CN215611282U - Device for mixing aviation gasoline and additive - Google Patents
Device for mixing aviation gasoline and additive Download PDFInfo
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- CN215611282U CN215611282U CN202121854380.7U CN202121854380U CN215611282U CN 215611282 U CN215611282 U CN 215611282U CN 202121854380 U CN202121854380 U CN 202121854380U CN 215611282 U CN215611282 U CN 215611282U
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- stirring
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Abstract
The utility model provides a device for mixing aviation gasoline and an additive, and relates to the technical field of aviation gasoline production. The device for mixing the aviation gasoline and the additive comprises an oil storage tank, a mixing tank, an agent storage tank and a stirring mechanism. The oil storage tank is provided with an oil inlet, a partition plate is transversely arranged in the oil storage tank, an oil transfer pump is arranged on the upper side of the partition plate, and a flow transmitter is arranged at the outlet of the oil transfer pump. The mixing tank is provided with an oil outlet and is arranged at the top of the oil storage tank, and the oil transfer pump is communicated with the mixing tank. The agent storage tank is arranged at the top of the oil storage tank and is communicated with the mixing tank through a metering pump. The stirring mechanism comprises a stirring motor, a stirring shaft and a stirring part. The stirring motor is arranged on the mixing tank, the stirring shaft is connected with an output shaft of the stirring motor in a transmission way, and the stirring part is arranged on the stirring shaft. The aviation gasoline and the additive can be fully mixed under the action of the stirring mechanism, so that the service performance of the aviation gasoline is ensured.
Description
Technical Field
The utility model relates to the technical field of aviation gasoline production, in particular to a device for mixing aviation gasoline and an additive.
Background
A small amount of additive needs to be added in the production process of the aviation gasoline so as to improve the service performance of the aviation gasoline. At present, a manual operation mode is adopted, and after a tank body for storing aviation gasoline is opened, an additive is directly added into the aviation gasoline. The above mode has the problems of insufficient and uneven mixing of the additive and the aviation gasoline and unsatisfactory mixing effect.
SUMMERY OF THE UTILITY MODEL
In view of the above circumstances, the present invention provides a device for mixing aviation gasoline and an additive, which solves the technical problems presented in the background art.
In order to achieve the purpose, the utility model provides the following technical scheme:
an apparatus for blending aviation gasoline and an additive may generally comprise: oil storage tank, blending tank, storage agent jar and rabbling mechanism.
The oil storage tank is provided with an oil inlet, a partition plate is transversely arranged in the oil storage tank, an oil transfer pump is arranged on the upper side of the partition plate, and a flow transmitter is arranged at the outlet of the oil transfer pump.
The mixing tank is provided with an oil outlet and is arranged at the top of the oil storage tank, and the oil transfer pump is communicated with the mixing tank.
The agent storage tank is arranged at the top of the oil storage tank and communicated with the mixing tank through a metering pump, and the metering pump is arranged on the mixing tank and is associated with the flow transmitter. The agent storage tanks are multiple, the inlet of the metering pump is connected with a collecting pipe, the collecting pipe is radially connected with a plurality of branch pipes, and valves are arranged on the branch pipes so as to conveniently introduce corresponding types of additives into the mixing tanks according to needs.
The stirring mechanism comprises a stirring motor, a stirring shaft and a stirring part. The stirring motor is arranged on the mixing tank, the stirring shaft is connected with an output shaft of the stirring motor in a transmission way, and the stirring part is arranged on the stirring shaft.
Supply aviation petrol through the oil inlet to the oil storage tank in, can let in the blending tank with aviation petrol in the oil storage tank through the fuel delivery pump in, can let in the blending tank with the additive in the storage agent jar through the measuring pump in, aviation petrol and additive can the intensive mixing under rabbling mechanism's effect to guarantee aviation petrol's performance. The metering pump is associated with the flow transmitter, namely the metering pump and the flow transmitter enable the conveying amount of the additive and the conveying amount of the aviation gasoline to be controlled in a certain proportion in an interlocking mode, so that the conveying amount of the additive can be automatically adjusted according to the conveying amount of the aviation gasoline.
In some embodiments of the utility model, the stirring part is zigzag-shaped to better stir and mix the aviation gasoline and the additive.
In some embodiments of the present invention, a circulation tank communicated with the mixing tank is installed outside the mixing tank, the circulation tank is communicated with a circulation pump, the circulation pump is disposed on the upper side of the partition plate, the circulation pump is communicated with an oil return pipe, the oil return pipe is transversely disposed at the bottom of the mixing tank, and a plurality of oil return ports are radially disposed on the oil return pipe.
The arrangement of the circulating tank, the circulating pump and the oil return pipe can promote the flow of the aviation gasoline and the additive in the mixing tank, which is beneficial to the full mixing of the aviation gasoline and the additive.
In some embodiments of the present invention, a slide rail is disposed on the top of the oil storage tank, the slide rail is slidably connected to a bearing platform, the bearing platform has a plurality of receiving slots for receiving the agent storage tank, and the agent storage tank is connected to the branch pipes through a flexible hose.
The plummer can drive the storage tank and slide along the slide rail at the top of oil storage tank for additive in the storage tank can constantly rock, and in order to avoid making the effective molecule of additive gather because of the additive stews, thereby influence the mixed effect of additive and aviation gasoline.
In some embodiments of the utility model, a rotating motor is arranged at the top of the oil storage tank, a disc is mounted on an output shaft of the rotating motor, a push rod is fixedly arranged at one side of the bearing table, one end of the push rod is rotatably connected with a connecting rod, and one end of the connecting rod is rotatably connected to the edge of the disc.
The arrangement of the rotating motor, the disc, the push rod and the connecting rod facilitates the shaking of the bearing platform.
In some embodiments of the present invention, the receiving groove is opened at an edge of the carrier, and a locking mechanism for fixing the storage tank is disposed at the edge of the carrier. The locking mechanism comprises a stop lever, the left end of the stop lever is hinged with the bearing platform, and the right end of the stop lever is detachably connected with the bearing platform.
When putting into the holding tank with storing up the agent jar, can be by the edge of plummer, the inside of storing up the agent jar and pushing into the holding tank horizontally rotates the pin again, reaches the purpose of fixing storing up the agent jar in the holding tank through fixed pin.
In some embodiments of the utility model, a U-shaped block matched with the stop lever is fixedly arranged on the bearing table, and a fastening nut is screwed at the right end of the stop lever and can abut against the right side of the U-shaped block.
When the stop lever needs to be fixed, the right end of the stop lever is rotated into the notch of the U-shaped block, and the fastening nut is screwed down to be abutted against the right side of the U-shaped block so as to limit the rotation of the stop lever on the horizontal plane.
In some embodiments of the utility model, the holding tank is internally connected with a resisting plate through a compression spring, and the resisting plate, the holding tank and the stop lever are matched together to fix the agent storage tank.
The setting of abutting against the board and pressure spring for can fix multiple diameter in the holding tank and store up the agent jar.
The embodiment of the utility model at least has the following advantages or beneficial effects:
supply aviation petrol through the oil inlet to the oil storage tank in, can let in the blending tank with aviation petrol in the oil storage tank through the fuel delivery pump in, can let in the blending tank with the additive in the storage agent jar through the measuring pump in, aviation petrol and additive can the intensive mixing under rabbling mechanism's effect to guarantee aviation petrol's performance. The metering pump and the flow transmitter enable the conveying capacity of the additive and the conveying capacity of the aviation gasoline to be controlled in a certain proportion in an interlocking mode, so that the conveying capacity of the additive can be automatically adjusted according to the conveying capacity of the aviation gasoline.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present application, the drawings needed to be used in the description of the embodiments are briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present application, and it is obvious for those skilled in the art to obtain other drawings without creative efforts.
FIG. 1 is a schematic diagram of the structure of an apparatus for blending aviation gasoline and additives;
FIG. 2 is a cross-sectional view taken along line A-A of FIG. 1;
fig. 3 is a schematic structural view of the stop lever and the fastening nut.
Icon: 11-oil storage tank, 111-oil inlet, 112-clapboard, 113-oil transfer pump, 114-flow transmitter, 12-mixing tank, 121-oil outlet, 13-agent storage tank, 131-metering pump, 132-collecting pipe, 133-branch pipe, 134-telescopic hose, 141-stirring motor, 142-stirring shaft, 143-stirring part, 151-circulating tank, 152-circulating pump, 153-oil return pipe, 154-oil return port, 161-slide rail, 162-bearing platform, 163-containing tank, 165-rotating motor, 166-disc, 167-push rod, 168-connecting rod, 171-stop rod, 172-U-shaped block, 173-fastening nut, 174-abutting plate and 175-pressure spring.
Detailed Description
In the following, only certain exemplary embodiments are briefly described. As those skilled in the art will recognize, the described embodiments may be modified in various different ways, all without departing from the spirit or scope of the embodiments of the utility model. Accordingly, the drawings and description are to be regarded as illustrative in nature, and not as restrictive.
In the embodiments of the present invention, unless otherwise explicitly specified or limited, the terms "mounted," "connected," "fixed," and the like are to be construed broadly, e.g., as being fixedly connected, detachably connected, or integrated; the connection can be mechanical connection, electrical connection or communication; either directly or indirectly through intervening media, either internally or in any other relationship. Specific meanings of the above terms in the embodiments of the present invention can be understood by those of ordinary skill in the art according to specific situations.
Embodiments of the present invention will be described in detail below with reference to the accompanying drawings.
Referring to fig. 1 to 3, the present embodiment provides an apparatus for mixing aviation gasoline and an additive, which mainly includes: an oil storage tank 11, a mixing tank 12, an agent storage tank 13 and a stirring mechanism.
The oil storage tank 11 is provided with an oil inlet 111, a partition plate 112 is transversely arranged in the oil storage tank 11, a delivery pump 113 is arranged on the upper side of the partition plate 112, and a flow transmitter 114 is arranged at the outlet of the delivery pump 113.
The mixing tank 12 has an oil outlet 121 to facilitate the extraction of the well-mixed additive and aviation gasoline. The mixing tank 12 is disposed on the top of the oil storage tank 11, and the oil transfer pump 113 is communicated with the mixing tank 12.
The agent storage tank 13 is arranged on the top of the oil storage tank 11, the agent storage tank 13 is communicated with the mixing tank 12 through a metering pump 131, and the metering pump 131 is installed on the mixing tank 12 and is associated with the flow transmitter 114. The metering pump 131 is associated with the flow transmitter 114, i.e. the metering pump 131 and the flow transmitter 114 interlockingly control the delivery amount of the additive and the delivery amount of the aviation gasoline in a certain proportion so that the delivery amount of the additive can be automatically adjusted according to the delivery amount of the aviation gasoline. The storage tank 13 is provided with a plurality of storage tanks, the inlet of the metering pump 131 is connected with a collecting pipe 132, the collecting pipe 132 is radially connected with a plurality of branch pipes 133, and the branch pipes 133 are provided with valves so as to conveniently introduce corresponding types of additives into the mixing tank 12 according to requirements.
The stirring mechanism includes a stirring motor 141, a stirring shaft 142, and a stirring section 143. The stirring motor 141 is installed in the mixing tank 12, the stirring shaft 142 is connected to the output shaft of the stirring motor 141 in a transmission manner, and the stirring part 143 is installed on the stirring shaft 142.
Supplement aviation gasoline in to the oil storage tank 11 through oil inlet 111, can let in the aviation gasoline in the oil storage tank 11 in the blending tank 12 through transfer pump 113, can let in the additive in the agent storage tank 13 in the blending tank 12 through measuring pump 131, aviation gasoline and additive can the intensive mixing under the effect of rabbling mechanism to guarantee aviation gasoline's performance.
The stirring part 143 is zigzag-shaped to better stir and mix the aviation gasoline and the additive.
The circulation tank 151 that communicates with the blending tank 12 is installed to the outside of blending tank 12, and circulation tank 151 intercommunication has circulating pump 152, and circulating pump 152 sets up the upside at baffle 112, and circulating pump 152 intercommunication has oil return pipe 153, and oil return pipe 153 transversely sets up in the bottom of blending tank 12, radially has seted up a plurality of oil return openings 154 on the oil return pipe 153. The arrangement of the circulation tank 151, the circulation pump 152 and the oil return pipe 153 can promote the flow of the aviation gasoline and the additive in the mixing tank 12, which facilitates the sufficient mixing of the aviation gasoline and the additive.
The top of the oil storage tank 11 is provided with a slide rail 161, the slide rail 161 is slidably connected with a bearing platform 162, the bearing platform 162 is provided with a plurality of accommodating grooves 163 for accommodating the agent storage tank 13, and the agent storage tank 13 is connected with the branch pipe 133 through a telescopic hose 134. The bearing table 162 can drive the agent storage tank 13 to slide along the slide rail 161 at the top of the oil storage tank 11, so that the additive in the agent storage tank 13 can continuously shake, effective molecules of the additive are prevented from gathering due to standing of the additive, and the mixing effect of the additive and the aviation gasoline is influenced.
The top of the oil storage tank 11 is provided with a rotating motor 165, an output shaft of the rotating motor 165 is provided with a disc 166, one side of the bearing platform 162 is fixedly provided with a push rod 167, one end of the push rod 167 is rotatably connected with a connecting rod 168, and one end of the connecting rod 168 is rotatably connected with the edge of the disc 166. The arrangement of the rotary motor 165, the disc 166, the push rod 167 and the connecting rod 168 facilitates the shaking of the bearing platform 162.
A U-shaped block 172 matching with the stop rod 171 is fixedly arranged on the bearing table 162, a fastening nut 173 is screwed at the right end of the stop rod 171, and the fastening nut 173 can abut against the right side of the U-shaped block 172. When the stop lever 171 needs to be fixed, the right end of the stop lever 171 is rotated into the notch of the U-shaped block 172, and the fastening nut 173 is tightened to make the fastening nut 173 abut against the right side of the U-shaped block 172, so as to limit the rotation of the stop lever 171 on the horizontal plane.
The holding groove 163 is connected with a resisting plate 174 by a compression spring 175, and the resisting plate 174, the holding groove 163 and the blocking rod 171 cooperate together to fix the agent storage tank 13. The provision of the abutting plate 174 and the pressing spring 175 enables the accommodation groove 163 to hold the agent storage tanks 13 of various diameters therein.
The working principle of the device for mixing aviation gasoline and additive is as follows:
the additive in the corresponding agent storage tank 13 is introduced into the mixing tank 12 through the metering pump 131, and the aviation gasoline in the oil storage tank 11 is introduced into the mixing tank 12 through the oil transfer pump 113. The aviation gasoline and the additive in the mixing tank 12 are fully mixed under the action of the stirring mechanism and the circulating pump 152.
The rotary motor 165 can drive the bearing platform 162 and the agent storage tank 13 on the bearing platform 162 to move left and right so as to continuously shake the additive in the agent storage tank 13, thereby avoiding the accumulation of effective molecules of the additive due to the standing of the agent storage tank 13 and further influencing the mixing effect of the additive and the aviation gasoline.
Finally, it should be noted that: the present invention is not limited to the above-described preferred embodiments, but various modifications and changes can be made by those skilled in the art, and the embodiments and features of the embodiments of the present invention can be combined with each other arbitrarily without conflict. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (8)
1. An apparatus for blending aviation gasoline and an additive, comprising: the device comprises an oil storage tank, a mixing tank, an agent storage tank and a stirring mechanism;
the oil storage tank is provided with an oil inlet, a partition plate is transversely arranged in the oil storage tank, an oil transfer pump is arranged on the upper side of the partition plate, and a flow transmitter is arranged at the outlet of the oil transfer pump;
the mixing tank is provided with an oil outlet and is arranged at the top of the oil storage tank, and the oil transfer pump is communicated with the mixing tank;
the agent storage tank is arranged at the top of the oil storage tank and is communicated with the mixing tank through a metering pump, and the metering pump is arranged on the mixing tank and is associated with the flow transmitter; the metering pump is characterized in that a plurality of agent storage tanks are arranged, a collecting pipe is connected to an inlet of the metering pump, a plurality of branch pipes are radially connected to the collecting pipe, and valves are arranged on the branch pipes;
the stirring mechanism comprises a stirring motor, a stirring shaft and a stirring part; the stirring motor is installed in the mixing tank, the stirring shaft is in transmission connection with an output shaft of the stirring motor, and the stirring part is installed on the stirring shaft.
2. An apparatus for blending aviation gasoline and an additive as claimed in claim 1 wherein the blending portion is zigzag shaped.
3. The device for mixing aviation gasoline and additives according to claim 1, wherein a circulation tank communicated with the mixing tank is installed on the outer side of the mixing tank, the circulation tank is communicated with a circulation pump, the circulation pump is arranged on the upper side of the partition plate, the circulation pump is communicated with an oil return pipe, the oil return pipe is transversely arranged at the bottom of the mixing tank, and a plurality of oil return ports are radially formed in the oil return pipe.
4. A device for blending aviation gasoline and an additive as claimed in claim 1, wherein the top of the oil storage tank is provided with a slide rail, the slide rail is slidably connected with a bearing platform, the bearing platform is provided with a plurality of holding grooves for holding the agent storage tank, and the agent storage tank is connected with the branch pipe through a telescopic hose.
5. A device for mixing aviation gasoline and an additive according to claim 4, wherein a rotating motor is arranged at the top of the oil storage tank, a disc is mounted on an output shaft of the rotating motor, a push rod is fixedly arranged on one side of the bearing platform, one end of the push rod is rotatably connected with a connecting rod, and one end of the connecting rod is rotatably connected with the edge of the disc.
6. The device for mixing aviation gasoline and an additive according to claim 4, wherein the accommodating groove is formed at the edge of the bearing platform, and a locking mechanism for fixing the agent storage tank is arranged at the edge of the bearing platform; the locking mechanism comprises a stop lever, the left end of the stop lever is hinged with the bearing platform, and the right end of the stop lever is detachably connected with the bearing platform.
7. The device for mixing aviation gasoline and additives of claim 6, wherein a U-shaped block matched with the stop lever is fixedly arranged on the bearing table, a fastening nut is screwed at the right end of the stop lever, and the fastening nut can abut against the right side of the U-shaped block.
8. The device of claim 6, wherein a compression spring is connected to the receiving groove, and the compression spring, the compression plate, the receiving groove and the stop lever cooperate together to secure the storage tank.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121854380.7U CN215611282U (en) | 2021-08-10 | 2021-08-10 | Device for mixing aviation gasoline and additive |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121854380.7U CN215611282U (en) | 2021-08-10 | 2021-08-10 | Device for mixing aviation gasoline and additive |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215611282U true CN215611282U (en) | 2022-01-25 |
Family
ID=79896344
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121854380.7U Active CN215611282U (en) | 2021-08-10 | 2021-08-10 | Device for mixing aviation gasoline and additive |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215611282U (en) |
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2021
- 2021-08-10 CN CN202121854380.7U patent/CN215611282U/en active Active
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