Thermoelectric integrated comprehensive support equipment applied to polar plateau area

Abstract

The invention relates to the technical field of thermoelectric integrated equipment, and discloses thermoelectric integrated comprehensive guarantee equipment applied to a polar plateau district, the thermoelectric integrated comprehensive guarantee equipment comprises a combustion chamber, a combustion fan and an air inlet pipeline, the interior of the combustion chamber is fixedly connected with the outer surface of the air inlet pipeline, and an air outlet of the combustion fan is fixedly connected with the interior of the air inlet pipeline; the combustion chamber conducts combustion-supporting combustion operation on the interior of the combustion chamber through the transmission effect of the air inlet pipeline and the wind power combustion-supporting mechanism. According to the thermoelectric integrated comprehensive guarantee equipment applied to the polar plateau area, through the use of a large gear and a small gear, the wind speed can be increased, power input during combustion supporting is improved, wind power generated by a combustion-supporting fan can enter the combustion chamber, combustion-supporting combustion operation is conducted on the interior of the combustion chamber through a wind-power combustion-supporting mechanism, and the combustion-supporting effect is improved. The effects of providing combustion-supporting wind power for the combustion chamber and guaranteeing the smooth proceeding of the combustion process are achieved, and the combustion efficiency in reality is further improved.

Description

Technical Field

[0001] This invention relates to the field of thermoelectric integrated equipment technology, specifically a thermoelectric integrated comprehensive support equipment applied in extremely high-altitude areas. Background Technology

[0002] Extreme plateau regions typically refer to areas with altitudes above 5,000 meters and extremely harsh natural environments, characterized by low pressure and lack of oxygen, extreme temperature differences, strong radiation, and complex terrain. In response to the special environment of extreme plateau regions, integrated thermal power support equipment achieves energy self-sufficiency and efficient utilization by integrating technologies such as diesel hybrid power generation and waste heat recovery, meeting diverse needs such as heating, oxygen bar, and equipment operation.

[0003] Existing integrated thermal power support equipment has been put into practical use in extremely high-altitude areas (such as border outposts, scientific research stations and field camps on the Qinghai-Tibet Plateau). Through diesel hybrid power generation and waste heat recovery and utilization technology, it can stably supply power and heat in extreme low temperature and low oxygen environments, effectively solving the problem of difficult supply of traditional energy.

[0004] When using diesel-electric hybrid power generation, combustion fans are required. These fans are typically electrically driven. However, in high-altitude areas with weak or off-grid power grids, power outages can directly paralyze the combustion system. Long-term reliance on electricity significantly increases the burden on the fuel system. Furthermore, since the electricity comes from diesel generators, it negates the environmental benefits of combustion optimization. In remote high-altitude areas, this reduces the overall reliability and sustainability of the equipment. Moreover, the abundant wind energy resources on the plateau are not being integrated, resulting in a waste of natural energy and reducing the equipment's practical utilization efficiency.

[0005] Although the combustion-supporting fan can be driven by wind power for combustion assistance, insufficient wind speed will reduce its effectiveness, thus affecting the efficiency of diesel power generation. When the wind speed decreases or there are no wind intermittent periods, the speed and air supply of the combustion-supporting fan will decrease accordingly, resulting in insufficient oxygen supply to the combustion chamber and incomplete combustion of diesel fuel. This not only reduces the thermal energy conversion efficiency but also produces a large amount of unburned carbon particles and carbon monoxide, among other harmful substances. Incomplete combustion will also cause fluctuations in the generator set's output power, seriously affecting the quality of power supply. Furthermore, the inability to uniformly distribute the combustion-supporting air into the combustion chamber during combustion will further affect the power generation efficiency. Uneven distribution of the combustion-supporting air will cause an imbalance in the temperature field within the combustion chamber, potentially leading to localized areas of overheating at high temperatures or flameout at low temperatures, further deteriorating combustion efficiency and reducing the overall effectiveness of the equipment in actual use. Summary of the Invention

[0006] To address the shortcomings of existing technologies, this invention provides an integrated thermal and power support equipment applicable to extremely high-altitude regions. It has the advantages of utilizing wind power for combustion assistance and further improving the efficiency of wind-assisted combustion, thus solving the problems mentioned in the background technology.

[0007] The present invention provides the following technical solution: a thermal power integrated support equipment for use in extremely high-altitude areas, comprising a combustion chamber, a combustion-supporting fan and an air inlet duct, wherein the interior of the combustion chamber is fixedly connected to the outer surface of the air inlet duct, the air outlet of the combustion-supporting fan is fixedly connected to the interior of the air inlet duct, and the combustion chamber performs combustion-supporting operation through the transmission action of the air inlet duct and the wind-powered combustion-supporting mechanism. The wind-powered combustion mechanism has a wind-power inlet end connected to a wind-power acceleration conversion mechanism that converts wind power into rotation. The wind-power acceleration mechanism has a wind-power uniform entry mechanism connected to its power output end. The wind-power acceleration conversion mechanism has an air intake mechanism connected to its air intake end. The air intake mechanism ensures high efficiency of air intake by changing its own position. The wind speed conversion mechanism changes the wind force entering the combustion chamber by varying the wind force, and the wind force uniform entry mechanism can uniformly deliver the wind force entering the combustion chamber. The wind-powered combustion-aiding mechanism includes a wind speed-up conversion mechanism, a wind uniform entry mechanism, and an air intake mechanism.

[0008] Preferably, the wind power acceleration conversion mechanism includes a combustion shell, an extension plate, a fixing block, a first connecting shaft, fan blades, a large gear, a small gear, a second connecting shaft, and air inlet blades. The inner wall of the combustion shell is fixedly installed to the outer surface of the combustion chamber. The left side of the extension plate is fixedly connected to the right side of the combustion shell. The bottom of the fixing block is fixedly installed to the top of the extension plate. The outer surface of the first connecting shaft is rotatably connected to the inner wall of the fixing block. One side of the fan blade is fixedly connected to the outer surface of the first connecting shaft. The inside of the large gear is fixedly installed to the outer surface of the first connecting shaft. The outer surface of the small gear meshes with the outer surface of the large gear. The outer surface of the second connecting shaft is fixedly connected to the inside of the small gear.

[0009] Preferably, the wind uniform entry mechanism includes a first pulley, a drive belt, a second pulley, a third connecting shaft, and uniform blades. The interior of the first pulley is fixedly installed on the outer surface of one end of the second connecting shaft. The inner ring of the drive belt is drivenly connected to the outer surface of the first pulley. The outer surface of the second pulley is drivenly connected to the inner ring of the drive belt. The outer surface of the third connecting shaft is fixedly installed on the interior of the second pulley. One side of the uniform blades is fixedly installed on the outer surface of the third connecting shaft. The outer surface of the third connecting shaft is rotatably connected to the inner wall of the air inlet duct.

[0010] Preferably, the air intake mechanism includes a protective box, an air intake guide pipe, and a filter screen. The bottom of the protective box is fixedly connected to the top of the extension plate. The outer surface of the bottom end of the air intake guide pipe is rotatably snapped into the inner wall of the protective box. The outer surface of the filter screen is fixedly installed inside the air intake guide pipe. An impurity discharge groove is provided on one side of the inside of the air intake guide pipe.

[0011] Preferably, the outer surface of the connecting shaft is rotatably connected to the inner wall of the combustion-supporting blower, a connecting pipe is fixedly installed at the air outlet end of the combustion-supporting blower, a sealing block is fixedly installed on the outer surface of the connecting pipe, and the surface of the sealing block is fixedly installed with the inside of the air inlet pipe.

[0012] Preferably, a mounting base is fixedly installed on the upper surface of the extension plate, and the upper surface of the mounting base is fixedly connected to the bottom of the combustion fan.

[0013] Preferably, a sealing cover is installed on the upper surface of the combustion shell, a gallium nitride igniter is provided inside the back of the combustion shell, a connecting pipe is fixedly installed inside the combustion shell, an oil pyrolysis tank is fixedly installed on the outer surface of one end of the connecting pipe, an oil inlet is provided inside the oil pyrolysis tank, and an atomizing nozzle is fixedly installed on one end of the connecting pipe.

[0014] Preferably, an oil seepage plate is fixedly installed inside the combustion shell, and an inclined baffle is fixedly installed inside the combustion shell, with the inclined baffle positioned above the combustion chamber.

[0015] Preferably, a thermoelectric generator is connected inside the combustion shell. The output end of the thermoelectric generator is fixedly connected to a first transmission pipe. A heat dissipation component is fixedly connected to the outer surface of one end of the first transmission pipe. A second transmission pipe is fixedly installed at the output end of the thermoelectric generator. A heat exchange chamber is fixedly connected to the outer surface of one end of the second transmission pipe. A heat conduction plate is provided at the output end of the heat exchange chamber.

[0016] Preferably, the combustion shell is internally connected to an exhaust gas inlet pipe, and a waste heat recovery device is fixedly connected to the outer surface of one end of the exhaust gas inlet pipe. The output end of the waste heat recovery device is fixedly connected to a combustion-supporting outlet pipe, and the outer surface of one end of the combustion-supporting outlet pipe is fixedly installed with the inner wall of the combustion chamber.

[0017] Compared with the prior art, the present invention has the following beneficial effects: 1. This integrated thermoelectric support equipment, applied in extremely high-altitude areas, uses large and small gears to increase wind speed, thereby increasing power input during combustion. The wind generated by the combustion fan enters the combustion chamber and, through the wind-assisted combustion mechanism, performs combustion-assisted combustion operations inside the combustion chamber, achieving the effect of providing combustion-assisted wind to the combustion chamber, ensuring the smooth progress of the combustion process, and further improving combustion efficiency in practice.

[0018] 2. This integrated thermoelectric support equipment, applied in extremely high-altitude areas, uses pulley one and pulley two in conjunction with the transmission belt to efficiently transmit the high-speed rotational power of connecting shaft two to connecting shaft three, which allows the airflow to enter the combustion chamber evenly.

[0019] 3. This integrated thermal power support equipment, applied in extremely high-altitude areas, features a rotating air intake duct that automatically adjusts its azimuth angle according to wind direction. The use of filters and impurity discharge channels prevents the accumulation of sand from affecting the airflow, further improving air intake efficiency in practice. Attached Figure Description

[0020] Figure 1 This is a schematic diagram of the overall structure of the device of the present invention; Figure 2 For the present invention Figure 1 A top-view structural diagram; Figure 3 For the present invention Figure 1 Internal structure diagram; Figure 4 For the present invention Figure 1 A schematic diagram of the rear structure; Figure 5 For the present invention Figure 1 Schematic diagram of the cross-sectional structure; Figure 6 For the present invention Figure 1 Partial structural diagram; Figure 7 For the present invention Figure 1 A schematic diagram of the combustion-supporting component structure.

[0021] In the diagram: 1. Combustion shell; 2. Sealing cover; 3. Combustion chamber; 4. Gallium nitride igniter; 5. Fuel pyrolysis tank; 6. Connecting pipe; 7. Atomizing nozzle; 8. Oil seepage plate; 9. Sloping baffle; 10. Oil inlet; 11. Thermoelectric generator assembly; 12. Transmission pipe one; 13. Heat dissipation assembly; 14. Transmission pipe two; 15. Heat exchange chamber; 16. Heat transfer plate; 17. Waste heat recovery unit; 18. Exhaust gas inlet pipe; 19. Combustion aid outlet pipe; 20. Extension plate; 21. Protective shield. 21. Protective housing; 22. Inlet air guide pipe; 23. Filter screen; 24. Impurity discharge groove; 25. Mounting base; 26. Combustion fan; 27. Connecting pipe; 28. Inlet air pipe; 29. ​​Sealing block; 30. Fixing block; 31. Connecting shaft one; 32. Fan blades; 33. Large gear; 34. Small gear; 35. Connecting shaft two; 36. Inlet air blades; 37. Belt pulley one; 38. Drive belt; 39. Belt pulley two; 40. Connecting shaft three; 41. Uniform blades. Detailed Implementation

[0022] The following will clearly and completely describe the technical solutions in the embodiments of the present invention in conjunction with the accompanying drawings. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0023] Please see Figure 7 A comprehensive thermoelectric support equipment for use in extremely high-altitude areas includes a combustion chamber 3, a combustion-supporting fan 26, and an air inlet duct 28. The interior of the combustion chamber 3 is fixedly connected to the outer surface of the air inlet duct 28, and the air outlet of the combustion-supporting fan 26 is fixedly connected to the interior of the air inlet duct 28. The combustion chamber 3 performs combustion-supporting operation through the transmission of the air inlet duct 28 and through the wind-powered combustion-supporting mechanism. The wind-powered combustion mechanism has a wind-powered inlet end connected to a wind-powered speed-up conversion mechanism that converts wind power into rotation. The power output end of the wind-powered speed-up mechanism is connected to a wind-powered uniform inlet mechanism, and the air inlet end of the wind-powered speed-up conversion mechanism is connected to an air inlet mechanism. The air inlet mechanism ensures the high efficiency of air intake by changing its own position. The wind speed conversion mechanism changes the wind force entering the combustion chamber 3 by varying the wind force, and the wind force uniform entry mechanism can uniformly deliver the wind force entering the combustion chamber 3. The wind-powered combustion mechanism includes a wind speed-up conversion mechanism, a wind speed uniform entry mechanism, and an air intake mechanism. The wind speed-up conversion mechanism includes a combustion shell 1, an extension plate 20, a fixing block 30, a connecting shaft 31, a fan blade 32, a large gear 33, a small gear 34, a connecting shaft 35, and an air intake blade 36. The inner wall of the combustion shell 1 is fixedly installed to the outer surface of the combustion chamber 3. The left side of the extension plate 20 is fixedly connected to the right side of the combustion shell 1. The bottom of the fixing block 30 is fixedly installed to the top of the extension plate 20. The outer surface of the connecting shaft 31 is rotatably connected to the inner wall of the fixing block 30. One side of the fan blade 32 is connected to the outer surface of the connecting shaft 31. The large gear 33 is fixedly connected to the outer surface of the connecting shaft 31. The outer surface of the small gear 34 meshes with the outer surface of the large gear 33. The outer surface of the connecting shaft 35 is fixedly connected to the inner surface of the small gear 34. The outer surface of the connecting shaft 35 is rotatably connected to the inner wall of the combustion fan 26. A connecting pipe 27 is fixedly installed at the air outlet of the combustion fan 26. A sealing block 29 is fixedly installed on the outer surface of the connecting pipe 27. The surface of the sealing block 29 is fixedly installed to the inner surface of the air inlet pipe 28. A mounting base 25 is fixedly installed on the upper surface of the extension plate 20. The upper surface of the mounting base 25 is fixedly connected to the bottom of the combustion fan 26.

[0024] Specifically, the large gear 33 meshes with the small gear 34, and the small gear 34 is rotatably connected to the inner wall of the combustion fan 26 via the connecting shaft 25. This structural combination realizes the conversion of wind power into rotation and changes the rotation speed through gear transmission. In turn, the wind power entering the combustion chamber 3 is adjusted according to different wind conditions, thereby improving the wind power conversion efficiency and flexibly adjusting the wind power to meet the combustion requirements. The wind power generated by the combustion fan 26 can smoothly enter the combustion chamber 3 through the connecting pipe 27 and the air inlet pipe 28. At the same time, the sealing block 29 plays a sealing role to prevent wind power leakage, thereby ensuring the effective transmission of wind power and improving the combustion effect.

[0025] Please see Figure 7 The wind uniform entry mechanism includes a pulley 37, a drive belt 38, a pulley 39, a connecting shaft 40, and uniform blades 41. The interior of the pulley 37 is fixedly installed on the outer surface of one end of the connecting shaft 35. The inner ring of the drive belt 38 is connected to the outer surface of the pulley 37. The outer surface of the pulley 39 is connected to the inner ring of the drive belt 38. The outer surface of the connecting shaft 40 is fixedly installed on the interior of the pulley 39. One side of the uniform blades 41 is fixedly installed on the outer surface of the connecting shaft 40. The outer surface of the connecting shaft 40 is rotatably connected to the inner wall of the air inlet duct 28.

[0026] Specifically, with the help of the transmission belt 38, when the connecting shaft 2 35 drives the pulley 1 37 to rotate, the power can be smoothly and effectively transmitted to the pulley 2 39, achieving stable long-distance power transmission and ensuring the coordinated work between different components. After the pulley 2 39 obtains power through the transmission belt 38, it rotates, and the connecting shaft 3 40 fixedly installed inside it rotates accordingly, thereby driving the uniform blades 41 fixed on the outer surface of the connecting shaft 3 40 to rotate. The rotation of the uniform blades 41 can stir and guide the air force entering the air intake duct 28, achieving the effect of making the air force entering the combustion chamber 3 more uniform, optimizing the combustion effect, and the adjusted air force is further homogenized before being sent into the combustion chamber 3. This realizes a continuous process of air force from acceleration to uniform distribution, achieving the effect of improving combustion efficiency, making combustion more complete and stable, and improving the performance of the entire thermoelectric integrated protection equipment.

[0027] Please see Figure 6 The air intake mechanism includes a protective box 21, an air intake guide pipe 22, and a filter screen 23. The bottom of the protective box 21 is fixedly connected to the top of the extension plate 20. The outer surface of the bottom end of the air intake guide pipe 22 is rotatably snapped onto the inner wall of the protective box 21. The outer surface of the filter screen 23 is fixedly installed inside the air intake guide pipe 22. An impurity discharge groove 24 is provided on one side of the inside of the air intake guide pipe 22.

[0028] Specifically, the bottom of the protective box 21 is fixedly connected to the top of the extension plate 20. The extension plate 20 provides a stable and suitable installation position for the protective box 21, which in turn protects the internal components from damage caused by external environmental factors such as collisions, rain, and sandstorms. This ensures the overall structural stability and safety of the air intake mechanism. The bottom outer surface of the air intake guide pipe 22 is rotatably engaged with the inner wall of the protective box 21. This design allows the air intake guide pipe 22 to rotate at a certain angle within the protective box 21. During air intake, the angle of the air intake guide pipe 22 can be flexibly adjusted according to changes in the external wind direction, making the air intake smoother and more efficient. This improves air intake efficiency and adapts to different wind conditions. The filter 23 effectively filters dust, impurities, and other particulate matter from the air, preventing these impurities from entering critical parts such as the combustion chamber 3 and affecting the normal operation and service life of the equipment. This ensures the cleanliness of the air entering the equipment. Impurities intercepted by the filter 23 can be discharged from the air intake pipe 22 through the impurity discharge groove 24 under the action of gravity or airflow. This avoids impurities accumulating and clogging the filter 23 in the air intake pipe 22, thus affecting the air intake effect. This ensures that the filter 23 remains unobstructed and maintains the long-term stable operation of the air intake mechanism. All the structures work together. The protective box 21 provides protection and a mounting base, the air intake pipe 22 allows for flexible air intake, the filter 23 filters air impurities, and the impurity discharge groove 24 discharges the intercepted impurities. Together, they ensure that the equipment can obtain a clean, sufficient, and stable air supply in extremely high-altitude areas, thereby improving the overall performance and reliability of the equipment.

[0029] Please see Figure 1 , Figure 2 , Figure 3 and Figure 4A sealing cover 2 is installed on the upper surface of the combustion shell 1. A gallium nitride igniter 4 is installed inside the back of the combustion shell 1. A connecting pipe 6 is fixedly installed inside the combustion shell 1. An oil pyrolysis tank 5 is fixedly installed on the outer surface of one end of the connecting pipe 6. An oil inlet 10 is provided inside the oil pyrolysis tank 5. An atomizing nozzle 7 is fixedly installed at one end of the connecting pipe 6. An oil seepage plate 8 is fixedly installed inside the combustion shell 1. An inclined baffle 9 is fixedly installed inside the combustion shell 1 and is positioned above the combustion chamber 3. A thermoelectric generator assembly 11 is connected inside the combustion shell 1. The output end of the combustion chamber 1 is fixedly connected to a transmission pipe 12. A heat dissipation component 13 is fixedly connected to the outer surface of one end of the transmission pipe 12. A transmission pipe 14 is fixedly installed at the output end of the thermoelectric generator 11. A heat exchange chamber 15 is fixedly connected to the outer surface of one end of the transmission pipe 14. A heat conduction plate 16 is provided at the output end of the heat exchange chamber 15. An exhaust gas inlet pipe 18 is connected inside the combustion chamber 1. A waste heat recovery device 17 is fixedly connected to the outer surface of one end of the exhaust gas inlet pipe 18. A combustion-supporting outlet pipe 19 is fixedly connected to the output end of the waste heat recovery device 17, and the outer surface of one end of the combustion-supporting outlet pipe 19 is fixedly installed to the inner wall of the combustion chamber 3.

[0030] Specifically, the sealing cover 2 is installed on the upper surface of the combustion shell 1, and the two fit together tightly to form a relatively enclosed space. This effectively prevents the loss of heat generated during combustion, improves combustion efficiency, and prevents external impurities from entering the combustion shell 1 and interfering with the combustion process. This achieves the effect of ensuring a stable combustion environment and improving combustion thermal efficiency. The gallium nitride igniter 4 is located inside the back of the combustion shell 1. Utilizing the high-performance characteristics of gallium nitride material, it can quickly generate a high-temperature electric spark at a lower voltage, accurately igniting the combustible mixture in the combustion chamber 3. This ensures the timeliness and reliability of ignition, enabling the equipment to start smoothly and burn stably even in harsh environments such as extremely high-altitude areas, thus improving the equipment's ignition performance and adaptability. Fuel enters the fuel pyrolysis chamber 5 through the fuel inlet 10. After specific treatment within the fuel pyrolysis chamber 5, it is transported to the atomizing nozzle 7 through the connecting pipe 6. The atomizing nozzle 7 atomizes the fuel into fine particles, allowing it to mix thoroughly with air to form a uniform combustible mixture. This combination improves the combustion efficiency of the fuel, making combustion more complete, reducing fuel waste and pollutant emissions, and achieving the effect of optimizing the combustion process and improving energy utilization. The fuel permeation plate 8 is fixedly installed inside the combustion shell 1. It allows the fuel to slowly and evenly permeate out, further controlling the fuel supply and supply speed. In conjunction with the atomizing nozzle 7, it can more precisely adjust the concentration of the combustible mixture, ensuring the stability and controllability of the combustion process, achieving the effect of finely adjusting combustion parameters and improving combustion quality. The high temperature generated during combustion creates a temperature difference on both sides of the thermoelectric generator 11, thereby generating electricity. Electrical energy is transmitted to the heat dissipation component 13 through transmission pipe 12. The heat dissipation component 13 dissipates excess heat to ensure the normal operation of the thermoelectric generator component 11. At the same time, some electrical energy is transmitted to the heat exchange chamber 15 through transmission pipe 14. The heat exchange chamber 15 transfers heat to other parts that need to be heated through the heat transfer plate 16, realizing the secondary utilization of energy. This combination realizes combined heat and power, improves the comprehensive utilization efficiency of energy, and achieves the effect of improving the energy utilization efficiency of equipment. The exhaust gas generated by combustion enters the waste heat recovery unit 17 through the exhaust gas inlet pipe 18. The waste heat recovery unit 17 recovers the residual heat in the exhaust gas and heats it. The heated gas is then transported to the combustion chamber 3 as combustion gas through the combustion-supporting outlet pipe 19. This not only reduces the waste of exhaust gas heat and improves energy utilization, but also uses the recovered heat to preheat the combustion-supporting gas, making the combustion more complete and further improving the combustion efficiency, thus achieving the effects of energy saving, emission reduction, and improved combustion effect.

[0031] Working principle: In use, under the low-oxygen environment of extremely high-altitude areas, the combustion-supporting blower 26 delivers air to the combustion chamber 3 through the air inlet duct 28. The wind-powered combustion mechanism further optimizes combustion efficiency using natural wind energy. When the outside airflow enters the air inlet guide pipe 22, the filter screen 23 filters impurities, which are discharged through the impurity outlet trough 24. Then, the airflow impacts the blower blades 32, driving the connecting shaft 31 to rotate. Through the meshing transmission of the large gear 33 and the small gear 34, the low-speed wind power is converted into the high-speed rotation of the connecting shaft 35, driving the combustion-supporting blower 26 to increase pressure. At the same time, the pulley 37 drives the pulley 39 to rotate via the transmission belt 38, making... The uniform blades 41 rotate within the air inlet duct 28, distributing the airflow evenly to the combustion chamber 3. Within the combustion chamber 3, fuel enters the fuel cracking box 5 from the fuel inlet 10, is cracked, and then sprayed out through the atomizing nozzle 7. After mixing with the uniform airflow, the fuel is ignited by the gallium nitride igniter 4. The high-temperature gas heats the thermoelectric generator 11 to generate electricity. The waste heat is introduced into the heat dissipation component 13 and the heat exchange chamber 15 through the first transmission pipe 12 and the second transmission pipe 14, respectively. The latter outputs heat energy through the heat transfer plate 16. The exhaust gas enters the waste heat recovery unit 17 through the exhaust gas inlet pipe 18 to preheat the combustion air, and finally returns to the combustion chamber 3 through the combustion outlet pipe 19, forming a closed-loop high-efficiency thermodynamic cycle.

[0032] It should be noted that the electrical components and equipment mentioned above all use external power sources. The circuits, electronic components, and modules involved in this invention are all existing technologies, which can be fully implemented by those skilled in the art, and need not be elaborated upon. The scope of protection of this invention does not involve improvements to the internal structure and methods. Furthermore, in this document, relational terms such as "first" and "second" are used only to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Moreover, the terms "comprising," "including," or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements includes not only those elements but also other elements not expressly listed, or elements inherent to such a process, method, article, or apparatus.

[0033] While embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions, and variations may be made to these embodiments without departing from the principles and spirit of the invention, and that the scope of the invention is defined by the appended claims and their equivalents.

Claims

1. A comprehensive thermoelectric support system for use in extremely high-altitude regions, characterized in that: It includes a combustion chamber (3), a combustion-supporting fan (26), and an air inlet duct (28). The interior of the combustion chamber (3) is fixedly connected to the outer surface of the air inlet duct (28), and the outlet of the combustion-supporting fan (26) is fixedly connected to the interior of the air inlet duct (28). The combustion chamber (3) performs combustion-supporting operation inside the combustion chamber (3) through the transmission action of the air inlet duct (28) and through the wind-powered combustion-supporting mechanism. The wind-powered combustion mechanism has a wind-power inlet end connected to a wind-power acceleration conversion mechanism that converts wind power into rotation. The wind-power acceleration mechanism has a wind-power uniform entry mechanism connected to its power output end. The wind-power acceleration conversion mechanism has an air intake mechanism connected to its air intake end. The air intake mechanism ensures high efficiency of air intake by changing its own position. The wind speed conversion mechanism makes the wind entering the combustion chamber (3) change continuously by the different wind forces, and the wind uniform entry mechanism can uniformly deliver the wind entering the combustion chamber (3). The wind-powered combustion-aiding mechanism includes a wind speed-up conversion mechanism, a wind uniform entry mechanism, and an air intake mechanism.

2. The integrated thermoelectric support equipment for use in extremely high-altitude areas according to claim 1, characterized in that: The wind power acceleration conversion mechanism includes a combustion shell (1), an extension plate (20), a fixing block (30), a connecting shaft one (31), a fan blade (32), a large gear (33), a small gear (34), a connecting shaft two (35), and an air inlet blade (36). The inner wall of the combustion shell (1) is fixedly installed with the outer surface of the combustion chamber (3). The left side of the extension plate (20) is fixedly connected with the right side of the combustion shell (1). The bottom of the fixing block (30) is fixedly installed with the top of the extension plate (20). The outer surface of the connecting shaft one (31) is rotatably connected with the inner wall of the fixing block (30). One side of the fan blade (32) is fixedly connected with the outer surface of the connecting shaft one (31). The interior of the large gear (33) is fixedly installed with the outer surface of the connecting shaft one (31). The outer surface of the small gear (34) meshes with the outer surface of the large gear (33). The outer surface of the connecting shaft two (35) is fixedly connected with the interior of the small gear (34).

3. The integrated thermoelectric support equipment for use in extremely high-altitude areas according to claim 2, characterized in that: The wind uniform entry mechanism includes a pulley one (37), a transmission belt (38), a pulley two (39), a connecting shaft three (40), and uniform blades (41). The interior of the pulley one (37) is fixedly installed on the outer surface of one end of the connecting shaft two (35). The inner ring of the transmission belt (38) is connected to the outer surface of the pulley one (37). The outer surface of the pulley two (39) is connected to the inner ring of the transmission belt (38). The outer surface of the connecting shaft three (40) is fixedly installed on the interior of the pulley two (39). One side of the uniform blades (41) is fixedly installed on the outer surface of the connecting shaft three (40). The outer surface of the connecting shaft three (40) is rotatably connected to the inner wall of the air inlet duct (28).

4. The integrated thermoelectric support equipment for use in extremely high-altitude areas according to claim 2, characterized in that: The air intake mechanism includes a protective box (21), an air intake guide pipe (22), and a filter screen (23). The bottom of the protective box (21) is fixedly connected to the top of the extension plate (20). The outer surface of the bottom end of the air intake guide pipe (22) is rotatably snapped into the inner wall of the protective box (21). The outer surface of the filter screen (23) is fixedly installed inside the air intake guide pipe (22). An impurity discharge groove (24) is provided on one side of the inside of the air intake guide pipe (22).

5. The integrated thermoelectric support equipment for use in extremely high-altitude areas according to claim 2, characterized in that: The outer surface of the connecting shaft 2 (35) is rotatably connected to the inner wall of the combustion fan (26). A connecting pipe (27) is fixedly installed at the air outlet of the combustion fan (26). A sealing block (29) is fixedly installed on the outer surface of the connecting pipe (27). The surface of the sealing block (29) is fixedly installed inside the air inlet pipe (28).

6. The integrated thermoelectric support equipment for use in extremely high-altitude areas according to claim 2, characterized in that: An mounting base (25) is fixedly installed on the upper surface of the extension plate (20), and the upper surface of the mounting base (25) is fixedly connected to the bottom of the combustion fan (26).

7. The integrated thermoelectric support equipment for use in extremely high-altitude areas according to claim 2, characterized in that: A sealing cover plate (2) is installed on the upper surface of the combustion shell (1). A gallium nitride igniter plug (4) is provided inside the back of the combustion shell (1). A connecting pipe (6) is fixedly installed inside the combustion shell (1). An oil pyrolysis tank (5) is fixedly installed on the outer surface of one end of the connecting pipe (6). An oil inlet (10) is provided inside the oil pyrolysis tank (5). An atomizing nozzle (7) is fixedly installed at one end of the connecting pipe (6).

8. The integrated thermoelectric support equipment for use in extremely high-altitude areas according to claim 2, characterized in that: An oil seepage plate (8) is fixedly installed inside the combustion shell (1), and an inclined baffle (9) is fixedly installed inside the combustion shell (1), with the inclined baffle (9) positioned above the combustion chamber (3).

9. The integrated thermoelectric support equipment for use in extremely high-altitude areas according to claim 2, characterized in that: The combustion shell (1) is equipped with a thermoelectric generator assembly (11) inside. The output end of the thermoelectric generator assembly (11) is fixedly connected to a transmission pipe (12). A heat dissipation assembly (13) is fixedly connected to the outer surface of one end of the transmission pipe (12). A transmission pipe (14) is fixedly installed at the output end of the thermoelectric generator assembly (11). A heat exchange chamber (15) is fixedly connected to the outer surface of one end of the transmission pipe (14). A heat transfer plate (16) is provided at the output end of the heat exchange chamber (15).

10. The integrated thermoelectric support equipment for use in extremely high-altitude areas according to claim 2, characterized in that: The combustion shell (1) is connected to an exhaust gas inlet pipe (18). A waste heat recovery device (17) is fixedly connected to the outer surface of one end of the exhaust gas inlet pipe (18). A combustion-supporting outlet pipe (19) is fixedly connected to the output end of the waste heat recovery device (17). The outer surface of one end of the combustion-supporting outlet pipe (19) is fixedly installed with the inner wall of the combustion chamber (3).

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