CN219844905U - Cover plate for reducing oil mist of popcorn - Google Patents
Cover plate for reducing oil mist of popcorn Download PDFInfo
- Publication number
- CN219844905U CN219844905U CN202321208310.3U CN202321208310U CN219844905U CN 219844905 U CN219844905 U CN 219844905U CN 202321208310 U CN202321208310 U CN 202321208310U CN 219844905 U CN219844905 U CN 219844905U
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- China
- Prior art keywords
- hole
- screw
- sleeve
- stirring rod
- oil mist
- Prior art date
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- 239000003595 mist Substances 0.000 title claims abstract description 20
- 235000002017 Zea mays subsp mays Nutrition 0.000 title claims abstract description 17
- 241000482268 Zea mays subsp. mays Species 0.000 title claims abstract description 17
- 238000003756 stirring Methods 0.000 claims abstract description 33
- 230000000149 penetrating effect Effects 0.000 claims abstract description 5
- 239000012634 fragment Substances 0.000 claims description 15
- 239000010705 motor oil Substances 0.000 claims description 10
- 240000007594 Oryza sativa Species 0.000 claims description 3
- 235000007164 Oryza sativa Nutrition 0.000 claims description 3
- 235000009566 rice Nutrition 0.000 claims description 3
- 238000004519 manufacturing process Methods 0.000 abstract description 9
- 230000003044 adaptive effect Effects 0.000 abstract description 5
- 238000001125 extrusion Methods 0.000 abstract description 5
- 238000000034 method Methods 0.000 abstract description 4
- 230000008569 process Effects 0.000 abstract description 2
- 239000003921 oil Substances 0.000 description 12
- 235000014571 nuts Nutrition 0.000 description 5
- 230000008859 change Effects 0.000 description 3
- 239000002360 explosive Substances 0.000 description 3
- 238000012423 maintenance Methods 0.000 description 3
- 238000005452 bending Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 235000017060 Arachis glabrata Nutrition 0.000 description 1
- 244000105624 Arachis hypogaea Species 0.000 description 1
- 235000010777 Arachis hypogaea Nutrition 0.000 description 1
- 235000018262 Arachis monticola Nutrition 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 230000005489 elastic deformation Effects 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000010030 laminating Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 235000020232 peanut Nutrition 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 125000006850 spacer group Chemical group 0.000 description 1
- 230000008093 supporting effect Effects 0.000 description 1
- 238000009834 vaporization Methods 0.000 description 1
- 230000008016 vaporization Effects 0.000 description 1
Landscapes
- Food-Manufacturing Devices (AREA)
Abstract
The utility model provides a cover plate for reducing oil mist of popcorn, which comprises a top cover arranged on one side of a machine head, wherein two sides of the machine head are respectively connected with the top cover through connecting rods, one side of the machine head is provided with a rotary disk, the bottom of the rotary disk is provided with a stirring rod, the top cover comprises a first through hole, the stirring rod is arranged in the first through hole in a penetrating way, an adaptive shrinkage assembly is detachably arranged on the first through hole, the adaptive shrinkage assembly comprises a sleeve, a plurality of ejector blocks are arranged in the sleeve along the circumferential direction, one side of each ejector block is provided with an arc surface, the plurality of arc surfaces are connected to form a shrinkage port, the side wall of the stirring rod is abutted against the arc surface, and the ejector blocks can radially move along the sleeve under the extrusion of the stirring rod. The utility model has ingenious design, can greatly reduce the size of the hole site in the rotation process of the stirring rod, reduce the difficulty of manufacturing and debugging, ensure the stability of integral production and ensure small oil mist escape.
Description
Technical Field
The utility model relates to the technical field of popcorn peanut production, in particular to a cover plate for reducing oil mist of popcorn.
Background
In the process of popcorn production, oil and sugar are required to be added, vaporization of the oil and the sugar is carried out under the high-temperature condition, and corresponding hole sites are required to be formed in the center of the cover plate when the stirring rod rotates. The gasified oil-sugar mixture escapes from the hole site in the center of the cover plate into a production workshop, and then is attached to the surface of equipment, meanwhile, oil mist in the workshop is heavier, the whole production environment is affected, and the cover plate and the machine head are generally directly welded through a connecting rod, so that the later-stage assembly and disassembly cleaning maintenance is very inconvenient.
The position that traditional apron can't adapt to the stirring rod carries out the adjustment of hole site, leads to the oil mist escape volume great, uses inconvenient, and equipment production is influenced, and clear time interval is shorter simultaneously, has increased operating personnel's burden, consequently needs the improvement.
Disclosure of Invention
The utility model provides a cover plate for reducing oil mist of a popcorn machine, which solves the problems that the traditional popcorn frying cover plate is large in hole opening, cannot adapt to the position and the size of a stirring rod to carry out self-adaptive adjustment, is large in oil mist escape amount, inconvenient to detach and troublesome to clean and maintain.
In order to solve the technical problems, the utility model adopts the following technical scheme: a apron for reducing puffed rice engine oil fog, including setting up the top cap in aircraft nose one side, the aircraft nose both sides are connected through connecting rod and top cap respectively, and one side of aircraft nose is equipped with the rotary disk, and the rotary disk bottom is equipped with the stirring rod, and the top cap includes first through-hole, and the stirring rod wears to establish in first through-hole, and detachable is equipped with self-adaptation shrink subassembly on the first through-hole, and self-adaptation shrink subassembly includes the sleeve, is equipped with a plurality of kicking blocks along circumference in the sleeve, and kicking block one side is equipped with the arc surface, and a plurality of arc surfaces are connected and are formed the shrink mouth, and the lateral wall of stirring rod supports and leans on the arc surface, and the kicking block receives the stirring rod extrusion and can follow sleeve radial movement.
In the preferred scheme, the aircraft nose both sides are equipped with first screw thread post respectively, are equipped with the cavity in the connecting rod, and cavity one side runs through and is equipped with first spout, first screw thread post and first spout sliding connection, and first screw thread post passes through the nut and is connected with the connecting rod.
In the preferred scheme, first screw post one side parallel is equipped with two otic placodes, is equipped with first screw hole on the otic placode, and the screw wears to establish at first screw hole, and the bottom of screw is equipped with the gasket, and the gasket supports the lateral wall that leans on the connecting rod.
In the preferred scheme, the cavity opposite side runs through and is equipped with the second spout, and second spout and first spout set up perpendicularly, are equipped with T type slider in the second spout, and T type slider and top cap are fixed.
In the preferred scheme, be equipped with the second screw hole on the top cap, T type slider both sides are equipped with second screw thread post and third screw hole respectively, and the second screw thread post is located second screw hole, still runs through on the connecting rod and is equipped with the second through-hole, and second spout one side is equipped with dodges the hole, dodges hole width and T type slider size phase-match, and the screw wears to establish in the second through-hole, screw and third screw hole threaded connection.
In the preferred scheme, the first through-hole outside is equipped with the ring, and the sleeve bottom is equipped with the bottom plate, and the bottom plate passes through screw and ring to be connected, is equipped with a plurality of third through-holes on the sleeve, and relative arc surface one side is equipped with the shell fragment on the kicking block, and the shell fragment wears to establish in the third through-hole, and the cover is equipped with the spring on the shell fragment, and the shell fragment passes through nut and telescopic connection.
In the preferred scheme, the bottom of kicking block is equipped with the push rod, and the shell fragment downside is equipped with the kink, and the kink passes through the screw and is connected with the top cap.
In the preferred scheme, sleeve upper portion still is equipped with the shade, is equipped with the fourth through-hole in the middle of the shade, and the stirring rod wears to establish in the fourth through-hole, shade and sleeve threaded connection.
The beneficial effects of the utility model are as follows: adopt convenient ann to tear structural design open, guaranteed that the connecting rod can be quick respectively with aircraft nose and apron assemble to easily carry out convenient maintenance in the later stage, set up self-adaptation shrink subassembly in the first through-hole position of apron, wherein the kicking block can be better utilize the circular arc face laminating of self at the stirring rod lateral wall, when the rotatory in-process of stirring rod, extrusion promotes the kicking block outwards to remove, when the stirring rod leaves the kicking block of contact, this kicking block receives the elastic force of spring and resumes to initial condition, has guaranteed the operating condition stability of shrink mouth. The utility model has smart design, convenient operation and good economic benefit.
Drawings
The utility model is further illustrated by the following examples in conjunction with the accompanying drawings:
FIG. 1 is a schematic view of the overall structure of the present utility model in state one;
FIG. 2 is a schematic front view of FIG. 1;
FIG. 3 is a left side schematic view of FIG. 1;
FIG. 4 is a schematic view of the overall structure of the present utility model in state two;
FIG. 5 is a schematic view of the explosive structure of FIG. 1 in state one;
FIG. 6 is an enlarged schematic view at A of FIG. 5;
FIG. 7 is a schematic view of the explosive structure of FIG. 1 in a second state;
FIG. 8 is a schematic view of the roof mounted adaptive retraction assembly of FIG. 1;
fig. 9 is a schematic view of the explosive structure of the adaptive retraction assembly of the present utility model.
In the figure: a handpiece 1; a first threaded post 101; an ear plate 102; a first screw hole 103; a rotating disc 2; a stirring rod 3; a top cover 4; a first through hole 401; a second threaded hole 402; a circular ring 403; a connecting rod 5; a first chute 501; a second chute 502; avoidance hole 503; a second through hole 504; a T-shaped slider 505; a second threaded post 506; a third threaded hole 507; an adaptive retraction assembly 6; a sleeve 601; a base 602; a third through hole 603; a top block 604; an arc surface 605; push rod 606; a spring 607; a spring 608; a mask 609; a fourth through hole 610; a bent portion 611; a constriction 612; a screw 7; a nut 8; a spacer 9.
Detailed Description
1-9, a apron for reducing puffed rice engine oil fog, including setting up top cap 4 in aircraft nose 1 one side, aircraft nose 1 both sides are connected through connecting rod 5 and top cap 4 respectively, one side of aircraft nose 1 is equipped with rotary disk 2, rotary disk 2 bottom is equipped with stirring rod 3, top cap 4 includes first through-hole 401, stirring rod 3 wears to establish in first through-hole 401, be equipped with self-adaptation shrink subassembly 6 on the first through-hole 401, self-adaptation shrink subassembly 6 includes sleeve 601, be equipped with a plurality of kicking blocks 604 along circumference in the sleeve 601, kicking block 604 one side is equipped with circular arc face 605, a plurality of circular arc faces 605 are connected and are formed shrink mouths 612, the lateral wall of stirring rod 3 supports and leans on circular arc face 605, kicking block 604 is received stirring rod 3 extrusion and can follow sleeve 601 radial movement. From this structure to make aircraft nose 1 can be convenient drive top cap 4 through connecting rod 5, change of angle carries out, when needs production, cover top cap 4 to the popcorn fryer at first, then stirring rod 3 rotation lets popcorn abundant and auxiliary material such as oily sugar mix, guarantee to be heated abundant, and at the rotatory in-process of stirring rod 3, the kicking block 604 of different positions then carries out the adjustment of self position according to the change of stirring rod 3 position, receive stirring rod 3's extrusion and keep away from first through-hole 401 center, a plurality of kicking blocks 604 cooperation form the shrink mouth 612 that the bore is less than the diameter of first through-hole 401, the diameter of shrink mouth 612 is less than the stirring rod 3 of different diameters and inclination, convenient to use, and is effectual, the degree of difficulty of preparation and debugging has been reduced simultaneously.
In the preferred scheme, the aircraft nose 1 both sides are equipped with first screw thread post 101 respectively, are equipped with the cavity in the connecting rod 5, and cavity one side runs through and is equipped with first spout 501, first screw thread post 101 and first spout 501 sliding connection, and first screw thread post 101 passes through nut 8 and connecting rod 5 to be connected. The connecting rod 5 is made for square pipe, from this structure to make can be convenient install connecting rod 5 on the aircraft nose 1, and holistic position is adjustable, simple operation.
In the preferred scheme, two otic placodes 102 are arranged in parallel on one side of the first threaded column 101, a first threaded hole 103 is arranged on the otic placode 102, a screw 7 is arranged in the first threaded hole 103 in a penetrating mode, a gasket 9 is arranged at the bottom of the screw 7, and the gasket 9 abuts against the outer side wall of the connecting rod 5. From this structure to make can carry out further locking to connecting rod 5 fixed, holistic supporting effect is good, and it is more stable to pass the power.
In a preferred scheme, a second chute 502 is penetrated and arranged on the other side of the cavity, the second chute 502 and the first chute 501 are vertically arranged, a T-shaped sliding block 505 is arranged in the second chute 502, and the T-shaped sliding block 505 is fixed with the top cover 4. With this structure, the cover 4 can be firmly connected with the cover, and the whole assembly and disassembly are convenient.
In the preferred scheme, be equipped with second screw hole 402 on the top cap 4, T type slider 505 both sides are equipped with second screw thread post 506 and third screw hole 507 respectively, and second screw thread post 506 is located second screw hole 402, still runs through on the connecting rod 5 and is equipped with second through-hole 504, and second spout 502 one side is equipped with dodges hole 503, dodges hole 503 width and T type slider 505 size assorted, and screw 7 wears to establish in second through-hole 504, screw 7 and third screw hole 507 threaded connection. From this structure to make can carry out quick installation through T type slider 505 with top cap 4, and then when needs are novel clean the maintenance to the part, dismantle conveniently, holistic outward appearance uniformity is good, does not have obvious screw to expose, and the impression is effectual, has avoided connecting rod 5 inside to be attached by the oil mist easily simultaneously.
In the preferred scheme, the outside of first through-hole 401 is equipped with ring 403, and sleeve 601 bottom is equipped with bottom plate 602, and bottom plate 602 passes through screw 7 and ring 403 to be connected, is equipped with a plurality of third through-holes 603 on the sleeve 601, and relative arc face 605 one side is equipped with shell fragment 607 on the kicking block 604, and shell fragment 607 wears to establish in third through-hole 603, and the cover is equipped with spring 608 on the shell fragment 607, and shell fragment 607 passes through nut 8 and sleeve 601 to be connected. From this structure to make the installation and disassembly of sleeve 601 convenient, shell fragment 607 has guaranteed holistic leakproofness from the downside simultaneously good, has avoided the oil mist to escape from the gap between shrink mouth 612 and the sleeve 601 inside wall, and can adapt to the position change of stirring rod 3, and production is stable.
In a preferred scheme, a push rod 606 is arranged at the bottom of the top block 604, a bending part 611 is arranged at the lower side of the elastic sheet 607, and the bending part 611 is connected with the top cover 4 through a screw 7. With this structure, the spring piece 611 can secure its own position, and at the same time, it is convenient to provide the elastic deformation force for restoring the initial position to the top block 604.
In a preferred scheme, the upper portion of the sleeve 601 is further provided with a shade 609, a fourth through hole 610 is formed in the middle of the shade 609, the stirring rod 3 is arranged in the fourth through hole 610 in a penetrating mode, and the shade 609 is in threaded connection with the sleeve 601. From this structure to make further restrict the oil mist escape mouth, guarantee that holistic oil mist escape volume is controllable, the result of use is better.
The above embodiments are only preferred embodiments of the present utility model, and should not be construed as limiting the present utility model, and the scope of the present utility model should be defined by the claims, including the equivalents of the technical features in the claims. I.e., equivalent replacement modifications within the scope of this utility model are also within the scope of the utility model.
Claims (8)
1. A apron for reducing puffed rice engine oil fog, characterized by: including top cap (4) that sets up in aircraft nose (1) one side, aircraft nose (1) both sides are connected through connecting rod (5) and top cap (4) respectively, one side of aircraft nose (1) is equipped with rotary disk (2), rotary disk (2) bottom is equipped with stirring rod (3), top cap (4) are including first through-hole (401), stirring rod (3) are worn to establish in first through-hole (401), detachable is equipped with self-adaptation shrink subassembly (6) on first through-hole (401), self-adaptation shrink subassembly (6) include sleeve (601), be equipped with a plurality of kicking blocks (604) along circumference in sleeve (601), kicking block (604) one side is equipped with arc surface (605), a plurality of arc surface (605) are connected and are formed shrink mouth (612), the lateral wall of stirring rod (3) supports and leans on arc surface (605), kicking block (604) are pressed along sleeve (601) radial movement by stirring rod (3).
2. A cover for reducing popcorn engine oil mist as set forth in claim 1, wherein: the machine head (1) both sides are equipped with first screw thread post (101) respectively, are equipped with the cavity in connecting rod (5), and cavity one side runs through and is equipped with first spout (501), first screw thread post (101) and first spout (501) sliding connection, and first screw thread post (101) are connected through nut (8) and connecting rod (5).
3. A cover for reducing popcorn engine oil mist as set forth in claim 1, wherein: two lug plates (102) are arranged on one side of the first threaded column (101) in parallel, a first threaded hole (103) is formed in each lug plate (102), a screw (7) is arranged in each first threaded hole (103) in a penetrating mode, a gasket (9) is arranged at the bottom of each screw (7), and the gaskets (9) are abutted against the outer side walls of the connecting rods (5).
4. A cover for reducing popcorn engine oil mist as set forth in claim 2, wherein: the other side of the cavity is provided with a second chute (502) in a penetrating way, the second chute (502) and the first chute (501) are vertically arranged, a T-shaped sliding block (505) is arranged in the second chute (502), and the T-shaped sliding block (505) is fixed with the top cover (4).
5. A cover for reducing popcorn engine oil mist as set forth in claim 4, wherein: be equipped with second screw hole (402) on top cap (4), T type slider (505) both sides are equipped with second screw thread post (506) and third screw hole (507) respectively, second screw thread post (506) are located second screw hole (402), still run through on connecting rod (5) and be equipped with second through-hole (504), second spout (502) one side is equipped with dodges hole (503), dodge hole (503) width and T type slider (505) size phase-match, screw (7) wear to establish in second through-hole (504), screw (7) and third screw hole (507) threaded connection.
6. A cover for reducing popcorn engine oil mist as set forth in claim 1, wherein: the outside of first through-hole (401) is equipped with ring (403), sleeve (601) bottom is equipped with bottom plate (602), bottom plate (602) are connected with ring (403) through screw (7), be equipped with a plurality of third through-holes (603) on sleeve (601), relative arc surface (605) one side is equipped with shell fragment (607) on kicking block (604), shell fragment (607) wears to establish in third through-hole (603), the cover is equipped with spring (608) on shell fragment (607), shell fragment (607) are connected with sleeve (601) through nut (8).
7. A cover for reducing popcorn engine oil mist as set forth in claim 6, wherein: the bottom of kicking block (604) is equipped with push rod (606), and shell fragment (607) downside is equipped with kink (611), and kink (611) are connected with top cap (4) through screw (7).
8. A cover for reducing popcorn engine oil mist as set forth in claim 1, wherein: the upper portion of sleeve (601) still is equipped with shade (609), is equipped with fourth through-hole (610) in the middle of shade (609), and stirring rod (3) wears to establish in fourth through-hole (610), and shade (609) and sleeve (601) threaded connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321208310.3U CN219844905U (en) | 2023-05-18 | 2023-05-18 | Cover plate for reducing oil mist of popcorn |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321208310.3U CN219844905U (en) | 2023-05-18 | 2023-05-18 | Cover plate for reducing oil mist of popcorn |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219844905U true CN219844905U (en) | 2023-10-20 |
Family
ID=88319085
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321208310.3U Active CN219844905U (en) | 2023-05-18 | 2023-05-18 | Cover plate for reducing oil mist of popcorn |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219844905U (en) |
-
2023
- 2023-05-18 CN CN202321208310.3U patent/CN219844905U/en active Active
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |