Aircraft thermal management system based on jet impingement cooling

Abstract

The invention discloses an aircraft thermal management system based on jet impingement cooling, and relates to the technical field of aircraft thermal management cooling systems.The aircraft thermal management system comprises an equipment cabin, a plurality of placement plates are arranged on the inner side of the equipment cabin, a chipset is placed between every two adjacent placement plates, and cooling grooves are formed in the placement plates; an air cooling assembly is arranged between every two adjacent containing plates, and the chipsets are cooled through the air cooling assemblies. According to the cooling device, the air cooling assembly is installed, the air cooling assembly can utilize the draught fan to generate air flow, liquid nitrogen is limited to the ventilation holes through the thin pipes, air at the ventilation holes becomes cold air, the air flow passes through the cold air area and is blown to the chipset, by adjusting the orientation of the ventilation openings, accurate heat dissipation can be conducted on the chipset, and the heat dissipation effect is improved.

Description

Technical Field

[0001] The present invention relates to the technical field of aircraft thermal management and heat dissipation systems, and in particular to an aircraft thermal management system based on jet impingement cooling. Background Art

[0002] An aircraft thermal management and cooling system is an instrument for cooling the heat source of an aircraft. With the development of science and technology, the performance requirements of aircraft are getting higher and higher. While improving the performance, the heat load of the aircraft is greatly increased, and a large amount of additional heat will inevitably be generated, which will increase the thermal management and cooling pressure of the aviation system. In view of this, traditional devices are not perfect, and there is no facility that can combine wind cooling and liquid nitrogen cooling to reduce the temperature, and the heat dissipation efficiency is low. An aircraft thermal management and cooling system and its use method can provide convenience for staff.

[0003] The defects of existing aircraft thermal management and cooling systems are: 1. EP3505449B1 discloses an electric aircraft engine cooling system. The electric aircraft engine cooling system disclosed above mainly considers the heat dissipation from the electrical system through the guide vanes. The cooling system can provide sufficient cooling without adding additional resistance to the aircraft. The problem of using wind cooling and liquid nitrogen cooling together to reduce the temperature is not considered, which reduces the heat dissipation efficiency.

[0004] 2. US9475574B2 discloses a heat dissipation system for an aircraft drive wheel drive assembly. The heat dissipation system for an aircraft drive wheel drive assembly disclosed above mainly considers how to modify the existing aircraft to improve heat distribution and extend the operation and service life of the wheel drive assembly and the drive device. It does not consider the problem of reducing condensation water on the surface of the transport pipe, which reduces the service life of the transport pipe.

[0005] 3. US7522413B2 discloses a heat dissipation system. The heat dissipation system disclosed above mainly considers how to divide a computer case into a plurality of heat dissipation chambers according to the arrangement of heat-generating components, so that each heat dissipation chamber has at least one heat-generating component to facilitate heat dissipation. It does not consider the problem of circulating and purifying the air in the equipment box to increase the service life of the chipset.

[0006] 4. CN110015435B discloses an electric aircraft and its heat dissipation system, method, equipment and storage medium. The electric aircraft and its heat dissipation system, method, equipment and storage medium disclosed above mainly consider how to improve the heat dissipation efficiency of the motor driver, and at the same time can monitor the health status of the motor driver in real time and increase the service life of the motor driver. It does not consider the problem of using the cold air around the storage tank for cooling, which reduces the resource utilization rate. Summary of the invention

[0007] The object of the present invention is to provide an aircraft thermal management system based on jet impingement cooling to solve the problems raised in the above background technology.

[0008] To achieve the above-mentioned purpose, the present invention provides the following technical solutions: an aircraft thermal management system based on jet impingement cooling, comprising an equipment cabin, a plurality of placement plates inside the equipment cabin, a chipset placed between two adjacent placement plates, a cooling groove opened inside the placement plates, an air cooling component arranged between two adjacent placement plates, the air cooling component cooling the chipset; The air cooling component includes two fans, and the two fans are installed on the back of the equipment cabin through connecting parts. An air duct is installed on the output end of the fan. A plurality of connecting pipes are installed through the front of the air duct. The connecting pipe runs through the back of the equipment cabin. A fixed pipe is installed on the outside of the connecting pipe, and the fixed pipe is located between two adjacent placement plates. A ventilation hole is opened through the front of the fixed pipe, and a plurality of thin tubes are installed in the ventilation hole. The thin tubes run through the fixed pipe and the inside of the placement plate and are connected with the cooling groove. An inner tube is placed on the inner side of the fixed tube, and the inner tube is higher than the connecting tube. A ventilation opening is opened on the front of the inner tube, and the ventilation opening is smaller than the ventilation hole.

[0009] Preferably, a door is installed on the front of the equipment cabin through hinges, a storage tank is installed on the top of the placement plate near the top, the inside of the storage tank is filled with liquid nitrogen, a temperature sensor is installed on the bottom of the placement plate, a transport pipe is installed through one side of the equipment cabin, and one end of the transport pipe is communicated with the storage tank, a plurality of branch pipes are installed through one side of the transport pipe close to the equipment cabin, a one-way valve is installed on the outside of the branch pipe, a short pipe is installed through one side of the placement plate, one end of the short pipe is communicated with the branch pipe, and the other end of the short pipe is communicated with the cooling tank, a recovery pipe is installed through the other side of the equipment cabin, and the recovery pipe is communicated with the cooling tank, a heat exchanger is installed on the outside of the recovery pipe, a stop valve is installed on the outside of the recovery pipe, and the stop valve is located at the bottom of the heat exchanger, a recovery tank is installed on the inner side of the bottom wall of the equipment cabin, and the recovery tank is communicated with one end of the recovery pipe, a water collecting component is provided on the outside of the transport pipe, and the water collecting component is used to collect water stains on the outside of the transport pipe.

[0010] Preferably, a sliding hole is opened on the front side of the fixed tube, and the sliding hole is located at the bottom of the ventilation hole. A sliding plate is placed inside the sliding hole, and the sliding plate is connected to the inner tube.

[0011] Preferably, a purification component is provided on one side of the equipment cabin, and the purification component is used to purify the air inside the equipment cabin. The purification component includes a bellows, and the bellows is located at the back of the equipment cabin, and a square hole is opened through one side of the bellows, and a purification box is installed on one side of the bellows, and the bellows is communicated with the purification box through the square hole, a return air duct is installed through the lower front of the purification box, and one end of the return air duct passes through one side of the equipment cabin, a sealing ring is placed through the top of the purification box, a sealing plate is installed through the inner side of the sealing ring, a handle is installed on the top of the sealing plate, an electrostatic filter material is installed on the bottom of the sealing plate, and two A limit plate is provided, and the limit plates are respectively located on the front and back of the electrostatic filter material, a filter is installed on the inner side of the purification box, and the filter is located on the front side of the electrostatic filter material, a square tube is installed through the bottom of the purification box, and the square tube is located in front of the filter, a round tube is installed at the bottom of the square tube, a threaded plate is installed on the inner thread of the round tube, a rotating ring is installed on the side of the threaded plate away from the equipment cabin, a connecting rod is installed on the other side of the threaded plate, a round plate is installed at one end of the connecting rod, a rubber ring is installed on the outside of the round plate, and a circulation component is provided on the top of the bellows, and the circulation component is used to improve the utilization of cold air around the storage tank.

[0012] Preferably, two square boxes are installed through the top of the bellows, a protective net is installed on the inner side of the square boxes, a fan is installed on the top of the protective net, a plurality of cryogenic tubes are installed through the back of the equipment cabin, and the cryogenic tubes are located between two adjacent placement plates, the cryogenic tubes are communicated with the inner side of the square box, a blowing port is provided on the side of the cryogenic tube close to the chipset, a liquid storage tank is provided inside the cryogenic tube, a plurality of through pipes are installed through the top of the cryogenic tube, one end of the through pipes is communicated with the liquid storage tank, and the other end of the through pipes is communicated with the cooling tank.

[0013] Preferably, the water collection component includes a fine mesh, and the fine mesh is mounted on the outside of the transport pipe, a protective shell is installed on one side of the equipment cabin, and the protective shell is located on the outside of the transport pipe and the branch pipe, a guide ring is installed on the inside of the protective shell, a partition is installed on the inside of the protective shell, and the partition is located at the bottom of the guide ring, a plurality of fiber rods are installed through the inside of the partition, a plurality of leakage pipes are installed through the bottom of the protective shell, and the leakage pipes correspond to the fiber rods one by one, the leakage pipes pass through the inside of the return air duct, and a water collecting box is installed at the bottom of the leakage pipe.

[0014] Preferably, the circulation component includes an air collecting duct, and the air collecting duct is installed through the top of the wind box, an air collecting plate is installed on the top of the air collecting duct, a guide plate is installed on the top of the air collecting plate, a collecting plate is installed at one end of the guide plate, and the collecting plate is installed on the back of the equipment cabin, and the outer sides of the air collecting duct, the air collecting plate, the guide plate and the collecting plate are covered with a heat insulation plate, and an air outlet is opened through the back of the equipment cabin at the position corresponding to the collecting plate.

[0015] Preferably, a control module is provided inside the equipment compartment, and the control module includes a sensing unit and an execution unit; The sensing unit is used to sense the temperature of the chipset, while the execution unit is used to cool the chipset using liquid nitrogen and wind power; The sensing unit includes a temperature sensor disposed at the bottom of the placement plate; The execution unit includes a one-way valve arranged on the outside of the branch pipe, a heat exchanger and a stop valve arranged on the outside of the recovery pipe, and a fan arranged on the back of the equipment compartment. When the temperature sensor senses that the temperature of the chipset has risen, the temperature sensor transmits a start signal to the one-way valve, the heat exchanger, the stop valve and the fan through electrical components. The one-way valve and the stop valve are started to transport the liquid nitrogen inside the storage tank to the inside of the cooling tank through the transport pipe for cooling. The liquid nitrogen absorbs heat and reacts to generate ammonia and water, which are cooled through the heat exchanger and then recovered to the recovery tank through the recovery pipe. The fan is started for wind heat dissipation.

[0016] Preferably, a method for using an aircraft thermal management system based on jet impingement cooling is as follows: S1. First, the staff opens the one-way valve and the stop valve at the same time, so that the liquid nitrogen inside the storage tank enters the inside of the cooling tank, absorbs the heat inside the placement plate, and the liquid nitrogen absorbs the heat and decomposes into ammonia and water. The ammonia and water inside the cooling tank enter the inside of the recovery tank through the recovery pipe for storage; S2. Then the staff grabs the slide plate and moves it, so that the slide plate drives the inner tube to rotate inside the fixed tube, so that the inner tube drives the vent to move to a position facing the middle of the placement plate, and then installs the chipset between two adjacent placement plates, so that the placement plates absorb the heat inside the chipset through contact, thereby cooling the chipset; S3. The staff starts the fan to blow the air inside the bellows into the inside of the fixed tube, so that the air inside the fixed tube passes through the vents and holes and blows toward the chipset to cool the chipset. At the same time, the air contacts the capillary tube, causing the temperature to drop and become cold air, so that the cold air blows toward the chipset to improve the cooling effect of air cooling. S4. When liquid nitrogen enters the inner side of the transport pipe, the temperature of the transport pipe decreases, causing the air around the transport pipe to contact the transport pipe and condense into small water droplets that drip along the fiber rod to the inner side of the water collecting box. The fiber rod seals the partition through water, so that water can only move downward through the fiber rod. The water at the bottom of the partition cannot reach the top of the partition, so that the water at the top of the partition gradually decreases, reducing the condensation of water on the surface of the transport pipe and reducing the corrosion of water to the transport pipe; S5. The air enters the inner side of the equipment cabin, which increases the air pressure inside the equipment cabin. Under the action of the pressure, the air inside the equipment cabin enters the inner side of the purification box through the return air duct. The air first contacts the filter in the purification box, so that the filter filters out the larger dust in the air. The air passes through the electrostatic filter material, and the fine particles are adsorbed on the surface of the electrostatic filter material, so that the passing air is purified, reducing the contact between dust and the chipset. S6. At the same time, the air inside the equipment cabin moves upward to the location of the storage tank under the action of air pressure. The liquid nitrogen inside the storage tank will lower the temperature of the environment around the storage tank, so that the air dissipates heat and becomes cold air when passing around the storage tank. The cold air passes through the air outlet and enters the inside of the bellows under the action of air pressure. Then, the cold air enters the inside of the equipment cabin again under the action of the fan to cool the chipset, thereby improving the utilization of the cold air around the storage tank.

[0017] Preferably, in step S5, the following steps are also included: S51. The staff member grasps the handle and moves it upward, so that the handle drives the sealing plate and the sealing ring to move out of the purification box under the action of external force, and the sealing plate drives the electrostatic filter material to move out of the inner side of the purification box, so as to facilitate the cleaning of the electrostatic filter material; S52. The staff member grasps the rotating ring and rotates it, so that the rotating ring drives the threaded plate to rotate under the action of external force, so that the threaded plate moves away from the equipment cabin by utilizing the thread action with the round tube, and the threaded plate is moved out of the inner side of the round tube to release the seal of the round tube. Then, the staff member grasps the rotating ring and moves it away from the equipment cabin, so that the rotating ring drives the round plate and the rubber ring to move through the threaded plate and the connecting rod, so that the round plate and the rubber ring clean out the dust inside the round tube.

[0018] Compared with the prior art, the present invention has the following beneficial effects: 1. The present invention is equipped with an air cooling component, which can generate airflow by using a fan to confine liquid nitrogen at the ventilation holes through a thin tube, so that the air at the ventilation holes becomes cold air. The airflow passes through the cold air area and blows toward the chipset. By adjusting the direction of the ventilation port, the chipset can be accurately cooled to improve the heat dissipation effect.

[0019] 2. The present invention is equipped with a transport pipe. When liquid nitrogen enters the inner side of the transport pipe, the air around the transport pipe contacts the transport pipe and condenses into small water droplets attached to the outer side of the transport pipe. The small water droplets contact the fine mesh, which reduces the surface tension of the small water droplets. The small water droplets slide downward under the action of their own gravity and fall to the top of the partition. The fiber rods absorb water and get wet, so that the water inside the fiber rods forms water droplets at the bottom of the fiber rods and falls to the inner side of the corresponding leakage pipe. The water droplets pass through the leakage pipe and enter the inner side of the water collecting box. The fiber rods seal the partition with water, so that water can only move downward through the fiber rods. The water at the bottom of the partition cannot come to the top of the partition, so that the water at the top of the partition gradually decreases, thereby reducing the condensation of water on the surface of the transport pipe and reducing the corrosion of water to the transport pipe.

[0020] 3. The present invention is equipped with an equipment cabin, and air enters the inner side of the equipment cabin, so that the air pressure inside the equipment cabin increases, and the air inside the equipment cabin enters the inner side of the return air duct under the action of pressure, so that the air passes through the return air duct and contacts the surface of the leakage pipe, and condensed water passes through the inside of the leakage pipe to reduce the temperature of the leakage pipe. The air passing around the leakage pipe can cool the air, and the cooled air enters the inner side of the purification box, and the air first contacts the filter in the purification box, so that the filter filters out larger dust in the air, and the larger dust falls downward through the square tube and enters the inner side of the round tube, and the air passes through the electrostatic filter material, and the electrostatic filter material uses static electricity to attract and capture particles, and adsorbs fine particles on the surface of the electrostatic filter material, so that the air passing through is purified, and the purified air passes through the square hole and enters the inner side of the bellows, and enters the inner side of the equipment cabin under the action of the fan, so as to realize air circulation purification and reduce the contact between dust and the chipset.

[0021] 4. The present invention is equipped with an equipment cabin. The air inside the equipment cabin moves upward under the action of air pressure, so that the air moves to the location of the storage tank and contacts the surface of the storage tank. The liquid nitrogen inside the storage tank will lower the temperature of the environment around the storage tank, so that the air dissipates heat and becomes cold air when passing around the storage tank. The cold air passes through the air outlet under the action of air pressure and enters the inner side of the collecting plate. The cold air passes through the collecting plate and moves downward under the guidance of the guide plate and enters the inner side of the air collecting pipe, and then enters the inner side of the bellows through the air collecting pipe. Subsequently, the cold air enters the inner side of the equipment cabin again under the action of the fan to cool the chipset. The heat insulation board can prevent the cold air from absorbing heat during the movement, thereby improving the utilization of the cold air resources around the storage tank. BRIEF DESCRIPTION OF THE DRAWINGS

[0022] Figure 1 It is a schematic diagram of the overall structure of the present invention; Figure 2 It is a schematic diagram of the three-dimensional structure of the equipment cabin of the present invention; Figure 3 It is a schematic diagram of the overall front cross-sectional structure of the present invention; Figure 4 It is a schematic diagram of the overall side section structure of the present invention; Figure 5 It is a schematic diagram of the three-dimensional structure of the fixed tank of the present invention; Figure 6 It is a schematic diagram of the cross-sectional structure of the purification box of the present invention; Figure 7 It is a schematic diagram of the three-dimensional structure of the threaded plate of the present invention; Figure 8 It is a schematic diagram of the three-dimensional structure of the wind collecting plate of the present invention; Fig. 9 It is a schematic diagram of the cross-sectional structure of a square box of the present invention; Fig.10It is a schematic diagram of the cross-sectional structure of the cryogenic tank of the present invention; Fig.11 It is a flow chart of the present invention.

[0023] In the figure: 1. Equipment cabin; 2. Hatch door; 3. Placement plate; 4. Storage tank; 5. Transport pipe; 6. Branch pipe; 7. Check valve; 8. Short pipe; 9. Cooling tank; 10. Recovery pipe; 11. Heat exchanger; 12. Stop valve; 13. Recovery tank; 14. Fan; 15. Air duct; 16. Connecting pipe; 17. Fixed pipe; 18. Ventilation hole; 19. Thin tube; 20. Sliding hole; 21. Slide plate; 22. Inner pipe; 23. Ventilation port; 24. Bellows; 25. Square hole; 26. Purification box; 27. Return air duct; 28. Sealing ring; 29. ​​Closing plate; 30. Handle; 31. Electrostatic filter material; 32. Limit plate ; 33. Filter; 34. Square tube; 35. Round tube; 36. Threaded plate; 37. Rotating ring; 38. Connecting rod; 39. Round plate; 40. Rubber ring; 41. Fine mesh; 42. Protective shell; 43. Guide ring; 44. Partition; 45. Fiber rod; 46. Leakage pipe; 47. Water collecting box; 48. Air collecting pipe; 49. Air collecting plate; 50. Guide plate; 51. Collecting plate; 52. Heat insulation board; 53. Air outlet; 54. Chip set; 55. Square box; 56. Protective net; 57. Fan; 58. Low temperature pipe; 59. Air outlet; 60. Liquid storage tank; 61. Through pipe; 62. Temperature sensor. DETAILED DESCRIPTION

[0024] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. 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 creative work are within the scope of protection of the present invention.

[0025] In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "two ends", "one end", "the other end" and the like indicate positions or positional relationships based on the positions or positional relationships shown in the drawings, and are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as limiting the present invention. In addition, the terms "first" and "second" are used for descriptive purposes only and cannot be understood as indicating or implying relative importance.

[0026] In the description of the present invention, it should be noted that, unless otherwise clearly specified and limited, the terms "installed", "provided with", "connected", etc. should be understood in a broad sense. For example, "connected" means fixed connection, detachable connection, or integral connection; mechanical connection, electrical connection; direct connection, indirect connection through an intermediate medium, and internal communication between two components. For ordinary technicians in this field, the specific meanings of the above terms in the present invention are understood according to specific circumstances.

[0027] See also Figure 1 , Figure 2 , Figure 3 and Figure 4 , Fig. 9 , an embodiment of the present invention: an aircraft thermal management system based on jet impingement cooling, comprising an equipment cabin 1, a door 2 is installed on the front of the equipment cabin 1 through a hinge, comprising an equipment cabin 1, a plurality of placement plates 3 on the inner side of the equipment cabin 1, a chipset 54 is placed between two adjacent placement plates 3, a cooling groove 9 is opened inside the placement plates 3, the equipment cabin 1 can provide a stable support for the placement plates 3, the placement plates 3 can provide a placement space for the chipset 54, the placement plates 3 can provide an opening space for the chipset 54, a storage tank 4 is installed on the top of the placement plate 3 near the top, the inner side of the storage tank 4 is filled with liquid nitrogen, a temperature sensor 62 is installed on the bottom of the placement plate 3, a transport pipe 5 is installed through one side of the equipment cabin 1, and one end of the transport pipe 5 is connected to the storage tank 4 A plurality of branch pipes 6 are installed through the side of the transport pipe 5 close to the equipment cabin 1, a one-way valve 7 is installed on the outside of the branch pipe 6, a short pipe 8 is installed through one side of the placement plate 3, and one end of the short pipe 8 is communicated with the branch pipe 6, and the other end of the short pipe 8 is communicated with the cooling tank 9, the placement plate 3 can provide a stable support for the storage tank 4, the transport pipe 5 can provide a circulation channel for the liquid nitrogen inside the storage tank 4, the one-way valve 7 can be installed through the other side of the equipment cabin 1. A recovery pipe 10 is installed, and the recovery pipe 10 is communicated with the cooling tank 9, a heat exchanger 11 is installed on the outside of the recovery pipe 10, a stop valve 12 is installed on the outside of the recovery pipe 10, and the stop valve 12 is located at the bottom of the heat exchanger 11, a recovery tank 13 is installed on the inner side of the bottom wall of the equipment cabin 1, and the recovery tank 13 is communicated with one end of the recovery pipe 10.

[0028] In this embodiment, the staff opens the one-way valve 7 and the stop valve 12 at the same time, so that the liquid nitrogen inside the storage tank 4 enters the inner side of the transport pipe 5, and the liquid nitrogen passes through the transport pipe 5 and the branch pipe 6 to enter the inner side of the short pipe 8, and the liquid nitrogen enters the inner side of the cooling tank 9 through the short pipe 8. Due to the low temperature of the liquid nitrogen, the heat flows from the placement plate 3 with a higher temperature to the liquid nitrogen through heat conduction, so that the liquid nitrogen absorbs the heat inside the placement plate 3, and the liquid nitrogen absorbs the heat and decomposes into ammonia and water. The ammonia and water inside the cooling tank 9 enter the inner side of the heat exchanger 11 through the recovery pipe 10, and the heat exchanger 11 cools the ammonia and water and transports them to the inner side of the recovery tank 13 through the stop valve 12 for storage, thereby saving cooling medium and energy.

[0029] See also Figure 1 , Figure 3 , Figure 4 and Figure 5 An embodiment of the present invention is as follows: an aircraft thermal management system based on jet impingement cooling, comprising an air cooling component, the air cooling component comprising two fans 14, and the two fans 14 are installed on the back of an equipment cabin 1 through a connecting component, an air duct 15 is installed at the output end of the fan 14, a plurality of connecting pipes 16 are installed through the front of the air duct 15, the connecting pipe 16 runs through the back of the equipment cabin 1, the equipment cabin 1 can provide a stable support for the fan 14, the fan 14 can provide a stable support for the air duct 15, a fixed pipe 17 is installed on the outside of the connecting pipe 16, and the fixed pipe 17 is located between two adjacent placement plates 3, a ventilation hole 18 is opened through the front of the fixed pipe 17, a plurality of thin pipes 19 are installed in the ventilation hole 18, and the thin pipe 19 runs through the fixed pipe 17 and the inside of the placement plate 3 and the cooling groove 9 The fixed tube 17 is connected to each other, and can provide a space for the ventilation hole 18 to pass through, and the ventilation hole 18 can provide a circulation channel for air. An inner tube 22 is placed on the inner side of the fixed tube 17, and the inner tube 22 is higher than the connecting tube 16 to prevent the inner tube 22 from blocking the connecting tube 16, so that the connecting tube 16 can blow air into the inner side of the inner tube 22. A ventilation hole 23 is provided on the front side of the inner tube 22, and the ventilation hole 23 is smaller than the ventilation hole 18. The inner tube 22 can provide a space for the ventilation hole 23. When the ventilation hole 18 is connected to the ventilation hole 23, the air inside the inner tube 22 can be blown to the outside through the ventilation hole 18 and the ventilation hole 23. A sliding hole 20 is provided on the front side of the fixed tube 17, and the sliding hole 20 is located at the bottom of the ventilation hole 18. A slide plate 21 is placed on the inner side of the sliding hole 20, and the slide plate 21 is connected to the inner tube 22.

[0030] In this embodiment, the staff member grabs the slide plate 21 and moves it, so that the slide plate 21 moves left and right along the inner side of the slide hole 20 under the action of external force, and the slide plate 21 drives the inner tube 22 to rotate inside the fixed tube 17, so that the inner tube 22 drives the vent 23 to move to a position facing the middle of the placement plate 3, and the staff member starts the fan 14, so that the fan 14 blows the air inside the bellows 24 into the inner side of the air duct 15, and the air inside the air duct 15 passes through the connecting tube 16 and enters the inner side of the fixed tube 17, so that the air inside the fixed tube 17 passes through the vent 23 and the vent 18 and blows toward the chipset 54, so as to cool down the chipset 54, and at the same time, the liquid nitrogen inside the cooling tank 9 enters the inner side of the capillary 19 under the action of gravity, so as to reduce the temperature of the air around the capillary 19, and when the air passes through the vent 18, the air contacts the capillary 19, so as to reduce the temperature and become cold air, so that the cold air is blown toward the chipset 54, and the chipset 54 is cooled down by liquid nitrogen and wind force at the same time, so as to improve the cooling effect.

[0031] See also Figure 1 , Figure 3 , Figure 4 and Figure 7An embodiment of the present invention is as follows: an aircraft thermal management system based on jet impingement cooling, comprising a purification component, the purification component is used to purify the air inside the equipment cabin 1, the purification component comprises a bellows 24, and the bellows 24 is located at the back of the equipment cabin 1, the bellows 24 is composed of a square plate, and is used to isolate the fan 14 from the outside, so as to facilitate the air circulation inside the equipment cabin 1, a square hole 25 is opened through one side of the bellows 24, a purification box 26 is installed on one side of the bellows 24, and the bellows 24 is connected to the purification box 26 through the square hole 25. 6 is connected, a return air duct 27 is installed through the front side of the purification box 26, and one end of the return air duct 27 passes through one side of the equipment cabin 1. The wind box 24 can provide a through-opening space for the square hole 25, so that the air inside the equipment cabin 1 can enter the inner side of the wind box 24 along the return air duct 27 and the purification box 26. A sealing ring 28 is placed through the top of the purification box 26, and a sealing plate 29 is installed through the inner side of the sealing ring 28. A handle 30 is installed on the top of the sealing plate 29, and an electrostatic filter material 31 is installed on the bottom of the sealing plate 29. The bottom wall of the purification box 26 is provided with a sealing ring 28, and a sealing plate 29 is installed on the inner side of the sealing ring 28. Two limit plates 32 are installed on the sides, and the limit plates 32 are respectively located on the front and back of the electrostatic filter material 31. The sealing plate 29 can provide a stable support for the electrostatic filter material 31, and the sealing plate 29 can provide a stable support for the handle 30. The handle 30 can provide a grasping support for the staff, so that the staff can remove the sealing plate 29 and the electrostatic filter material 31 through the handle 30. A filter screen 33 is installed on the inner side of the purification box 26, and the filter screen 33 is located on the front of the electrostatic filter material 31. A square tube 34 is installed through the bottom of the purification box 26, and the square tube 34 is installed through the bottom of the purification box 26. The tube 34 is located in front of the filter screen 33, and a round tube 35 is installed at the bottom of the square tube 34. A threaded plate 36 is installed on the inner thread of the round tube 35. A rotating ring 37 is installed on the side of the threaded plate 36 away from the equipment cabin 1, and a connecting rod 38 is installed on the other side of the threaded plate 36. A round plate 39 is installed at one end of the connecting rod 38, and a rubber ring 40 is installed on the outer side of the round plate 39. The purification box 26 can provide a space for the square tube 34 to pass through, and at the same time provide a circulation channel for larger dust particles. The round tube 35 can provide a collection space for dust particles.

[0032] In this embodiment, air enters the inner side of the equipment cabin 1, so that the air pressure inside the equipment cabin 1 increases, and the air inside the equipment cabin 1 enters the inner side of the return air duct 27 under the action of pressure, so that the air passes through the return air duct 27 and contacts the surface of the leakage pipe 46, and condensed water passes through the inner side of the leakage pipe 46, so that the temperature of the leakage pipe 46 is reduced. The air can be cooled by passing around the leakage pipe 46, and the cooled air enters the inner side of the purification box 26. The air first contacts the filter 33 in the purification box 26, so that the filter 33 filters out larger dust in the air. The larger dust falls downward through the square tube 34 and enters the inner side of the circular tube 35. The air that has filtered the large dust continues to move toward the back along the inner side of the purification box 26, so that the air passes through the electrostatic filter material 31. The electrostatic filter material 31 uses static electricity to attract and capture particles, and adsorbs fine particles on the surface of the electrostatic filter material 31, so that the air passing through is purified. The purified air passes through the square hole 25 and enters the inner side of the bellows 24, and enters the inner side of the equipment compartment 1 under the action of the fan 14, so as to realize air circulation purification and reduce the contact between dust and the chipset 54.

[0033] See also Figure 1 , Fig. 9 and Fig.10 The present invention provides an embodiment: an aircraft thermal management system based on jet impingement cooling, comprising a bellows 24, two square boxes 55 are installed through the top of the bellows 24, a protective net 56 is installed on the inner side of the square box 55, a fan 57 is installed on the top of the protective net 56, the square box 55 can provide a stable support for the protective net 56, the protective net 56 can provide a stable support for the fan 57, the fan 57 is started to blow the air inside the bellows 24 to the inner side of the square box 55, a plurality of cryogenic pipes 58 are installed through the back of the equipment cabin 1, and the cryogenic pipes 58 are installed on the inner side of the square box 55. 58 is located between two adjacent placement plates 3, the low-temperature tube 58 is communicated with the inner side of the square box 55, a blowing port 59 is provided on one side of the low-temperature tube 58 close to the chipset group 54, a liquid storage tank 60 is provided inside the low-temperature tube 58, a plurality of through pipes 61 are installed through the top of the low-temperature tube 58, one end of the through pipe 61 is communicated with the liquid storage tank 60, and the other end of the through pipe 61 is communicated with the cooling tank 9, the equipment cabin 1 can provide a stable support for the low-temperature tube 58, the low-temperature tube 58 is made of a material with high heat conduction efficiency, and the low-temperature tube 58 can provide a space for the liquid storage tank 60.

[0034] In this embodiment, the liquid nitrogen inside the cooling tank 9 enters the inner side of the liquid storage tank 60 through the through pipe 61, and the liquid nitrogen absorbs a large amount of heat through the cryogenic tube 58. When the air inside the cryogenic tube 58 contacts the inner wall of the cryogenic tube 58, the heat of the air is transferred to the liquid nitrogen through the cryogenic tube 58, so that the air inside the cryogenic tube 58 becomes cold air. Then the staff starts the fan 57, so that the fan 57 blows the air inside the bellows 24 into the inner side of the square box 55, so that the air passes through the square box 55 and enters the inner side of the cryogenic tube 58, so that the air inside the cryogenic tube 58 becomes cold air, and the cold air is blown to the chipset 54 through the blowing port 59 for cooling.

[0035] See also Figure 1 , Figure 3 , an embodiment of the present invention is: an aircraft thermal management system based on jet impingement cooling, comprising a water collection component, the water collection component comprising a fine mesh 41, and the fine mesh 41 is sleeved on the outside of the transport pipe 5, a protective shell 42 is installed on one side of the equipment cabin 1, and the protective shell 42 is located on the outside of the transport pipe 5 and the branch pipe 6, the protective shell 42 is a heat-insulating material to reduce the contact of external heat with the transport pipe 5, a guide ring 43 is installed on the inner side of the protective shell 42, a partition 44 is installed on the inner side of the protective shell 42, and the partition 44 is located at the bottom of the guide ring 43, the protective shell 42 can provide a stable support for the partition 44, the partition 44 can separate the protective shell 42 into two upper and lower parts, a plurality of fiber rods 45 are installed through the interior of the partition 44, a plurality of leakage pipes 46 are installed through the bottom of the protective shell 42, and the leakage pipes 46 correspond to the fiber rods 45 one by one, the leakage pipes 46 pass through the interior of the return air pipe 27, and a water collection box 47 is installed at the bottom of the leakage pipe 46.

[0036] In this embodiment, when liquid nitrogen enters the inner side of the transport pipe 5, the temperature of the transport pipe 5 is reduced, so that the air around the transport pipe 5 contacts the transport pipe 5 and condenses into small water droplets attached to the outer side of the transport pipe 5. The small water droplets contact the fine mesh 41, so that the fine mesh 41 reduces the surface tension of the small water droplets. The small water droplets slide down along the surface of the transport pipe 5 under the action of their own gravity, so that the small water droplets fall to the top of the partition 44. The water on the top of the partition 44 gathers to the middle position of the partition 44 under the guidance of the guide ring 43. The water on the top of the partition 44 contacts the fiber rod 45, and the fiber rod 45 absorbs water and gets wet, so that the inner side of the fiber rod 45 Under the action of its own gravity, water moves downward along the fiber rod 45, so that water passes through the fiber rod 45 and forms water droplets at the bottom of the fiber rod 45 and falls to the inside of the corresponding leakage pipe 46. The water droplets pass through the leakage pipe 46 and enter the inside of the water collecting box 47, so that the moisture in the air at the top of the partition 44 moves to the bottom of the partition 44 through the fiber rod 45. The fiber rod 45 seals the partition 44 with water, so that water can only move downward through the fiber rod 45, and the moisture at the bottom of the partition 44 cannot reach the top of the partition 44, so that the moisture at the top of the partition 44 gradually decreases, thereby reducing the condensation of water on the surface of the transport pipe 5 and reducing the corrosion of the transport pipe 5 by water.

[0037] See also Figure 1 , Figure 4 and Figure 8 An embodiment of the present invention is as follows: an aircraft thermal management system based on jet impingement cooling, comprising a circulation component, the circulation component comprising an air collecting duct 48, and the air collecting duct 48 is installed through the top of the wind box 24, a wind collecting plate 49 is installed on the top of the air collecting duct 48, a guide plate 50 is installed on the top of the air collecting plate 49, a collecting plate 51 is installed at one end of the guide plate 50, and the collecting plate 51 is installed on the back of the equipment cabin 1, the outer sides of the air collecting duct 48, the air collecting plate 49, the guide plate 50 and the collecting plate 51 are covered with a heat insulation plate 52, and an air outlet 53 is opened through the back of the equipment cabin 1 at a position corresponding to the collecting plate 51.

[0038] In this embodiment, the air inside the equipment cabin 1 moves upward under the action of air pressure, so that the air moves to the position of the storage tank 4, so that the air contacts the surface of the storage tank 4, and the liquid nitrogen inside the storage tank 4 lowers the temperature of the surrounding environment of the storage tank 4, so that the air dissipates heat and becomes cold air when passing around the storage tank 4. The cold air continues to move toward the back under the action of air pressure, so that the cold air passes through the air outlet 53 and enters the inner side of the collecting plate 51. The cold air passes through the collecting plate 51 and moves downward under the guidance of the guide plate 50, so that the cold air passes through the inner side of the guide plate 50 and enters the inner side of the air collecting pipe 48 under the action of the air collecting plate 49, and enters the inner side of the bellows 24 through the air collecting pipe 48. Then, the cold air enters the inner side of the equipment cabin 1 again under the action of the fan 14 to cool the chipset 54. The heat insulation plate 52 can prevent the cold air from absorbing heat during the movement, thereby improving the utilization of the cold air around the storage tank 4.

[0039] See also Figure 1 , Figure 2 , Figure 3 and Figure 4 , an embodiment provided by the present invention: an aircraft thermal management system based on jet impingement cooling, comprising an equipment cabin 1, a control module is arranged inside the equipment cabin 1, and the control module comprises a sensing unit and an execution unit; The sensing unit is used to sense the temperature of the chipset 54, and the execution unit is used to dissipate the heat of the chipset 54 using liquid nitrogen and wind power; The sensing unit includes a temperature sensor 62 disposed at the bottom of the placement plate 3; The execution unit includes a one-way valve 7 arranged on the outside of the branch pipe 6 and a heat exchanger 11 and a stop valve 12 arranged on the outside of the recovery pipe 10, and a fan 14 arranged on the back of the equipment compartment 1. When the temperature sensor 62 senses that the temperature of the chipset 54 has increased, the temperature sensor 62 transmits a start signal to the one-way valve 7, the heat exchanger 11, the stop valve 12 and the fan 14 through electrical components. The one-way valve 7 and the stop valve 12 are started to transport the liquid nitrogen inside the storage tank 4 to the inside of the cooling tank 9 through the transport pipe 5 for cooling. The liquid nitrogen absorbs heat to generate ammonia and water, which are cooled through the heat exchanger 11 and then recovered to the recovery tank 13 through the recovery pipe 10. The fan 14 is started for wind heat dissipation.

[0040] Further, a method for using an aircraft thermal management system based on jet impingement cooling is as follows: S1. First, the staff opens the one-way valve 7 and the stop valve 12 at the same time, so that the liquid nitrogen inside the storage tank 4 enters the inner side of the cooling tank 9, absorbs the heat inside the placement plate 3, and the liquid nitrogen absorbs the heat and decomposes into ammonia and water. The ammonia and water inside the cooling tank 9 enter the inner side of the recovery tank 13 through the recovery pipe 10 for storage; S2, the staff then grabs the slide plate 21 and moves it, so that the slide plate 21 drives the inner tube 22 to rotate inside the fixed tube 17, so that the inner tube 22 drives the vent 23 to move to a position facing the middle of the placement plate 3, and then installs the chipset 54 between two adjacent placement plates 3, so that the placement plates 3 absorb the heat inside the chipset 54 through contact, and cool the chipset 54; S3, the staff starts the fan 14, so that the fan 14 blows the air inside the bellows 24 into the inside of the fixed tube 17, so that the air inside the fixed tube 17 passes through the vent 23 and the vent hole 18 and blows toward the chipset 54, so as to cool down the chipset 54. At the same time, the air contacts the capillary 19, so that the temperature is reduced and becomes cold air, so that the cold air is blown toward the chipset 54, so as to improve the cooling effect of air cooling; S4. When liquid nitrogen enters the inner side of the transport pipe 5, the temperature of the transport pipe 5 decreases, so that the air around the transport pipe 5 contacts the transport pipe 5 and condenses into small water droplets, which drip along the fiber rod 45 to the inner side of the water collecting box 47. The fiber rod 45 seals the partition 44 with water, so that water can only move downward through the fiber rod 45. The water at the bottom of the partition 44 cannot reach the top of the partition 44, so that the water at the top of the partition 44 gradually decreases, reducing the condensation of water on the surface of the transport pipe 5 and reducing the corrosion of water to the transport pipe 5; S5. The air enters the inner side of the equipment cabin 1, so that the air pressure inside the equipment cabin 1 increases, and the air inside the equipment cabin 1 enters the inner side of the purification box 26 through the return air duct 27 under the action of the pressure. The air first contacts the filter 33 in the purification box 26, so that the filter 33 filters out the larger dust in the air. The air passes through the electrostatic filter material 31, and the fine particles are adsorbed on the surface of the electrostatic filter material 31, so that the passing air is purified, and the contact between the dust and the chipset 54 is reduced; S6. At the same time, the air inside the equipment cabin 1 moves upward to the location of the storage tank 4 under the action of air pressure. The liquid nitrogen inside the storage tank 4 will lower the temperature of the environment around the storage tank 4, so that the air dissipates heat and becomes cold air when passing around the storage tank 4. The cold air passes through the air outlet 53 and enters the inside of the bellows 24 under the action of air pressure. Then, the cold air enters the inside of the equipment cabin 1 again under the action of the fan 14 to cool the chipset 54, thereby improving the utilization of the cold air around the storage tank 4.

[0041] Furthermore, in step S5, the following steps are also included: S51, the staff member grasps the handle 30 and moves it upward, so that the handle 30 drives the sealing plate 29 and the sealing ring 28 to move out of the purification box 26 under the action of external force, so that the sealing plate 29 drives the electrostatic filter material 31 to move out of the inner side of the purification box 26, so as to facilitate the cleaning of the electrostatic filter material 31; S52. The staff member grabs the rotating ring 37 and rotates it, so that the rotating ring 37 drives the threaded plate 36 to rotate under the action of external force, so that the threaded plate 36 uses the threaded action with the round tube 35 to move in the direction away from the equipment cabin 1, and moves the threaded plate 36 out of the inner side of the round tube 35 to release the seal of the round tube 35. Then, the staff member grabs the rotating ring 37 and moves it in the direction away from the equipment cabin 1, so that the rotating ring 37 drives the round plate 39 and the rubber ring 40 to move through the threaded plate 36 and the connecting rod 38, so that the round plate 39 and the rubber ring 40 clean out the dust on the inner side of the round tube 35.

[0042] The working principle of the present invention is as follows: before using the aircraft thermal management system based on jet impingement cooling, it is necessary to check whether the aircraft thermal management system based on jet impingement cooling has problems that affect its use. When the staff needs to use the aircraft thermal management system based on jet impingement cooling, they should first rotate the grab slide plate 21, point the vent 23 of the inner tube 22 toward the middle of the placement plate 3, place the chipset 54 on the top of the placement plate 3, and the temperature sensor 62 detects that the temperature is high, starts the one-way valve 7 and the stop valve 12, and the liquid nitrogen flows from the storage tank 4 through the placement plate 3 into the recovery tank 13. The fan 14 is started to allow the cold air to pass through the ventilation holes 18 and the ventilation holes 23 to dissipate the heat of the chipset 54. Part of the air on the inside of the equipment cabin 1 passes through the return air duct 27 and the purification box 26 to purify the air and enter the wind box 24. The air is then blown into the equipment cabin 1 by the fan 14 to form an air circulation. Another part of the gas in the equipment cabin 1 enters the wind box 24 through the air collecting port 48 to form a second air circulation, making full use of the cold air generated by the liquid nitrogen, and using the liquid nitrogen and wind power to cooperate to improve the heat dissipation effect.

[0043] It will be apparent to those skilled in the art that the invention is not limited to the details of the exemplary embodiments described above and that the invention may be implemented in other specific forms without departing from the spirit or essential features of the invention. Therefore, the embodiments should be considered in all respects as exemplary and non-restrictive, and the scope of the invention is defined by the appended claims rather than the foregoing description, and it is intended that all variations within the meaning and range of equivalent elements of the claims be included in the invention. Any reference numeral in a claim should not be considered to limit the claim to which it relates.

Claims

1. An aircraft thermal management system based on jet impingement cooling, characterized in that: It comprises an equipment cabin (1), a plurality of placement plates (3) are arranged inside the equipment cabin (1), a chipset (54) is placed between two adjacent placement plates (3), a cooling groove (9) is provided inside the placement plates (3), an air cooling component is arranged between two adjacent placement plates (3), and the air cooling component cools the chipset (54); The air cooling assembly comprises two fans (14), and the two fans (14) are installed on the back of the equipment cabin (1) through a connecting component. The output end of the fan (14) is installed with a duct (15). The front of the duct (15) is penetrated by a plurality of connecting pipes (16). The connecting pipes (16) penetrate the back of the equipment cabin (1). A fixed pipe (17) is installed on the outside of the connecting pipe (16), and the fixed pipe (17) is located between two adjacent placement plates (3). A ventilation hole (18) is provided on the front side of the fixed tube (17), a plurality of thin tubes (19) are installed in the ventilation hole (18), and the thin tubes (19) pass through the fixed tube (17) and the interior of the placement plate (3) and communicate with the cooling groove (9), an inner tube (22) is placed on the inner side of the fixed tube (17), and the inner tube (22) is higher than the connecting tube (16), and a ventilation opening (23) is provided on the front side of the inner tube (22), and the ventilation opening (23) is smaller than the ventilation hole (18).

2. The aircraft thermal management system based on jet impingement cooling according to claim 1, characterized in that: The front of the equipment cabin (1) is provided with a door (2) via hinges, a storage tank (4) is installed on the top of a placement plate (3) near the top, the inner side of the storage tank (4) is filled with liquid nitrogen, a temperature sensor (62) is installed on the bottom of the placement plate (3), a transport pipe (5) is installed through one side of the equipment cabin (1), and one end of the transport pipe (5) is connected to the storage tank (4), a plurality of branch pipes (6) are installed through one side of the transport pipe (5) near the equipment cabin (1), a non-return valve (7) is installed on the outer side of the branch pipe (6), a short pipe (8) is installed through one side of the placement plate (3), and one end of the short pipe (8) is connected to the branch pipe (6). The other end of the short pipe (8) is in communication with the cooling trough (9); a recovery pipe (10) is installed through the other side of the equipment cabin (1), and the recovery pipe (10) is in communication with the cooling trough (9); a heat exchanger (11) is installed on the outside of the recovery pipe (10); a stop valve (12) is installed on the outside of the recovery pipe (10), and the stop valve (12) is located at the bottom of the heat exchanger (11); a recovery tank (13) is installed on the inner side of the bottom wall of the equipment cabin (1), and the recovery tank (13) is in communication with one end of the recovery pipe (10); a water collection component is provided on the outside of the transport pipe (5), and the water collection component is used to collect water stains on the outside of the transport pipe (5).

3. The aircraft thermal management system based on jet impingement cooling according to claim 1, characterized in that: A sliding hole (20) is provided on the front side of the fixed tube (17), and the sliding hole (20) is located at the bottom of the ventilation hole (18). A sliding plate (21) is placed inside the sliding hole (20), and the sliding plate (21) is connected to the inner tube (22).

4. The aircraft thermal management system based on jet impingement cooling according to claim 2, characterized in that: A purification component is provided on one side of the equipment cabin (1), and the purification component is used to purify the air inside the equipment cabin (1). The purification component includes a bellows (24), and the bellows (24) is located at the back of the equipment cabin (1). A square hole (25) is provided on one side of the bellows (24). A purification box (26) is installed on one side of the bellows (24), and the bellows (24) is connected to the purification box (26) through the square hole (25). A return air duct (27) is installed on the lower front of the purification box (26), and one end of the return air duct (27) passes through one side of the equipment cabin (1). A sealing ring (28) is placed on the top of the purification box (26), and a sealing plate (29) is installed on the inner side of the sealing ring (28). A handle (30) is installed on the top of the sealing plate (29), and an electrostatic filter material (31) is installed on the bottom of the sealing plate (29). Two limit plates ( The cleaning box (26) is provided with a filter screen (33) on the inner side thereof, and the filter screen (33) is located on the front side of the electrostatic filter material (31). A square tube (34) is installed through the bottom of the cleaning box (26), and the square tube (34) is located on the front side of the filter screen (33). A round tube (35) is installed on the bottom of the square tube (34). A threaded plate (36) is installed on the inner side of the round tube (35). A rotating ring (37) is installed on the side of the threaded plate (36) away from the equipment cabin (1). A connecting rod (38) is installed on the other side of the threaded plate (36). A circular plate (39) is installed on one end of the connecting rod (38). A rubber ring (40) is installed on the outer side of the circular plate (39). A circulation component is provided on the top of the bellows (24). The circulation component is used to improve the utilization of cold air around the storage tank (4).

5. The aircraft thermal management system based on jet impingement cooling according to claim 4, characterized in that: Two square boxes (55) are installed through the top of the wind box (24), a protective net (56) is installed on the inner side of the square box (55), and a fan (57) is installed on the top of the protective net (56). A plurality of cryogenic tubes (58) are installed through the back of the equipment cabin (1), and the cryogenic tubes (58) are located between two adjacent placement plates (3). The cryogenic tubes (58) are communicated with the inner side of the square box (55), and a blowing port (59) is provided on one side of the cryogenic tube (58) close to the chipset (54). A liquid storage tank (60) is provided inside the cryogenic tube (58), and a plurality of through pipes (61) are installed through the top of the cryogenic tube (58), and one end of the through pipes (61) is communicated with the liquid storage tank (60), and the other end of the through pipes (61) is communicated with the cooling tank (9).

6. The aircraft thermal management system based on jet impingement cooling according to claim 2, characterized in that: The water collection component comprises a fine net (41), and the fine net (41) is mounted on the outside of the transport pipe (5). A protective shell (42) is installed on one side of the equipment cabin (1), and the protective shell (42) is located on the outside of the transport pipe (5) and the branch pipe (6). A guide ring (43) is installed on the inside of the protective shell (42). A partition (44) is installed on the inside of the protective shell (42), and the partition (44) is located at the bottom of the guide ring (43). A plurality of fiber rods (45) are installed through the inside of the partition (44). A plurality of leakage pipes (46) are installed through the bottom of the protective shell (42), and the leakage pipes (46) correspond to the fiber rods (45) one by one. The leakage pipes (46) penetrate the inside of the return air pipe (27), and a water collection box (47) is installed at the bottom of the leakage pipe (46).

7. The aircraft thermal management system based on jet impingement cooling according to claim 5, characterized in that: The circulation component comprises an air collecting duct (48), and the air collecting duct (48) is installed through the top of the wind box (24), an air collecting plate (49) is installed on the top of the air collecting duct (48), a guide plate (50) is installed on the top of the air collecting plate (49), a collecting plate (51) is installed at one end of the guide plate (50), and the collecting plate (51) is installed on the back of the equipment cabin (1), and the outer sides of the air collecting duct (48), the air collecting plate (49), the guide plate (50) and the collecting plate (51) are covered with a heat insulation plate (52), and an air outlet (53) is opened through the back of the equipment cabin (1) at a position corresponding to the collecting plate (51).

8. The aircraft thermal management system based on jet impingement cooling according to claim 7, characterized in that: A control module is arranged inside the equipment compartment (1), and the control module comprises a sensing unit and an execution unit; The sensing unit is used to sense the temperature of the chipset (52), and the execution unit is used to use liquid nitrogen and wind power to dissipate the heat of the chipset (52); The sensing unit comprises a temperature sensor (62) arranged at the bottom of the placement plate (3); The execution unit comprises a one-way valve (7) arranged outside the branch pipe (6), a heat exchanger (11) and a stop valve (12) arranged outside the recovery pipe (10), and a fan (14) arranged at the back of the equipment cabin (1). When the temperature sensor (62) senses that the temperature of the chipset (54) has increased, the temperature sensor (62) transmits a start signal to the one-way valve (7), the heat exchanger (11), the stop valve (12) and the fan (14) through an electrical element. The one-way valve (7) and the stop valve (12) are started to transport the liquid nitrogen inside the storage tank (4) through the transport pipe (5) to the inside of the cooling tank (9) for cooling. The liquid nitrogen absorbs heat to generate ammonia and water, which are cooled through the heat exchanger (11) and then recovered to the recovery tank (13) through the recovery pipe (10). The fan (14) is started to dissipate heat by wind.

9. A method for using an aircraft thermal management system based on jet impingement cooling according to any one of claims 1 to 8, characterized in that: The usage is as follows: S1. First, the staff opens the one-way valve (7) and the stop valve (12) at the same time, so that the liquid nitrogen inside the storage tank (4) enters the inside of the cooling tank (9) to absorb the heat inside the placement plate (3). The liquid nitrogen absorbs the heat and decomposes into ammonia and water. The ammonia and water inside the cooling tank (9) enter the inside of the recovery tank (13) through the recovery pipe (10) for storage; S2, the staff then grabs the slide plate (21) and moves it, so that the slide plate (21) drives the inner tube (22) to rotate inside the fixed tube (17), so that the inner tube (22) drives the vent (23) to move to a position facing the middle of the placement plate (3), and then installs the chipset (54) to a position between two adjacent placement plates (3), so that the placement plates (3) absorb the heat inside the chipset (54) through contact, thereby cooling the chipset (54); S3, the staff starts the fan (14), so that the fan (14) blows the air inside the bellows (24) into the inside of the fixed tube (17), so that the air inside the fixed tube (17) passes through the vent (23) and the vent (18) and blows toward the chipset (54), thereby cooling the chipset (54). At the same time, the air contacts the capillary (19), causing the temperature to drop and become cold air, so that the cold air is blown toward the chipset (54), thereby improving the cooling effect of air cooling; S4. When the liquid nitrogen enters the inner side of the transport pipe (5), the temperature of the transport pipe (5) decreases, causing the air around the transport pipe (5) to contact the transport pipe (5) and condense into small water droplets, which drip along the fiber rods (45) to the inner side of the water collecting box (47). The fiber rods (45) seal the partition (44) with water, so that water can only move downward through the fiber rods (45). The water at the bottom of the partition (44) cannot reach the top of the partition (44), so that the water at the top of the partition (44) gradually decreases, thereby reducing the condensation of water on the surface of the transport pipe (5) and reducing the corrosion of the water to the transport pipe (5); S5, air enters the inner side of the equipment cabin (1), causing the air pressure inside the equipment cabin (1) to increase, so that the air inside the equipment cabin (1) enters the inner side of the purification box (26) through the return air duct (27) under the action of the pressure, and the air first contacts the filter (33) in the purification box (26), so that the filter (33) filters out larger dust in the air, and the air passes through the electrostatic filter material (31), and fine particles are adsorbed on the surface of the electrostatic filter material (31), so that the air passing through is purified, and the contact between dust and the chipset (54) is reduced; S6. At the same time, the air inside the equipment cabin (1) moves upward to the location of the storage tank (4) under the action of air pressure. The liquid nitrogen inside the storage tank (4) lowers the temperature of the environment around the storage tank (4), causing the air to dissipate heat and become cold air when passing around the storage tank (4). The cold air passes through the air outlet (53) and enters the inside of the bellows (24) under the action of air pressure. Subsequently, the cold air enters the inside of the equipment cabin (1) again under the action of the fan (14) to cool the chipset (54), thereby improving the utilization of the cold air around the storage tank (4).

10. The method for using the aircraft thermal management system based on jet impingement cooling according to claim 9, characterized in that: In the step S5, the following steps are also included: S51, the staff member grasps the handle (30) and moves it upward, so that the handle (30) drives the sealing plate (29) and the sealing ring (28) to move out of the purification box (26) under the action of external force, so that the sealing plate (29) drives the electrostatic filter material (31) to move out of the inner side of the purification box (26), so as to facilitate the cleaning of the electrostatic filter material (31); S52. The staff member grasps the rotating ring (37) and rotates it, so that the rotating ring (37) drives the threaded plate (36) to rotate under the action of external force, so that the threaded plate (36) moves in a direction away from the equipment cabin (1) by means of the threaded action with the round tube (35), and moves the threaded plate (36) out of the inner side of the round tube (35), thereby releasing the seal on the round tube (35). Then, the staff member grasps the rotating ring (37) and moves it in a direction away from the equipment cabin (1), so that the rotating ring (37) drives the round plate (39) and the rubber ring (40) to move through the threaded plate (36) and the connecting rod (38), so that the round plate (39) and the rubber ring (40) clean out the dust inside the round tube (35).

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