CN212472408U - Flow channel assembly - Google Patents
Flow channel assembly Download PDFInfo
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- CN212472408U CN212472408U CN201922470082.7U CN201922470082U CN212472408U CN 212472408 U CN212472408 U CN 212472408U CN 201922470082 U CN201922470082 U CN 201922470082U CN 212472408 U CN212472408 U CN 212472408U
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- 238000005520 cutting process Methods 0.000 claims abstract description 170
- 230000007935 neutral effect Effects 0.000 claims description 27
- 238000004891 communication Methods 0.000 claims description 26
- 239000000463 material Substances 0.000 abstract description 9
- 238000000926 separation method Methods 0.000 abstract description 3
- 238000004519 manufacturing process Methods 0.000 description 15
- 238000005516 engineering process Methods 0.000 description 7
- 239000000654 additive Substances 0.000 description 6
- 230000000996 additive effect Effects 0.000 description 6
- 238000000034 method Methods 0.000 description 5
- 238000012545 processing Methods 0.000 description 5
- 230000006837 decompression Effects 0.000 description 4
- 238000005266 casting Methods 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 230000000694 effects Effects 0.000 description 1
- 239000008187 granular material Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 238000012797 qualification Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 239000002893 slag Substances 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
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Abstract
The utility model discloses a runner subassembly relates to vibration material disk and makes technical field to avoid causing the runner structure to damage because of cutting separation operation, and reduce the cutting resistance when cutting reservation cutting structure, reduce the cutting degree of difficulty, easily obtain the runner structure that separates each other. The flow channel assembly comprises at least two flow channel structures, a reserved cutting structure and a pressure reducing structure, wherein the reserved cutting structure is arranged between every two adjacent flow channel structures; the pressure reducing structure is formed on the reserved cutting structure.
Description
Technical Field
The utility model relates to a vibration material disk makes technical field, concretely relates to runner subassembly.
Background
Additive manufacturing is a technique that uses various materials to print a component layer by layer based on a digital model file. It is often used in the fields of mold manufacturing, industrial design, and the like. Compared with a casting process, the material increase manufacturing technology is adopted to process the runner with the characteristics of small size, thin wall thickness, bent structure and the like, so that the rejection rate of runner parts can be reduced, and the size precision of the runner parts can be improved.
However, generally, only one runner part can be processed at one time by adopting an additive manufacturing technology, and the production efficiency is low. When a plurality of runner parts of disposable processing, a plurality of runner parts are interconnected together, need cut the separation to a plurality of runner parts that the processing was accomplished, and its cutting degree of difficulty is great, and the runner part is fragile, increases the rejection rate on foot.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a runner subassembly to when overcoming and adopting a plurality of runner parts of additive manufacturing technology one-time processing, need cut the separation to a plurality of runner parts that processing was accomplished, its cutting degree of difficulty is great, and the easy damage runner part increases the technical problem of rejection rate on foot.
In order to achieve the above object, the present invention provides a flow channel assembly. The runner assembly includes:
at least two flow path structures;
the reserved cutting structure is arranged between two adjacent runner structures;
and a pressure relief structure formed on the reserved cutting structure.
Compared with the prior art, the utility model provides an among the runner subassembly, be provided with between two adjacent runner structures and reserve the cutting structure to be formed with decompression structure on reserving the cutting structure. After a plurality of runner structures are processed at one time, when linear cutting is carried out at the reserved cutting structure, due to the existence of the pressure reducing structure, the cutting resistance in the process of cutting the reserved cutting structure can be reduced, the cutting difficulty is reduced, the runner structures which are separated from each other and have complete structures are easy to obtain.
Furthermore, the reserved cutting structure is provided with a neutral surface, and the pressure reducing structure is arranged on the neutral surface of the reserved cutting structure.
Furthermore, the reserved cutting structure is provided with a neutral surface, and the pressure reducing structure is at least one group of through holes formed in the reserved cutting structure; each group of through holes are distributed along the height direction of the reserved cutting structure; the axis of each group of through holes is parallel to the neutral plane of the reserved cutting structure; each group of through holes are distributed along the circumferential direction of the reserved cutting structure.
Furthermore, the reserved cutting structure is provided with an annular cutting reference groove, and at least one group of through holes are located in the annular cutting reference groove.
Further, the plane of the neutral plane of the reserved cutting structure penetrates through the group of through holes.
Further, the inner side walls of at least one group of through holes comprise a plane part and a curved surface part which enclose the through holes along the circumferential direction of the through holes; the neutral surface of the reserved cutting structure and the plane part included by the inner side wall of the at least one group of through holes are in the same plane.
Further, the axes of the through holes in the same group are intersected with the axis of the reserved cutting structure at one point.
Further, the at least one set of through holes includes a plurality of through holes that communicate with each other.
Furthermore, the pressure reducing structure also comprises at least one group of communicating grooves arranged in the reserved cutting structure; the at least one set of through holes comprises at least two through holes; two adjacent through holes in the same group of through holes are communicated through at least one group of communicating grooves; and/or the presence of a gas in the gas,
the pressure reducing structure also comprises at least one group of communicating holes arranged in the reserved cutting structure; the at least one set of through holes comprises at least two through holes; two adjacent through holes included in the same group of through holes are communicated through at least one group of communication holes.
Furthermore, the reserved cutting structure comprises at least one annular connecting part, each annular connecting part is located between two adjacent flow channel structures and is connected with the two adjacent flow channel structures, and at least one through hole is formed in each annular connecting part.
Drawings
Fig. 1 is a schematic structural view of a flow channel assembly provided in an embodiment of the present invention after cutting along a reserved cutting structure;
fig. 2 is a front view of a runner assembly provided by an embodiment of the present invention;
FIG. 3 is a cross-sectional view of the structure of FIG. 1 taken along line A-A;
FIG. 4 is an enlarged view of the structure of FIG. 3 at a selected box;
fig. 5 is an enlarged view of a structure of a ring-shaped cutting reference groove according to an embodiment of the present invention.
Wherein, 1 is a flow channel structure, 2 is a reserved cutting structure, 21 is an annular connecting part, 3 is a pressure reducing structure, 31 is a through hole, 311 is a plane part, 312 is a curved surface part, 32 is a communicating groove, 33 is a communicating hole, and 4 is an annular cutting reference groove.
Detailed Description
The following description of the embodiments according to the present invention is made with reference to the accompanying drawings. In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention, however, the present invention may be practiced in other ways than those specifically described herein, and the present invention is not limited to the specific embodiments disclosed below.
Additive manufacturing is a technique that uses various materials to print a component layer by layer based on a digital model file. It is often used in the fields of mold manufacturing, industrial design, and the like. Compared with a casting process, the material increase manufacturing technology is adopted to process the runner with the characteristics of small size, thin wall thickness, bent structure and the like, so that the rejection rate of runner parts can be reduced, and the size precision of the runner parts can be improved.
At present, the flow passage part can be processed at one time by adopting an additive manufacturing technology. However, the number of the runner parts to be processed at one time is only one, so that the three-dimensional model of the runner part needs to be introduced again before each processing, and operations such as slicing and layering are performed, so that the production efficiency of the runner part is low. In order to solve the problem of low production efficiency of the runner parts, a plurality of runner parts can be processed and formed at one time. Different from a runner part processed at one time, when a plurality of runner parts are processed at one time, a cutting reserved part with certain specification is formed between two adjacent runner parts, so that after the plurality of runner parts are formed, cutting needs to be carried out at the cutting reserved part, and the plurality of runner parts are separated.
However, the strength of the cutting reserved part formed between two adjacent runner parts is high, so that the cutting resistance is high, the cutting difficulty is high when the adjacent runner parts are cut and separated, and the runner parts are easy to damage.
The technical problems that when a plurality of runner parts are machined at one time by the aid of an additive manufacturing technology, the machined runner parts need to be cut and separated, cutting difficulty is high, the runner parts are prone to damage, and rejection rate is increased are solved.
As shown in fig. 1 and 2, an embodiment of the present invention provides a flow channel assembly. The runner assembly includes: at least two flow channel structures 1, a cutting structure 2 and a pressure reducing structure 3 are reserved. The reserved cutting structure 2 is arranged between two adjacent flow passage structures 1. The pressure relief structure 3 is formed on the preliminary cutting structure 2. It is to be understood that the pressure relief structure 3 may be formed inside the reserved cutting structure 2, or may be formed at the outer circumference of the reserved cutting structure 2.
The following describes an actual cutting process of the flow channel assembly provided by the embodiment of the present invention, taking the flow channel assembly including two flow channel structures 1 as an example. It should be understood that the flow channel assembly includes, from bottom to top, a first flow channel structure, a reserved cutting structure 2, a second flow channel structure, and a pressure relief structure 3 formed on the reserved cutting structure 2. The reserved cutting structures 2 are respectively connected with the first flow channel structure and the second flow channel structure.
In order to obtain the first flow channel structure and the second flow channel structure which are separated from each other and have high forming precision, under the action of the pressure reducing structure 3 formed by the reserved cutting structure 2, the cutting tool cuts the reserved cutting structure 2 under small resistance, so that the first flow channel structure and the second flow channel structure are completely separated.
According to the structure and the actual cutting process of the flow channel assembly provided by the embodiment, the reserved cutting structure 2 is arranged between the two adjacent flow channel structures 1, and the pressure reducing structure 3 formed on the reserved cutting structure 2 can reduce the structural strength of the reserved cutting structure 2. After a plurality of runner structures 1 are processed at one time, linear cutting can be carried out at the reserved cutting structure 2, the cutting resistance of a cutting tool can be reduced under the action of the pressure reducing structure 3, the cutting difficulty is reduced, and the runner structures 1 which are separated from each other and have complete structures are easy to obtain.
As a possible realization, the reserved cutting structure 2 has a neutral plane. The pressure reducing structure 3 is arranged on the neutral surface of the reserved cutting structure 2. It should be understood that the neutral plane of the reserved cutting structure 2 is a plane where the balance point is located, and when the cutting tool performs linear cutting on the neutral plane of the reserved cutting structure 2, the cutting force applied to the flow channel assembly is relatively balanced, so that the structural integrity of the flow channel structure 1 in the linear cutting process can be further ensured. When the decompression structure 3 is arranged on the neutral surface of the reserved cutting structure 2, the cutting tool cuts the neutral surface of the reserved cutting structure 2, so that the molding precision of the flow channel structure 1 can be further improved, the cutting resistance is reduced, and the flow channel structures 1 separated from each other are easily obtained.
As a possible realization, the pressure reducing structure 3 is a hollow structure provided on the reserved cutting structure 2. When the material increase manufacturing technology is adopted and the hollow part of the decompression structure 3 is manufactured, the hollow part is not required to be molded and manufactured, the waste of material powder is avoided, and the production cost is saved. Meanwhile, the whole weight of the flow channel assembly can be reduced, and the flow channel assembly is convenient to carry when the cutting and separating operation is carried out subsequently.
In an alternative way, as shown in fig. 3, when the pressure reducing structure 3 is a hollow structure, the hollow structure is at least one set of through holes 31 opened on the reserved cutting structure 2. The through hole 31 is a through hole in a broad sense, and the cross-sectional shape in the radial direction thereof may be a circle, a semicircle, a rectangle, an ellipse, or the like, which is not listed here.
The sets of through holes 31 are distributed along the height direction of the reserved cutting structure 2. The axis of each set of through holes 31 is parallel to the neutral plane of the reserved cutting structure 2. Each set of through holes 31 is distributed along the circumference of the reserved cutting structure 2. At this moment, cutting tool cuts in a plurality of planes department on reserving cutting structure 2, all can reduce the cutting resistance under decompression structure 3's effect, reduces the cutting degree of difficulty.
When the pressure reducing structure 3 is formed on the neutral surface of the reserved cutting structure 2, the plane of the neutral surface of the reserved cutting structure 2 penetrates through the group of through holes 31. At this time, when the reserved cutting structure 2 is cut, the through hole 31 does not need to be partially cut, and the cutting resistance is reduced. And, the granule slagging scorification that drops to cutting structure 2 is reserved can be discharged through-hole 31, can further reduce the cutting degree of difficulty.
In one example, as shown in fig. 2, when the cross section of the at least one set of through holes 31 in the radial direction is approximately semicircular, the inner side wall of the at least one set of through holes 31 includes a flat surface portion 311 and a curved surface portion 312 surrounding the through holes 31 in the circumferential direction of the through holes 31. The neutral plane of the reserved cutting structure 2 is in the same plane with the plane portion 311 included in the inner side wall of the at least one set of through holes 31. At this time, the cutting tool cuts along the plane where the plane portion 311 of the through hole 31 is located, the area of the reserved cutting structure 2 that needs to be cut by the cutting tool is minimized, and the cutting resistance can be further reduced.
Exemplarily, on the premise of saving material powder, in order to further ensure that the flow channel structure 1 is not damaged by the cutting and separating operation, the height of the reserved cutting structure 2 is set to be 3mm to 4 mm. The height of the reserved cutting structure 2 is the same as the height direction of the flow channel structure 1. And, the height of the at least one through hole 31 provided in the reserved cutting structure 2 is 2mm to 3mm, and the width of the plane portion 311 of the at least one through hole 31 is 2.5mm to 4 mm. The height direction of the at least one through hole 31 is the same as the height direction of the flow channel structure 1. The width direction of the at least one through hole 31 is perpendicular to the height direction of the flow channel structure 1.
In one example, as shown in fig. 1, the axes of the same set of through holes 31 intersect the axis of the reserved cutting structure 2 at a point. At this time, the axes of the set of through holes 31 are located in the same plane, and their intersection points intersect with the axis of the preliminary cutting structure 2, so that the flow channel assembly has high symmetry. Based on this, when utilizing the cutting stage property to reserve cutting structure 2 and cutting, can guarantee that the cutting force that the runner subassembly received is comparatively balanced, avoid runner structure 1 to damage.
When the neutral plane of the reserved cutting structure 2 is in the same plane as the plane portion 311 included in the inner side wall of at least one set of through holes 31, if the axis of the same set of through holes 31 intersects the axis of the reserved cutting structure 2 at a point. At this time, the cutting tool does not need to cut the hollow portion of the through hole in the neutral plane range, and cutting resistance can be reduced. And, the cutting tool cuts at the neutral plane of the reserved cutting structure 2, so that the stress of the runner assembly is balanced during the cutting operation.
Illustratively, as shown in fig. 1, the pressure relief structure 3 includes a set of through holes 31, and the set of through holes 31 includes 12 through holes 31, and axes of the 12 through holes 31 are located on the neutral plane of the reserved cutting structure 2 and intersect with the axis of the reserved cutting structure 2 at a point, that is, the 12 through holes 31 are uniformly distributed on the neutral plane of the reserved cutting structure 2 in a radial manner.
To further reduce the cutting resistance, the at least one set of through holes 31 comprises a plurality of through holes 31 communicating with each other. At this moment, the cutting tool cuts the reserved cutting structure 2 and the dropped particle slag can be discharged out of the reserved cutting structure 2 through the through holes 31 which are communicated with each other, so that the cutting difficulty can be further reduced.
In one example, the pressure relief structure 3 further comprises at least one set of communication grooves 32 opening in the reserved cutting structure 2. The at least one set of through holes 31 comprises at least two through holes 31; two adjacent through holes 31 included in the same group of through holes 31 communicate with each other through at least one communication groove 32. The communication groove 32 may be a U-shaped groove, a V-shaped groove, etc., which are not illustrated herein.
Illustratively, as shown in fig. 1, the pressure reducing structure 3 includes two sets of communication grooves 32, the two sets of communication grooves 32 are disposed at intervals in the reserved cutting structure 2, and each set of communication grooves 32 includes 12 communication grooves 32, and each communication groove 32 has an arc-shaped cross section in the axial direction. The communication grooves 32 in the same group and the communication grooves 32 in the two groups are communicated through the through holes 31.
As shown in fig. 1 and 4, when the communication grooves 32 are U-shaped grooves, the height of the communication grooves 32 in the extending direction of at least two flow channel structures 1 is 2mm to 3mm, the width of the communication grooves 32 in the direction perpendicular to the extending direction of at least two flow channel structures 1 is 2.5mm to 4mm, at least one set of the communication grooves 32 includes at least two communication grooves 32, and the distance between two adjacent communication grooves 32 is 4mm to 6 mm. Of course, the specification, number and arrangement of the communication grooves 32 can be set according to actual conditions.
In another example, the pressure relief structure 3 further comprises at least one set of communication holes 33 opening in the preliminary cutting structure 2. The at least one set of through holes 31 comprises at least two through holes 31; adjacent two through holes 31 included in the same group of through holes 31 communicate through at least one group of communication holes 33.
It is understood that the volume occupied by the pressure-reducing structure 3 within the reserved cutting structure 2 can be increased regardless of whether the pressure-reducing structure 3 includes the communication groove 32 or the communication hole 33. Based on this, the volume that cutting tool cut reserved cutting structure 2 is littleer, has further reduced the cutting degree of difficulty.
In a possible implementation manner, the pressure reducing structure 3 may be a corrugated pressure reducing structure, a broken line annular pressure reducing structure, or the like, and may be provided according to actual situations.
As a possible implementation manner, as shown in fig. 1 to 4, in order to further improve the cutting accuracy and avoid damage to the flow channel structure 1, an annular cutting reference groove 4 is formed at the reserved cutting structure 2, and at least one group of through holes 31 is located in the annular cutting reference groove 4. It should be understood that, the annular cutting reference groove 4 with the sunken characteristic exists in the circumference of reserving cutting structure 2, and at this moment, aim at annular cutting reference groove 4 with cutting tool's cutting direction, can more accurately fix a position that needs the cutting to reserve cutting structure 2 is cut in the scope that annular cutting reference groove 4 was injectd, can guarantee that the cutting direction can not deviate, ensures runner structure 1 shaping precision, improves runner structure 1's finished product qualification rate. Meanwhile, at least one group of through holes 31 are located in the annular cutting reference groove 4, so that cutting resistance can be reduced on the premise that the cutting direction is not deviated.
As for the structure of the annular cutting reference groove 4, a U-shaped groove, a V-shaped groove, etc. can be mentioned, which are not listed here.
As shown in fig. 5, when the annular cutting reference groove 4 is a U-shaped groove, the distance C from the groove bottom of the annular cutting reference groove 4 to the notch of the annular cutting reference groove 4 is 0.1mm to 0.2 mm. The minimum distance L from the side surface of the annular cutting reference groove 4 to the surface of the flow channel structure 1 is 0.1mm to 0.2 mm. Of course, the specification of the annular cutting reference groove 4 may be set according to actual conditions.
As another possible implementation manner, in order to further reduce the cutting resistance and reduce the cutting difficulty; the reserved cutting structure 2 comprises at least one annular connection 21. Each annular connecting portion 21 is located between and connected to two adjacent flow passage structures 1. Each annular connecting portion 21 is provided with at least one through hole 31, and the structure of the through hole 31 can be referred to above.
When at least one of the annular connecting portions 21 includes a plurality of annular connecting portions 21 fitted together, the adjacent two annular connecting portions 21 have a space therebetween to form the aforementioned communication groove 32. At least one through hole 31 opened in the plurality of annular connection portions 21 communicates with each other at the interval.
The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention, and various modifications and changes may be made by those skilled in the art. 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 (9)
1. A flow channel assembly, comprising:
at least two flow path structures;
the reserved cutting structure is arranged between two adjacent runner structures;
and a pressure relief structure formed on the pre-cut structure; the reserved cutting structure is provided with a neutral surface, and the pressure reducing structure is arranged on the neutral surface of the reserved cutting structure.
2. The flow channel assembly of claim 1, wherein the pre-cut structure has a neutral surface, and the pressure relief structure is at least one set of through holes provided on the pre-cut structure; each group of through holes are distributed along the height direction of the reserved cutting structure; the axis of each group of through holes is parallel to the neutral plane of the reserved cutting structure; each group of through holes are distributed along the circumferential direction of the reserved cutting structure.
3. The flow channel assembly of claim 2, wherein the pre-cut structure defines an annular cutting reference groove, and the at least one set of through holes are located in the annular cutting reference groove.
4. The flow channel assembly of claim 2, wherein the plane of the neutral plane of the precut structure extends through a set of through holes.
5. The flow channel assembly according to claim 2, wherein the inner side wall of the at least one set of through holes comprises a flat surface portion and a curved surface portion surrounding the through holes in a circumferential direction of the through holes; the neutral surface of the reserved cutting structure and the plane part included by the inner side wall of the at least one group of through holes are in the same plane.
6. The flow channel assembly of claim 2, wherein the axes of the through holes of the same set intersect the axis of the precut structure at a point.
7. The flow channel assembly of claim 2, wherein the at least one set of through holes comprises a plurality of interconnected through holes.
8. The flow channel assembly of claim 2, wherein the pressure relief structure further comprises at least one set of communication channels opening into the precut structure; the at least one set of vias includes at least two vias; two adjacent through holes in the same group of through holes are communicated through the at least one group of communication grooves; and/or the presence of a gas in the gas,
the pressure reducing structure also comprises at least one group of communicating holes arranged in the reserved cutting structure; the at least one set of vias includes at least two vias; two adjacent through holes included in the same group of through holes are communicated through the at least one group of communication holes.
9. The flow channel assembly as claimed in any one of claims 1 to 8, wherein the preformed cutting structure comprises at least one annular connecting portion, each annular connecting portion is located between and connected to two adjacent flow channel structures, and each annular connecting portion has at least one through hole.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201922470082.7U CN212472408U (en) | 2019-12-31 | 2019-12-31 | Flow channel assembly |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201922470082.7U CN212472408U (en) | 2019-12-31 | 2019-12-31 | Flow channel assembly |
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Publication Number | Publication Date |
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CN212472408U true CN212472408U (en) | 2021-02-05 |
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CN201922470082.7U Active CN212472408U (en) | 2019-12-31 | 2019-12-31 | Flow channel assembly |
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CN (1) | CN212472408U (en) |
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2019
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Address after: Room 201, 2nd Floor, No. 5999 Wuxing Avenue, Zhili Town, Wuxing District, Huzhou City, Zhejiang Province, 313008 (self declared) Patentee after: Xinjinghe Laser Technology Co.,Ltd. Country or region after: China Address before: 102206 513-4, unit 1, 5 / F, building 1, yard 1, Neng Dong Road, Shahe Town, Changping District, Beijing Patentee before: XINJINGHE LASER TECHNOLOGY DEVELOPMENT (BEIJING) Co.,Ltd. Country or region before: China |
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