of hangar shell, the electric push rod is fixedly connected to the inside lower portion of hangar shell, the parking platform is fixedly connected to the upper portion of electric push rod, the refrigerating plant is set up in the lower portion of electric push rod, the heat radiation mechanism is set up between parking platform and refrigerating plant, the adjusting mechanism is set up in the left and right sides of hangar shell.

[0007] The heat radiation mechanism is composed of telescopic pipeline, fixed pipeline, gas collection cavity and air outlet, the inside lower portion of the hangar shell is provided with a mounting cavity, the refrigerating plant is fixedly installed in the inside of the mounting cavity, the bottom end of the telescopic pipeline is fixedly connected to the upper portion of the mounting cavity, and the fixed pipeline is fixedly connected to the upper portion of the telescopic pipeline.

[0008] The adjusting mechanism is composed of motor, first bevel gear set, transmission rod, second bevel gear set, lead screw, threaded block and baffle, the left and right sides of the hangar shell are symmetrically provided with air holes, the baffle is arranged outside the air hole, the motor is fixedly connected to the outside of the hangar shell, the output end of the motor is fixedly connected with a connecting shaft, the first bevel gear set is arranged outside the connecting shaft, the transmission rod is arranged outside the first bevel gear set, and the second bevel gear set is symmetrically arranged at the front and rear ends of the transmission rod.

[0009] It is to be noted in the scheme that the inside of the parking platform is symmetrically provided with a gas collection cavity, and the lower portion of the gas collection cavity is fixedly connected with the top end of the fixed pipeline, and the top end of the gas collection cavity is provided with an air outlet.

[0010] It is further to be noted that the first bevel gear set and the second bevel gear set are respectively composed of driving bevel gear and driven bevel gear, and the driving bevel gear and the driven bevel gear are meshed with each other.

[0011] It is further to be noted that the driving bevel gear of the first bevel gear set is fixedly connected with the connecting shaft, the transmission rod penetrates the driven bevel gear of the first bevel gear set, and the transmission rod is fixedly connected with the driven bevel gear.

[0012] As a preferred embodiment, the driving bevel gear of the second bevel gear set is fixedly connected with the end of the transmission rod, and the bottom end of the lead screw is fixedly connected with the driven bevel gear of the second bevel gear set.

[0013] As a preferred embodiment, the lead screw is fixedly connected above the second bevel gear set, the threaded block is threadedly connected outside the lead screw, and the baffle is fixedly connected between the threaded blocks.

[0014] As a preferred implementation, the temperature sensor is fixedly connected to the top of the interior of the hangar shell, and the temperature sensor is electrically connected with the refrigeration device and the motor respectively.

[0015] Compared with the prior art, the unmanned aerial vehicle hangar heat dissipation combination device provided by the utility model has at least the following beneficial effects:

[0016] (1) By setting the refrigeration device and the heat dissipation mechanism, the unmanned aerial vehicles at various positions above the parking platform can be air-cooled and heat-dissipated, so as to reduce thermal resistance and heat accumulation, improve heat dissipation uniformity, and ensure normal operation of the unmanned aerial vehicle hangar.

[0017] (2) By setting the refrigeration device, the heat dissipation mechanism, the adjusting mechanism and the temperature sensor, the environmental temperature inside the hangar shell is monitored in real time through the temperature sensor, so that the operation of the motor is controlled, the lifting height of the baffle is controlled, the shielding area of the air vent is adjusted, the air flow efficiency is adjusted, and the best heat dissipation effect is achieved. BRIEF DESCRIPTION OF DRAWINGS

[0018] Figure 1 It is a perspective view structural schematic diagram of the utility model;

[0019] Figure 2 It is a sectional view structural schematic diagram of the utility model;

[0020] Figure 3 It is a heat dissipation mechanism structural schematic diagram of the utility model;

[0021] Figure 4 It is an adjusting mechanism structural schematic diagram of the utility model.

[0022] In the drawing: 1, hangar shell; 2, electric control sliding cover; 3, electric push rod; 4, parking platform; 5, refrigeration device; 6, heat dissipation mechanism; 7, adjusting mechanism; 8, temperature sensor; 601, telescopic pipeline; 602, fixed pipeline; 603, gas collection cavity; 604, air outlet; 701, air vent; 702, motor; 703, first bevel gear set; 704, transmission rod; 705, second bevel gear set; 706, screw rod; 707, threaded block; 708, baffle. DETAILED DESCRIPTION

[0023] The utility model will be further described below in combination with examples.

[0024] Please refer to Figures 1-4The utility model provides a kind of unmanned aerial vehicle hangar heat dissipation combination equipment, including hangar shell 1, electric control sliding cover 2, electric push rod 3, parking platform 4, refrigerating plant 5, heat dissipation mechanism 6, adjusting mechanism 7 and temperature sensor 8, electric control sliding cover 2 is slidably connected in the upper left and right sides of hangar shell 1, electric push rod 3 is fixedly connected in the inside lower of hangar shell 1 symmetrically, parking platform 4 is fixedly connected in the upper of electric push rod 3, refrigerating plant 5 is set in the lower of electric push rod 3, heat dissipation mechanism 6 is set between parking platform 4 and refrigerating plant 5, adjusting mechanism 7 is symmetrically set in the left and right sides of hangar shell 1.

[0025] Heat dissipation mechanism 6 is composed of telescopic duct 601, fixed duct 602, gas collection chamber 603 and air outlet 604, the inside lower of hangar shell 1 is provided with installation cavity, refrigerating plant 5 is fixedly installed in the inside of installation cavity, the bottom end of telescopic duct 601 is fixedly connected in the upper of installation cavity, fixed duct 602 is fixedly connected in the upper of telescopic duct 601 symmetrically.

[0026] Adjusting mechanism 7 is composed of motor 702, first bevel gear set 703, transmission rod 704, second bevel gear set 705, screw rod 706, threaded block 707 and baffle 708, the left and right sides of hangar shell 1 are symmetrically provided with air hole 701, baffle 708 is set in the outside of air hole 701, motor 702 is fixedly connected in the outside of hangar shell 1, and the output end of motor 702 is fixedly connected with connecting shaft, first bevel gear set 703 is set in the outside of connecting shaft, transmission rod 704 is set in the outside of first bevel gear set 703, second bevel gear set 705 is symmetrically set in the front and back ends of transmission rod 704.

[0027] Further as Figure 1 , Figure 2 And Figure 3 It is worth noting that the inside of parking platform 4 is symmetrically provided with gas collection chamber 603, and the lower end of gas collection chamber 603 is fixedly connected with the top end of fixed duct 602, and the top end of gas collection chamber 603 is provided with air outlet 604.

[0028] Through the setting of air outlet 604, cold air can be evenly sent to the upper side of parking platform 4, and the unmanned aerial vehicle above is evenly cooled, improving the cooling effect.

[0029] According to the above working process: by setting refrigerating plant 5 and heat dissipation mechanism 6, the unmanned aerial vehicle above parking platform 4 can be air-cooled and cooled at each position, to reduce thermal resistance and heat accumulation, improve the uniformity of heat dissipation, and ensure the normal operation of unmanned aerial vehicle hangar.

[0030] Further as Figure 1 , Figure 2 And Figure 4As shown in the first bevel gear set 703, the second bevel gear set 705 is composed of driving bevel gear and driven bevel gear respectively, and the driving bevel gear and the driven bevel gear are meshed with each other, the driving bevel gear of the first bevel gear set 703 is fixedly connected with the connecting shaft, the transmission rod 704 penetrates the driven bevel gear of the first bevel gear set 703, and the transmission rod 704 is fixedly connected with the driven bevel gear, the driving bevel gear of the second bevel gear set 705 is fixedly connected with the end of the transmission rod 704, and the bottom end of the lead screw 706 is fixedly connected with the driven bevel gear of the second bevel gear set 705.

[0031] Further as shown in Figure 1 、 Figure 2 and Figure 4 , it is worth noting that the lead screw 706 is fixedly connected above the second bevel gear set 705, the threaded block 707 is threadedly connected outside the lead screw 706, and the baffle plate 708 is fixedly connected between the threaded blocks 707.

[0032] The threaded blocks 707 on both sides are threadedly connected outside the lead screw 706 respectively, so as to avoid the threaded blocks 707 from rotating with the lead screw 706, and ensure that the baffle plate 708 moves simultaneously, thereby improving the lifting stability of the baffle plate 708.

[0033] Further as shown in Figure 1 、 Figure 2 and Figure 4 , it is worth noting that the temperature sensor 8 is fixedly connected inside and above the hangar shell 1, and the temperature sensor 8 is electrically connected with the refrigeration device 5 and the motor 702 respectively.

[0034] The temperature sensor 8 can monitor the temperature inside the hangar in real time, and adjust the ventilation area of the air vent 701 in real time according to the temperature, so as to achieve the best heat dissipation effect.

[0035] The refrigeration device 5 is composed of a liquid cooling plate, a liquid pump, a heat exchange fan and the like, which are all mature prior art. The cold air is delivered to the inside of the air collection cavity 603 through the telescopic pipeline 601 and the fixed pipeline 602, and is blown to the inside of the hangar shell 1 through the air outlet 604, so as to dissipate heat for the unmanned aerial vehicle above.

[0036] The scheme has the following working process: in use, first control the electric control sliding cover 2 to open, control the parking platform 4 to rise through the electric push rod 3, make the unmanned aerial vehicle stably park above the parking platform 4, then control the parking platform 4 to move down and make the unmanned aerial vehicle enter the inside of the hangar shell 1, close the electric control sliding cover 2; the temperature sensor 8 is used to monitor the temperature inside in real time, when reaching the predetermined threshold, open the refrigeration device 5, the cold air is transported to the inside of the air collection cavity 603 through the telescopic pipeline 601 and the fixed pipeline 602, blows to the inside of the hangar shell 1 through the air outlet 604, carries out heat dissipation to the unmanned aerial vehicle above, at the same time, the temperature sensor 8 monitors the temperature inside, controls the motor 702 to drive the connecting shaft to rotate, drives the transmission rod 704 to rotate through the first bevel gear set 703, drives the lead screw 706 to rotate through the second bevel gear set 705, drives the baffle 708 to rise through the threaded block 707, changes the shielding area of the air hole 701, adjusts the air flow efficiency, thereby adjusts the temperature inside, to realize the best heat dissipation effect.

[0037] In summary: through the setting of the refrigeration device 5 and the heat dissipation mechanism 6, the unmanned aerial vehicle above the parking platform 4 can be air-cooled and heat-dissipated at each position, so as to reduce the thermal resistance and heat accumulation, improve the heat dissipation uniformity, and ensure the normal operation of the unmanned aerial vehicle hangar; through the setting of the refrigeration device 5, the heat dissipation mechanism 6, the adjusting mechanism 7 and the temperature sensor 8, the environmental temperature inside the hangar shell 1 is monitored in real time through the temperature sensor 8, thereby controlling the operation of the motor 702, controlling the lifting height of the baffle 708, adjusting the shielding area of the air hole 701, adjusting the air flow efficiency, to realize the best heat dissipation effect.

Claims

1. A drone hangar heat dissipation assembly, comprising a hangar shell (1), an electrically controlled sliding cover (2), an electric push rod (3), a landing platform (4), a cooling device (5), a heat dissipation mechanism (6), an adjustment mechanism (7), and a temperature sensor (8), characterized in that: The electrically controlled sliding cover (2) is slidably connected to the upper left and right sides of the hangar shell (1), the electric push rod (3) is symmetrically fixedly connected to the lower interior of the hangar shell (1), the stop platform (4) is fixedly connected to the upper part of the electric push rod (3), the refrigeration device (5) is located below the electric push rod (3), the heat dissipation mechanism (6) is located between the stop platform (4) and the refrigeration device (5), and the adjustment mechanism (7) is symmetrically located on the left and right sides of the hangar shell (1). The heat dissipation mechanism (6) consists of a telescopic pipe (601), a fixed pipe (602), an air collection chamber (603), and an air outlet (604). An installation cavity is provided at the bottom of the interior of the hangar shell (1). The refrigeration device (5) is fixedly installed inside the installation cavity. The bottom end of the telescopic pipe (601) is fixedly connected to the top of the installation cavity. The fixed pipe (602) is symmetrically fixedly connected to the top of the telescopic pipe (601). The adjustment mechanism (7) consists of a motor (702), a first bevel gear group (703), a transmission rod (704), a second bevel gear group (705), a lead screw (706), a threaded block (707), and a baffle (708). Ventilation holes (701) are symmetrically provided on both sides of the left and right plates of the hangar shell (1). The baffle (708) is located outside the ventilation holes (701). The motor (702) is fixedly connected to the outside of the hangar shell (1), and a connecting shaft is fixedly connected to the output end of the motor (702). The first bevel gear group (703) is located outside the connecting shaft. The transmission rod (704) is located outside the first bevel gear group (703). The second bevel gear group (705) is symmetrically arranged at the front and rear ends of the transmission rod (704).

2. The unmanned aerial vehicle hangar heat dissipation combination device according to claim 1, characterized in that: The machine stop (4) has symmetrically arranged air collection chambers (603) inside, and the bottom of the air collection chamber (603) is fixedly connected to the top of the fixed pipe (602). The top of the air collection chamber (603) is provided with an air outlet (604).

3. The unmanned aerial vehicle hangar heat dissipation combination device according to claim 2, characterized in that: The first bevel gear group (703) and the second bevel gear group (705) are respectively composed of active bevel gears and driven bevel gears, and the active bevel gears and driven bevel gears mesh with each other.

4. The unmanned aerial vehicle hangar heat dissipation combination device according to claim 3, characterized in that: The active bevel gear of the first bevel gear group (703) is fixedly connected to the connecting shaft, and the transmission rod (704) passes through the driven bevel gear of the first bevel gear group (703), and the transmission rod (704) is fixedly connected to the driven bevel gear.

5. The unmanned aerial vehicle hangar heat dissipation combination device according to claim 4, characterized in that: The active bevel gear of the second bevel gear group (705) is fixedly connected to the end of the transmission rod (704), and the bottom end of the lead screw (706) is fixedly connected to the driven bevel gear of the second bevel gear group (705).

6. The unmanned aerial vehicle hangar heat dissipation combination device according to claim 5, characterized in that: The lead screw (706) is fixedly connected above the second bevel gear assembly (705), the threaded block (707) is threadedly connected to the outside of the lead screw (706), and the baffle (708) is fixedly connected between the threaded blocks (707).

7. The unmanned aerial vehicle hangar heat dissipation combination device according to claim 6, characterized in that: The temperature sensor (8) is fixedly connected to the upper interior of the hangar shell (1), and the temperature sensor (8) is electrically connected to the refrigeration device (5) and the motor (702) respectively.

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