CN103192027A - Partial cooling method of cold iron in investment casting - Google Patents

Partial cooling method of cold iron in investment casting Download PDF

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Publication number
CN103192027A
CN103192027A CN2013101054625A CN201310105462A CN103192027A CN 103192027 A CN103192027 A CN 103192027A CN 2013101054625 A CN2013101054625 A CN 2013101054625A CN 201310105462 A CN201310105462 A CN 201310105462A CN 103192027 A CN103192027 A CN 103192027A
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China
Prior art keywords
chill
wax
shell
casting
model
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Pending
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CN2013101054625A
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Chinese (zh)
Inventor
吕志刚
申辰
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Tsinghua University
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Tsinghua University
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Priority to CN2013101054625A priority Critical patent/CN103192027A/en
Publication of CN103192027A publication Critical patent/CN103192027A/en
Pending legal-status Critical Current

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Abstract

The invention provides a partial cooling technology of cold iron in investment casting. The partial cooling technology comprises the following steps of: 1, manufacturing a wax model by a general investment casting process; 2, designing the cold iron and a wax block which has the same shape and dimension as the cold iron, according to the shape of the outer surface of a hot spot of a casting, and then manufacturing the cold iron and the wax block, wherein the inner surfaces of the designed cold iron and the wax block are clung to the outer surface of the hot spot of the casting in shape, and the cold iron and the wax block are provided with positioning platforms; 3, fixing the wax block to a part requiring partial chilling on the wax model, and tightly clinging to the surface of the wax model; 4 manufacturing a housing at the surface of the wax model, and exposing part of the positioning platform of the wax block from a model housing; 5, dewaxing the model housing; 6, roasting the model housing at high temperature; 7, fixing the cold ion in an opening of the model housing, and positioning through the positioning platform; and 8, casting after preheating the model housing, wherein the partial chilling effect is realized in the cold iron. By carrying out the steps mentioned above, the heat exchange at the hot spot of the casting can be improved, the chilling effect can be realized, and as a result, the purpose of reducing the defect of dispersed shrinkage of a shrinkage cavity in the casting can be realized.

Description

The local cooling means of a kind of model casting chill
Technical field
The present invention relates to the model casting technical field, be specifically related to the local cooling means of a kind of model casting chill.
Background technology
In casting field, for the intricate casting that has thermal center, be easy to generate quality problems such as shrinkage cavity, shrinkage porosite at the thermal center place.In sand casting, thereby the cooldown rate that can increase the foundry goods part by the mode of placing chill in sand mold reaches control cooling effect in proper order.The application of chill is very ripe in the sand casting, but for model casting, places chill and have certain difficulty, also is not widely used in the actual production.At present, some relevant researchs have appearred in the chill technology of model casting, such as: in shell, preset the effect that the internal densener identical with casting material reaches local Quench.The weak point of this scheme is: chill finally becomes the part of foundry goods, can bring into foundry goods such as impurity, oxide skin; Chill can not reuse in addition.
Summary of the invention
In order to solve above-mentioned the deficiencies in the prior art, the object of the present invention is to provide the local cooling means of a kind of model casting chill, can process the chill that can reuse according to the shape at foundry goods thermal center place, utilize the characteristics of chill good heat conduction effect, reach the effect of the local Quench of foundry goods.
For achieving the above object, the technical solution adopted in the present invention is:
The local cooling means of a kind of model casting chill comprises the steps:
Step 1: at first make wax-pattern according to normal full form casting process;
Step 2: according to the external surface shape at foundry goods thermal center place design chill and with chill shape, measure-alike wax stone, the external surface shape at the chill of design and the inner surface of wax stone and foundry goods thermal center place is fitted, and make chill and wax stone have positioning table, make chill and wax stone then;
Step 3: wax stone is fixed in the position that needs local Quench on the wax-pattern, and fits with the wax-pattern surface is tight;
Step 4: at wax-pattern surface shell processed, the positioning table part on the wax stone is exposed to outside the shell;
Step 5: with the shell dewaxing, wax-pattern and wax stone are removed, form local opening at shell;
Step 6: shell is carried out high-temperature roasting;
Step 7: chill is fixed in the shell opening part, locatees by positioning table;
Step 8: pour into a mould after the shell preheating, the part that chill is exposed to outside the shell is forced cooling.
Step 7 is described to be fixed in the shell opening part with chill, the slit between chill and the shell need be sealed.
The described mode that adopts brushing paint that is sealed into makes the slit between chill and the shell obtain sealing.
The described forced cooling method of step 8 is for blowing or water-cooled.
The local cooling means of model casting chill of the present invention utilizes the chill at foundry goods thermal center place to strengthen local heat exchange, thereby reaches local chill effect; The advantage of this method is: 1, can be according to the shape and size flexible design chill at foundry goods thermal center place, and chill can reuse; 2, with together roasting of shell, the oxide of having avoided producing in the roasting process does not enter foundry goods to chill; 3, can use forced cooling methods such as air blowing or water-cooled to chill, further strengthen local chill effect.
Description of drawings
Fig. 1 is the schematic diagram of chill among the present invention.
Fig. 2 is the schematic diagram that wax stone is fixed in the wax-pattern surface.
Fig. 3 is the schematic diagram (partly cut-away) that chill is fixed in shell.
The specific embodiment
Below in conjunction with the drawings and specific embodiments the present invention is described in further detail.
The local cooling means of a kind of model casting chill of the present invention comprises the steps:
Step 1: at first carry out the compacting of wax-pattern and the assembly welding of running gate system according to normal full form casting process;
Step 2: according to the external surface shape at foundry goods thermal center place design chill and with chill shape, measure-alike wax stone, the external surface shape at the chill of design and the inner surface of wax stone and foundry goods thermal center place is fitted, and make chill and wax stone have positioning step, make chill and wax stone then; Be illustrated in figure 1 as the chill schematic diagram of making, should guarantee that the outer wall at chill inner surface and foundry goods thermal center place can fit tightly, reserve positioning table simultaneously, be used for the location of chill on shell, dewaxing back with fixing.
Step 3: wax stone is fixed in the position that needs local Quench on the wax-pattern, and fits with the wax-pattern surface is tight; Be illustrated in figure 2 as the schematic diagram that is fixed in the wax-pattern surface with wax stone, wax stone is fixed in the heat energy-saving position on the wax-pattern, should guarantee fitting tightly of wax stone and wax-pattern;
Step 4: at wax-pattern surface shell processed, the positioning table part of wax stone is exposed to outside the shell; In every layer of shell process processed, pick coating after, carry out stucco after the coating in the wax stone outside wiped, the positioning table part of wax stone outside is exposed to outside the shell;
Step 5: with the shell dewaxing, wax stone removes in shell with wax-pattern, makes shell form opening at the wax stone place, is used for fixedly chill;
Step 6: shell is carried out high-temperature roasting;
Step 7: after the roasting, the chill of making is in advance placed the shell opening part, locate by positioning table; The place, slit of chill and shell seals with bonding with coating;
Step 8: after the shell preheating, pour into a mould; The part that chill is exposed to outside the shell is forced cooling; The heat conductivility of chill is higher than type shell material far away, so can be to the local chill effect that forms of foundry goods, the effect of reach fast cooling, cooling off fast.Present embodiment is blown by the outside to chill in order to strengthen local chill effect, strengthens the heat radiation of chill, reaches bigger cooling rate.
Reclaim chill foundry goods shelling back, can reuse.
Invention has been described by above-described embodiment, can carry out multiple variation, modification, replacement and distortion to embodiment under the situation that does not break away from principle of the present invention and aim, and scope of the present invention is defined by the claims.

Claims (4)

1. the local cooling means of model casting chill is characterized in that: comprise the steps:
Step 1: at first make wax-pattern according to normal full form casting process;
Step 2: according to the external surface shape at foundry goods thermal center place design chill and with chill shape, measure-alike wax stone, the external surface shape at the chill of design and the inner surface of wax stone and foundry goods thermal center place is fitted, and make chill and wax stone have positioning table, make chill and wax stone then;
Step 3: wax stone is fixed in the position that needs local Quench on the wax-pattern, and fits with the wax-pattern surface is tight;
Step 4: at wax-pattern surface shell processed, the positioning table part on the wax stone is exposed to outside the shell;
Step 5: with the shell dewaxing, wax-pattern and wax stone are removed, form local opening at shell;
Step 6: shell is carried out high-temperature roasting;
Step 7: chill is fixed in the shell opening part, locatees by positioning table;
Step 8: pour into a mould after the shell preheating, the part that chill is exposed to outside the shell is forced cooling.
2. the local cooling technology of a kind of model casting chill according to claim 1, it is characterized in that: step 7 is described to be fixed in the shell opening part with chill, the slit between chill and the shell need be sealed.
3. the local cooling technology of a kind of model casting chill according to claim 2, it is characterized in that: the described mode that adopts brushing paint that is sealed into makes the slit between chill and the shell obtain sealing.
4. the local cooling technology of a kind of model casting chill according to claim 1, it is characterized in that: the described forced cooling method of step 8 is for blowing or water-cooled.
CN2013101054625A 2013-03-28 2013-03-28 Partial cooling method of cold iron in investment casting Pending CN103192027A (en)

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Application Number Priority Date Filing Date Title
CN2013101054625A CN103192027A (en) 2013-03-28 2013-03-28 Partial cooling method of cold iron in investment casting

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Application Number Priority Date Filing Date Title
CN2013101054625A CN103192027A (en) 2013-03-28 2013-03-28 Partial cooling method of cold iron in investment casting

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CN103192027A true CN103192027A (en) 2013-07-10

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Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103394644A (en) * 2013-07-30 2013-11-20 河北师范大学 Casting method capable of preventing precise investment casting from generating hot-spot shrinkage holes
CN103464684A (en) * 2013-09-23 2013-12-25 贵州安吉航空精密铸造有限责任公司 Precise investment casting method
CN103464683A (en) * 2013-09-05 2013-12-25 贵州安吉航空精密铸造有限责任公司 Investment casting method
CN103495702A (en) * 2013-10-11 2014-01-08 西安航空动力股份有限公司 Precision investment casting method capable of changing coagulation and heat dissipation conditions of casting
CN103978156A (en) * 2014-03-04 2014-08-13 清华大学 Method for controlling coagulation and cooling of investment castings
CN104368756A (en) * 2014-11-07 2015-02-25 沈阳黎明航空发动机(集团)有限责任公司 Method for complex-structure, thick and large castings of aero-engine by use of investment casting for contoured densener
CN104439199A (en) * 2014-11-21 2015-03-25 安徽涌诚机械有限公司 Robot base and frame casting process
CN104493090A (en) * 2014-12-11 2015-04-08 贵州红林机械有限公司 Investment casting pouring method of thin-wall aluminum alloy casting
CN105537522A (en) * 2016-02-22 2016-05-04 江苏钜源机械有限公司 Technological method of using internal chill for expendable pattern negative pressure casting
CN105750499A (en) * 2016-04-21 2016-07-13 清华大学 Method of utilizing conformal cold iron and forced convection to locally cool investment casting
CN106363139A (en) * 2016-11-29 2017-02-01 贵州安吉航空精密铸造有限责任公司 Method for overcoming rarefaction defect of case shell casting
CN106623785A (en) * 2016-12-19 2017-05-10 洛阳市金峰铸造有限公司 Casting structure for silica sol investment casting
CN107695300A (en) * 2017-11-24 2018-02-16 四川共享铸造有限公司 A kind of sand core structure for preventing that chill from dropping
CN107790636A (en) * 2017-10-27 2018-03-13 共享装备股份有限公司 A kind of fixing device and fixing means of 3D printing casting technique internal densener
CN109396345A (en) * 2018-12-10 2019-03-01 中国船舶重工集团公司第十二研究所 A method of for investment casting formwork part Quench
CN109396341A (en) * 2018-11-23 2019-03-01 安徽应流铸业有限公司 The method of chill is bonded in a kind of lost wax casting technique
CN109465393A (en) * 2018-11-05 2019-03-15 西安飞机工业(集团)有限责任公司 A kind of quenching method at the thick big position of investment-casting
CN109500359A (en) * 2018-12-17 2019-03-22 嘉善鑫海精密铸件有限公司 Application of the internal densener in full form casting process
CN110076298A (en) * 2019-03-15 2019-08-02 启东市聚旺铸造有限公司 Shell manufacturing process for casting closed impeller
CN110976770A (en) * 2019-12-24 2020-04-10 十堰市金海丰精密铸造有限公司 Method for eliminating shrinkage cavity in precision casting based on chilling block
CN111054901A (en) * 2019-12-31 2020-04-24 西安西工大超晶科技发展有限责任公司 Method for solving streamline defect at lower end of ZL210A alloy casting linear chilling block
CN111097876A (en) * 2019-12-03 2020-05-05 清华大学 Method for applying chilling block to 3D printing sand mold
CN111761032A (en) * 2020-07-30 2020-10-13 陕西柴油机重工有限公司 Manufacturing method of complex camshaft cold core box sand core of large diesel engine body
CN111957891A (en) * 2020-08-13 2020-11-20 山东泰山钢铁集团有限公司 Manufacturing method of investment casting bidirectional pump impeller
CN112317689A (en) * 2020-10-23 2021-02-05 中国科学院金属研究所 Method for reducing high-temperature alloy casting microscopic shrinkage porosity
CN112743059A (en) * 2019-10-29 2021-05-04 中船海洋动力部件有限公司 Novel chill is used in casting
CN113996751A (en) * 2021-10-13 2022-02-01 中国航发北京航空材料研究院 Method for refining local structure grains by titanium alloy precision casting

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101406932A (en) * 2008-11-10 2009-04-15 泉州腾达精铸有限公司 Precision-investment casting method
CN101758181A (en) * 2009-08-31 2010-06-30 滨海县万恒铸业有限公司 Novel process for adding chill modeling on wax mold
CN101767193A (en) * 2009-12-25 2010-07-07 沈阳工业大学 Process method for eliminating loose of thick and large casting of high-temperature alloy

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101406932A (en) * 2008-11-10 2009-04-15 泉州腾达精铸有限公司 Precision-investment casting method
CN101758181A (en) * 2009-08-31 2010-06-30 滨海县万恒铸业有限公司 Novel process for adding chill modeling on wax mold
CN101767193A (en) * 2009-12-25 2010-07-07 沈阳工业大学 Process method for eliminating loose of thick and large casting of high-temperature alloy

Cited By (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103394644A (en) * 2013-07-30 2013-11-20 河北师范大学 Casting method capable of preventing precise investment casting from generating hot-spot shrinkage holes
CN103464683B (en) * 2013-09-05 2015-07-22 贵州安吉航空精密铸造有限责任公司 Investment casting method
CN103464683A (en) * 2013-09-05 2013-12-25 贵州安吉航空精密铸造有限责任公司 Investment casting method
CN103464684A (en) * 2013-09-23 2013-12-25 贵州安吉航空精密铸造有限责任公司 Precise investment casting method
CN103495702A (en) * 2013-10-11 2014-01-08 西安航空动力股份有限公司 Precision investment casting method capable of changing coagulation and heat dissipation conditions of casting
CN103978156A (en) * 2014-03-04 2014-08-13 清华大学 Method for controlling coagulation and cooling of investment castings
CN103978156B (en) * 2014-03-04 2016-08-17 清华大学 A kind of method controlling investment-casting solidification and cooling
CN104368756A (en) * 2014-11-07 2015-02-25 沈阳黎明航空发动机(集团)有限责任公司 Method for complex-structure, thick and large castings of aero-engine by use of investment casting for contoured densener
CN104368756B (en) * 2014-11-07 2016-04-20 沈阳黎明航空发动机(集团)有限责任公司 By the method for contoured chill model casting aero-engine complex structure thick and large casting
CN104439199A (en) * 2014-11-21 2015-03-25 安徽涌诚机械有限公司 Robot base and frame casting process
CN104493090A (en) * 2014-12-11 2015-04-08 贵州红林机械有限公司 Investment casting pouring method of thin-wall aluminum alloy casting
CN105537522A (en) * 2016-02-22 2016-05-04 江苏钜源机械有限公司 Technological method of using internal chill for expendable pattern negative pressure casting
CN105750499A (en) * 2016-04-21 2016-07-13 清华大学 Method of utilizing conformal cold iron and forced convection to locally cool investment casting
CN105750499B (en) * 2016-04-21 2018-02-09 清华大学 A kind of method using profile-followed chill and forced convertion to investment-casting Local cooling
CN106363139A (en) * 2016-11-29 2017-02-01 贵州安吉航空精密铸造有限责任公司 Method for overcoming rarefaction defect of case shell casting
CN106623785A (en) * 2016-12-19 2017-05-10 洛阳市金峰铸造有限公司 Casting structure for silica sol investment casting
CN107790636B (en) * 2017-10-27 2019-09-24 共享装备股份有限公司 A kind of the fixation device and fixing means of 3D printing casting technique internal densener
CN107790636A (en) * 2017-10-27 2018-03-13 共享装备股份有限公司 A kind of fixing device and fixing means of 3D printing casting technique internal densener
CN107695300A (en) * 2017-11-24 2018-02-16 四川共享铸造有限公司 A kind of sand core structure for preventing that chill from dropping
CN109465393A (en) * 2018-11-05 2019-03-15 西安飞机工业(集团)有限责任公司 A kind of quenching method at the thick big position of investment-casting
CN109396341A (en) * 2018-11-23 2019-03-01 安徽应流铸业有限公司 The method of chill is bonded in a kind of lost wax casting technique
CN109396345A (en) * 2018-12-10 2019-03-01 中国船舶重工集团公司第十二研究所 A method of for investment casting formwork part Quench
CN109500359A (en) * 2018-12-17 2019-03-22 嘉善鑫海精密铸件有限公司 Application of the internal densener in full form casting process
CN110076298A (en) * 2019-03-15 2019-08-02 启东市聚旺铸造有限公司 Shell manufacturing process for casting closed impeller
CN112743059A (en) * 2019-10-29 2021-05-04 中船海洋动力部件有限公司 Novel chill is used in casting
CN111097876A (en) * 2019-12-03 2020-05-05 清华大学 Method for applying chilling block to 3D printing sand mold
CN111097876B (en) * 2019-12-03 2021-06-08 清华大学 Method for applying chilling block to 3D printing sand mold
CN110976770A (en) * 2019-12-24 2020-04-10 十堰市金海丰精密铸造有限公司 Method for eliminating shrinkage cavity in precision casting based on chilling block
CN111054901A (en) * 2019-12-31 2020-04-24 西安西工大超晶科技发展有限责任公司 Method for solving streamline defect at lower end of ZL210A alloy casting linear chilling block
CN111761032A (en) * 2020-07-30 2020-10-13 陕西柴油机重工有限公司 Manufacturing method of complex camshaft cold core box sand core of large diesel engine body
CN111957891A (en) * 2020-08-13 2020-11-20 山东泰山钢铁集团有限公司 Manufacturing method of investment casting bidirectional pump impeller
CN112317689A (en) * 2020-10-23 2021-02-05 中国科学院金属研究所 Method for reducing high-temperature alloy casting microscopic shrinkage porosity
CN112317689B (en) * 2020-10-23 2021-11-05 中国科学院金属研究所 Method for reducing high-temperature alloy casting microscopic shrinkage porosity
CN113996751A (en) * 2021-10-13 2022-02-01 中国航发北京航空材料研究院 Method for refining local structure grains by titanium alloy precision casting

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Application publication date: 20130710