CN204777250U - Domatic vibration feeding machine of different angles has on fuselage inner bottom - Google Patents
Domatic vibration feeding machine of different angles has on fuselage inner bottom Download PDFInfo
- Publication number
- CN204777250U CN204777250U CN201520301793.0U CN201520301793U CN204777250U CN 204777250 U CN204777250 U CN 204777250U CN 201520301793 U CN201520301793 U CN 201520301793U CN 204777250 U CN204777250 U CN 204777250U
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- CN
- China
- Prior art keywords
- domatic
- angle
- fuselage
- vibration feeder
- inner bottom
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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- 238000007599 discharging Methods 0.000 claims description 14
- 238000010521 absorption reaction Methods 0.000 claims description 3
- 239000000463 material Substances 0.000 abstract description 26
- 230000000694 effects Effects 0.000 abstract description 7
- 230000005284 excitation Effects 0.000 abstract 2
- 230000035939 shock Effects 0.000 abstract 1
- 238000013467 fragmentation Methods 0.000 description 5
- 238000006062 fragmentation reaction Methods 0.000 description 5
- 238000012216 screening Methods 0.000 description 5
- 239000004566 building material Substances 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000011236 particulate material Substances 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
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Abstract
The utility model provides a domatic vibration feeding machine of different angles has on fuselage inner bottom includes the fuselage, excitation unit and shock attenuation unit, wherein, the inner bottom of fuselage is formed by a plurality of domatic combinations with the different angle slopes of same direction from relative pan feeding mouth to discharge gate, thereby form at the fuselage inner bottom by a plurality of domatic vibration feeding machines with the different angle slopes of same direction, wherein, it has two domatic as the example with angle slope to use, the first domatic angle alpha 2 of the relative second of 1 domatic angle of angle alpha is less, can effectively reduce the initial velocity of the material of the free fall mode of passing through whereabouts. The material gets into the machine by the pan feeding mouth, and is domatic and by the vibration effect that the excitation unit produced through the multi -angle, reaches even and possess very high per hour thruput by discharge gate exhaust material, and the time that makes the material stop in mechanical equipment simultaneously is elongated, and the number of times that is vibrated increases, and the material can be discharged from the discharge gate very uniformly to promote the homocline effect.
Description
Technical field
The utility model relates to a kind of vibration feeder, more particularly, relates to and a kind ofly has the domatic vibration feeder of different angles in fuselage the end.
Background technology
Vibration feeder is the homocline machinery before being arranged in fragmentation, screening plant, can make the material by this machinery, and the bulk and the particulate material that are generally building materials can evenly fall after its adjustment.But in the fuselage of existing vibration feeder the discharging opening from the feeding mouth of front portion to rear portion is the domatic of unique angle at the end.An angle like this domatic, if angle is excessive, then homocline effect is bad; If angle too small, then the total inventory by machinery per hour is little.Therefore, when vibration feeder machine operation, material freely falls to from feeding mouth the material curtain that the interior end is formed is normal distribution, and namely intermediate material is many, and both sides material is few, and bad to the homocline effect of material, throughput is also undesirable.This obviously affects fragmentation, the crudy of screening plant, work efficiency and service life.This is that can a technical personnel in the art reach function of homogenizing materials to vibration feeder and improve throughput problem in the urgent need to address.
Summary of the invention
The purpose of this utility model is the deficiency existed in material process to overcome above-mentioned existing vibration feeder, through in-depth study, according to the distribution of material on the interior end and flow feature, and a kind of being arranged at the end in it proposed has the domatic vibration feeder of different angles.
The technical scheme realizing above object is to provide a kind ofly has the domatic vibration feeder of different angles in fuselage the end, comprise fuselage, exciting unit and vibration absorption unit, wherein, the front portion of fuselage has feeding mouth, rear portion has discharging opening, here, the interior end of described fuselage is with domatic the combining of same direction different angles inclination by some from relative feeding mouth to discharging opening.
Vibration feeder as previously discussed, wherein, described domatic be 2, namely first is domatic and second domatic, and first is domaticly positioned at anterior at the bottom of fuselage and forms α 1 angle with horizontal surface, and second is domaticly positioned at postmedian at the bottom of fuselage and forms α 2 angle with horizontal surface.
Vibration feeder as previously discussed, wherein, the second domatic angle [alpha] 2 is more than or equal to the first domatic angle [alpha] 1.
Vibration feeder as previously discussed, wherein, described first domatic length L1 is equal to or less than the second domatic length L2.
Vibration feeder as previously discussed, wherein, the first domatic angle [alpha] 1 is 5 °-45 °, and the second domatic angle [alpha] 2 is 5 °-45 °.
Vibration feeder as previously discussed, wherein, the interior end of described fuselage is Wear-resisting bottom plate.
Therefore, the interior end of fuselage is with domatic the combining of same direction different angles inclination by some from relative feeding mouth to discharging opening, thus be formed in the end in fuselage by some domatic vibration feeders tilted with same direction different angles, wherein, to have two domatic with angle, the first domatic domatic angle of angle [alpha] 1 angle [alpha] 2 domatic relative to second is less, effectively can be decreased through the initial velocity of the material that free-falling body mode falls.Material enters machine by feeding mouth, the vibrating effect that is domatic and that produced by exciting unit by multi-angle, reach the material of being discharged by discharging opening evenly and have very high thruput per hour, make the time of material stop in mechanical equipment elongated simultaneously, by the increased frequency vibrated, material can be discharged from discharging opening very equably, thus promotes homocline effect.
Accompanying drawing explanation
Fig. 1 is schematic front view of the present invention;
Fig. 2 is the cutaway view after the removal exciting unit of Fig. 1.
Detailed description of the invention
Refer to Fig. 1 and Fig. 2, there is shown and a kind ofly have the domatic vibration feeder of different angles in fuselage the end, comprise fuselage 1, exciting unit 2 and vibration absorption unit 3, wherein, wherein, the front portion of fuselage 1 has feeding mouth 11, this feeding mouth is specifically positioned on fuselage end face so that charging, rear portion has discharging opening 12, this discharging opening to be generally positioned at the bottom of fuselage on 13 or bottom surface to facilitate discharging, the interior end 13 is domatic, the interior end 13 of described fuselage domatic from relative feeding mouth 11 to discharging opening 12 be by some tilt with same direction different angles domaticly to combine, namely can 2, 3 or 4 domatic combinations, this is conducive to solving the material entering fuselage and expects that when free fall curtain is normal distribution, namely intermediate material is many, in the few situation of both sides material, the domatic continuous action that different angles on the interior end 13 tilt changes material that is middle and both sides into expects curtain uniformly, and enter fragmentation, screening plant.
In addition, the described interior end 13 is a Wear-resisting bottom plate or abrasion-proof backing block, also can be multiple with the combination of the abrasion-proof backing block with this base plate with same different angles face of slope on non-abrasive base plate.
As one of preferred embodiment of the present utility model, on the interior end 13, described domatic by 2 or form by 2, namely first domatic 131 and second domatic 132, first domatic 131 is positioned at 13 front portions at the bottom of fuselage and forms the angle of α 1 with horizontal surface, and second domatic 132 is positioned at 13 postmedians at the bottom of fuselage and forms the angle of α 2 with horizontal surface.
Make as the angle [alpha] 2 that preferred embodiment two, second of the present utility model is domatic and be more than or equal to the first domatic angle [alpha] 1.Their concrete range of choice is first domatic 131, and the angle [alpha] 1 of the angle formed with horizontal surface is 5 °-45 °, second domatic 132, and the angle [alpha] 2 of the angle formed with horizontal surface is 5 °-45 °.
As preferred embodiment three of the present utility model, the described length L1 of first domatic 131 is equal to or less than the length L2 of second domatic 132.
In the sand line processed (there is the feeding capacity of 300t/h) of the equipment such as the feeding of model SP-300, fragmentation and screening, use before vibration feeder of the present utility model (K8601.01) being arranged in fragmentation, screening plant.During operation, material enters vibration feeder by feeding mouth, the vibration that is domatic and that produced by exciting unit by its different angles, make the material of discharging from discharging opening evenly and have very high thruput per hour, that is by this vibration feeder function, material is adjusted, larger throughput can be obtained, have again fine homocline effect, the throughput and the homocline that solve vibration feeder are difficult to satisfactory to both parties situation.
Claims (6)
1. one kind has the domatic vibration feeder of different angles in fuselage the end, comprise fuselage, exciting unit and vibration absorption unit, wherein, the front portion of fuselage has feeding mouth, rear portion has discharging opening, it is characterized in that, the interior end of described fuselage is with domatic the combining of same direction different angles inclination by some from relative feeding mouth to discharging opening.
2. vibration feeder as claimed in claim 1, it is characterized in that, the interior end of described fuselage is Wear-resisting bottom plate.
3. vibration feeder as claimed in claim 1, it is characterized in that, described domatic be 2, namely first is domatic and second domatic, first to be domaticly positioned at the bottom of fuselage anterior and to form α 1 angle with horizontal surface, and second is domaticly positioned at postmedian at the bottom of fuselage and forms α 2 angle with horizontal surface.
4. vibration feeder as claimed in claim 3, is characterized in that, the second domatic angle [alpha] 2 is more than or equal to the first domatic angle [alpha] 1.
5. vibration feeder as claimed in claim 3, is characterized in that, described first domatic length L1 is equal to or less than the second domatic length L2.
6. the vibration feeder according to any one of claim 3 to 5, is characterized in that, the first domatic angle [alpha] 1 is 5 °-45 °, and the second domatic angle [alpha] 2 is 5 °-45 °.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520301793.0U CN204777250U (en) | 2015-05-12 | 2015-05-12 | Domatic vibration feeding machine of different angles has on fuselage inner bottom |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520301793.0U CN204777250U (en) | 2015-05-12 | 2015-05-12 | Domatic vibration feeding machine of different angles has on fuselage inner bottom |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204777250U true CN204777250U (en) | 2015-11-18 |
Family
ID=54517349
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520301793.0U Expired - Fee Related CN204777250U (en) | 2015-05-12 | 2015-05-12 | Domatic vibration feeding machine of different angles has on fuselage inner bottom |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204777250U (en) |
-
2015
- 2015-05-12 CN CN201520301793.0U patent/CN204777250U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20151118 Termination date: 20200512 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |