Automatic temperature control steam condensing device of aviation tire vulcanizing machine
By combining the design of drainage, supply, stirring, filtration, drying and gas supply mechanisms, the problem of difficult recovery and reuse of steam and condensate in traditional devices is solved, realizing the filtration of condensate and the drying and reuse of steam, thus improving the practicality of the aircraft tire vulcanizing machine.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- QINGDAO SENTURY TIRE CO LTD
- Filing Date
- 2025-05-20
- Publication Date
- 2026-06-09
AI Technical Summary
Traditional automatic temperature control steam decondensation devices for tire vulcanizing machines are unable to effectively recover and reuse the steam and condensate discharged from aircraft tire vulcanizing machines.
A device was designed that includes mechanisms for draining, supplying, stirring, filtering, drying, and supplying steam. Through the combined use of these mechanisms, condensate and steam are treated and reused. The specific steps include condensate filtration, flocculant stirring, steam drying, and steam supply.
It enables the effective treatment and reuse of condensate and steam, improves the practicality of the equipment, and enhances the performance of the aircraft tire vulcanizing machine.
Smart Images
Figure CN224335138U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the technical field of automatic temperature control steam condensation removal device for tire vulcanizing machines, and in particular to an automatic temperature control steam condensation removal device for aviation tire vulcanizing machines. Background Technology
[0002] The aircraft tire vulcanizing machine is a key piece of equipment specifically designed for the vulcanization of aircraft tires. Through a high-temperature, high-pressure environment, the rubber tire undergoes vulcanization within a precision mold, ensuring that the tire meets the performance requirements for high strength, high-temperature resistance, and impact resistance under extreme conditions. It is an indispensable core piece of equipment in the aircraft tire manufacturing process, directly determining the tire's quality and safety.
[0003] For example, the prior art represented by the automatic temperature control steam condensation device for tire vulcanizing machines disclosed in the utility model patent application number CN202222326069.6 mainly consists of an observation window, a straight ball valve, a controller, a condensation pipe, an alarm, a control box, and a throttle valve. Automatic temperature control steam condensation of the tire vulcanizing machine is achieved through the cooperation of the observation window, the straight ball valve, the controller, the condensation pipe, the alarm, the control box, and the throttle valve.
[0004] Traditional automatic temperature control steam decondensation devices for tire vulcanizing machines have difficulty in recovering and reusing the steam and condensate discharged from the aircraft tire vulcanizing machine during use. Utility Model Content
[0005] To solve the above-mentioned technical problems, this utility model provides an automatic temperature-controlled steam condensate removal device for an aircraft tire vulcanizing machine. The filtered condensate is discharged to the gas supply mechanism via a liquid supply mechanism, and the steam discharged from the aircraft tire vulcanizing machine is discharged to the drying mechanism. The dried steam is then discharged to the aircraft tire vulcanizing machine via the gas supply mechanism. The device also provides steam to the aircraft tire vulcanizing machine by activating the gas supply mechanism, thereby improving the practicality of the equipment.
[0006] This utility model discloses an automatic temperature-controlled steam condensation removal device for an aircraft tire vulcanizing machine, comprising a liquid discharge mechanism; it also includes a liquid supply mechanism, a stirring mechanism, a filtering mechanism, a drying mechanism, and a gas supply mechanism. The liquid discharge mechanism is located between the drying mechanism and the gas supply mechanism, and the liquid discharge mechanism and the liquid supply mechanism are connected. The filtering mechanism is located inside the liquid supply mechanism, and the stirring mechanism is located inside the filtering mechanism. The drying mechanism and the gas supply mechanism are both located to the left of the liquid supply mechanism, and the gas supply mechanism is located in front of the drying mechanism. By activating the liquid discharge mechanism, the condensate from the aircraft tire vulcanizing machine is discharged into the liquid supply mechanism, and then discharged to the filter mechanism. Inside the facility, workers supply flocculant to the filtration unit via the liquid supply mechanism. The stirring mechanism agitates the flocculant and condensate to ensure a thorough reaction. After flocculation, the filtration unit filters out impurities. The filtered condensate is then discharged to the gas supply unit via the liquid supply mechanism. Steam from the aircraft tire vulcanizing machine is discharged to the drying unit for drying. The dried steam is then discharged back into the aircraft tire vulcanizing machine via the gas supply unit, which supplies steam to the machine, thus improving the equipment's usability.
[0007] Preferably, the drainage mechanism includes a first pipe, a control valve, a first centrifugal pump, and a second pipe. The input end of the first pipe is connected to the aircraft tire vulcanizing machine, and a control valve is installed on the first pipe. The output end of the first pipe is connected to the input end of the first centrifugal pump, and the output end of the first centrifugal pump is connected to the input end of the second pipe. The output end of the second pipe is connected to the liquid supply mechanism, and the output end of the second pipe is located above the filtration mechanism. By starting the first centrifugal pump, the condensate in the aircraft tire vulcanizing machine is discharged through the control valve to the second pipe and into the filtration mechanism, thereby improving the practicality of the equipment.
[0008] Preferably, the liquid supply mechanism includes a liquid supply tank, a drug inlet pipe, a third pipe, a second centrifugal pump, and a fourth pipe. The output end of the drug inlet pipe is connected to the top of the liquid supply tank, the input end of the first centrifugal pump is connected to the lower outer wall of the liquid supply tank, the output end of the third pipe is connected to the input end of the second centrifugal pump, the output end of the second centrifugal pump is connected to the input end of the fourth pipe, and the output end of the fourth pipe is connected to the air supply mechanism. The liquid supply tank supports the filtration mechanism. The flocculant is discharged into the filtration mechanism through the drug inlet pipe. By starting the second centrifugal pump, the filtered flocculant is discharged into the air supply mechanism through the third and fourth pipes to supply liquid to the air supply mechanism, thereby improving the practicality of the equipment.
[0009] Preferably, the stirring mechanism includes a first motor, a reducer, a stirring shaft, and multiple sets of stirring blades. The output end of the first motor is connected to the input end of the reducer, and the top end of the stirring shaft is mounted on the output end of the reducer. Multiple stirring blades are provided on the stirring shaft. By starting the first motor and driving it through the reducer, the stirring shaft is slowly rotated. The multiple stirring blades stir the condensate in the filtration mechanism, allowing the condensate and flocculant to react fully and improving the practicality of the equipment.
[0010] Preferably, the filtration mechanism includes a filter barrel, a discharge pipe, a gear ring, a gear, and a second motor. The bottom end of the filter barrel is installed on the input end of the discharge pipe, and the outer wall of the discharge pipe is rotatably installed on the bottom end of the liquid supply tank. A valve is provided on the input end of the discharge pipe. The inner ring of the gear ring is installed on the outer wall of the discharge pipe, and the outer ring of the gear ring meshes with the outer ring of the gear. The inner ring of the gear is installed on the output end of the second motor. By starting the second motor, the gear rotates, and the discharge pipe rotates through the meshing of the gear and the gear ring. The discharge pipe connects to the filter barrel, and the rotating filter barrel filters the condensate, improving the practicality of the equipment.
[0011] Preferably, the drying mechanism includes a fifth pipe, a drying cylinder, a rotating shaft, multiple separation baffles, and a sixth pipe. The inlet end of the fifth pipe is connected to the exhaust port of the aircraft tire vulcanizing machine, and the outlet end of the fifth pipe is connected to the inlet end of the drying cylinder. The two ends of the rotating shaft are rotatably installed inside the drying cylinder. The multiple separation baffles are inclinedly installed on the rotating shaft. The inlet end of the sixth pipe is connected to the bottom end of the drying cylinder, and a valve is installed on the outlet end of the sixth pipe. The outlet end of the sixth pipe is connected to the outer wall of the first pipe and is located to the right of the control valve. Steam is discharged into the drying cylinder through the fifth pipe and then onto the multiple separation baffles. The rotating shaft rotates due to the multiple separation baffles, and the multiple separation baffles separate the moisture in the steam. The separated moisture is discharged through the first pipe, improving the practicality of the equipment.
[0012] Preferably, the gas supply mechanism includes a heating tank, a heater, a three-way pipe, a steam pump, and a seventh pipe. The heater is installed on the outer wall of the heating tank. The three-way pipe has two sets of inlet ends, each equipped with a valve. One set of inlet ends of the three-way pipe is connected to the outer wall of the drying cylinder, and the other set of inlet ends is connected to the top of the heating tank. The outlet end of the three-way pipe is connected to the inlet end of the steam pump, and the outlet end of the steam pump is connected to the inlet end of the seventh pipe. The outlet end of the seventh pipe is connected to the aircraft tire vulcanizing machine. By activating the heater, the liquid inside the heating tank is heated, causing it to steam. By activating the steam pump, the steam is discharged through the three-way pipe and the seventh pipe into the aircraft tire vulcanizing machine, thus supplying steam and improving the practicality of the equipment.
[0013] Compared with the prior art, the beneficial effects of this utility model are as follows: by activating the draining mechanism, the condensate of the aircraft tire vulcanizing machine is discharged into the supply mechanism, and then discharged into the filtration mechanism. The flocculant is discharged into the filtration mechanism by the operator through the supply mechanism. The flocculant and condensate are stirred by activating the stirring mechanism to ensure a full reaction. After flocculation, the impurities after flocculation are filtered by activating the filtration mechanism. The filtered condensate is discharged into the gas supply mechanism by the supply mechanism. The steam discharged from the aircraft tire vulcanizing machine is discharged into the drying mechanism, and the steam is dried by the drying mechanism. The dried steam is discharged into the aircraft tire vulcanizing machine by the gas supply mechanism, and the steam in the aircraft tire vulcanizing machine is supplied by activating the gas supply mechanism, thereby improving the practicality of the equipment. Attached Figure Description
[0014] Figure 1 This is an isometric sectional view of the present invention;
[0015] Figure 2 This is an isometric schematic diagram of the drainage mechanism of this utility model;
[0016] Figure 3 This is an isometric schematic diagram of the liquid supply mechanism of this utility model;
[0017] Figure 4 This is an isometric schematic diagram of the stirring mechanism of this utility model;
[0018] Figure 5 This is an isometric schematic diagram of the filter mechanism of this utility model;
[0019] Figure 6 This is an isometric sectional view of the drying mechanism of this utility model;
[0020] Figure 7 This is an isometric schematic diagram of the gas supply mechanism of this utility model.
[0021] The attached diagram is labeled as follows: 01, Drainage mechanism; 11, First pipe; 12, Control valve; 13, First centrifugal pump; 14, Second pipe; 02, Liquid supply mechanism; 21, Liquid supply tank; 22, Drug inlet pipe; 23, Third pipe; 24, Second centrifugal pump; 25, Fourth pipe; 03, Stirring mechanism; 31, First motor; 32, Reducer; 33, Stirring shaft; 34, Stirring blades; 04, Filtration mechanism; 41, Filter tank; 42, Discharge pipe; 43, Gear ring; 44, Gear; 45, Second motor; 05, Drying mechanism; 51, Fifth pipe; 52, Drying cylinder; 53, Rotating shaft; 54, Separation baffle; 55, Sixth pipe; 06, Gas supply mechanism; 61, Heating tank; 62, Heater; 63, T-connector; 64, Steam pump; 65, Seventh pipe. Detailed Implementation
[0022] To facilitate understanding of this utility model, a more complete description will be given below with reference to the accompanying drawings. This utility model can be implemented in many different forms and is not limited to the embodiments described herein. Rather, these embodiments are provided to make the disclosure of this utility model more thorough and complete.
[0023] Example 1
[0024] like Figure 1 As shown, an automatic temperature-controlled steam decondensation device for an aircraft tire vulcanizing machine includes a draining mechanism 01; it also includes a supplying mechanism 02, a stirring mechanism 03, a filtering mechanism 04, a drying mechanism 05, and a gas supply mechanism 06. The draining mechanism 01 is located between the drying mechanism 05 and the gas supply mechanism 06. The draining mechanism 01 is connected to the supplying mechanism 02. The filtering mechanism 04 is located inside the supplying mechanism 02. The stirring mechanism 03 is located inside the filtering mechanism 04. The drying mechanism 05 and the gas supply mechanism 06 are both located to the left of the supplying mechanism 02. The gas supply mechanism 06 is located in front of the drying mechanism 05.
[0025] The condensate from the aircraft tire vulcanizing machine is discharged to the supply mechanism 02 by activating the drainage mechanism 01, and then discharged to the filtration mechanism 04 via the supply mechanism 02. The flocculant is then discharged to the filtration mechanism 04 via the supply mechanism 02 by the operator. The stirring mechanism 03 is activated to stir the flocculant and condensate, ensuring a thorough reaction. After flocculation, the filtration mechanism 04 is activated to filter the impurities. The filtered condensate is then discharged to the gas supply mechanism 06 via the supply mechanism 02. The steam discharged from the aircraft tire vulcanizing machine is discharged to the drying mechanism 05, where it is dried. The dried steam is then discharged back into the aircraft tire vulcanizing machine via the gas supply mechanism 06, which in turn supplies steam to the machine, improving the equipment's practicality.
[0026] like Figure 2 As shown, the drainage mechanism 01 includes a first pipe 11, a control valve 12, a first centrifugal pump 13, and a second pipe 14. The input end of the first pipe 11 is connected to the aircraft tire vulcanizing machine. The control valve 12 is installed on the first pipe 11. The output end of the first pipe 11 is connected to the input end of the first centrifugal pump 13. The output end of the first centrifugal pump 13 is connected to the input end of the second pipe 14. The output end of the second pipe 14 is connected to the liquid supply mechanism 02, and the output end of the second pipe 14 is located above the filter mechanism 04.
[0027] like Figure 3As shown, the liquid supply mechanism 02 includes a liquid supply tank 21, a drug inlet pipe 22, a third pipe 23, a second centrifugal pump 24, and a fourth pipe 25. The output end of the drug inlet pipe 22 is connected to the top of the liquid supply tank 21, the input end of the third pipe 23 is connected to the lower outer wall of the liquid supply tank 21, the output end of the third pipe 23 is connected to the input end of the second centrifugal pump 24, the output end of the second centrifugal pump 24 is connected to the input end of the fourth pipe 25, and the output end of the fourth pipe 25 is connected to the air supply mechanism 06.
[0028] like Figure 4 As shown, the stirring mechanism 03 includes a first motor 31, a reducer 32, a stirring shaft 33, and multiple sets of stirring blades 34. The output end of the first motor 31 is connected to the input end of the reducer 32. The top end of the stirring shaft 33 is mounted on the output end of the reducer 32. Multiple stirring blades 34 are provided on the stirring shaft 33.
[0029] like Figure 5 As shown, the filtration mechanism 04 includes a filter barrel 41, a discharge pipe 42, a gear ring 43, a gear 44, and a second motor 45. The bottom end of the filter barrel 41 is installed on the input end of the discharge pipe 42. The outer wall of the discharge pipe 42 is rotatably installed on the bottom end of the liquid supply tank 21. A valve is provided on the input end of the discharge pipe 42. The inner ring of the gear ring 43 is installed on the outer wall of the discharge pipe 42. The outer ring of the gear ring 43 meshes with the outer ring of the gear 44. The inner ring of the gear 44 is installed on the output end of the second motor 45.
[0030] The condensate in the aircraft tire vulcanizing machine is discharged through the control valve 12 to the second pipe 14 and then to the filter mechanism 04 by starting the first centrifugal pump 13. The liquid supply tank 21 supports the filter mechanism 04. The flocculant is discharged into the filter mechanism 04 through the inlet pipe 22. The filtered flocculant is discharged through the third pipe 23 to the fourth pipe 25 and then to the air supply mechanism 06 by starting the second centrifugal pump 24. The air supply mechanism 06 is supplied with liquid. The stirring shaft 33 is slowly rotated by starting the first motor 31 and driving the reducer 32. The condensate in the filter mechanism 04 is stirred by multiple stirring blades 34, so that the condensate and flocculant can react fully. The gear 44 is rotated by starting the second motor 45. The gear 44 and the gear ring 43 mesh to rotate the discharge pipe 42. The discharge pipe 42 is connected to the filter barrel 41. The condensate is filtered by the rotation of the filter barrel 41, which improves the practicality of the equipment.
[0031] Example 2
[0032] like Figure 6 and Figure 7As shown, based on Embodiment 1, it also includes a drying mechanism 05 and an air supply mechanism 06. The drying mechanism 05 includes a fifth pipe 51, a drying cylinder 52, a rotating shaft 53, multiple separation baffles 54, and a sixth pipe 55. The input end of the fifth pipe 51 is connected to the exhaust port of the aircraft tire vulcanizing machine, and the output end of the fifth pipe 51 is connected to the input end of the drying cylinder 52. The two ends of the rotating shaft 53 are respectively rotatably installed inside the drying cylinder 52. The multiple separation baffles 54 are respectively inclinedly installed on the rotating shaft 53. The input end of the sixth pipe 55 is connected to the bottom end of the drying cylinder 52, and a valve is provided on the output end of the sixth pipe 55. The output end of the sixth pipe 55 is connected to the outer wall of the first pipe 11. The gas supply mechanism 06 includes a heating tank 61, a heater 62, a three-way pipe 63, a steam pump 64, and a seventh pipe 65. The heater 62 is installed on the outer wall of the heating tank 61. The three-way pipe 63 is provided with two sets of input ends, and valves are provided on the two sets of input ends of the three-way pipe 63 respectively. One set of input ends of the three-way pipe 63 is connected to the outer wall of the drying cylinder 52, and the other set of input ends of the three-way pipe 63 is connected to the top of the heating tank 61. The output end of the three-way pipe 63 is connected to the input end of the steam pump 64. The output end of the steam pump 64 is connected to the input end of the seventh pipe 65. The output end of the seventh pipe 65 is connected to the aircraft tire vulcanizing machine.
[0033] Steam is discharged into the drying cylinder 52 through the fifth pipe 51, and then onto multiple separation baffles 54. The rotating shaft 53 rotates through the multiple separation baffles 54, and the multiple separation baffles 54 separate the moisture in the steam. The separated moisture is discharged through the first pipe 11. The heating tank 61 is heated by starting the heater 62, so that the liquid in the heating tank 61 turns into steam. The steam pump 64 is started, and the steam is discharged into the aircraft tire vulcanizing machine through the three-way pipe 63 via the seventh pipe 65 to supply steam to the machine and improve the practicality of the equipment.
[0034] like Figures 1 to 7As shown, this utility model discloses an automatic temperature-controlled steam condensation device for an aircraft tire vulcanizing machine. During operation, the first centrifugal pump 13 is activated to discharge condensate from the aircraft tire vulcanizing machine through control valve 12 to the second pipe 14 and then to the filter mechanism 04. Next, the liquid supply tank 21 supports the filter mechanism 04, and the flocculant is discharged into the filter mechanism 04 through the inlet pipe 22. The second centrifugal pump 24 is activated to discharge the filtered flocculant through the third pipe 23 to the fourth pipe 25 and then to the gas supply mechanism 06, supplying liquid to the gas supply mechanism 06. Then, the first motor 31 is activated, which, driven by the reducer 32, slowly rotates the stirring shaft 33. Multiple stirring blades 34 stir the condensate in the filter mechanism 04, ensuring a thorough reaction between the condensate and the flocculant. Then, by starting the second motor 45, the gear 44 rotates. The gear 44 meshes with the gear ring 43, causing the discharge pipe 42 to rotate. The discharge pipe 42 is connected to the filter barrel 41. The condensate is filtered by the rotating filter barrel 41. Then, the steam is discharged into the drying cylinder 52 through the fifth pipe 51. The steam is discharged onto multiple separation baffles 54. The rotating shaft 53 rotates through the multiple separation baffles 54. The multiple separation baffles 54 separate the moisture in the steam. The separated moisture is discharged through the first pipe 11. Finally, the heater 62 is started to heat the heating barrel 61, causing the liquid in the heating barrel 61 to turn into steam. The steam pump 64 is started to send the steam through the three-way pipe 63 to the aircraft tire vulcanizing machine through the seventh pipe 65 to supply steam and improve the practicality of the equipment.
[0035] The first centrifugal pump 13, the second centrifugal pump 24, the first motor 31, the reducer 32, the second motor 45, and the heater 62 of this utility model are commercially available. Technical personnel in this industry only need to install and operate them according to the accompanying instruction manual, without requiring any creative work from those skilled in the art.
[0036] The main functions achieved by this utility model are as follows: the filtered condensate is discharged into the gas supply mechanism 06 through the liquid supply mechanism 02, the steam discharged from the aircraft tire vulcanizing machine is discharged into the drying mechanism 05, the steam is dried by the drying mechanism 05, and the dried steam is discharged into the aircraft tire vulcanizing machine through the gas supply mechanism 06. The steam in the aircraft tire vulcanizing machine is supplied by starting the gas supply mechanism 06, thereby improving the practicality of the equipment.
[0037] The above description is only a preferred embodiment of the present utility model. It should be noted that for those skilled in the art, several improvements and modifications can be made without departing from the technical principles of the present utility model, and these improvements and modifications should also be considered within the protection scope of the present utility model.
Claims
1. An automatic temperature-controlled steam condensation device for an aircraft tire vulcanizing machine, comprising a draining mechanism (01); characterized in that, It also includes a liquid supply mechanism (02), a stirring mechanism (03), a filtering mechanism (04), a drying mechanism (05), and a gas supply mechanism (06). The draining mechanism (01) is located between the drying mechanism (05) and the gas supply mechanism (06). The draining mechanism (01) is connected to the liquid supply mechanism (02). The filtering mechanism (04) is located inside the liquid supply mechanism (02). The stirring mechanism (03) is located inside the filtering mechanism (04). The drying mechanism (05) and the gas supply mechanism (06) are both located to the left of the liquid supply mechanism (02). The gas supply mechanism (06) is located in front of the drying mechanism (05).
2. The automatic temperature-controlled steam decondensation device for an aircraft tire vulcanizing machine as described in claim 1, characterized in that, The draining mechanism (01) includes a first pipe (11), a control valve (12), a first centrifugal pump (13), and a second pipe (14). The input end of the first pipe (11) is connected to the aircraft tire vulcanizing machine. The control valve (12) is installed on the first pipe (11). The output end of the first pipe (11) is connected to the input end of the first centrifugal pump (13). The output end of the first centrifugal pump (13) is connected to the input end of the second pipe (14). The output end of the second pipe (14) is connected to the liquid supply mechanism (02). The output end of the second pipe (14) is located above the filter mechanism (04).
3. The automatic temperature-controlled steam decondensation device for an aircraft tire vulcanizing machine as described in claim 2, characterized in that, The liquid supply mechanism (02) includes a liquid supply tank (21), a drug inlet pipe (22), a third pipe (23), a second centrifugal pump (24), and a fourth pipe (25). The output end of the drug inlet pipe (22) is connected to the top of the liquid supply tank (21), the input end of the third pipe (23) is connected to the lower outer wall of the liquid supply tank (21), the output end of the third pipe (23) is connected to the input end of the second centrifugal pump (24), the output end of the second centrifugal pump (24) is connected to the input end of the fourth pipe (25), and the output end of the fourth pipe (25) is connected to the gas supply mechanism (06).
4. The automatic temperature-controlled steam decondensation device for an aircraft tire vulcanizing machine as described in claim 1, characterized in that, The stirring mechanism (03) includes a first motor (31), a reducer (32), a stirring shaft (33), and multiple sets of stirring blades (34). The output end of the first motor (31) is connected to the input end of the reducer (32). The top end of the stirring shaft (33) is installed on the output end of the reducer (32). Multiple stirring blades (34) are provided on the stirring shaft (33).
5. The automatic temperature-controlled steam decondensation device for an aircraft tire vulcanizing machine as described in claim 1, characterized in that, The filtration mechanism (04) includes a filter barrel (41), a discharge pipe (42), a gear ring (43), a gear (44), and a second motor (45). The bottom end of the filter barrel (41) is installed on the input end of the discharge pipe (42). The outer wall of the discharge pipe (42) is rotatably installed on the bottom end of the liquid supply tank (21). A valve is provided on the input end of the discharge pipe (42). The inner ring of the gear ring (43) is installed on the outer wall of the discharge pipe (42). The outer ring of the gear ring (43) meshes with the outer ring of the gear (44). The inner ring of the gear (44) is installed on the output end of the second motor (45).
6. The automatic temperature control steam decondensation device for an aircraft tire vulcanizing machine as described in claim 2, characterized in that, The drying mechanism (05) includes a fifth pipe (51), a drying cylinder (52), a rotating shaft (53), multiple separation baffles (54) and a sixth pipe (55). The input end of the fifth pipe (51) is connected to the exhaust port of the aircraft tire vulcanizing machine, and the output end of the fifth pipe (51) is connected to the input end of the drying cylinder (52). The two ends of the rotating shaft (53) are respectively rotatably installed inside the drying cylinder (52). Multiple separation baffles (54) are respectively inclinedly installed on the rotating shaft (53). The input end of the sixth pipe (55) is connected to the bottom end of the drying cylinder (52). A valve is provided on the output end of the sixth pipe (55). The output end of the sixth pipe (55) is connected to the outer wall of the first pipe (11) and is located to the right of the control valve (12).
7. The automatic temperature control steam decondensation device for an aircraft tire vulcanizing machine as described in claim 6, characterized in that, The gas supply mechanism (06) includes a heating barrel (61), a heater (62), a three-way pipe (63), a steam pump (64), and a seventh pipe (65). The heater (62) is installed on the outer wall of the heating barrel (61). The three-way pipe (63) is provided with two sets of input ends, and valves are provided on the two sets of input ends of the three-way pipe (63). One set of input ends of the three-way pipe (63) is connected to the outer wall of the drying cylinder (52), and the other set of input ends of the three-way pipe (63) is connected to the top of the heating barrel (61). The output end of the three-way pipe (63) is connected to the input end of the steam pump (64), and the output end of the steam pump (64) is connected to the input end of the seventh pipe (65). The output end of the seventh pipe (65) is connected to the aircraft tire vulcanizing machine.