CN205085348U - A device for preparing turbine blade integral cast system - Google Patents
A device for preparing turbine blade integral cast system Download PDFInfo
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- CN205085348U CN205085348U CN201520890564.7U CN201520890564U CN205085348U CN 205085348 U CN205085348 U CN 205085348U CN 201520890564 U CN201520890564 U CN 201520890564U CN 205085348 U CN205085348 U CN 205085348U
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Abstract
The utility model relates to a device for preparing turbine blade integral cast system, include: the cope match -plate pattern has been seted up on the terminal surface of cope match -plate pattern and has been annotated the wax mouth, and the cope match -plate pattern lower extreme has set gradually first module, the second module, third module and fourth module, the inside cup runner of having seted up of first module, annotate wax mouth and cup runner intercommunication, the second module and fourth module are inside has offered cylindrical cavity, and circumference is provided with the cross gate on the cylindrical cavity, the cup neck department intercommunication of the inside cylindrical cavity one end of the second module and cup runner, the other end and the inside owner who sets up of third module water the one end intercommunication, main water the other end with the inside cylindrical cavity intercommunication of fourth module. Having reduced the quantity of the gating system preparation frock, having saved the tooling manufacture expense, improved production efficiency, the whole the gating system that suppresses out simultaneously owing to having saved manual concatenation link, has reduced defects such as welding seam, scald, has improved module quality and metal casting quality.
Description
Technical field:
The utility model relates to blade running gate system preparing technical field, is specifically related to a kind of device for the preparation of the integrated poured system of turbo blade.
Background technology:
In model casting field, the running gate system of wax part is made up of cell cubes such as cup, main running channel, cross gate, ingates, and these running gate system cell cubes need by respective frock, obtains after carrying out casting operation.The process using running gate system frock in the past to prepare running gate system is: patternmaker suppresses the fusible pattern → combination workmans such as cup, main running channel, cross gate and carries out weldering and cut process on wax injector by the frock of different units body, makes the dimensions of these cell cube fusible patterns and shape meet technological requirement → again these satisfactory cell cube fusible pattern weldering cuttves are spliced into complete running gate system framework.Whole running gate system preparation process is completely by workman's manual operations, difficulty is very large, and the compression tooling used is many, operation is loaded down with trivial details, the running gate system scale error of manual splicing is large, uniformity is poor, easily bring the defect such as weld seam, scald, the quality of running gate system is difficult to be guaranteed, and is unfavorable for long-term, batch production.
Utility model content:
The purpose of this utility model is to provide a kind of a kind of device for the preparation of the integrated poured system of turbo blade for improving turbo blade running gate system preparation quality and production efficiency.
For achieving the above object, the utility model is by the following technical solutions:
A kind of device for the preparation of the integrated poured system of turbo blade that the utility model provides, comprise: cope match-plate pattern, the end face of cope match-plate pattern offers casting mouth, cope match-plate pattern lower end is disposed with the first module, second module, 3rd module and four module, described first inside modules offers cup-shaped cast gate, described casting mouth is communicated with cup-shaped cast gate, described second module and four module inside offer cylindrical cavity, on cylindrical cavity, circumference is provided with cross gate, cylindrical cavity one end of described second inside modules is communicated with the cup neck place of cup-shaped cast gate, main running channel one end that the other end and the 3rd inside modules are offered is communicated with, the main running channel other end is communicated with the cylindrical cavity of described four module inside.
On the cylindrical cavity of described second module and four module, circumference is provided with 8 cross gates respectively, and cross gate is evenly distributed on the periphery of cylindrical cavity, angle at 45 ° between two adjacent cross gates.
Described cope match-plate pattern sidewall is provided with upper lug, and the 3rd module lower sides and four module sidewall correspondence are provided with lower lug, is inserted with bolt, locks between described upper lug and lower lug.
Described cope match-plate pattern and the first module, the first module and the second module, the second module and the 3rd module and the 3rd all affixed by pin between module and four module.
Described first module, the second module and the 3rd module fasten composition by two pieces of modules, and two pieces of modules are symmetrical structure.
A kind of device for the preparation of the integrated poured system of turbo blade of the utility model is achieved in that four module as base, fixedly mount the 3rd module successively above, second module and the first module, cope match-plate pattern is arranged on above the first module, high temperature wax liquid is injected along the casting mouth on cope match-plate pattern, wax liquid fills the cross gate that cylindrical cavity in four module and the second module and circumference thereof are arranged, main running channel in 3rd module and the cup-shaped cast gate in the first module, after wax liquid cooling forming, lay down modules, the forming blocks of taking out is the running gate system that need prepare.
The beneficial effect of a kind of device for the preparation of the integrated poured system of turbo blade of the utility model: decrease the quantity that running gate system prepares frock, save frock manufacturing expense, improve production efficiency, the integrated poured system simultaneously suppressed, link is spliced by hand owing to eliminating, decrease the defect such as weld seam, scald, improve module quality and metal casting quality, be applied to the running gate system preparation field of model casting turbo blade, improve turbo blade running gate system quality, save frock manufacturing expense, improve production efficiency simultaneously.Can in the blade class foundry goods model casting field promotion and application of other type.
Accompanying drawing illustrates:
Fig. 1 is the structural representation of a kind of device for the preparation of the integrated poured system of turbo blade of the utility model;
Fig. 2 is the cross-sectional view of a kind of device for the preparation of the integrated poured system of turbo blade of the utility model;
Fig. 3 is the sectional view of a kind of device for the preparation of the integrated poured system of turbo blade of the utility model;
Fig. 4 is the structural representation of the integrated poured system of turbo blade that need prepare;
Fig. 5 is a kind of top view of cope match-plate pattern of the device for the preparation of the integrated poured system of turbo blade;
Fig. 6 is a kind of top view of the first module of the device for the preparation of the integrated poured system of turbo blade;
Fig. 7 is a kind of top view of the second module of the device for the preparation of the integrated poured system of turbo blade;
Fig. 8 is a kind of top view of the 3rd module of the device for the preparation of the integrated poured system of turbo blade;
Fig. 9 is a kind of top view of four module of the device for the preparation of the integrated poured system of turbo blade;
1-cope match-plate pattern, 2-casting mouth, 3-first module, 4-second module, 5-the 3rd module, 6-four module, 7-cup-shaped cast gate, 8-cylindrical cavity, 9-cross gate, the main running channel of 10-, 11-upper lug, lug under 12-, 13-pin, 14-bolt.
Detailed description of the invention:
Below in conjunction with embodiment, the utility model is described in further detail.
According to Fig. 1 ~ Fig. 3, a kind of device for the preparation of the integrated poured system of turbo blade, comprise: cope match-plate pattern 1, the end face of cope match-plate pattern 1 offers casting mouth 2, cope match-plate pattern 1 lower end is disposed with the first module 3, second module 4, 3rd module 5 and four module 6, described first module 3 inside offers cup-shaped cast gate 7, described casting mouth 2 is communicated with cup-shaped cast gate 7, described second module 4 and four module 6 inside offer cylindrical cavity 8, on cylindrical cavity 8, circumference is provided with cross gate 9, described cylindrical cavity 8 one end of second module 4 inside is communicated with the cup neck place of cup-shaped cast gate 7, main running channel 10 one end that the other end is offered with the 3rd module 5 inside is communicated with, main running channel 10 other end is communicated with the cylindrical cavity 8 of described four module 6 inside.
As shown in figures 7 and 9, on the cylindrical cavity 8 of described second module 4 and four module 6, circumference is provided with 8 cross gates 9 respectively, and cross gate 9 is evenly distributed on the periphery of cylindrical cavity 8, angle at 45 ° between two adjacent cross gates 9.
As shown in Fig. 5, Fig. 8 and Fig. 9, described cope match-plate pattern 1 sidewall is provided with upper lug 11, and the 3rd module 5 lower sides and four module 6 sidewall correspondence are provided with lower lug 12, be inserted with bolt 14, lock between described upper lug 11 and lower lug 12.
As shown in Fig. 5 ~ Fig. 9, described cope match-plate pattern 1 and the first module 3, first module 3 and the second module 4, second module 4 and the 3rd module 5 and all affixed by pin 13 between the 3rd module 5 and four module 6.
As shown in Fig. 7 ~ Fig. 9, described first module 3, second module 4 and the 3rd module 5 fasten composition by the module of the two pieces of symmetrical structures in left and right, after prepared by running gate system, respectively the first module 3, second module 4 and the 3rd module 5 can be split in the horizontal direction, be convenient to the disengaging of running gate system fusible pattern.
A kind of device for the preparation of the integrated poured system of turbo blade of the utility model is achieved in that four module 6 as base, fixedly mount the 3rd module 5 successively above, second module 4 and the first module 3, cope match-plate pattern 1 is arranged on above the first module 3, high temperature wax liquid is injected along the casting mouth 2 on cope match-plate pattern 1, wax liquid fills the cross gate 9 that cylindrical cavity 8 in four module 6 and the second module 4 and circumference thereof are arranged, main running channel 10 in 3rd module 5 and the cup-shaped cast gate 7 in the first module 3, after wax liquid cooling forming, lay down modules, as shown in Figure 4, the forming blocks of taking out is the running gate system that need prepare, the wax part of blade shape is bonded in the corresponding position of running gate system, complete docking of running gate system and wax part.
Finally should be noted that: above embodiment is only in order to illustrate that the technical solution of the utility model is not intended to limit, although be described in detail the utility model with reference to above-described embodiment, those of ordinary skill in the field are to be understood that: still can modify to detailed description of the invention of the present utility model or equivalent replacement, and not departing from any amendment of the utility model spirit and scope or equivalent replacement, it all should be encompassed in the middle of this right.
Claims (5)
1. the device for the preparation of the integrated poured system of turbo blade, it is characterized in that: comprising: cope match-plate pattern, the end face of cope match-plate pattern offers casting mouth, cope match-plate pattern lower end is disposed with the first module, second module, 3rd module and four module, described first inside modules offers cup-shaped cast gate, described casting mouth is communicated with cup-shaped cast gate, described second module and four module inside offer cylindrical cavity, on cylindrical cavity, circumference is provided with cross gate, cylindrical cavity one end of described second inside modules is communicated with the cup neck place of cup-shaped cast gate, main running channel one end that the other end and the 3rd inside modules are offered is communicated with, the main running channel other end is communicated with the cylindrical cavity of described four module inside.
2. a kind of device for the preparation of the integrated poured system of turbo blade according to claim 1, it is characterized in that: on the cylindrical cavity of described second module and four module, circumference is provided with 8 cross gates respectively, cross gate is evenly distributed on the periphery of cylindrical cavity, angle at 45 ° between two adjacent cross gates.
3. a kind of device for the preparation of the integrated poured system of turbo blade according to claim 1, it is characterized in that: described cope match-plate pattern sidewall is provided with upper lug, 3rd module lower sides and four module sidewall correspondence are provided with lower lug, be inserted with bolt between described upper lug and lower lug, lock.
4. a kind of device for the preparation of the integrated poured system of turbo blade according to claim 1, is characterized in that: described cope match-plate pattern and the first module, the first module and the second module, the second module and the 3rd module and the 3rd all affixed by pin between module and four module.
5. a kind of device for the preparation of the integrated poured system of turbo blade according to claim 1, is characterized in that: described first module, the second module and the 3rd module fasten composition by the module of two pieces of symmetrical structures.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520890564.7U CN205085348U (en) | 2015-11-10 | 2015-11-10 | A device for preparing turbine blade integral cast system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520890564.7U CN205085348U (en) | 2015-11-10 | 2015-11-10 | A device for preparing turbine blade integral cast system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205085348U true CN205085348U (en) | 2016-03-16 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520890564.7U Active CN205085348U (en) | 2015-11-10 | 2015-11-10 | A device for preparing turbine blade integral cast system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205085348U (en) |
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2015
- 2015-11-10 CN CN201520890564.7U patent/CN205085348U/en active Active
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| GR01 | Patent grant | ||
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Address after: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6 Patentee after: Chinese Hangfa Shenyang Liming Aero engine limited liability company Address before: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6 Patentee before: Liming Aeroplane Engine (Group) Co., Ltd., Shenyang City |