CN217919817U - Novel scraper machine aircraft nose is scraped in self-cleaning - Google Patents
Novel scraper machine aircraft nose is scraped in self-cleaning Download PDFInfo
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- CN217919817U CN217919817U CN202221632223.6U CN202221632223U CN217919817U CN 217919817 U CN217919817 U CN 217919817U CN 202221632223 U CN202221632223 U CN 202221632223U CN 217919817 U CN217919817 U CN 217919817U
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- aircraft nose
- head
- mainboard
- install
- head pulley
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- 238000004140 cleaning Methods 0.000 title claims abstract description 15
- 238000005728 strengthening Methods 0.000 claims abstract description 9
- 238000009434 installation Methods 0.000 claims abstract description 8
- 230000000903 blocking effect Effects 0.000 claims description 10
- 230000003014 reinforcing effect Effects 0.000 claims description 7
- 235000000396 iron Nutrition 0.000 claims description 3
- 230000002950 deficient Effects 0.000 abstract description 9
- 238000007790 scraping Methods 0.000 abstract description 6
- 238000013329 compounding Methods 0.000 abstract description 2
- 230000009286 beneficial effect Effects 0.000 abstract 1
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000009825 accumulation Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000010030 laminating Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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Abstract
The utility model relates to a machinery for the granary, in particular to novel scrape trigger aircraft nose from clear. The technical scheme is as follows: including aircraft nose casing, head pulley, aircraft nose dam device, base, the bottom installation base of aircraft nose casing, install the head pulley at the inner chamber of aircraft nose casing the outside installation aircraft nose dam device of head pulley, aircraft nose dam device is including keeping off material mainboard, strengthening rib, head race, shirt rim, keeps off the front end of material mainboard and is equipped with the head race for install the both sides at the head pulley, keep off material mainboard rear end and install the strengthening rib, keep off the both sides of material mainboard and be equipped with and be used for being connected fixed shirt rim with aircraft nose shells inner wall. The beneficial effects are that: the utility model discloses avoid the defective material to stop in the aircraft nose position to supplementary the self-cleaning function who has realized scraping the trigger avoids causing stifled problem of quick-witted, perhaps avoids the defective material to get into last grain position of storehouse and causes the compounding.
Description
Technical Field
The utility model relates to a machinery for the granary, in particular to novel scrape trigger aircraft nose from clear.
Background
At present, in machinery for a grain bin, scraper machines are common machinery and are various, and especially when materials are conveyed into a plurality of grain storage bin positions, most of the scraper machines cannot avoid accumulation of residual materials at machine heads, so that machine blockage is easily caused, or the residual materials enter the last grain storage bin position to cause material mixing; the main problems are as follows: the key point is how to realize self-cleaning backflow by residual materials accumulated on the machine head of the scraper machine, so that a novel self-cleaning scraper machine head is urgently needed to be designed.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a novel scrape trigger aircraft nose from clearing to the above-mentioned defect that prior art exists, come the supplementary self-cleaning function that realizes scraping the trigger from clearing.
The utility model provides a novel scrape trigger aircraft nose from clear, its technical scheme is: including aircraft nose casing (1), head pulley (2), aircraft nose dam device (3), base (4), bottom installation base (4) of aircraft nose casing (1), install head pulley (2) in the inner chamber of aircraft nose casing (1), bearing (2.3) in bearing holder (2.2) are passed through to one side of head pulley (2) are connected, connecting axle (2.1) is installed to the opposite side, wherein, the outside installation aircraft nose dam device (3) of head pulley (2), aircraft nose dam device (3) including keeping off material mainboard (3.1), strengthening rib (3.2), head pulley groove (3.4), shirt rim (3.7), the front end that keeps off material mainboard (3.1) is equipped with head pulley groove (3.4) for install the both sides in head pulley (2), strengthening rib (3.2) are installed to fender mainboard (3.1) rear end, the both sides that keep off material mainboard (3.1) be equipped with shirt rim (3.7) that are used for with aircraft nose casing (1) inner wall connection fixed.
Preferably, the front end of the material blocking main plate (3.1) is provided with an arc-shaped head (3.3) which is positioned at two sides of the head wheel groove (3.4).
Preferably, the lower part of the arc-shaped head (3.3) is provided with a shaft groove (3.5) which is of a concave arc-shaped structure.
Preferably, the reinforcing rib (3.2) is of a long strip structure and is fixedly arranged in the middle of the material blocking main board (3.1) through a bolt (3.6).
Preferably, the head pulley (2) adopts a gear for driving the chain to rotate in the inner cavity of the handpiece shell (1).
Preferably, screw holes are uniformly distributed in the skirt edge (3.7), and the nose material blocking device (3) is fixed on the inner wall of the nose shell (1) through screws.
The front end of the handpiece shell (1) is provided with a slope structure (1.2), and two sides of the handpiece shell (1) are provided with reinforcing angle irons (1.1).
The utility model has the advantages that: the utility model discloses a it is two-layer about separating into the aircraft nose casing to set up the fender material mainboard, the lower floor drives the entry that the graininess grain was transferred to the scraper blade normally to promote through the chain, the purpose on the upper strata of formation then is with the defective material upset upper strata, the rethread chain drives the scraper blade and reversely carries the tail position with the defective material and carry once more, avoid the defective material to stop in the aircraft nose position, thereby the supplementary function of clearing oneself that has realized scraping the trigger, avoid causing the problem of stifled machine, perhaps avoid the defective material to get into last grain position and cause the compounding.
Drawings
Fig. 1 is a schematic side view of the present invention;
fig. 2 is a top view of the present invention;
fig. 3 is a perspective view of the present invention;
FIG. 4 is a schematic structural view of a nose stock stop;
in the upper diagram: aircraft nose casing 1, head pulley 2, aircraft nose dam device 3, base 4, strengthen angle bar 1.1, slope structure 1.2, connecting axle 2.1, bearing support 2.2, bearing 2.3, keep off material mainboard 3.1, strengthening rib 3.2, arc head 3.3, head pulley groove 3.4, shaft groove 3.5, bolt 3.6, shirt rim 3.7.
Detailed Description
The preferred embodiments of the present invention will be described in conjunction with the accompanying drawings, and it will be understood that they are presented herein only to illustrate and explain the present invention, and not to limit the present invention.
The front end of the material blocking main plate 3.1 is provided with an arc-shaped head 3.3 which is positioned at two sides of the head wheel groove 3.4 and can be better attached to a head wheel, and the arc-shaped head can play a role in guiding and better turning over residual materials; the below of arc head 3.3 is equipped with axle slot 3.5, for the arc structure of concavity, for the better laminating of connecting axle department with the head pulley, it is two-layer about making to keep off material mainboard 3.1 and separating into aircraft nose casing 1, the lower floor drives the normal graininess grain of promotion of scraper blade through the chain and transfers the entry to the granary, the purpose on the upper strata of formation then is to overturn the upper strata with the defective material, the rethread chain drives the scraper blade and carries the tail position once more with the defective material is reverse, avoid the defective material to stop in the aircraft nose position.
In addition, the reinforcing ribs 3.2 are of long strip-shaped structures and are fixedly installed in the middle of the material blocking main board 3.1 through the bolts 3.6, and therefore the effect of reinforcing the stability of the material blocking main board 3.1 can be achieved.
The head wheel 2 adopts a gear and is used for driving a chain to rotate in the inner cavity of the head shell 1, and the chain is provided with a plurality of scraping plates which can scrape grains to move forwards.
Screw holes are uniformly distributed on the skirt edge 3.7, and the nose material blocking device 3 is fixed on the inner wall of the nose shell 1 through screws.
In addition, the front end of the machine head shell 1 is provided with a slope structure 1.2, so that the space outside the head wheel 2 is increased, and the residual materials can be accumulated less; in addition, the two sides of the machine head shell 1 are provided with a plurality of groups of reinforcing angle irons 1.1, so that the outer wall of the machine head shell 1 is firmer and firmer.
When the utility model works, the scraper conveyor conveys granular grains into a plurality of grain bin positions, the chain in the scraper conveyor can drive the materials to move forward, and because of the motion inertia and the structural characteristics of the chain, the inevitable residual materials can be moved to the machine head and accumulated at the machine head; at the moment, the utility model plays a role of auxiliary self-cleaning, and firstly, the front end slope structure 1.2 of the nose shell 1 can ensure that the residual materials are less accumulated; secondly aircraft nose dam device 3 separates into upper and lower two-layer to the aircraft nose portion that the head wheel is backward, and the chain overturns the upper strata that keeps off material mainboard 3.1 to the realization clout removes to the tail direction of scraping the trigger along keeping off the upper strata of material mainboard 3.1, thoroughly realizes scraping the self-cleaning circulation of trigger.
The above description is only a preferred embodiment of the present invention, and any person skilled in the art may modify the present invention or modify it into an equivalent technical solution by using the technical solutions described above. Therefore, any simple modifications or equivalent changes made according to the technical solution of the present invention belong to the scope of the present invention as far as possible.
Claims (7)
1. The utility model provides a novel scraper blade aircraft nose is scraped in self-cleaning, includes aircraft nose casing (1), head pulley (2), aircraft nose dam device (3), base (4), the bottom installation base (4) of aircraft nose casing (1), install head pulley (2) at the inner chamber of aircraft nose casing (1), bearing (2.3) in bearing support (2.2) are passed through to one side of head pulley (2) are connected, connecting axle (2.1), characterized by are installed to the opposite side: the outside installation aircraft nose dam device (3) of head pulley (2), aircraft nose dam device (3) including keeping off material mainboard (3.1), strengthening rib (3.2), head race (3.4), shirt rim (3.7), the front end that keeps off material mainboard (3.1) is equipped with head race (3.4) for install the both sides in head pulley (2), keep off material mainboard (3.1) rear end and install strengthening rib (3.2), the both sides that keep off material mainboard (3.1) be equipped with be used for with fixed shirt rim (3.7) of aircraft nose casing (1) inner wall connection.
2. The novel self-cleaning scraper machine head as claimed in claim 1, characterized in that: the front end of the material blocking main board (3.1) is provided with an arc-shaped head (3.3) which is positioned at two sides of the head wheel groove (3.4).
3. The novel self-cleaning scraper machine head as claimed in claim 2, characterized in that: the lower part of the arc-shaped head (3.3) is provided with a shaft groove (3.5) which is of a concave arc-shaped structure.
4. The novel self-cleaning scraper machine head as claimed in claim 1, characterized in that: the reinforcing ribs (3.2) are of long strip-shaped structures and are fixedly arranged in the middle of the material blocking main board (3.1) through bolts (3.6).
5. The novel self-cleaning scraper machine head as claimed in claim 1, characterized in that: the head wheel (2) adopts a gear and is used for driving the chain to rotate in the inner cavity of the head shell (1).
6. The novel self-cleaning scraper machine head as claimed in claim 1, characterized in that: the machine head material blocking device (3) is fixed on the inner wall of the machine head shell (1) through screws.
7. The novel self-cleaning scraper machine head as claimed in claim 1, characterized in that: the front end of the handpiece shell (1) is provided with a slope structure (1.2), and two sides of the handpiece shell (1) are provided with reinforcing angle irons (1.1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221632223.6U CN217919817U (en) | 2022-06-28 | 2022-06-28 | Novel scraper machine aircraft nose is scraped in self-cleaning |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221632223.6U CN217919817U (en) | 2022-06-28 | 2022-06-28 | Novel scraper machine aircraft nose is scraped in self-cleaning |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217919817U true CN217919817U (en) | 2022-11-29 |
Family
ID=84184854
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221632223.6U Active CN217919817U (en) | 2022-06-28 | 2022-06-28 | Novel scraper machine aircraft nose is scraped in self-cleaning |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217919817U (en) |
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2022
- 2022-06-28 CN CN202221632223.6U patent/CN217919817U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A New Type of Self Cleaning Scraper Head Effective date of registration: 20231228 Granted publication date: 20221129 Pledgee: China Merchants Bank Co.,Ltd. Dongying Branch Pledgor: COFCO Yingchun Agricultural and Animal Husbandry Machinery (Shandong) Co.,Ltd. Registration number: Y2023980074850 |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right |