CN103084545B - Pouring technology of aluminum inlet manifold - Google Patents
Pouring technology of aluminum inlet manifold Download PDFInfo
- Publication number
- CN103084545B CN103084545B CN201310029764.9A CN201310029764A CN103084545B CN 103084545 B CN103084545 B CN 103084545B CN 201310029764 A CN201310029764 A CN 201310029764A CN 103084545 B CN103084545 B CN 103084545B
- Authority
- CN
- China
- Prior art keywords
- pouring
- gate
- inlet manifold
- air inlet
- aluminum alloy
- Prior art date
- 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.)
- Active
Links
Landscapes
- Molds, Cores, And Manufacturing Methods Thereof (AREA)
Abstract
The invention discloses a pouring technology of an aluminum inlet manifold, which is carried out by means of low pressure pouring. The pouring technology comprises the following technical measures of: (1) setting a pouring position of a casting, (2) setting a pouring system, and (3) carrying out a pouring operation. Compared with the prior art, the pouring technology has the advantages that as a sprue is directly communicated with pressurizer tanks, one sprue can be communicated with two pressurizer tanks for the adoption of the low pressure pouring mode, two aluminum inlet manifolds can be poured simultaneously, namely, two pieces can be obtained by once pouring, and production efficiency is extremely high; simultaneously, a specially shaped pouring gate does not needed to be arranged and preparation is very convenient so that a preparation period is very short and preparation cost is pretty low, and the pouring gate is very short so that mold-filling capacity is pretty good, pouring deficiency is not easy to happen, and rate of finished products is very high; and an original flash groove is canceled and the pouring gate is pretty short so that process yield is further improved.
Description
Technical field
The present invention relates to a kind of pouring technology of aluminum alloy air inlet manifold.
Background technology
At present, the pouring technology of the aluminum alloy air inlet manifold of prior art is all that what to adopt is gravity-assist pouring, is not horizontal gravity cast, the structure that to be exactly tilting type gravity-assist pouring or tilting type gravity-assist pouring pour into a mould with ladder; But the former pouring gate structure is more complicated, and sprue and rising head are all arranged on the position of aluminum alloy air inlet manifold away from pressurizer tank, be that dead head is all arranged on the flange face of aluminum alloy air inlet manifold, mold-filling capacity is poor, is prone to the defects such as cold shut and underpriming; Although and the latter can solve the problems such as the poor and cold shut of mold-filling capacity to a certain extent, also need to arrange snakelike main running channel and teeming road, mould preparation bothers, and manufacturing cycle is longer, and cost is also higher; And said method can only be all one, a type, and a secondary mould can only be poured into a mould a product, and production efficiency is lower, and dead head is relatively large, cause product yield (casting technique yield rate=foundry goods is heavy/mould heavy * 100%.Mould weight, is exactly the gross mass of running gate system+foundry goods, also just waters the required weight of molten iron of a mould.) lower.
Summary of the invention
The present invention is directed to the pouring technology that above problem provides a kind of mold-filling capacity better, not to be prone to that pouring defect, production efficiency are higher, mould preparation is simple, manufacturing cycle is shorter, cost is lower and can improve the aluminum alloy air inlet manifold of product yield.
The present invention overcomes the above problems technical scheme used: a kind of pouring technology with the aluminum alloy air inlet manifold of following steps is provided, adopts low-pressure casting mode to carry out, comprise following technical measures:
1), casting pouring position is set: aluminum alloy air inlet manifold chamber is adopted to horizontally set, and two aluminum alloy air inlet manifold chambeies are set, make the pressurizer tank in two aluminum alloy air inlet manifold chambeies all be positioned at the position of nearly down gate, flange face position, aluminum alloy air inlet manifold chamber (1) is all positioned on the position away from down gate;
2), running gate system is set: described running gate system comprises down gate and ingate, and its technical characterictic is: down gate is positioned at the bottom of whole running gate system, and down gate is communicated with two pressurizer tanks respectively by ingate;
3), pouring operation: be directly placed on low-pressure casting machine upper.
Adopt after above technique, compared with prior art, the present invention is because down gate is directly communicated with pressurizer tank, and by the mode of low-pressure casting, a down gate can be communicated with two pressurizer tanks, can to two aluminum alloy air inlet manifold chambeies, pour into a mould simultaneously, realize two, a type, production efficiency is higher; Simultaneously do not need special-shaped running channel is set, prepare more conveniently, make manufacturing cycle shorter, preparation cost is lower, and the shorter mold-filling capacity of running channel is better, is not also prone to pouring defect, and yield rate is higher; Moreover cancelled original rising head, and running channel is also shorter, and then improved product yield.Therefore the present invention has the advantages that mold-filling capacity better, is not prone to pouring defect, production efficiency is higher, mould preparation is simple, manufacturing cycle is shorter, cost is lower and can improve product yield.
As improvement, between described down gate and ingate, be provided with cross gate, described cross gate one end is communicated with down gate, the cross gate other end is communicated with ingate, for the relatively complicated aluminum alloy air inlet manifold chamber of some structures, arrange after cross gate, between cross gate and pressurizer tank, the quantity of ingate can be set according to the aluminum alloy air inlet manifold chamber of differing complexity, and then the speed of increase cast, prevent when the relatively complicated aluminum alloy air inlet manifold chamber of structure is poured into a mould, poring rate is compared with causing because of the cooling too fast pouring defect causing in part position slowly, ingate also has the effect of feeding simultaneously, further improve the yield rate of cast.
Accompanying drawing explanation
Fig. 1 is the structural representation of pouring gate structure of the pouring technology embodiment mono-of aluminum alloy air inlet manifold of the present invention.
Fig. 2 is the structural representation of pouring gate structure of the pouring technology embodiment bis-of aluminum alloy air inlet manifold of the present invention.
As shown in the figure: 1, aluminum alloy air inlet manifold chamber, 2, pressurizer tank, 3, down gate, 4, cross gate, 5, ingate.
The specific embodiment
Below in conjunction with the drawings and specific embodiments, the present invention is described further.
Embodiment mono-
As shown in Figure 1, a kind of pouring technology of aluminum alloy air inlet manifold, adopts low-pressure casting mode to carry out, and comprises following technical measures:
1), casting pouring position is set: aluminum alloy air inlet manifold chamber 1 is adopted to horizontally set, and two aluminum alloy air inlet manifold chambeies 1 are set, make the pressurizer tank 2 in two aluminum alloy air inlet manifold chambeies 1 all be positioned at the position of nearly down gate 3,1 flange face position, aluminum alloy air inlet manifold chamber is all positioned on the position away from down gate 3; Also can be regarded as two aluminum alloy air inlet manifold chambeies 1 symmetrical along the axis of down gate 3;
2, running gate system is set: described running gate system comprises down gate 3 and ingate 5, its technical characterictic is: down gate 3 is positioned at the bottom of whole running gate system, down gate 3 is communicated with two pressurizer tanks 2 respectively by ingate 5 that (quantity of ingate 5 is determined according to the size in aluminum alloy air inlet manifold chamber 1 and complexity, this example is two, respectively corresponding pressurizer tank 2 separately);
3, pouring operation: be directly placed on low-pressure casting machine upper.Low-pressure casting operating procedure is identical with the technological operation step of other alloy product of prior art.
Embodiment bis-
As shown in Figure 2, a kind of pouring technology of aluminum alloy air inlet manifold, adopts low-pressure casting mode to carry out, and comprises following technical measures:
1, casting pouring position is set: aluminum alloy air inlet manifold chamber 1 is adopted to horizontally set, and two aluminum alloy air inlet manifold chambeies 1 are set, make the pressurizer tank 2 in two aluminum alloy air inlet manifold chambeies 1 all be positioned at the position of nearly down gate 3,1 flange face position, aluminum alloy air inlet manifold chamber is all positioned on the position away from down gate 3;
2, running gate system is set: described running gate system comprises down gate 3 and ingate 5, and its technical characterictic is: down gate 3 is positioned at the bottom of whole running gate system, down gate 3 is communicated with two pressurizer tanks 2 respectively by ingate 5;
3, pouring operation: be directly placed on low-pressure casting machine upper.
Between described down gate 3 and pressurizer tank 2, be provided with cross gate 4, described cross gate 4 one end are communicated with down gate 3, cross gate 4 other ends are communicated with pressurizer tank 2, (quantity of ingate 5 is determined according to the size in aluminum alloy air inlet manifold chamber 1 and complexity between general cross gate 4 and pressurizer tank 2, more ingate 5 can be set, this example is eight, be divided into tetrad, every group of corresponding pressurizer tank 2 separately of difference).
Above embodiment is only preferred embodiment of the present invention, and the present invention is not limited only to above embodiment and has also allowed other structural change, allly in rights to independence claimed range of the present invention, changes, and all belongs to protection domain of the present invention.
Claims (2)
1. a pouring technology for aluminum alloy air inlet manifold, adopts low-pressure casting mode to carry out, and comprises following technical measures:
1), casting pouring position is set: aluminum alloy air inlet manifold chamber (1) is adopted to horizontally set, and two aluminum alloy air inlet manifold chambeies (1) are set, make the pressurizer tank (2) in two aluminum alloy air inlet manifold chambeies (1) all be positioned at the position of nearly down gate (3), flange face position, aluminum alloy air inlet manifold chamber (1) is all positioned on the position away from down gate (3);
2), running gate system is set: described running gate system comprises down gate (3) and ingate (5), its technical characterictic is: down gate (3) is positioned at the bottom of whole running gate system, and down gate (3) is communicated with two pressurizer tanks (2) respectively by ingate (5);
3), pouring operation: be directly placed on low-pressure casting machine upper.
2. the pouring technology of aluminum alloy air inlet manifold according to claim 1, it is characterized in that: between described down gate (3) and ingate (5), be provided with cross gate (4), described cross gate (4) one end is communicated with down gate (3), and cross gate (4) other end is communicated with ingate (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310029764.9A CN103084545B (en) | 2013-01-24 | 2013-01-24 | Pouring technology of aluminum inlet manifold |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310029764.9A CN103084545B (en) | 2013-01-24 | 2013-01-24 | Pouring technology of aluminum inlet manifold |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103084545A CN103084545A (en) | 2013-05-08 |
| CN103084545B true CN103084545B (en) | 2014-12-17 |
Family
ID=48197959
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310029764.9A Active CN103084545B (en) | 2013-01-24 | 2013-01-24 | Pouring technology of aluminum inlet manifold |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103084545B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10086429B2 (en) | 2014-10-24 | 2018-10-02 | GM Global Technology Operations LLC | Chilled-zone microstructures for cast parts made with lightweight metal alloys |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3880222A (en) * | 1972-10-09 | 1975-04-29 | Renault | Low-pressure casting devices |
| US4930461A (en) * | 1989-08-04 | 1990-06-05 | Outboard Marine Corporation | One-piece lost foam pattern for an intake manifold |
| JPH08132221A (en) * | 1994-11-10 | 1996-05-28 | Asahi Tec Corp | Method for removing core |
| JP5026806B2 (en) * | 2007-01-25 | 2012-09-19 | ヤマハ発動機株式会社 | Die casting mold |
| CN101590519B (en) * | 2009-06-26 | 2010-09-08 | 宁波强盛机械模具有限公司 | Process for casting aluminum alloy air intake manifold |
| US20110169186A1 (en) * | 2010-01-11 | 2011-07-14 | Brenda Bruman | Method for Producing Three Separate and Distinct Intake Manifolds from a Single Intake Manifold Casting For Three Different Multi-Cylinder Internal Combustion Engine Applications |
| CN202291355U (en) * | 2011-11-15 | 2012-07-04 | 上海镁镁合金压铸有限公司 | Sprue device for magnesium alloy front-end bracket die casting |
-
2013
- 2013-01-24 CN CN201310029764.9A patent/CN103084545B/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| CN103084545A (en) | 2013-05-08 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN202894216U (en) | Casting tooling for large-size and complicated framework type titanium alloy thin wall castings | |
| CN201841251U (en) | Four cylinder engine die-casting gate, gate runner structure | |
| CN102784902A (en) | Metal mold pressure regulating casting device | |
| CN202639226U (en) | Gating system of automobile brake support on vertical parting and modeling line | |
| CN203448631U (en) | Casting sand box capable of obliquely casting | |
| CN204353427U (en) | A kind of automotive brake disc-casting mould | |
| CN105033191A (en) | Belt pulley casting simulation analysis and optimization design method | |
| CN202461484U (en) | Automobile air conditioning compressor cylinder body die-casting die | |
| CN201921988U (en) | Diesel engine body casting mold | |
| CN204171286U (en) | With the running gate system of multistage separable type cross gate | |
| CN103084545B (en) | Pouring technology of aluminum inlet manifold | |
| CN204366023U (en) | A kind of foundry pouring vessles | |
| CN104338909A (en) | Wheel hub casting molding process | |
| CN204209090U (en) | Novel metal die casting | |
| CN207119752U (en) | For the system of risers of 358 sprocket wheels | |
| CN102941316B (en) | Production method for machine tool guide rail casts | |
| CN203437595U (en) | Gating system | |
| CN203541439U (en) | Runner system for investment casting process | |
| CN103600035A (en) | Manufacturing technology of walking machinery bracket casting | |
| CN203140745U (en) | Runner structure for aluminum allow intake manifold | |
| CN102527941A (en) | Pouring process of aluminum alloy air intake manifold | |
| CN202318532U (en) | Mold for casting molding of quartz crucible | |
| CN203917814U (en) | A kind of dead head structure of aluminium alloy water inlet pipe | |
| CN103506606A (en) | Technology for casting complex metallic aluminum thin-wall castings | |
| CN103464691A (en) | Casting method of driving-wheel fluted-disc blank |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |