A biological aviation kerosene recovery and separation device

Abstract

The present invention relates to the technical field of distillation and recovery, and discloses a separation device for recovering bio-aviation kerosene, including a support assembly, which includes a horizontal plate, a vertical plate, and a bottom plate. The vertical plate is fixed to the bottom of the horizontal plate, and the bottom plate is fixed to the bottom of the vertical plate; a heating assembly, which is fixed to the support assembly and includes a box body, a heat insulation plate, a fixing plate, a heating box, and a heating plate. Through this solution of the present invention, the waste heat generated during the distillation process can be recovered. As the key parts of the energy recovery system, the condensation assembly and the heat exchange assembly can achieve the transfer of heat from the high-temperature gas to the low-temperature bio-aviation kerosene raw material or other links that need heating. This reuse of heat can significantly reduce the input of external energy, thereby improving the energy utilization efficiency of the entire device, reducing production costs, and also helping to reduce thermal pollution to the environment, promoting the bio-aviation kerosene industry to develop in a more green and sustainable direction.

Description

Technical Field

[0001] The present invention relates to the technical field of distillation recovery, and particularly to a bio - aviation kerosene recovery and separation device. Background Art

[0002] With the rapid development of the global aviation industry, the demand for aviation kerosene continues to increase. At the same time, due to considerations of environmental sustainability and efficient resource utilization, bio - aviation kerosene, as a more environmentally friendly alternative energy source, has received extensive attention. The production of bio - aviation kerosene involves multiple complex processes, among which the recovery and separation link is crucial, and its quality and efficiency directly affect the final performance and production cost of bio - aviation kerosene.

[0003] In the process of bio - aviation kerosene recovery and separation, there are many technical challenges. Among them, the problem of energy consumption is particularly prominent. Taking the distillation operation as an example, it is one of the commonly used methods in the current bio - aviation kerosene recovery and separation process. Distillation is based on the difference in boiling points of different substances. By heating, the mixture is vaporized, and then it is separated into different components through condensation. However, this process of heating and vaporization requires a large amount of energy, which not only increases the production cost but also brings great pressure on the energy supply.

[0004] From the perspective of the overall energy utilization, traditional bio - aviation kerosene recovery and separation devices are often not fully designed to consider the recovery and utilization of energy. The waste heat generated during the distillation process is usually directly discharged into the environment, resulting in a huge waste of energy. This not only does not conform to the development trend of modern industrial energy conservation and emission reduction but also is not conducive to improving the economic benefits of bio - aviation kerosene production. Therefore, how to effectively reduce energy consumption and improve energy utilization efficiency has become an urgent problem in the technical field of bio - aviation kerosene recovery and separation. Summary of the Invention

[0005] The purpose of this part is to outline some aspects of the embodiments of the present invention and briefly introduce some preferred embodiments. Some simplifications or omissions may be made in this part, as well as in the abstract and title of the present application, to avoid obscuring the purpose of this part, the abstract, and the title. However, such simplifications or omissions cannot be used to limit the scope of the present invention.

[0006] In view of the above - mentioned and / or existing problems in the bio - aviation kerosene recovery and separation device, the present invention is proposed.

[0007] Therefore, the problem to be solved by the present invention is that the waste heat generated during the distillation process is usually directly discharged into the environment, resulting in a huge waste of energy.

[0008] To solve the above technical problems, the present invention provides the following technical solution: A biological aviation kerosene recovery and separation device, which includes a support assembly, comprising a horizontal plate, a vertical plate and a bottom plate, the vertical plate is fixed to the bottom of the horizontal plate, and the bottom plate is fixed to the bottom of the vertical plate;

[0009] A heating assembly, fixed to the support assembly, includes a box body, a heat insulation plate, a fixing plate, a heating box and a heating plate. The heat insulation plate is fixed to the inner wall of the box body. The fixing plate is fixedly connected to the bottom of the inner cavity of the box body. One side of the fixing plate away from the inner wall of the box body is fixedly connected to the bottom of the heating box. The heating plate is disposed through the bottom of the heating box;

[0010] A condensing assembly, disposed on one side of the heating assembly, includes a condensing box, a condensing pipe, a first delivery pump and a guiding plate. The condensing pipe is fixed to the inner cavity of the condensing box. The first delivery pump is fixed to the bottom of the condensing box. The first delivery pump is communicated with the condensing pipe. The guiding plate is fixed to the inner wall of the condensing box;

[0011] A recovery assembly, disposed below the condensing assembly, includes a recovery box and a connecting plate. The connecting plate is fixed to the top of the recovery box. The top of the connecting plate is fixedly connected to the condensing assembly;

[0012] A heat exchange assembly, fixed to one side of the condensing assembly, includes a heat exchange box, a net plate member and a heat exchange member. The net plate member is disposed through the top of the heat exchange box. The heat exchange member is disposed through one side of the heat exchange box. The net plate member includes a net plate main body and a sealing plate. The sealing plate is fixed to the top of the net plate main body. Uniformly distributed fixing screws are disposed through the top of the sealing plate. Fixing screw holes are formed in the top of the heat exchange box for cooperating with the fixing screws. The sealing plate and the heat exchange box are fixed by the fixing screws and the fixing screw holes. The heat exchange member includes a first heat conducting plate, a second heat conducting plate, heat exchange fins and heat conducting rods. The second heat conducting plate is fixed to one side of the first heat conducting plate. The heat exchange fins are uniformly fixed to the other side of the first heat conducting plate. The heat conducting rods are uniformly fixed to the side of the second heat conducting plate away from the first heat conducting plate;

[0013] A water bath assembly, fixed to the support assembly, includes a water storage tank and an oil storage tank. The oil storage tank is fixed to the bottom of the inner cavity of the water storage tank. One side of the oil storage tank is communicated with an oil filling pipe. One end of the oil filling pipe away from the oil storage tank penetrates to the outside of the water storage tank;

[0014] The heating box is communicated with the condensing box. The condensing box is communicated with the heat exchange box. One side of the top of the heat exchange box is communicated with an exhaust pipe. One side of the heat exchange member is communicated with the inner cavity of the water storage tank through the heat conducting rod for transferring the heat absorbed by the heat exchange assembly to the water storage tank.

[0015] As a preferred embodiment of the biological aviation kerosene recovery and separation device of the present invention, the following is provided: temperature sensors are respectively arranged through both sides of the top of the surface of the heating box, a liquid level sensor is arranged through the surface of the heating box and between the two temperature sensors, a vertical pipe is communicated with the top of the heating box, a residual discharge pipe is communicated with one side of the heating box, and the residual discharge pipe penetrates to the outside of the box body.

[0016] As a preferred embodiment of the biological aviation kerosene recovery and separation device of the present invention, the following is provided: a junction box, a controller and a backup power supply are respectively fixedly connected to the top of the bottom plate, the junction box is located on one side of the controller, the backup power supply is located on the other side of the controller, and anti-slip pads are respectively fixedly connected to both sides of the bottom of the bottom plate.

[0017] As a preferred embodiment of the biological aviation kerosene recovery and separation device of the present invention, the following is provided: a second delivery pump is fixedly connected to the bottom of the cross plate, the second delivery pump is communicated with the storage tank, the second delivery pump is communicated with a delivery pipe, and the delivery pipe is communicated with the heating box.

[0018] As a preferred embodiment of the biological aviation kerosene recovery and separation device of the present invention, the following is provided: a liquid guide groove and a delivery groove are respectively formed at the bottom of the inner cavity of the condensation box, the liquid guide groove is communicated with the delivery groove, a recovery pipe is communicated with the inner wall of the delivery groove, and the recovery pipe is communicated with the recovery box.

[0019] As a preferred embodiment of the biological aviation kerosene recovery and separation device of the present invention, the following is provided: a fixing sleeve is sleeved on the surface of the condensation pipe, a support plate is fixedly connected to the surface of the fixing sleeve, the support plate is fixedly connected to the inner wall of the condensation box, a cross pipe is communicated with one end of the condensation pipe far away from the first delivery pump, and the cross pipe is communicated with the water storage tank.

[0020] As a preferred embodiment of the biological aviation kerosene recovery and separation device of the present invention, the following is provided: a door body is movably connected to the surface of the box body through a hinge, a nameplate is fixedly connected to one side of the top of the front of the box body, an observation window is arranged through the left side of the front of the water storage tank, and a control panel is fixedly connected to the right side of the front of the water storage tank.

[0021] The beneficial effects of the present invention are as follows: through this solution, the waste heat generated during the distillation process can be recovered. The condensation component and the heat exchange component, as the key parts of the energy recovery system, can realize the transfer of heat from the high-temperature gas to the low-temperature biological aviation kerosene raw material or other links that need heating. This reuse of heat can significantly reduce the input of external energy, thereby improving the energy utilization efficiency of the entire device, reducing production costs, and also helping to reduce the thermal pollution to the environment, promoting the biological aviation kerosene industry to develop in a more green and sustainable direction. BRIEF DESCRIPTION OF THE DRAWINGS

[0022] To more clearly illustrate the technical solutions of the embodiments of the present invention, the following will briefly introduce the accompanying drawings required for the description of the embodiments. Obviously, the accompanying drawings in the following description are only some embodiments of the present invention. For those of ordinary skill in the art, without creative efforts, other accompanying drawings can be obtained based on these drawings. Among them:

[0023] Figure 1 It is a three-dimensional view of the first perspective structure of the bio-aviation kerosene recovery and separation device.

[0024] Figure 2 It is a three-dimensional view of the second perspective structure of the bio-aviation kerosene recovery and separation device.

[0025] Figure 3 It is a three-dimensional sectional view of the box body of the bio-aviation kerosene recovery and separation device.

[0026] Figure 4 It is a three-dimensional view of the partial structure of the bio-aviation kerosene recovery and separation device.

[0027] Figure 5 It is a three-dimensional sectional view of the condensation box of the bio-aviation kerosene recovery and separation device.

[0028] Figure 6 It is a three-dimensional sectional view of the heat exchange box of the bio-aviation kerosene recovery and separation device.

[0029] Figure 7 It is a three-dimensional sectional view of the water storage tank of the bio-aviation kerosene recovery and separation device.

[0030] Figure 8 It is a three-dimensional view of the recovery box of the bio-aviation kerosene recovery and separation device. Detailed implementation manners

[0031] To make the above objects, features, and advantages of the present invention more obvious and understandable, the following will make a detailed description of the specific implementation manners of the present invention in conjunction with the accompanying drawings of the specification.

[0032] In the following description, many specific details are set forth to fully understand the present invention. However, the present invention can also be implemented in other ways different from those described herein. Those skilled in the art can make similar generalizations without departing from the connotation of the present invention. Therefore, the present invention is not limited by the specific embodiments disclosed below.

[0033] Secondly, the so-called "one embodiment" or "embodiment" herein refers to a specific feature, structure, or characteristic that can be included in at least one implementation manner of the present invention. The phrase "in one embodiment" appearing in different places in this specification does not necessarily refer to the same embodiment, nor is it a separate or alternative embodiment that mutually excludes other embodiments. Example 1

[0034] Reference Figures 1-8 , which is the first embodiment of the present invention. This embodiment provides a device for recovering and separating bio - aviation kerosene. The device for recovering and separating bio - aviation kerosene includes a support assembly 100, which includes a cross - plate 101, a vertical plate 102, and a bottom plate 103. The vertical plate 102 is fixed to the bottom of the cross - plate 101, and the bottom plate 103 is fixed to the bottom of the vertical plate 102.

[0035] The support assembly 100 is used for support and fixation. The bottom of the cross - plate 101 and the top of the vertical plate 102 are fixedly connected by welding. The bottom of the vertical plate 102 and the top of the bottom plate 103 are fixedly connected by welding. The welding connection method can ensure the firmness of the workpiece connection, thereby improving the bearing capacity of the support assembly 100.

[0036] A heating assembly 200, fixed on the support assembly 100, includes a box body 201, a heat - insulating plate 202, a fixing plate 203, a heating box 204, and a heating plate 205. The heat - insulating plate 202 is fixed to the inner wall of the box body 201. The fixing plate 203 is fixedly connected to the bottom of the inner cavity of the box body 201. One side of the fixing plate 203 away from the inner wall of the box body 201 is fixedly connected to the bottom of the heating box 204. The heating plate 205 is disposed through the bottom of the heating box 204.

[0037] The heating assembly 200 is used to heat the bio - aviation kerosene. The box body 201 cooperates with the heat - insulating plate 202 to block the heat, thereby preventing heat loss during the heating process, improving the thermal energy utilization rate, saving heating energy. The fixing plate 203 is used to connect the heating box 204 and the box body 201, and at the same time is used to stably support the heating box 204. The heating plate 205 cooperates with the heating box 204 to heat the bio - aviation kerosene.

[0038] A condensing assembly 300, disposed on one side of the heating assembly 200, includes a condensing box 301, a condensing pipe 302, a first delivery pump 303, and a guiding plate 304. The condensing pipe 302 is fixed to the inner cavity of the condensing box 301. The first delivery pump 303 is fixed to the bottom of the condensing box 301. The first delivery pump 303 is communicated with the condensing pipe 302. The guiding plate 304 is fixed to the inner wall of the condensing box 301.

[0039] The condensing assembly 300 is used to condense the steam. A water inlet pipe is communicated with the surface of the first delivery pump 303. By connecting the water inlet pipe with an external normal - temperature water source by the user and starting the first delivery pump 303, the first delivery pump 303 works to deliver the water body to the condensing pipe 302. The condensing pipe 302 cooperates with the water body to cool down the steam. At this time, the water body is heated. The guiding plate 304 can guide the flow of the steam, increasing the contact area between the steam and the condensing pipe 302, thereby ensuring the condensing effect.

[0040] The recovery component 400 is arranged below the condensation component 300 and includes a recovery tank 401 and a connection plate 402. The connection plate 402 is fixed to the top of the recovery tank 401, and the top of the connection plate 402 is fixedly connected to the condensation component 300.

[0041] The condensed liquid is collected through the recovery component 400. The bottom of the connection plate 402 and the top of the recovery tank 401 are fixedly connected by welding. The top of the connection plate 402 and the bottom of the condensation tank 301 are fixedly connected by welding. The welding connection method can ensure the firmness of the workpiece connection. The recovery tank 401 is used for temporarily storing the recovered liquid.

[0042] The heat exchange component 500 is fixed to one side of the condensation component 300 and includes a heat exchange tank 501, a mesh plate member 502, and a heat exchange member 503. The mesh plate member 502 is disposed through the top of the heat exchange tank 501, and the heat exchange member 503 is disposed through one side of the heat exchange tank 501.

[0043] The condensation tank 301 transports the condensed gas to the heat exchange tank 501. At this time, the gas still has residual heat. The gas is refined through the mesh plate member 502, so that the gas is evenly transported to the surface of the heat exchange member 503 to ensure the heat exchange effect. The heat exchange member 503 can absorb the residual heat of the gas.

[0044] The water bath component 600 is fixed to the support component 100 and includes a water storage tank 601 and an oil storage tank 602. The oil storage tank 602 is fixed to the bottom of the inner cavity of the water storage tank 601. One side of the oil storage tank 602 is communicated with a fuel filling pipe 6021, and one end of the fuel filling pipe 6021 away from the oil storage tank 602 penetrates to the outside of the water storage tank 601.

[0045] The heated water body of the condensation component 300 is transported to the water storage tank 601. The heat absorbed by the heat exchange member 503 reheats the water body inside the water storage tank 601. The hot water inside the water storage tank 601 can preheat the bio-aviation kerosene in the oil storage tank 602, thereby reducing the heat required for the heating component 200 to heat the bio-aviation kerosene. In addition, the hot water inside the water storage tank 601 can also be transported to a designated position through a water delivery device for utilization, improving the energy utilization rate. The fuel filling pipe 6021 is used for replenishing the bio-aviation kerosene. Embodiment 2

[0046] Refer to Figures 1-8 , which is the second embodiment of the present invention. This embodiment is based on the previous embodiment.

[0047] Specifically, temperature sensors 2041 are penetrated and arranged on both sides of the top surface of the heating box 204, a liquid level sensor 2042 is penetrated and arranged on the surface of the heating box 204 and between the two temperature sensors 2041, a vertical pipe 2043 is communicated with the top of the heating box 204, a residual liquid discharge pipe 2044 is communicated with one side of the heating box 204, and the residual liquid discharge pipe 2044 penetrates to the outside of the box body 201.

[0048] The number of the temperature sensors 2041 is two. The temperature inside the heating box 204 can be accurately detected through the two temperature sensors 2041, so as to realize accurate temperature control. The liquid level sensor 2042 is used to detect the liquid level height inside the heating box 204, so as to timely supplement bio-aviation kerosene and avoid dry burning damage to the heating box 204 and the heating plate 205. Opening the vertical pipe 2043 can balance the internal and external pressures when adding bio-aviation kerosene, and the residual liquid discharge pipe 2044 can discharge the residual liquid.

[0049] Specifically, a junction box 1031, a controller 1032 and a backup power supply 1033 are respectively fixedly connected to the top of the bottom plate 103. The junction box 1031 is located on one side of the controller 1032, and the backup power supply 1033 is located on the other side of the controller 1032. Anti-slip pads 1034 are fixedly connected to both sides of the bottom of the bottom plate 103.

[0050] The junction box 1031 is used for connecting and transporting electric energy. The controller 1032 is used for circuit control. The circuit connection mode and control program belong to the prior art, so they will not be elaborated in this application document. The backup power supply 1033 is used for storing and providing electric energy, so as to provide temporary power supply when power is cut off. The anti-slip pads 1034 can increase the friction force, so as to improve the stability of the bio-aviation kerosene recovery and separation device during use.

[0051] Specifically, a second delivery pump 1011 is fixedly connected to the bottom of the cross plate 101. The second delivery pump 1011 is communicated with the storage oil tank 602, and the second delivery pump 1011 is communicated with a delivery pipe 1012. The delivery pipe 1012 is communicated with the heating box 204.

[0052] When the liquid level sensor 2042 monitors that the bio-aviation kerosene inside the heating box 204 is lacking, the second delivery pump 1011 is started. The second delivery pump 1011 works to deliver the preheated bio-aviation kerosene to the delivery pipe 1012, and the delivery pipe 1012 delivers the preheated bio-aviation kerosene to the inner cavity of the heating box 204, so as to supplement the bio-aviation kerosene.

[0053] Specifically, a liquid guide groove 3011 and a delivery groove 3012 are respectively formed at the bottom of the inner cavity of the condensation box 301. The liquid guide groove 3011 is communicated with the delivery groove 3012, and a recovery pipe 3013 is communicated with the inner wall of the delivery groove 3012. The recovery pipe 3013 is communicated with the recovery box 401.

[0054] The liquid condensed by the condenser tube 302 is transported to the conveying tank 3012 through the liquid guiding groove 3011. The conveying tank 3012 transports the liquid to the recovery pipe 3013, and the recovery pipe 3013 transports the liquid to the recovery tank 401. The recovery tank 401 collects and temporarily stores the liquid, and a valve is connected to the surface of the recovery tank 401, which can discharge the recovered liquid.

[0055] Specifically, a fixing sleeve 3021 is sleeved on the surface of the condenser tube 302. A support plate 3022 is fixedly connected to the surface of the fixing sleeve 3021, and the support plate 3022 is fixedly connected to the inner wall of the condensation box 301. One end of the condenser tube 302 far from the first delivery pump 303 is communicated with a horizontal tube 3023, and the horizontal tube 3023 is communicated with the water storage tank 601.

[0056] The fixing sleeve 3021 is clamped and fixed with the condenser tube 302. The fixing sleeve 3021 is used to support and fix the condenser tube 302. The support plate 3022 is used to install the fixing sleeve 3021 on the inner wall of the condensation box 301. The horizontal tube 3023 is used to transport hot water into the inner cavity of the water storage tank 601. Embodiment 3

[0057] Refer to Figures 1-8 , which is the third embodiment of the present invention, and this embodiment is based on the first two embodiments.

[0058] Specifically, the mesh plate member 502 includes a mesh plate main body 5021 and a sealing plate 5022. The sealing plate 5022 is fixed to the top of the mesh plate main body 5021. Fixing screws 5023 evenly distributed are arranged through the top of the sealing plate 5022. Fixing screw holes matching with the fixing screws 5023 are formed in the top of the heat exchange box 501. The sealing plate 5022 and the heat exchange box 501 are fixedly connected through the fixing screws 5023 and the fixing screw holes.

[0059] The mesh plate main body 5021 is used to guide and disperse the gas, so as to ensure the heat exchange effect. The sealing plate 5022 is used to seal the heat exchange box 501. When the mesh plate main body 5021 is not needed, the user can remove the fixing screws 5023 with tools, so that the sealing plate 5022 and the mesh plate main body 5021 can be disassembled, and then the sealing plate 5022 can be installed alone.

[0060] Specifically, the heat exchange member 503 includes a first heat conducting plate 5031, a second heat conducting plate 5032, heat exchange fins 5033 and heat conducting rods 5034. The second heat conducting plate 5032 is fixed to one side of the first heat conducting plate 5031. The heat exchange fins 5033 are evenly fixed to the other side of the first heat conducting plate 5031. The heat conducting rods 5034 are evenly fixed to the side of the second heat conducting plate 5032 far from the first heat conducting plate 5031.

[0061] The evenly distributed heat exchange fins 5033 can efficiently absorb the residual heat in the exhaust gas. The heat is transferred to the first heat conducting plate 5031 through the heat exchange fins 5033, then to the second heat conducting plate 5032 by the first heat conducting plate 5031, and then to the heat conducting rod 5034 by the second heat conducting plate 5032. The evenly distributed heat conducting rods 5034 can heat the water body, thus realizing the recovery of waste heat.

[0062] Specifically, the heating box 204 is communicated with the condensation box 301, the condensation box 301 is communicated with the heat exchange box 501, and a exhaust pipe 5011 is communicated with one side of the top of the heat exchange box 501.

[0063] The exhaust pipe 5011 is used to discharge the gas after waste heat recovery.

[0064] Specifically, a door body 2011 is movably connected to the surface of the box body 201 through a hinge. A nameplate 2012 is fixedly connected to one side of the top of the front surface of the box body 201. An observation window 6011 is arranged through the left side of the front surface of the water storage tank 601, and a control panel 6012 is fixedly connected to the right side of the front surface of the water storage tank 601.

[0065] A sealing body is arranged at the connection between the door body 2011 and the box body 201. The sealing body can ensure the sealing performance at the connection between the door body 2011 and the box body 201, thus avoiding heat loss. The user can open the door body 2011 to repair the components in the inner cavity of the box body 201. The relevant information of the bio - aviation kerosene recovery and separation device is marked on the surface of the nameplate 2012, which is convenient for the user to understand and use the bio - aviation kerosene recovery and separation device. The observation window is used to observe the liquid level of the water body, so as to timely transport the excess hot water to the designated place for use and avoid excessive water. The control panel 6012 is used to input control signals and display working information.

[0066] During use, the heat is blocked by the box body 201 in cooperation with the heat insulation plate 202, thereby preventing heat loss during the heating process, improving the utilization rate of thermal energy, saving heating energy, the fixing plate 203 is used to connect the heating box 204 and the box body 201, and at the same time is used to stably support the heating box 204, the heating plate 205 cooperates with the heating box 204 to heat the bio-aviation kerosene, the steam generated inside the heating box 204 is transported to the condensation box 301, a water inlet pipe is communicated with the surface of the first transfer pump 303, by the user connecting the water inlet pipe with an external normal temperature water source, starting the first transfer pump 303, the first transfer pump 303 works to transport the water body to the condensation pipe 302, the steam is cooled by the cooperation of the condensation pipe 302 and the water body, at this time the water body is heated, the guiding plate 304 can guide the flow of the steam, increasing the contact area between the steam and the condensation pipe 302, thereby ensuring the condensation effect, the condensed liquid is collected by the recovery assembly 400, the condensation box 301 transports the condensed gas to the heat exchange box 501, at this time the gas still has residual heat, the gas is refined by the mesh plate part 502, so that the gas is evenly transported to the surface of the heat exchange part 503, ensuring the heat exchange effect, the heat exchange part 503 can absorb the residual heat of the gas, the water body heated by the condensation assembly 300 is transported to the water storage tank 601, the heat absorbed by the heat exchange part 503 reheats the water body inside the water storage tank 601, the hot water inside the water storage tank 601 can preheat the bio-aviation kerosene in the fuel storage tank 602, thereby reducing the heat required for the heating assembly 200 to heat the bio-aviation kerosene, in addition, the hot water inside the water storage tank 601 can also be transported to a designated position through a water delivery device for utilization, improving the energy utilization rate.

[0067] It should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention and not to limit them. Although the present invention has been described in detail with reference to the preferred embodiments, those of ordinary skill in the art should understand that the technical solutions of the present invention can be modified or equivalently replaced without departing from the spirit and scope of the technical solutions of the present invention, and they should all be covered within the scope of the claims of the present invention.

Claims

1. A biological aviation kerosene recovery and separation device, characterized in that: including, a support component (100), comprising a horizontal plate (101), a vertical plate (102) and a bottom plate (103), wherein the vertical plate (102) is fixed to the bottom of the horizontal plate (101), and the bottom plate (103) is fixed to the bottom of the vertical plate (102); a heating component (200), fixed on the support component (100), comprising a box body (201), a heat insulation plate (202), a fixing plate (203), a heating box (204) and a heating plate (205), wherein the heat insulation plate (202) is fixed to the inner wall of the box body (201), the fixing plate (203) is fixedly connected to the bottom of the inner cavity of the box body (201), one side of the fixing plate (203) away from the inner wall of the box body (201) is fixedly connected to the bottom of the heating box (204), and the heating plate (205) is disposed through the bottom of the heating box (204); a condensation component (300), disposed on one side of the heating component (200), comprising a condensation box (301), a condensation pipe (302), a first delivery pump (303) and a guiding plate (304), wherein the condensation pipe (302) is fixed to the inner cavity of the condensation box (301), the first delivery pump (303) is fixed to the bottom of the condensation box (301), the first delivery pump (303) is communicated with the condensation pipe (302), and the guiding plate (304) is fixed to the inner wall of the condensation box (301); a recovery component (400), disposed below the condensation component (300), comprising a recovery box (401) and a connecting plate (402), wherein the connecting plate (402) is fixed to the top of the recovery box (401), and the top of the connecting plate (402) is fixedly connected to the condensation component (300); The heat exchange component (500), fixed to one side of the condensation component (300), includes a heat exchange box (501), a mesh plate component (502) and a heat exchange component (503). The mesh plate component (502) is disposed through the top of the heat exchange box (501), and the heat exchange component (503) is disposed through one side of the heat exchange box (501). The mesh plate component (502) includes a mesh plate main body (5021) and a sealing plate (5022). The sealing plate (5022) is fixed to the top of the mesh plate main body (5021). The top of the sealing plate (5022) is provided with uniformly distributed fixing screws (5023) therethrough. The top of the heat exchange box (501) is provided with fixing screw holes for cooperating with the fixing screws (5023). The sealing plate (5022) and the heat exchange box (501) are fixedly connected by the fixing screws (5023) and the fixing screw holes. The heat exchange component (503) includes a first heat conducting plate (5031), a second heat conducting plate (5032), heat exchange fins (5033) and heat conducting rods (5034). The second heat conducting plate (5032) is fixed to one side of the first heat conducting plate (5031). The heat exchange fins (5033) are uniformly fixed to the other side of the first heat conducting plate (5031). The heat conducting rods (5034) are uniformly fixed to the side of the second heat conducting plate (5032) away from the first heat conducting plate (5031). The water bath component (600), fixed to the support component (100), includes a water storage tank (601) and an oil storage tank (602). The oil storage tank (602) is fixed to the bottom of the inner cavity of the water storage tank (601) and is completely immersed in the water body of the inner cavity of the water storage tank (601). One side of the oil storage tank (602) is communicated with an oil filling pipe (6021). One end of the oil filling pipe (6021) away from the oil storage tank (602) penetrates to the outside of the water storage tank (601). The heating box (204) is communicated with the condensation box (301), the condensation box (301) is communicated with the heat exchange box (501). One side of the top of the heat exchange box (501) is communicated with an exhaust pipe (5011). One side of the heat exchange component (503) is communicated with the inner cavity of the water storage tank (601) through the heat conducting rod (5034) for transferring the heat absorbed by the heat exchange component (500) to the water storage tank (601).

2. The biological aviation kerosene recovery and separation device according to claim 1, characterized in that: Both sides of the top surface of the heating box (204) are provided with temperature sensors (2041) therethrough. A liquid level sensor (2042) is disposed through the surface of the heating box (204) and between the two temperature sensors (2041). The top of the heating box (204) is communicated with a vertical pipe (2043). One side of the heating box (204) is communicated with a waste discharge pipe (2044). The waste discharge pipe (2044) penetrates to the outside of the box body (201).

3. The biological aviation kerosene recovery and separation device according to claim 1, characterized in that: On the top of the bottom plate (103), a junction box (1031), a controller (1032), and a backup power supply (1033) are fixedly connected respectively. The junction box (1031) is located on one side of the controller (1032), and the backup power supply (1033) is located on the other side of the controller (1032). Anti-slip pads (1034) are fixedly connected to both sides of the bottom of the bottom plate (103).

4. The biological aviation kerosene recovery and separation device according to claim 1, characterized in that: A second delivery pump (1011) is fixedly connected to the bottom of the cross plate (101). The second delivery pump (1011) is communicated with the fuel tank (602). The second delivery pump (1011) is communicated with a delivery pipe (1012), and the delivery pipe (1012) is communicated with the heating tank (204).

5. The bio-aviation kerosene recovery and separation device according to claim 1, characterized in that: A liquid guide groove (3011) and a delivery groove (3012) are respectively formed at the bottom of the inner cavity of the condensation tank (301). The liquid guide groove (3011) is communicated with the delivery groove (3012). A recovery pipe (3013) is communicated with the inner wall of the delivery groove (3012), and the recovery pipe (3013) is communicated with the recovery tank (401).

6. The biological aviation kerosene recovery and separation device according to claim 1, characterized in that: A fixing sleeve (3021) is sleeved on the surface of the condensation pipe (302). A support plate (3022) is fixedly connected to the surface of the fixing sleeve (3021). The support plate (3022) is fixedly connected to the inner wall of the condensation tank (301). One end of the condensation pipe (302) far away from the first delivery pump (303) is communicated with a cross pipe (3023), and the cross pipe (3023) is communicated with the water storage tank (601).

7. The biological aviation kerosene recovery and separation device according to claim 1, characterized in that: A door body (2011) is movably connected to the surface of the box body (201) through a hinge. A nameplate (2012) is fixedly connected to one side of the top of the front surface of the box body (201). An observation window is arranged through the left side of the front surface of the water storage tank (601), and a control panel (6012) is fixedly connected to the right side of the front surface of the water storage tank (601).

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