CN115138255B - Device for mixing aviation fuel and additive - Google Patents
Device for mixing aviation fuel and additive Download PDFInfo
- Publication number
- CN115138255B CN115138255B CN202211044438.0A CN202211044438A CN115138255B CN 115138255 B CN115138255 B CN 115138255B CN 202211044438 A CN202211044438 A CN 202211044438A CN 115138255 B CN115138255 B CN 115138255B
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- mixing chamber
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01F—MIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
- B01F27/00—Mixers with rotary stirring devices in fixed receptacles; Kneaders
- B01F27/80—Mixers with rotary stirring devices in fixed receptacles; Kneaders with stirrers rotating about a substantially vertical axis
- B01F27/92—Mixers with rotary stirring devices in fixed receptacles; Kneaders with stirrers rotating about a substantially vertical axis with helices or screws
- B01F27/922—Mixers with rotary stirring devices in fixed receptacles; Kneaders with stirrers rotating about a substantially vertical axis with helices or screws with two or more helices, e.g. with intermeshing helices
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01F—MIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
- B01F27/00—Mixers with rotary stirring devices in fixed receptacles; Kneaders
- B01F27/80—Mixers with rotary stirring devices in fixed receptacles; Kneaders with stirrers rotating about a substantially vertical axis
- B01F27/85—Mixers with rotary stirring devices in fixed receptacles; Kneaders with stirrers rotating about a substantially vertical axis with two or more stirrers on separate shafts
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01F—MIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
- B01F35/00—Accessories for mixers; Auxiliary operations or auxiliary devices; Parts or details of general application
- B01F35/71—Feed mechanisms
- B01F35/717—Feed mechanisms characterised by the means for feeding the components to the mixer
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- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Mixers Of The Rotary Stirring Type (AREA)
Abstract
The invention belongs to the field of mixing equipment, and relates to a device for mixing aviation fuel and an additive, which comprises a mixing chamber and a base, wherein a feed inlet and a sealing cover are arranged on the mixing chamber; still include angle adjustment mechanism, two supplementary rabbling mechanisms and driving medium, angle adjustment mechanism is used for carrying out angle modulation to the base, supplementary rabbling mechanism is used for stirring aviation fuel and additive in the mixing chamber, the driving medium is used for the turning force transmission with the mixing chamber to two supplementary rabbling mechanisms on, the top of base is equipped with the mount pad, the base sets up on angle adjustment mechanism, two supplementary rabbling mechanisms set up respectively on the top and the bottom of mixing chamber, the driving medium sets up on the top of mount pad. The invention can fully mix the aviation fuel and the additive, thereby improving the mixing efficiency.
Description
Technical Field
The invention relates to the field of mixing equipment, in particular to a device for mixing aviation fuel and additives.
Background
The aviation fuel is also called jet fuel and aviation kerosene, is mainly prepared by refining kerosene fraction distilled from crude oil and sometimes adding additives, can also be produced by hydrocracking heavy distillate distilled from crude oil, is divided into two categories of wide-fraction boiling point (60-280 ℃) and kerosene type boiling point (150-315 ℃), and is widely used for various jet airplanes. In order to ensure the combustion efficiency of aviation fuel, a specific additive is usually added into the aviation fuel, the process is called mixing, and then the traditional mixing method has the problems of insufficient mixing and low mixing efficiency.
Notice is additive mixing arrangement for alcohol group fuel production that CN207478489U discloses, includes base, compounding room and compounding controller, the base top is provided with the bracing piece, be provided with the aeration machine on the bracing piece, the aeration machine pass through the aeration pipe with the compounding room is connected, compounding room both sides are provided with sealing valve, the compounding room is connected with the shaft coupling through the transfer line, the compounding controller is connected with the compounding motor, compounding motor side is provided with the action wheel, the action wheel is connected with the follower through driving belt, the follower with the transfer line is connected. According to the patent, the alcohol-based fuel and the additive can be mixed and stirred by a method of simultaneous aeration and rotation, so that the mixing speed is increased.
However, the above patents still have drawbacks: although the mixing chamber rotates always, when the compounding, its rotational speed is unchangeable continuously, therefore make alcohol group fuel and additive in the mixing chamber under the supplementary circumstances of stirring not, the position change of alcohol group fuel and additive is slower, though the aeration machine can improve the speed of compounding through aeration pipe to carrying out aeration treatment in the mixing chamber, the aeration treatment effect of aeration pipe to the one end of being connected with the mixing chamber is preferred, the one end of keeping away from the aeration pipe receives aeration treatment effect not good, the mixing chamber can't guarantee when rotating that the alcohol group fuel that is close to aeration pipe one end in the mixing chamber, additive and the alcohol group fuel of keeping away from aeration pipe one end, additive can realize the position and change completely, thereby it is poor to lead to the alcohol group fuel of the one end of keeping away from the aeration pipe and the mixed effect of additive, to sum up, this patent has the unsatisfactory problem of compounding effect.
Disclosure of Invention
The technical problem to be solved by the invention is as follows: the problems that the material mixing is insufficient and the material mixing efficiency is low in the traditional material mixing method are solved.
The invention provides a device for mixing aviation fuel and additives, which comprises a mixing chamber and a base, wherein the mixing chamber is provided with a feed inlet and a detachable sealing cover for sealing the feed inlet, two ends of the mixing chamber are respectively provided with a support shaft, the base is provided with two rotating supports and a support frame, the two support frames are provided with a reduction box and a rotating motor, the two rotating support frames are symmetrically arranged at two sides of the mixing chamber, the mixing chamber is rotationally arranged on the two rotating support frames through the two support shafts, the support frame is positioned at the side of one rotating support frame, the reduction box is in transmission connection with one support shaft, and the rotating motor is connected on the reduction box; the device comprises a base, and is characterized by further comprising an angle adjusting mechanism, two auxiliary stirring mechanisms and a transmission part, wherein the angle adjusting mechanism is used for adjusting the angle of the base, the auxiliary stirring mechanisms are used for stirring aviation fuel and additives in a mixing chamber, the transmission part is used for transmitting the rotating force of the mixing chamber to the two auxiliary stirring mechanisms, the top of the base is provided with an installation seat, the installation seat is positioned between two rotating supports, the base is arranged on the angle adjusting mechanism, the two auxiliary stirring mechanisms are respectively arranged on the top and the bottom of the mixing chamber, the transmission part is arranged on the top of the installation seat, and the two auxiliary stirring mechanisms are both in transmission connection with the transmission part; can let the aviation fuel in the hybrid chamber and the position change of additive accelerate through angle adjustment mechanism, can improve aviation fuel and additive compounding effect through the cooperation between two supplementary rabbling mechanisms and the driving medium.
In some embodiments, the angle adjusting mechanism includes a bottom frame, a half gear, a pushing electric push rod, a slide way, a slide rail and a rack, wherein rotating shafts are arranged at two ends of the base, the base is rotatably arranged on the bottom frame through the two rotating shafts, the half gear is arranged at the center of the bottom of the base, the half gear and the rotating shafts are coaxial, the pushing electric push rod and the slide way are positioned under the half gear, the slide rail is slidably arranged on the slide way, the tail end of the slide rail is fixedly connected with the output end of the pushing electric push rod, the rack is arranged at the top of the slide rail, and the rack is meshed with the half gear; this can drive the base to swing about the axis of the shaft.
In some embodiments, the auxiliary stirring mechanism comprises a mounting disc, a stirring rod, a worm gear and a worm, wherein two symmetrically arranged rotating seats are arranged on the mounting disc, a spiral stirring blade is arranged on the stirring rod, pressing rollers are arranged at two ends of the worm, the mounting disc is hermetically arranged at the top or the bottom of the mixing chamber, the stirring rod is rotatably arranged at the center of the mounting disc, the spiral stirring blade is positioned in the mixing chamber, the worm gear is arranged at one end far away from the spiral stirring blade, the worm is rotatably arranged on the two rotating seats, and the worm is meshed with the worm gear; utilize pivoted mixing chamber cooperation driving medium to let the puddler rotation, even make helical mixing blade can stir the aviation fuel and the additive in the mixing chamber and mix.
In some embodiments, the outer surface of the pressing roller is provided with a first anti-skid grain; increase the friction between the pressing roller and the transmission member.
In some embodiments, the transmission member is a transmission ring, the inner side wall of the transmission ring is provided with second anti-slip threads, and the pressing roller is abutted against the inner wall of the transmission ring; this can let two stirring vane can continue to stir the mixing to aviation fuel and additive.
In some embodiments, the transmission part is a transmission arc-shaped block, and a third anti-slip pattern is arranged on the inner side wall of the transmission arc-shaped block; this can make two stirring vane can be intermittent type nature stir the mixing to aviation fuel and additive.
In some embodiments, both ends of the top of the transmission arc-shaped block are provided with inner chamfers; the pressing roller can enter the inner side wall of the transmission arc-shaped block conveniently in a pressing mode.
In some embodiments, at least two guide seats are arranged on the outer side wall of the mounting disc, at least two guide rods matched with the guide seats are arranged at the top and the bottom of the mixing chamber, a connecting plate is arranged in the middle of each guide rod, a spring is sleeved on each guide rod, a limiting handle is arranged at one end, away from the connecting plate, of each guide rod, the mounting disc is arranged on the top or the bottom of the mixing chamber in a sliding and sealing mode, all the guide rods are arranged in all the guide seats in a sliding mode respectively, and two ends of each spring are fixedly connected with the connecting plate and the guide seats respectively; let and support and press the gyro wheel and have certain buffer distance on the inside wall that enters into transmission arc piece, improve stability.
The invention has the beneficial effects that:
according to the device for mixing the aviation fuel and the additive, the aviation fuel and the additive can be fully mixed through mutual matching of the angle adjusting mechanism, the two auxiliary stirring mechanisms and the transmission part, and the mixing speed is improved.
Secondly, according to the device for mixing the aviation fuel and the additive, the mixing chamber is driven to rotate around the axis of the supporting shaft by the matching of the rotating motor and the reduction gearbox, and meanwhile, the pressing roller on the auxiliary stirring mechanism can be in interference fit with the transmission part, so that the stirring shaft and the spiral stirring blade rotate to perform auxiliary stirring and mixing on the aviation fuel and the additive in the mixing chamber, and the mixing is more sufficient.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and other drawings can be obtained by those skilled in the art without creative efforts.
FIG. 1 is a schematic perspective view of a first apparatus for blending aviation fuel and additives in accordance with the present invention;
FIG. 2 is a schematic perspective view of a second embodiment of the apparatus for blending aviation fuel and additive according to the present invention;
FIG. 3 is a partial cross-sectional view of the angle adjustment mechanism;
FIG. 4 is a partial schematic view of an angle adjustment mechanism;
FIG. 5 is a schematic view of the first embodiment of the driving member in cooperation with the auxiliary stirring mechanism;
FIG. 6 is a cross-sectional view of the mixing chamber;
FIG. 7 is a schematic view of a second embodiment of a transmission member in cooperation with an auxiliary stirring mechanism.
Reference numerals: 1. a mixing chamber; 11. a feed inlet; 12. sealing the cover; 13. a support shaft; 14. a guide rod; 15. a connecting plate; 16. a spring; 17. a limiting handle; 2. a base; 21. rotating the bracket; 22. a support frame; 23. a reduction gearbox; 24. rotating the motor; 25. a mounting base; 26. a rotating shaft; 3. an angle adjusting mechanism; 31. a bottom frame; 32. a half gear; 33. pushing the electric push rod; 34. a slideway; 35. a slide rail; 36. a rack; 4. an auxiliary stirring mechanism; 41. installing a disc; 411. a rotating seat; 412. a guide seat; 42. a stirring rod; 421. a helical mixing blade; 43. a worm gear; 44. a worm; 441. pressing the roller; 5. a drive ring; 6. the arc-shaped block is driven; 61. and (6) inner chamfering.
Detailed Description
The technical solutions of the present invention will be described clearly and completely with reference to the accompanying drawings, and it should be understood that the described embodiments are some, but not all embodiments of the present invention.
In this embodiment, as shown in fig. 1 to 7, a device for mixing aviation fuel and additives includes a mixing chamber 1 and a base 2, a feed inlet 11 and a detachable cover 12 for sealing the feed inlet 11 are provided on the mixing chamber 1, support shafts 13 are provided at both ends of the mixing chamber 1, two rotating supports 21 and supports 22 are provided on the base 2, a reduction box 23 and a rotating motor 24 are provided on the two supports 22, the two rotating supports 22 are symmetrically provided at both sides of the mixing chamber 1, the mixing chamber 1 is rotatably provided on the two rotating supports 22 through the two support shafts 13, the supports 22 are located beside one of the rotating supports 21, the reduction box 23 is in transmission connection with one of the support shafts 13, and the rotating motor 24 is connected to the reduction box 23; still include angle adjustment mechanism 3, two supplementary rabbling mechanisms 4 and driving medium, angle adjustment mechanism 3 is used for carrying out angle modulation to base 2, supplementary rabbling mechanism 4 is used for stirring aviation fuel and additive in the mixing chamber 1, the driving medium is used for the turning force transmission with mixing chamber 1 to two supplementary rabbling mechanisms 4 on, the top of base 2 is equipped with mount pad 25, and mount pad 25 is located between two runing rest 21, base 2 sets up on angle adjustment mechanism 3, two supplementary rabbling mechanisms 4 set up respectively on mixing chamber 1's top and bottom, the driving medium sets up on the top of mount pad 25, two supplementary rabbling mechanisms 4 all are connected with the driving medium transmission.
Aviation fuel and additives are added into the mixing chamber 1 through the feed port 11, then the mixing chamber 1 is driven to rotate around the axis of the supporting shaft 13 by the cooperation of the rotating motor 24 and the reduction gearbox 23, meanwhile, the angle adjusting mechanism 3 works, the angle adjusting mechanism 3 comprises a bottom frame 31, a half gear 32, a pushing electric push rod 33, a slide way 34, a slide way 35 and a rack 36, rotating shafts 26 are arranged at two ends of the base 2, the base 2 is rotatably arranged on the bottom frame 31 through the two rotating shafts 26, the half gear 32 is arranged at the center of the bottom of the base 2, the half gear 32 and the rotating shafts 26 are coaxial, the pushing electric push rod 33 and the slide way 34 are positioned right below the half gear 32, the slide way 35 is slidably arranged on the slide way 34, the tail end of the slide way 35 is fixedly connected with the output end of the pushing electric push rod, the rack 36 is arranged at the top of the slide way 35, the rack 36 is meshed with the half gear 32, as shown in fig. 3 and 4, the pushing electric push rod 33 drives the slide way 35 to reciprocate in the slide way 34, the slide way to move synchronously, the rack 36 drives the half gear 32 to rotate around the axis of the shaft 26, the axis, the axial line of the base 2, the aviation fuel and the aviation fuel are prevented from swinging slowly, the aviation fuel and additives are prevented from swinging along the axial direction of the industrial push rod 33, the industrial push rod, the aviation fuel and the aviation fuel are prevented from swinging chamber from being changed slowly, the aviation fuel and the aviation fuel are prevented from swinging chamber, the aviation fuel and the aviation fuel are prevented from swinging of the aviation fuel and the aviation fuel are prevented from swinging chamber from swinging along the aviation fuel and the aviation fuel are prevented from swinging chamber, and the aviation fuel in the aviation fuel are prevented from swinging chamber, and the aviation fuel are prevented from swinging slowly, and the aviation fuel from swinging along the aviation fuel.
When the mixing chamber 1 is driven by the rotating motor 24 and the reduction gearbox 23 to rotate around the axis of the supporting shaft 13, the two auxiliary stirring mechanisms 4 can cooperate with a transmission member to perform auxiliary stirring on aviation fuel and additives in the mixing chamber 1, each auxiliary stirring mechanism 4 comprises a mounting disc 41, a stirring rod 42, a worm wheel 43 and a worm 44, two rotating seats 411 which are symmetrically arranged are arranged on the mounting disc 41, a spiral stirring blade 421 is arranged on the stirring rod 42, pressing rollers 441 are arranged at two ends of each worm 44, in order to increase the friction force between the pressing rollers 441 and the transmission member, a first anti-slip pattern is arranged on the outer surface of each pressing roller 441, the mounting disc 41 is hermetically arranged at the top or the bottom of the mixing chamber 1, the stirring rod 42 is rotatably arranged at the center of the mounting disc 41, the spiral stirring blade 421 is positioned in the mixing chamber 1, the worm wheel 43 is arranged at one end far away from the spiral stirring blade 421, the worm 44 is rotatably arranged on the two rotating seats 411, and the worm 44 is meshed with the worm wheel 43.
The auxiliary stirring mechanism 4 can operate continuously, but also intermittently, depending mainly on the shape of the transmission member, thus providing two embodiments of the transmission member:
first embodiment of the Transmission
The transmission part is a transmission ring 5, second anti-slip patterns are arranged on the inner side wall of the transmission ring 5, the friction force between the pressing roller 441 and the transmission ring 5 can be further improved through the design of the second anti-slip patterns, the stop rotation of the stirring rod 42 caused by the slipping is avoided, the pressing roller 441 is abutted against the inner wall of the transmission ring 5, when the mixing chamber 1 rotates around the axis of the support shaft 13, the mixing chamber 1 drives the mounting disc 41 to synchronously rotate, the pressing roller 441 on the mounting disc 41 is matched with the transmission ring 5 to enable the pressing roller 441 to continuously rotate, the pressing roller 441 drives the worm 44 to synchronously rotate, the worm 44 drives the worm wheel 43 to rotate, the worm wheel 43 drives the stirring rod 42 and the spiral stirring blade 421 to continuously rotate, and the spiral stirring blade 421 can continuously stir the aviation fuel and the additive in the mixing chamber 1, so that the mixing effect of the aviation fuel and the additive is further improved.
Second embodiment of the Transmission
The transmission medium is transmission arc piece 6, be equipped with third anti-skidding line on the inside wall of transmission arc piece 6, the frictional force between suppression gyro wheel 441 and transmission arc piece 6 can further be improved in the design of third anti-skidding line, mixing chamber 1 is when rotating around the axis of back shaft 13, mixing chamber 1 drives mounting disc 41 and suppression gyro wheel 441 and carries out synchronous rotation, when suppression gyro wheel 441 enters the effect region of transmission arc piece 6 inside wall, in order to make the effect region that suppression gyro wheel 441 enters transmission arc piece 6 inside wall, all be equipped with inner chamfer 61 at the both ends at transmission arc piece 6 top, utilize inner chamfer 61 to guide suppression gyro wheel 441, suppression gyro wheel 441 and transmission arc piece 6 inside wall are contacted the back and are taken place the rotation, suppression gyro wheel 441 drives worm 44 and carries out synchronous rotation, worm 44 drives worm wheel 43 and rotates, worm wheel 43 drives puddler 42 and helical stirring vane 421 and carries out the rotation again, suppression gyro wheel 441 breaks away from transmission arc piece 6 and just ends the effect of rotation. As is well known, because of the effect of gravity, aviation fuel and additive in the mixing chamber 1 are piled up downwards, there will be no material blank area in the inside high-end department of mixing chamber 1, and the supplementary rabbling mechanism 4 that is in high-end department at this moment belongs to invalid stirring operation if carrying out supplementary stirring work, and it has invalid stirring operation to last supplementary stirring promptly, but this problem has been avoided in intermittent type nature stirring, and supplementary rabbling mechanism 4 only rotates along with mixing chamber 1 to low-end department and contradicts with transmission arc piece 6 and just takes place supplementary stirring operation.
Furthermore, due to the fact that the pressing roller 441 is intermittently abutted against the transmission arc-shaped block 6 and then is prone to being damaged due to overlarge pressing force, at least two guide seats 412 are arranged on the outer side wall of the mounting disc 41, at least two guide rods 14 matched with the guide seats 412 are arranged at the top and the bottom of the mixing chamber 1, a connecting plate 15 is installed in the middle of each guide rod 14, a spring 16 is sleeved on each guide rod 14, a limiting handle 17 is arranged at one end, far away from the connecting plate 15, of each guide rod 14, the mounting disc 41 is arranged at the top or the bottom of the mixing chamber 1 in a sliding and sealing mode, all the guide rods 14 are arranged in all the guide seats 412 in a sliding mode respectively, and two ends of each spring 16 are fixedly connected with the connecting plate 15 and the guide seats 412 respectively; after the pressing roller 441 enters the inner side wall of the transmission arc-shaped block 6, the pressing roller 441 is pressed to drive the mounting disc 41 to slide towards the direction of the mixing chamber 1, all the guide seats 412 on the mounting disc 41 can press all the springs 16 to be in a compressed state, the compression distance of the springs 16 can be used as the movement buffer distance of the mounting disc 41, so that the service life of the pressing roller 441 is prolonged, the stability is improved, and after the pressing roller 441 is separated from the transmission arc-shaped block 6, the elastic force of the springs 16 can drive the pressing roller 441 to recover to the initial position.
Finally, it should be noted that: the above embodiments are only used to illustrate the technical solution of the present invention, and not to limit the same; while the invention has been described in detail and with reference to the foregoing embodiments, it will be understood by those skilled in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some or all of the technical features may be equivalently replaced; and the modifications or the substitutions do not make the essence of the corresponding technical solutions depart from the scope of the technical solutions of the embodiments of the present invention.
Claims (6)
1. The device for mixing the aviation fuel and the additive comprises a mixing chamber (1) and a base (2), and is characterized in that a feed inlet (11) and a detachable sealing cover (12) for sealing the feed inlet (11) are arranged on the mixing chamber (1), supporting shafts (13) are arranged at two ends of the mixing chamber (1), two rotating supports (21) and two supporting frames (22) are arranged on the base (2), a reduction box (23) and a rotating motor (24) are arranged on the two supporting frames (22), the two rotating supports (22) are symmetrically arranged at two sides of the mixing chamber (1), the mixing chamber (1) is rotatably arranged on the two rotating supports (22) through the two supporting shafts (13), the supporting frames (22) are positioned beside one rotating support (21), the reduction box (23) is in transmission connection with one of the supporting shafts (13), and the rotating motor (24) is connected to the reduction box (23);
still include angle adjustment mechanism (3), two supplementary rabbling mechanisms (4) and driving medium, angle adjustment mechanism (3) are used for carrying out angle modulation to base (2), angle adjustment mechanism (3) include underframe (31), half gear (32), pass electric putter (33), slide (34), slide rail (35) and rack (36), the both ends of base (2) all are equipped with pivot (26), base (2) rotate through two pivot (26) and set up on underframe (31), half gear (32) set up the center department in base (2) bottom, and half gear (32) and pivot (26) coaxial line, pass electric putter (33) and slide (34) and be located half gear (32) under, slide rail (35) slide and set up on slide (34), and the tail end of slide rail (35) and the output fixed connection who promotes electric putter, rack (36) set up at the top of slide rail (35), and rack (36) and half gear (32) meshing, the supplementary rabbling mechanism (4) are used for carrying out auxiliary mixing disk (41), aviation stirring dish (41) and aviation stirring rod (41), two rotating seats (411) which are symmetrically arranged are arranged on the mounting disc (41), the stirring rod (42) is provided with a spiral stirring blade (421), two ends of the worm (44) are both provided with a pressing roller (441), the mounting plate (41) is arranged on the top or the bottom of the mixing chamber (1) in a sealing way, the stirring rod (42) is rotatably arranged at the center of the mounting plate (41), the spiral stirring blade (421) is positioned in the mixing chamber (1), the worm wheel (43) is arranged at one end far away from the spiral stirring blade (421), the worm (44) is rotationally arranged on the two rotating seats (411), and the worm (44) is meshed with the worm wheel (43), the transmission piece is used for transmitting the rotating force of the mixing chamber (1) to the two auxiliary stirring mechanisms (4), the transmission part is a transmission circular ring (5) or a transmission arc-shaped block (6), the top of the base (2) is provided with a mounting seat (25), and the mounting seat (25) is positioned between the two rotating brackets (21), the base (2) is arranged on the angle adjusting mechanism (3), the two auxiliary stirring mechanisms (4) are respectively arranged on the top and the bottom of the mixing chamber (1), the transmission part sets up on the top of mount pad (25), and two supplementary rabbling mechanisms (4) all are connected with the transmission part transmission.
2. An apparatus for blending aviation fuel and additives according to claim 1, wherein: the outer surface of the pressing roller (441) is provided with first anti-skidding grains.
3. An arrangement for mixing aviation fuel and an additive according to claim 1, wherein: and second anti-skid grains are arranged on the inner side wall of the transmission circular ring (5), and the pressing roller (441) is abutted against the inner wall of the transmission circular ring (5).
4. An apparatus for blending aviation fuel and additives according to claim 1, wherein: and third anti-skidding threads are arranged on the inner side wall of the transmission arc-shaped block (6).
5. An arrangement for mixing aviation fuel and additives according to claim 1 or 4, wherein: and inner chamfers (61) are arranged at two ends of the top of the transmission arc-shaped block (6).
6. An arrangement for mixing aviation fuel and an additive according to claim 1, wherein: be equipped with two at least guide holder (412) on the lateral wall of mounting disc (41), the top and the bottom of mixing chamber (1) all are equipped with two at least and guide holder (412) complex guide bar (14), the mid-mounting of guide bar (14) has connecting plate (15), the cover is equipped with spring (16) on guide bar (14), the one end that connecting plate (15) were kept away from in guide bar (14) is equipped with spacing handle (17), mounting disc (41) sliding seal sets up on the top or the bottom of mixing chamber (1), and all guide bar (14) slide respectively and set up in all guide holders (412), the both ends of spring (16) respectively with connecting plate (15) and guide holder (412) fixed connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211044438.0A CN115138255B (en) | 2022-08-30 | 2022-08-30 | Device for mixing aviation fuel and additive |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211044438.0A CN115138255B (en) | 2022-08-30 | 2022-08-30 | Device for mixing aviation fuel and additive |
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| CN115138255A CN115138255A (en) | 2022-10-04 |
| CN115138255B true CN115138255B (en) | 2022-11-25 |
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| CN113230953A (en) * | 2018-10-24 | 2021-08-10 | 崔映雪 | Linkage conduction device for transverse oscillation of medical test tube |
| CN110065164A (en) * | 2019-05-17 | 2019-07-30 | 陈常 | A kind of building building cement is stirred system and method |
| CN110640902A (en) * | 2019-09-26 | 2020-01-03 | 海南大学 | Swing type concrete uniform stirring device |
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| CN212736527U (en) * | 2020-05-20 | 2021-03-19 | 亚泰集团哈尔滨建材有限公司 | Novel from formula cement concrete mixer that falls |
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