CN220466382U

CN220466382U - Aviation oil storage device

Info

Publication number: CN220466382U
Application number: CN202321709715.5U
Authority: CN
Inventors: 马义川; 董祐诚; 付铭; 陈渝
Original assignee: Avic Southwest Storage And Transportation Co ltd
Current assignee: Avic Southwest Storage And Transportation Co ltd
Priority date: 2023-07-03
Filing date: 2023-07-03
Publication date: 2024-02-09
Anticipated expiration: 2033-07-03

Abstract

The utility model relates to the technical field of aviation oil tanks and discloses an aviation oil storage device which comprises an outer shell and an inner shell, wherein a cavity is formed between the outer wall of the outer shell and the inner wall of the inner shell, a temperature sensor is fixedly arranged on the inner wall of the inner shell, a refrigeration component for cooling aviation oil is fixedly sleeved on the outer wall of the inner shell, and radiating fins are uniformly distributed on the outer wall of the refrigeration component. According to the utility model, through the cooperation among the temperature sensor, the heating assembly, the junction box and the inner shell, the heating effect on aviation oil in the inner shell is realized by utilizing the arrangement of the heating assembly, the problem of slow heating of the cylindrical heating plate in the technical content is effectively solved, and the contact area between the heating plate and the inner shell is increased by adopting the mode that the heating plate in the heating assembly is wound on the outer wall of the inner shell, so that the heating speed of aviation oil is increased, and the heating efficiency of aviation oil is improved.

Description

Aviation oil storage device

Technical Field

The utility model relates to the technical field of aviation fuel tanks, in particular to an aviation fuel storage device.

Background

Aviation fuel can also be called aviation fuel, and refers to a fuel variety specially designed for an aircraft, has higher quality than fuel used by a heating system and an automobile, and generally contains different additives to reduce the risks of icing and explosion caused by high temperature, and is stored by a storage device.

The existing aviation oil storage device is simple in structure and single in function, cannot achieve a good heat preservation effect in colder areas, and is quite easy to freeze; in addition, the current storage device cannot regulate the temperature of the fuel oil in the storage device according to the external condition, cannot resist the influence caused by bad weather, and has poor practicability, so in order to improve the practicability of the aviation fuel oil storage device, the technical structure for controlling the temperature of the storage device is proposed in the prior art to assist the use of the storage device, for example, the patent of the utility model with the publication number of CN202120823260.4 is presented, and the utility model provides an aviation fuel oil anti-icing storage device which comprises a storage tank body; the storage tank is internally provided with a heat preservation inner cavity, the space between the storage tank and the heat preservation inner cavity is vacuumized, the top end of the outer edge surface of the storage tank is electroplated with an insulating layer, one side of the storage tank is fixedly provided with an oil pump, one end of the oil pump, which faces the storage tank, is fixedly connected with a liquid outlet pipe which extends into the heat preservation inner cavity, the other end of the oil pump is fixedly provided with a temperature regulating copper pipe, one end of the temperature regulating copper pipe, which is far away from the oil pump, is fixedly connected with a liquid taking pipe which extends into the heat preservation inner cavity, and the outer edge surface of the liquid taking pipe is fixedly provided with a valve I; the top of the outer edge surface of the temperature-adjusting copper pipe is fixedly provided with a cylindrical heating piece, and the bottom of the outer edge surface of the temperature-adjusting copper pipe is fixedly provided with a cylindrical refrigerating piece. Through adopting above-mentioned technical scheme, when the weather is cold or hot, can open the oil pump and pass through liquid pipe, temperature adjusting copper pipe and drain pipe, accomplish the circulation of fuel, make the continuous bottom of fuel of bottom take out to the top, rethread cartridge heating piece or cartridge refrigeration piece heat or cool down it, can adjust and control inside fuel temperature according to external condition to resist the influence that bad weather brought, the practicality is stronger.

From the above disclosure, in theory, implementation of the related technical structure is beneficial to control the temperature of the aviation oil in the storage device, but according to the description of the above disclosure, it can be known that the temperature of the aviation oil is controlled by the barrel type refrigerating plate and the barrel type heating plate for controlling the temperature of the oil in the temperature adjusting copper pipe, the oil is pumped from the storage tank to the temperature adjusting copper pipe and then is controlled, and then returned to the storage tank, at this time, because the flow rate of the temperature adjusting copper pipe for passing the oil is limited, the volume in the storage tank is too large, and the temperature of the oil in the storage tank can be excessively long due to the adoption of the mode of circularly heating the oil entering the temperature adjusting copper pipe, so that the temperature controlling efficiency of the oil is reduced by the temperature controlling device, and the utilization rate of the barrel type refrigerating plate and the barrel type heating plate is reduced.

Disclosure of Invention

Aiming at the defects of the prior art, the utility model provides an aviation oil storage device which has the advantages of realizing the real-time monitoring of the internal temperature of the storage device, accelerating the speed of increasing and decreasing the temperature of the oil in the storage device and improving the efficiency of increasing and decreasing the temperature of the oil, and solves the problems in the prior art.

The utility model provides the following technical scheme: the utility model provides an aviation oil storage device, includes shell body, inner shell body, form the cavity between the outer wall of shell body and the inner wall of inner shell body, the inner wall fixed mounting of inner shell body has temperature sensor, the outer wall fixed sleeve of inner shell body has been used for cooling aviation oil's refrigeration subassembly, the outer wall evenly distributed of refrigeration subassembly has radiating fin, the outer wall fixed mounting of inner shell body has the heating element who is used for heating aviation oil, the heating element distributes including the outer wall of shell body with refrigeration subassembly is crisscross, the left side fixed mounting of shell body has the terminal box, and the external power that has of terminal box, the upper end fixed mounting of inner shell body has the oil outlet pipe that is located the shell body top.

Preferably, the lower terminal surface fixed mounting of shell body has the base, the outer wall evenly distributed of base has the installation piece, the inner wall screw thread of installation piece has cup jointed fastening bolt.

Preferably, the temperature sensor is fixedly connected with the controller through a power transmission line, the back of the controller is fixedly connected with the outer wall of the outer shell, a display screen is arranged on the front of the controller, and adjusting keys positioned on the front of the controller are distributed below the display screen.

Preferably, the refrigerating assembly comprises water guide pipes, the water guide pipes are uniformly distributed on the outer wall of the inner shell, and two adjacent water guide pipes are fixedly connected through an elbow pipe.

Preferably, the upper end fixed mounting at the aqueduct back has the inlet tube, the below of inlet tube is provided with the outlet pipe, and the front end of outlet pipe and the back fixed connection of aqueduct, the one end fixed mounting that the aqueduct was kept away from to the inlet tube has water-cooling radiator, and the positive lower extreme of water-cooling radiator and the rear end fixed connection of outlet pipe, the water-cooling radiator openly and the back fixed connection of shell body.

Preferably, the heating assembly comprises a heating plate, the inner wall of the heating plate is fixedly sleeved with the outer wall of the inner shell, and the left side of the heating plate is fixedly connected with the junction box through an upper wiring terminal and a lower wiring terminal respectively.

Preferably, a flange plate is fixedly arranged at the upper end of the oil outlet pipe, and through holes communicated with the inside are formed in the upper end face and the lower end face of the flange plate.

Compared with the prior art, the utility model has the following beneficial effects:

1. according to the utility model, through the cooperation among the refrigeration assembly, the temperature sensor, the inner shell and the outer shell, the cooling effect on aviation oil in the inner shell is realized by utilizing the installation of the refrigeration assembly, the heating problem of the cylinder type refrigeration piece in the technical content is effectively solved, the cooling mode of the cylinder type refrigeration piece in the technical content is replaced by adopting the mode that the water guide pipes in the refrigeration assembly are distributed on the outer wall of the inner shell, and the contact area of cooling liquid and aviation oil is increased, so that the cooling effect of aviation oil is improved.

2. According to the utility model, through the cooperation among the temperature sensor, the heating assembly, the junction box and the inner shell, the heating effect on aviation oil in the inner shell is realized by utilizing the arrangement of the heating assembly, the problem of slow heating of the cylindrical heating plate in the technical content is effectively solved, and the contact area between the heating plate and the inner shell is increased by adopting the mode that the heating plate in the heating assembly is wound on the outer wall of the inner shell, so that the heating speed of aviation oil is increased, and the heating efficiency of aviation oil is improved.

Drawings

FIG. 1 is a schematic diagram of the structure of the present utility model;

FIG. 2 is a rear view of the water-cooled radiator of the present utility model;

FIG. 3 is a front view of a flowline of the present utility model;

FIG. 4 is a front view of a heating assembly of the present utility model;

FIG. 5 is a diagram of a refrigeration assembly according to the present utility model;

fig. 6 is a cross-sectional view of the inner housing of the present utility model.

In the figure: 1. an outer housing; 2. an inner housing; 3. a temperature sensor; 4. a refrigeration assembly; 401. a water conduit; 402. bending the pipe; 5. a heat radiation fin; 6. a heating assembly; 601. a heating sheet; 602. a terminal; 7. a junction box; 8. an oil outlet pipe; 9. a base; 10. a mounting block; 11. a fastening bolt; 12. a controller; 13. a display screen; 14. adjusting the keys; 15. a water inlet pipe; 16. a water outlet pipe; 17. a water-cooled radiator; 18. a flange plate; 19. and a through hole.

Detailed Description

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

Referring to fig. 1 and 6, an aviation oil storage device comprises an outer shell 1 and an inner shell 2, a cavity is formed between the outer wall of the outer shell 1 and the inner wall of the inner shell 2, a heating component 6 for heating aviation oil is fixedly arranged on the outer wall of the inner shell 2, a temperature sensor 3 is fixedly arranged on the inner wall of the inner shell 2, the temperature sensor 3 is arranged to monitor the temperature of aviation oil in the inner shell 2 in real time, a refrigerating component 4 for cooling the aviation oil is fixedly sleeved on the outer wall of the inner shell 2, the refrigerating component 4 is arranged to cool the aviation oil, radiating fins 5 are uniformly distributed on the outer wall of the refrigerating component 4, the radiating fins 5 are matched with the refrigerating component 4 for use, cooling time of the oil is shortened, a heating component 6 for heating the aviation oil is fixedly arranged on the outer wall of the inner shell 2, the heating component 6 is arranged on the outer wall of the inner shell 2 in a staggered manner, a junction box 7 is fixedly arranged on the left side of the inner shell 2, the junction box 7 is externally connected with a power supply, the external power supply is connected to the junction box 7, the junction box 6 is used for cooling the aviation oil through the cooling component, the cooling component is arranged on the inner shell 2, and a dust pipe 8 is arranged on the inner shell 2, and a dust pipe is arranged on the inner shell 8.

The lower terminal surface fixed mounting of shell body 1 has base 9, and the installation of base 9 plays the supporting role of shell body 1, and the outer wall evenly distributed of base 9 has installation piece 10, and the installation of installation piece 10 provides the platform for the installation of fastening bolt 11, and fastening bolt 11 has been cup jointed to the inner wall screw thread of installation piece 10, and fastening bolt 11's setting plays the connection to installation piece 10 and mounting platform, reaches storage device's installation effect.

Referring to fig. 2 and 5, the temperature sensor 3 is fixedly connected with the controller 12 through a power line, the power line is arranged to connect the temperature sensor 3 with the controller 12, the back of the controller 12 is fixedly connected with the outer wall of the outer shell 1, the front of the controller 12 is provided with a display screen 13, the display screen 13 is arranged to display the temperature value of oil, an adjusting key 14 positioned on the front of the controller 12 is distributed below the display screen 13, and the adjusting key 14 controls the electric appliances of each component.

The refrigeration assembly 4 comprises water guide pipes 401, the water guide pipes 401 are uniformly distributed on the outer wall of the inner shell 2, two adjacent water guide pipes 401 are fixedly connected through an elbow pipe 402, and the arrangement of the elbow pipe 402 plays a role in supplying water to all layers of water guide pipes 401.

The upper end fixed mounting at the aqueduct 401 back has inlet tube 15, the installation of inlet tube 15 is the coolant liquid and enters into the inside of aqueduct 401 and provide the passageway, the below of inlet tube 15 is provided with outlet pipe 16, and the front end of outlet pipe 16 and the back fixed connection of aqueduct 401, the installation of outlet pipe 16 is the outflow of the inside coolant liquid of aqueduct 401 and provides the passageway, the one end fixed mounting that the aqueduct 401 was kept away from to inlet tube 15 has water-cooling radiator 17, the setting of water-cooling radiator 17 is the outflow of coolant liquid and provides the container, and the positive lower extreme of water-cooling radiator 17 and the rear end fixed connection of outlet pipe 16, water-cooling radiator 17 front and the back fixed connection of shell body 1.

Referring to fig. 3 and 4, the heating assembly 6 includes a heating plate 601, an inner wall of the heating plate 601 is fixedly sleeved with an outer wall of the inner housing 2, the heating plate 601 is wound around the outer wall of the inner housing 2, a contact area between oil and the heating plate 601 is increased, a heating time of the oil is shortened, and a left side of the heating plate 601 is fixedly connected with the junction box 7 through an upper terminal 602 and a lower terminal 602 respectively.

The flange 18 is fixedly arranged at the upper end of the oil outlet pipe 8, through holes 19 communicated with the inside are formed in the upper end face and the lower end face of the flange 18, and the flange 18 is convenient to connect with equipment due to the installation of the through holes 19.

Working principle: when the intelligent water cooling device is used, firstly, the real-time detection of aviation oil in the inner shell 2 is carried out according to the temperature sensor 3, the monitored temperature is displayed on the display screen 13 in a digital mode, then, when the temperature displayed on the display screen 13 is too low, the junction box 7 is connected with an external power supply, the heating of the heating plate 601 is carried out through the wiring terminal 602, the heating plate 601 is wound on the outer wall of the inner shell 2, at the moment, the heating of the heating plate 601 can increase the temperature of aviation oil in the inner shell 2, the heating effect of aviation oil in the inner shell 2 can be achieved, the value displayed on the display screen 13 is observed, the power supply of the junction box 7 is cut off when the temperature of the oil rises to a proper value, finally, when the temperature displayed on the display screen 13 is too high, the water cooling radiator 17 is started, the refrigerant in the water cooling radiator 17 is started and enters the inside of the water inlet pipe 15, the refrigerant enters the inside the water cooling pipe 401, and enters the inside of each layer of the water cooling pipe 401 through the inside the bent pipe 402, and then the refrigerant flows from the inside the water outlet pipe 16 to the inside the water cooling radiator 17, so that the circulating cooling effect of the refrigerant can be achieved, and the cooling effect of cooling oil can be achieved.

It is noted that relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Moreover, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Meanwhile, in the drawings of the present utility model, the filling pattern is only for distinguishing the layers, and is not limited in any way.

Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides an aviation oil storage device, includes shell body (1), interior casing (2), form the cavity between the outer wall of shell body (1) and the inner wall of interior casing (2), its characterized in that: the inner wall fixed mounting of inner shell (2) has temperature sensor (3), the outer wall fixed sleeve of inner shell (2) has been used for cooling aviation oil refrigerating module (4), the outer wall evenly distributed of refrigerating module (4) has fin (5), the outer wall fixed mounting of inner shell (2) has heating element (6) that are used for heating aviation oil, the outer wall of inner shell (2) is including heating element (6) and refrigerating module (4) crisscross distribution, the left side fixed mounting of outer shell (1) has terminal box (7), and terminal box (7) external have the power, the upper end fixed mounting of inner shell (2) has oil outlet pipe (8) that are located outer shell (1) top.

2. An aviation oil storage unit according to claim 1, wherein: the novel anti-theft device is characterized in that a base (9) is fixedly arranged on the lower end face of the outer shell body (1), mounting blocks (10) are uniformly distributed on the outer wall of the base (9), and fastening bolts (11) are sleeved on the inner wall of each mounting block (10) in a threaded manner.

3. An aviation oil storage unit according to claim 1, wherein: the temperature sensor (3) is fixedly connected with the controller (12) through a power transmission line, the back of the controller (12) is fixedly connected with the outer wall of the outer shell body (1), a display screen (13) is arranged on the front of the controller (12), and adjusting keys (14) positioned on the front of the controller (12) are distributed below the display screen (13).

4. An aviation oil storage unit according to claim 1, wherein: the refrigerating assembly (4) comprises water guide pipes (401), the water guide pipes (401) are uniformly distributed on the outer wall of the inner shell (2), and two adjacent water guide pipes (401) are fixedly connected through an elbow pipe (402).

5. An aviation oil storage unit in accordance with claim 4, wherein: the water inlet pipe (15) is fixedly arranged at the upper end of the back of the water guide pipe (401), the water outlet pipe (16) is arranged below the water inlet pipe (15), the front end of the water outlet pipe (16) is fixedly connected with the back of the water guide pipe (401), the water cooling radiator (17) is fixedly arranged at one end of the water inlet pipe (15) away from the water guide pipe (401), the front lower end of the water cooling radiator (17) is fixedly connected with the rear end of the water outlet pipe (16), and the front of the water cooling radiator (17) is fixedly connected with the back of the outer shell (1).

6. An aviation oil storage unit according to claim 1, wherein: the heating assembly (6) comprises a heating plate (601), the inner wall of the heating plate (601) is fixedly sleeved with the outer wall of the inner shell (2), and the left side of the heating plate (601) is fixedly connected with the junction box (7) through an upper wiring terminal (602) and a lower wiring terminal (602) respectively.

7. An aviation oil storage unit according to claim 1, wherein: the oil outlet pipe (8) is fixedly provided with a flange plate (18) at the upper end, and through holes (19) communicated with the inside are formed in the upper end face and the lower end face of the flange plate (18).