Cooling device, method, electronic device, storage medium and product

Abstract

This disclosure provides a cooling device, method, electronic device, storage medium, and product. The device includes a cooling component, a movable component, and a pressing component. The cooling component includes a support plate, a drive motor, a rotating rod, and a cooling fan. The support plate is disposed inside the nacelle near the fan blades. The drive motor is disposed on one side of the support plate. The output shaft of the drive motor is rotatably connected to the cooling fan. One side of the movable component is connected to the cooling component, and the other side of the movable component is connected to the pressing component. The pressing component includes an airbag. The airbag is disposed on the other side of the support plate. In summary, compared to existing methods that rely solely on a fan fixedly installed at one end of the nacelle for air cooling, this disclosure can easily achieve cold air coverage on both sides of the nacelle through the coordinated operation of the rotating rod, movable component, and airbag. Furthermore, the airbag-type pressing component has a simple structure, is flexible in adjustment, and can adapt to nacelles of different lengths, thus solving the problems of poor adaptability, low heat dissipation efficiency, and incomplete heat dissipation in existing solutions.

Description

Technical Field

[0001] This disclosure relates to the field of communication technology, and in particular to a cooling device, method, electronic device, storage medium, and product. Background Technology

[0002] Currently, the cooling method for wind turbine generators is generally air cooling. However, when the fan is installed at one end of the nacelle, the airflow generated by the fan is insufficient to reach the other end of the nacelle. This results in the nacelle's interior being unable to dissipate heat in time, leading to poor cooling performance and making it unsuitable for various scenarios. Summary of the Invention

[0003] This disclosure provides a cooling device, method, electronic device, storage medium, and product to address, to some extent, the problem of insufficient heat dissipation at the end of the cabin furthest from the fan.

[0004] According to one aspect of this disclosure, a cooling device is provided, comprising: a cooling component, a movable component, and a pressing component; the cooling component includes a support plate, a drive motor, a rotating rod, and a cooling fan; the support plate is disposed inside the engine compartment on one side near the fan blades; the drive motor is disposed on one side of the support plate; the output shaft of the drive motor is rotatably connected to the cooling fan; one side of the movable component is connected to the cooling component, and the other side of the movable component is connected to the pressing component; the pressing component includes an airbag; the airbag is disposed on the other side of the support plate.

[0005] Furthermore, according to one aspect of this disclosure, the device further includes at least one of the following: a power generation component, a sealing component, and a cleaning component; the power generation component includes a nacelle, fan blades, and a frame; the nacelle is located at the center of the top of the frame; the fan blades are located on one side outside the nacelle; the sealing component includes a movable plate and a sliding rod; the movable plate is slidably connected to the inside of the nacelle on the side near the fan blades; the sliding rod is located on the outside of the movable plate; the cleaning component includes a stop bar; the stop bar is located on the side of the nacelle away from the fan blades.

[0006] Furthermore, according to one aspect of this disclosure, the slide bar has an L-shaped structure, with its vertical end fixed to the outside of the movable plate.

[0007] Furthermore, according to one aspect of this disclosure, the movable component further includes: a movable rod, a telescopic spring, a movable block, a first support rod, a second support rod, and a movable ring; the movable rod is located at the center of the rotating rod; the telescopic spring is located on both sides of the center inside the cabin; the movable block is located on the telescopic spring; the first support rod is rotatably connected to the side of the movable block near the fan blade; the second support rod is rotatably connected to the side of the movable block away from the fan blade; and the movable ring is rotatably connected to the side of the second support rod away from the movable block.

[0008] Furthermore, according to one aspect of this disclosure, the ends of the movable rod are arc-shaped convex structures; the movable block is an arc-shaped convex structure.

[0009] In addition, according to one aspect of this disclosure, the extrusion component further includes: a limiting sleeve, an air outlet, and a through hole; the limiting sleeve is disposed on the side of the support plate away from the fan blade; the air outlet is distributed along the outer side of the airbag; the through hole and the air outlet are symmetrically distributed on the movable plate.

[0010] Furthermore, according to one aspect of this disclosure, the seal further includes: a first vent, a sealing plate, a second vent, and a retaining ring; the first vent is disposed on the side of the nacelle near the fan blade; the sealing plate is slidably connected to the side of the nacelle near the fan blade, and the sliding direction of the sealing plate is perpendicular to the axis of the rotating rod; the second vent is disposed on the side of the sealing plate away from the fan blade; and the retaining ring is disposed on the inner side of the sealing plate.

[0011] In addition, according to one aspect of this disclosure, the cleaning component further includes: a fixing rod, a brush, and an air inlet; the fixing rod is disposed on the side of the rotating rod away from the fan blades; the brush is disposed on the inner side of the fixing rod; and the air inlet is disposed on the side of the nacelle away from the fan blades.

[0012] According to another aspect of this disclosure, a cooling method is provided, the method comprising: driving a rotating rod to rotate a cooling fan by a drive motor to generate a first airflow, and driving a movable part to compress an airbag to generate a second airflow.

[0013] Furthermore, according to another aspect of this disclosure, the method also includes: when the rotating rod rotates, the brush cleans the edge of the air inlet.

[0014] According to another aspect of this disclosure, a cooling device is provided, comprising: a generating unit for driving a rotating rod to rotate a cooling fan via a drive motor to generate a first airflow, and driving a movable part to compress an airbag to generate a second airflow.

[0015] According to another aspect of this disclosure, an electronic device is provided, comprising: a memory for storing computer-readable instructions; and a processor for executing the computer-readable instructions, causing the electronic device to perform the method as described in any embodiment of one aspect.

[0016] According to another aspect of this disclosure, a non-transitory computer-readable storage medium is provided for storing computer-readable instructions that, when executed by a processor, cause the processor to perform the method as described in any embodiment of one aspect.

[0017] According to another aspect of this disclosure, a computer program product is provided, including a computer program that, when executed by a processor, implements the method as described in any embodiment of one aspect.

[0018] This disclosure provides a cooling device, method, electronic device, storage medium, and product. The disclosure utilizes a cooling component, a movable component, and a pressing component. The cooling component includes a support plate, a drive motor, a rotating rod, and a cooling fan. The support plate is disposed inside the engine compartment near the fan blades. The drive motor is disposed on one side of the support plate, and its output shaft is rotatably connected to the cooling fan. One side of the movable component is connected to the cooling component, and the other side is connected to the pressing component. The pressing component includes an air bladder, which is disposed on the other side of the support plate. Thus, when cooling is required, the cooling fan in the cooling component cools one side of the engine compartment, while the rotating rod in the cooling component can also drive the movable component to press the air bladder in the pressing component, cooling the other side of the engine compartment. Compared to existing methods that rely solely on fans fixed at one end of the cabin for air cooling, this invention can easily achieve airflow coverage on both sides of the cabin through the coordinated operation of rotating rods, movable parts, and airbags. At the same time, the airbag-type extrusion component has a simple structure and flexible adjustment, which can adapt to cabins of different lengths and specifications, thus solving the problems of poor adaptability, low heat dissipation efficiency, and incomplete heat dissipation in existing solutions.

[0019] It should be understood that both the foregoing general description and the following detailed description are exemplary and intended to provide further illustration of the claimed technology. Attached Figure Description

[0020] The above and other objects, features, and advantages of this disclosure will become more apparent from the more detailed description of the embodiments thereof in conjunction with the accompanying drawings. The drawings are provided to further illustrate the embodiments of this disclosure and form part of the specification. They are used together with the embodiments of this disclosure to explain the disclosure and do not constitute a limitation thereof. In the drawings, the same reference numerals generally represent the same components or steps.

[0021] Figure 1 This is a schematic diagram of the cooling device provided in the embodiments of this disclosure; Figure 2 This is a schematic diagram of the structure of the cooling component provided in the embodiments of this disclosure; Figure 3 This is a schematic diagram of the structure of the moving parts provided in the embodiments of this disclosure; Figure 4 This is a schematic diagram of the structure of the extrusion part provided in the embodiments of this disclosure; Figure 5 This is a schematic diagram of the structure of the power generation device provided in the embodiments of this disclosure; Figure 6 This is a schematic diagram of the structure of the sealing element provided in the embodiments of this disclosure; Figure 7 This is a schematic diagram of the structure of the cleaning component provided in an embodiment of this disclosure; Figure 8A structural block diagram of another cooling device provided in this embodiment of the present disclosure; Figure 9 A hardware block diagram of an electronic device provided in an embodiment of this disclosure; Figure 10 This is a schematic diagram of a computer-readable storage medium provided in an embodiment of this disclosure.

[0022] In the diagram, the labels represent: 11, frame; 12, nacelle; 13, fan blade; 21, support plate; 22, drive motor; 23, rotating rod; 24, cooling fan; 31, movable rod; 32, telescopic spring; 33, movable block; 34, first support rod; 35, movable plate; 36, second support rod; 37, movable ring; 41, limiting sleeve; 42, airbag; 43, air outlet; 44, through hole; 51, first exhaust port; 52, sealing plate; 53, second exhaust port; 54, retaining ring; 55, sliding rod; 61, stop bar; 62, fixing rod; 63, brush; 64, air inlet. Detailed Implementation

[0023] To make the objectives, technical solutions, and advantages of this disclosure more apparent, exemplary embodiments according to this disclosure will now be described in detail with reference to the accompanying drawings. Obviously, the described embodiments are merely some embodiments of this disclosure, and not all embodiments of this disclosure. It should be understood that this disclosure is not limited to the exemplary embodiments described herein.

[0024] Currently, the cooling method for wind turbine generators is generally air cooling. However, when the fan is installed at one end of the nacelle, the airflow generated by the fan is insufficient to reach the other end of the nacelle. This results in the nacelle's interior being unable to dissipate heat in time, leading to poor cooling performance and making it unsuitable for various scenarios.

[0025] Therefore, this application provides a cooling device. When cooling is required, a cooling fan in the cooling component cools one side of the cabin. Simultaneously, a rotating rod in the cooling component can also drive a movable component to compress the airbag in the extrusion component, cooling the other side of the cabin. First, please refer to... Figure 1 , Figure 1 This is a schematic diagram of the cooling device provided in an embodiment of the present disclosure. The cooling device includes: Cooling components, moving parts, and extruded parts; The cooling components include a support plate, a drive motor, a rotating rod, and a cooling fan; the support plate is located inside the engine compartment on the side near the fan blades; the drive motor is located on one side of the support plate; the output shaft of the drive motor is rotatably connected to the cooling fan. One side of the movable part is connected to the cooling part, and the other side of the movable part is connected to the extrusion part; The extrusion includes an airbag; the airbag is located on the other side of the support plate.

[0026] Specifically, the cooling component, as shown in Figure 1, is an integrated structure comprising a support plate 21 (a support base inside the nacelle near the fan blades), a drive motor (linked with the rotating rod to provide power to the cooling fan), and the cooling fan itself. Figure 1 Not shown in the diagram; the movable part corresponds to the linkage transmission mechanism formed by 31, 33, and 35 in the diagram, which transmits the power of the cooling component to the extrusion component through push-pull motion; the air bladder of the extrusion component corresponds to number 42, and is attached to the other side of the support plate 21, driving the movable part to move in conjunction through extrusion deformation. The specific structures of the cooling component, movable part, and extrusion component are described in detail below: The cooling component includes a support plate, a drive motor, a rotating rod, and a cooling fan. The structural diagram of the cooling component is as follows: Figure 2 This is a schematic diagram of the cooling component provided in an embodiment of this disclosure. Figure 2 As shown, the support plate 21 of the cooling component is a disc-shaped base, which forms the mounting reference of the component; a drive motor adapter structure 22 is provided on one side (used to fix the drive motor, the motor body is hidden in the figure), and the output shaft of the drive motor is coaxially connected to the rotating rod 23, which extends along the axial direction of the cooling component; the end of the rotating rod 23 is fixed to the cooling fan 24, and the fan blades are arranged radially; the entire cooling component is covered with a cylindrical shell, which not only protects the internal components, but also restricts the airflow direction, so that the airflow generated by the cooling fan 24 is output in a directional manner along the channel.

[0027] The movable component further includes: a movable rod, a telescopic spring, a movable block, a first support rod, a second support rod, and a movable ring; the movable rod is located at the center of the rotating rod; the telescopic spring is located on both sides of the center inside the cabin; the movable block is located at the position of the telescopic spring; the first support rod is rotatably connected to the side of the movable block near the fan blade; the second support rod is rotatably connected to the side of the movable block away from the fan blade; and the movable ring is rotatably connected to the side of the second support rod away from the movable block. For example, Figure 3 is a schematic diagram of the structure of the movable component provided in an embodiment of this disclosure. As shown in Figure 3, the movable rod 31 of the movable component is mounted parallel to the center of the rotating rod 23 of the cooling component, forming the main support shaft for power transmission; the telescopic springs 32 are symmetrically distributed on both sides of the center inside the cabin, and their ends are fixedly connected to the movable block 33 (slider structure, integrated hinge interface); the side of the movable block 33 near the fan blade is connected to the first support rod 34 through a hinge structure, and the side away from the fan blade is hinged to the second support rod 36; the end of the second support rod 36 is rotatably connected to the movable ring 37, which is adapted to be fitted to the outside of the support plate 21 of the cooling component, realizing the rotational connection between the movable component and the cooling component; when the rotating rod 23 rotates or the cooling component is displaced, the movable rod 31 drives the movable block 33 to compress or stretch the telescopic spring 32, and with the lever transmission of the first support rod 34 and the second support rod 36, the movable ring 37 is driven to pull the cooling component to deflect by an angle or move axially, and simultaneously squeeze the airbag through the connecting rod 35, achieving the synergistic effect of "heat dissipation and air supply + structural linkage".

[0028] It is important to note that the ends of the movable rod in the moving part are both arc-shaped convex structures; the movable block also has an arc-shaped convex structure. The arc-shaped convex contours of both are mutually adapted, forming a spherical-like contact fit. When the movable rod moves and displaces following the rotating rod, the arc-shaped convex surface can adaptively adjust the contact angle, avoiding jamming caused by rigid collisions. Simultaneously, the convex structure can concentrate stress transmission to the hinge area of ​​the movable block, enhancing the transmission response of the first and second support rods, ensuring smoother linkage between the compression / tensioning action of the telescopic spring and the deflection of the movable ring, and improving the overall mechanical life and motion accuracy of the moving part.

[0029] The extrusion component includes an air bladder; the extrusion component further includes: a limiting sleeve, an air outlet, and a through hole; the limiting sleeve is disposed on the side of the support plate away from the fan blade; the air outlet is distributed along the outer side of the air bladder; the through hole and the air outlet are symmetrically distributed on the movable plate. For example, Figure 4 is a schematic diagram of the structure of the extrusion component provided in an embodiment of this disclosure. As shown in Figure 4, the limiting sleeve 41 of the extrusion component is coaxially fitted onto the side of the support plate 21 away from the fan blade, forming the circumferential constraint boundary of the airbag 42 to prevent the airbag from expanding irregularly. The airbag 42 has a ring structure and is nested between the limiting sleeve 41 and the support plate 21. Its inner side is in contact with the transmission rod (extension of the movable rod 31) of the movable component and receives the mechanical extrusion force transmitted by the movable component. The air outlet 43 is evenly distributed circumferentially along the outer wall of the limiting sleeve 41. When the airbag 42 is compressed, the internal gas can be discharged directionally through the air outlet 43. The through holes 44, which are symmetrically distributed with the air outlet 43 (adapted to the ventilation structure of the movable plate 35, implicitly related in the figure), simultaneously connect the airflow inside and outside the cabin during the sliding process of the movable plate. This balances the air pressure inside and outside the airbag, prevents overpressure damage, and enhances the heat dissipation at the far end of the cabin with the help of the discharged airflow, realizing the functional coupling of "mechanical extrusion transmission + air pressure regulation heat dissipation".

[0030] The following will specifically describe how the cooling device of this disclosure further includes at least one of the following: Power generation components, seals, and cleaning components; The power generation component includes a nacelle, fan blades, and a frame; the nacelle is located at the center of the top of the frame; the fan blades are located on one side outside the nacelle. For example, Figure 5 This is a schematic diagram of the structure of a power generation device provided in an embodiment of this disclosure. Figure 5 As can be seen from Figure 5: the frame 11 of the power generation unit is a vertical column structure, which forms the supporting foundation of the device; the nacelle 12 is cylindrical and is horizontally installed at the center of the top of the frame 11, serving as the core nacelle for wind energy conversion and equipment housing; the fan blades 13 extend outward from the nacelle 12 as the center, and when the airflow drives the fan blades 13 to rotate, it can drive the power generation components (such as generators, transmission mechanisms, etc., not shown in the figure) inside the nacelle 12 to operate, realizing the conversion of wind energy into electrical energy.

[0031] The seal includes a movable plate and a sliding rod; the movable plate is slidably connected to the side of the nacelle near the fan blades; the sliding rod is located on the outside of the movable plate. The seal also includes: a first vent, a sealing plate, a second vent, and a retaining ring; the first vent is located on the side of the nacelle near the fan blades; the sealing plate is slidably connected to the side of the nacelle near the fan blades, and the sliding direction of the sealing plate is perpendicular to the axis of the rotating rod; the second vent is located on the side of the sealing plate away from the fan blades; the retaining ring is located on the inner side of the sealing plate. For example, Figure 6This is a schematic diagram of the structure of the sealing element provided in an embodiment of this disclosure. As shown in Figure 6, the first exhaust holes 51 of the sealing element are arrayed on the side wall of the nacelle 12 near the fan blades 13, forming an exhaust channel for hot airflow in the nacelle. The sealing plate 52 is a disc-shaped structure that slides along the radial direction of the nacelle (perpendicular to the axis of the rotating rod 23) to the inside of the nacelle. The second exhaust holes 53 are distributed on the side surface away from the fan blades, precisely matching the position of the first exhaust holes 51. The inner edge of the sealing plate 52 is fixedly connected to a retaining ring 54, which forms a limiting relationship with the movable ring 37 of the movable component (or the support plate 21 of the cooling component). When the cooling component moves axially, the support plate 21 pushes the retaining ring 54, causing the sealing plate 52 to slide. When the first exhaust holes 51 and the second exhaust holes 53 are selectively aligned or staggered, the hot air in the nacelle can be quickly discharged through the two exhaust holes, enhancing near-end heat dissipation. When staggered, the sealing plate 52 closes the first exhaust hole 51, forcing the cooling fan 24 to... The generated airflow is directed to the far end of the nacelle, and with the assistance of the airflow from the extrusion components, the heat dissipation path is dynamically controlled.

[0032] It is important to note that the sliding rod of the sealing element has an L-shaped structure, with its vertical end fixed to the outside of the movable plate. This L-shaped sliding rod provides axial sliding guidance for the movable plate, preventing it from deflecting and jamming. Furthermore, the annular trajectory of the sliding groove accommodates the positional adjustment of the movable plate as it moves in conjunction with the cooling component. When the movable component drives the cooling component to move axially, the movable plate slides synchronously. The cooperation between the L-shaped sliding rod and the sliding groove ensures the alignment accuracy of the first and second vent holes of the sealing plate, guaranteeing the reliability of the "sealing-heat dissipation" mode switching and enhancing the synergistic effect between the sealing element and the cooling system.

[0033] The cleaning component includes a baffle bar; the baffle bar is located on the side of the nacelle away from the fan blades; a fixing bar is located at the end of the rotating rod. The cleaning component also includes: a fixing bar, a brush, and an air inlet; the fixing bar is located on the side of the rotating rod away from the fan blades; the brush is located on the inner side of the fixing bar; the air inlet is located on the side of the nacelle away from the fan blades. For example, Figure 7 is a schematic diagram of the structure of the cleaning component provided in an embodiment of this disclosure. As shown in Figure 7: the baffle bar 62 of the cleaning component is an arc-shaped strip, circumferentially fixed to the inner wall of the nacelle 12 on the side away from the fan blades 13, forming an airflow guiding barrier; the fixing bar 63 extends radially from the end of the rotating rod 23 towards the inner wall of the nacelle, and a brush 64 is embedded on its inner side, the bristles of the brush closely adhering to the protective net 61 (mesh structure in the figure) at the front end of the cooling fan 24; an air inlet is opened around the protective net area on the far side wall of the nacelle (the gap between the baffle bar and the protective net in the figure indicates the airflow inlet). When the drive motor drives the rotating rod 23 to rotate, the fixed rod 63 rotates synchronously with the rotating rod, causing the brush 64 to perform circumferential cleaning along the surface of the protective net, removing the attached dust and debris, and preventing the mesh from clogging and weakening the air delivery capacity of the cooling fan; the baffle 62 changes the direction of the external cold air introduced by the air inlet, forming a vortex to assist the brush cleaning, while the cold air enters the cabin through the protective net, directly supplementing the cooling airflow, realizing the synergistic mechanism of "protective net self-cleaning + active cold source introduction", ensuring the heat dissipation efficiency and long-term reliability of the cooling system.

[0034] In one embodiment of this disclosure, when the power generator converts the mechanical energy of the fan blade 13 into electrical energy, in order to cool the interior of the nacelle 12 and ensure the stability of the mechanical energy conversion into electrical energy, the drive motor 22 is started. The drive motor 22 drives the rotating rod 23 to rotate, and the rotating rod 23 drives the cooling fan 24 to rotate. The cooling fan 24 introduces outside air into the nacelle 12 and cools the high-temperature gas inside the nacelle 12. During the cooling process, the rotation of the rotating rod 23 drives the movable rod 31 to rotate. When the movable rod 31 rotates to the outside of the movable block 33, the movable rod 31 applies a thrust to the movable block 33, causing the movable block 33 to move towards the inner wall of the nacelle 12. The movement of the movable block 33 drives the movable plate 35 and the movable ring 37 to move towards each other through the first support rod 34 and the second support rod 36, respectively. At this time, the movable plate... 35 does not obstruct the airbag 42, allowing the airbag 42 to automatically draw in air and collide. When the movable rod 31 rotates to a point where it does not contact the movable block 33, the movable block 33 resets under the elastic force of the telescopic spring 32 and moves inward. The inward movement of the movable block 33 drives the movable plate 35 and the movable ring 37 to move in opposite directions via the first support rod 34 and the second support rod 36, respectively. At this time, the movable plate 35 moves and compresses the airbag 42. Since the airbag 42 is blocked on both sides by the inner wall of the cabin 12 and the limiting sleeve 41, the gas inside the airbag 42 is discharged into the cabin 12 through the air outlet 43 and the through hole 44. This moves the gas in the cabin 12 away from the cooling fan 24 towards the cooling fan 24, so that the end of the cabin 12 away from the cooling fan 24 can be cooled by the cooling fan 24, resulting in excellent cooling effect.

[0035] In another embodiment of this disclosure, when the movable plate 35 slides inside the cabin 12 under the drive of the first support rod 34, the movable plate 35 drives the slide rod 55 to slide inside the retaining ring 54. When the slide rod 55 moves to the inner side of the retaining ring 54, the movable plate 35 continues to move, driving the slide rod 55 to move, so that the slide rod 55 drives the sealing plate 52 to move through the retaining ring 54. When the movable plate 35 compresses the airbag 42, the sealing plate 52 causes the second exhaust port 53 and the first exhaust port 51 to coincide, so that the airbag 42... The high-temperature gas inside the cabin 12 is driven to be discharged outward from the second exhaust port 53 and the first exhaust port 51, thereby accelerating the exchange speed between the high-temperature gas inside the cabin 12 and the outside gas. When the movable plate 35 moves away from the airbag 42, the movable plate 35 drives the slide rod 55 to push the retaining ring 54 in the opposite direction, so that the retaining ring 54 drives the sealing plate 52 to move in the opposite direction. When the second exhaust port 53 and the first exhaust port 51 are misaligned, the sealing plate 52 blocks the first exhaust port 51, thereby sealing the first exhaust port 51.

[0036] In another embodiment of this disclosure, when the rotating rod 23 drives the cooling fan 24 to rotate to cool the interior of the cabin 12, the rotating rod 23 drives the baffle 61 and the fixing rod 62 to rotate. The fixing rod 62 drives the brush 63 to rotate outside the air inlet 64. At this time, the baffle 61 blocks the inside of the air inlet 64, so that the brush 63 can clean the dust outside the air inlet 64. At the same time, the outside air can be introduced into the cabin 12 by the cooling fan 24 without obstruction, while the dust is blocked by the baffle 61 and will not enter the cabin 12.

[0037] This disclosure also provides a cooling method, including: The cooling fan is rotated by a drive motor, which generates a first airflow and causes the moving parts to compress the airbag, generating a second airflow.

[0038] In this disclosure, the first airflow is directly driven by a cooling fan and flows directionally along the side of the nacelle near the fan blades, quickly removing heat from the core components (such as the transmission mechanism) in that area. At the same time, the rotating rod compresses the airbag through the linkage of the moving parts, causing the gas inside the airbag to form a second airflow through the air outlet and through hole. This airflow diffuses along the side of the nacelle away from the fan blades, accurately covering the distant areas that are difficult to reach with traditional air cooling. The two airflows form a convection circulation inside the nacelle, significantly improving the uniformity and efficiency of heat dissipation throughout the entire area.

[0039] The cooling method disclosed herein also includes: when the rotating rod rotates, the brush cleans the edge of the air inlet.

[0040] In this disclosure, the rotating rod rotates simultaneously, driving the fixed rod and brush to rotate as well. The brush continuously cleans the edge of the air inlet, promptly removing attached dust and debris and preventing the air inlet from becoming clogged, which would reduce the amount of external cold air introduced. At the same time, the slight airflow disturbance generated during the cleaning process can also help the air inlet draw in more cold air, supplementing the cold source inside the cabin. This allows the cooling fan's air delivery efficiency to synergize with the introduction of external cold source, ensuring the stability of long-term heat dissipation and reducing the frequency of equipment maintenance due to air inlet blockage.

[0041] This disclosure also provides another cooling device. Figure 8 A structural block diagram of another cooling device provided in this disclosure embodiment is shown below. Figure 8 As shown, the cooling device 800 includes: The generating unit 801 is used to drive the rotating rod to rotate the cooling fan through the drive motor to generate a first airflow, and to drive the moving parts to squeeze the air bag to generate a second airflow.

[0042] Figure 9This is a hardware block diagram of an electronic device provided according to an embodiment of the present disclosure. The electronic device 900 according to an embodiment of the present disclosure includes at least a processor; and a memory for storing computer-readable instructions. When the computer-readable instructions are loaded and executed by the processor, the processor performs the cooling method described in any of the preceding embodiments of the present disclosure.

[0043] Figure 9 The illustrated electronic device 900 specifically includes a central processing unit (CPU) 901, a graphics processing unit (GPU) 902, and a memory 903. These units are interconnected via a bus 904. The CPU 901 and / or GPU 902 can function as the aforementioned processor, and the memory 903 can function as the aforementioned memory storing computer-readable instructions. Furthermore, the electronic device 900 may also include a communication unit 905, a storage unit 906, an output unit 907, an input unit 908, and an external device 909, all of which are also connected to the bus 904.

[0044] Figure 10 This is a schematic diagram of a computer-readable storage medium provided in an embodiment of this disclosure. (As shown...) Figure 10 As shown, a computer-readable storage medium 1000 according to an embodiment of the present disclosure stores computer-readable instructions 1001 thereon. When the computer-readable instructions 1001 are executed by a processor, the cooling method described above with reference to any embodiment of the present disclosure is performed. The computer-readable storage medium includes, but is not limited to, volatile memory and / or non-volatile memory. Volatile memory may include, for example, random access memory (RAM) and / or cache memory. Non-volatile memory may include, for example, read-only memory (ROM), hard disk, flash memory, optical disk, magnetic disk, etc.

[0045] This disclosure further provides a computer program product, including a computer program that, when executed by a processor, implements the cooling method described in any of the preceding embodiments of this disclosure.

[0046] The present disclosure provides a cooling device, method, electronic device, storage medium, and product. The disclosure utilizes a cooling component, a movable component, and a pressing component. The cooling component includes a support plate, a drive motor, a rotating rod, and a cooling fan. The support plate is disposed inside the engine compartment near the fan blades. The drive motor is disposed on one side of the support plate, and its output shaft is rotatably connected to the cooling fan. One side of the movable component is connected to the cooling component, and the other side is connected to the pressing component. The pressing component includes an air bladder, which is disposed on the other side of the support plate. Thus, when cooling is required, the cooling fan in the cooling component cools one side of the engine compartment, while the rotating rod in the cooling component can also drive the movable component to press the air bladder in the pressing component, cooling the other side of the engine compartment. Compared to existing methods that rely solely on fans fixed at one end of the cabin for air cooling, this invention can easily achieve airflow coverage on both sides of the cabin through the coordinated operation of rotating rods, movable parts, and airbags. At the same time, the airbag-type extrusion component has a simple structure and flexible adjustment, which can adapt to cabins of different lengths and specifications, thus solving the problems of poor adaptability, low heat dissipation efficiency, and incomplete heat dissipation in existing solutions.

[0047] Those skilled in the art will recognize that the units and algorithm steps of the various examples described in conjunction with the embodiments disclosed herein can be implemented in electronic hardware, or a combination of computer software and electronic hardware. Whether these functions are implemented in hardware or software depends on the specific application and design constraints of the technical solution. Those skilled in the art can use different methods to implement the described functions for each specific application, but such implementation should not be considered beyond the scope of this disclosure.

[0048] The basic principles of this disclosure have been described above with reference to specific embodiments. However, it should be noted that the advantages, benefits, and effects mentioned in this disclosure are merely examples and not limitations, and should not be considered as essential features of each embodiment of this disclosure. Furthermore, the specific details disclosed above are for illustrative and facilitative purposes only, and are not limitations. These details do not limit the scope of this disclosure to the necessity of employing the aforementioned specific details for implementation.

[0049] The block diagrams of devices, apparatuses, devices, and systems disclosed herein are merely illustrative examples and are not intended to require or imply that they must be connected, arranged, or configured in the manner shown in the block diagrams. As those skilled in the art will recognize, these devices, apparatuses, devices, and systems can be connected, arranged, and configured in any manner. Words such as “comprising,” “including,” “having,” etc., are open-ended terms meaning “including but not limited to,” and are used interchangeably with them. The terms “or” and “and” as used herein refer to the terms “and / or,” and are used interchangeably with them unless the context clearly indicates otherwise. The term “such as” as used herein refers to the phrase “such as but not limited to,” and is used interchangeably with it.

[0050] Additionally, as used herein, the "or" used in a list of items beginning with "at least one" indicates a separate list, such that a list of, for example, "at least one of A, B, or C" means A or B or C, or AB or AC or BC, or ABC (i.e., A and B and C). Furthermore, the word "exemplary" does not imply that the described example is preferred or better than other examples.

[0051] It should also be noted that in the systems and methods of this disclosure, the components or steps can be decomposed and / or recombined. These decompositions and / or recombinations should be considered as equivalent solutions to this disclosure.

[0052] Various changes, substitutions, and modifications can be made to the technology described herein without departing from the teachings defined by the appended claims. Furthermore, the scope of the claims of this disclosure is not limited to the specific aspects of the processes, machines, manufactures, events, means, methods, and actions described above. Currently existing or later-developed processes, machines, manufactures, events, means, methods, or actions that perform substantially the same function or achieve substantially the same result as the corresponding aspects described herein can be utilized. Therefore, the appended claims include such processes, machines, manufactures, events, means, methods, or actions within their scope.

[0053] The above description of the disclosed aspects is provided to enable any person skilled in the art to make or use this disclosure. Various modifications to these aspects will be readily apparent to those skilled in the art, and the general principles defined herein may be applied to other aspects without departing from the scope of this disclosure. Therefore, this disclosure is not intended to be limited to the aspects shown herein, but rather to be carried out within the widest scope consistent with the principles and novel features disclosed herein.

[0054] The above description has been given for purposes of illustration and description. Furthermore, this description is not intended to limit the embodiments of this disclosure to the forms disclosed herein. Although numerous exemplary aspects and embodiments have been discussed above, those skilled in the art will recognize certain variations, modifications, alterations, additions, and sub-combinations therein.

Claims

1. A cooling device, characterized by, The device includes: Cooling components, moving parts, and extruded parts; The cooling component includes a support plate, a drive motor, a rotating rod, and a cooling fan; the support plate is located inside the engine compartment near the fan blades; the drive motor is located on one side of the support plate; the output shaft of the drive motor is rotatably connected to the cooling fan. One side of the movable part is connected to the cooling part, and the other side of the movable part is connected to the extrusion part; The extrusion component includes an air bladder; the air bladder is disposed on the other side of the support plate.

2. The apparatus of claim 1, wherein, The device further includes at least one of the following: Power generation components, seals, and cleaning components; The power generation component includes a nacelle, fan blades, and a frame; the nacelle is located at the top center of the frame; the fan blades are located on one side outside the nacelle. The sealing element includes a movable plate and a sliding rod; the movable plate is slidably connected to the inside of the nacelle near the fan blade; the sliding rod is located on the outside of the movable plate; The cleaning component includes a stop lever; the stop lever is located on the side of the nacelle away from the fan blades.

3. The apparatus of claim 2, wherein, The slide bar has an L-shaped structure, and its vertical end is fixed to the outside of the movable plate.

4. The apparatus of claim 1, wherein, The movable component also includes: Movable rod, telescopic spring, movable block, first support rod, second support rod, and movable ring; The movable rod is located at the center of the rotating rod; the telescopic spring is located on both sides of the center of the cabin; the movable block is located on the telescopic spring; the first support rod is rotatably connected to the movable block on the side closer to the fan blade; the second support rod is rotatably connected to the movable block on the side away from the fan blade; the movable ring is rotatably connected to the second support rod on the side away from the movable block.

5. The apparatus of claim 4, wherein, The movable rod has arc-shaped convex structures at both ends; the movable block has an arc-shaped convex structure.

6. The apparatus of claim 1, wherein, The extrusion component also includes: Limit sleeve, vent hole and through hole; The limiting sleeve is disposed on the side of the support plate away from the fan blade; the air outlet is distributed along the outer side of the airbag; the through hole and the air outlet are symmetrically distributed on the movable plate.

7. The apparatus according to claim 2, characterized in that, The sealing element further includes: First exhaust port, sealing plate, second exhaust port, and retaining ring; The first exhaust port is located on the side of the nacelle near the fan blade; the sealing plate is slidably connected to the side of the nacelle near the fan blade, and the sliding direction of the sealing plate is perpendicular to the axis of the rotating rod; the second exhaust port is located on the side of the sealing plate away from the fan blade; the retaining ring is located on the inner side of the sealing plate.

8. The apparatus according to claim 2, characterized in that, The cleaning component also includes: Fixing rod, brush, and air inlet; The fixing rod is located on the side of the rotating rod away from the fan blade; the brush is located on the inner side of the fixing rod; and the air inlet is located on the side of the nacelle away from the fan blade.

9. A cooling method, characterized in that, The method includes: The cooling fan is rotated by a drive motor, which generates a first airflow and causes the moving parts to compress the airbag, generating a second airflow.

10. The method according to claim 9, characterized in that, The method further includes: When the rotating rod rotates, the brush cleans the edge of the air inlet.

11. A cooling device, characterized in that, The device includes: The generating unit is used to drive the rotating rod to rotate the cooling fan through the drive motor, generate the first airflow, and drive the moving parts to squeeze the air bag to generate the second airflow.

12. An electronic device, characterized in that, include: A processor for executing computer-readable instructions that cause the electronic device to perform the method as described in claim 9 or 10.

13. A non-transitory computer-readable storage medium for storing computer-readable instructions, characterized in that, When the computer-readable instructions are executed by a processor, the processor performs the method as described in claim 9 or 10.

14. A computer program product, characterized in that, Includes a computer program that, when executed by a processor, implements the method as described in claim 9 or 10.

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