CN104107879A - Ceramic secondary reinforcement method - Google Patents

Ceramic secondary reinforcement method Download PDF

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Publication number
CN104107879A
CN104107879A CN201410172292.7A CN201410172292A CN104107879A CN 104107879 A CN104107879 A CN 104107879A CN 201410172292 A CN201410172292 A CN 201410172292A CN 104107879 A CN104107879 A CN 104107879A
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CN
China
Prior art keywords
ceramic core
formwork
die shell
heating rate
ceramic
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Pending
Application number
CN201410172292.7A
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Chinese (zh)
Inventor
海潮
陈波
俞州
董茵
郭永华
刘丽亚
刘玉柱
郑元斌
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Xian Aviation Power Co Ltd
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Xian Aviation Power Co Ltd
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Publication date
Application filed by Xian Aviation Power Co Ltd filed Critical Xian Aviation Power Co Ltd
Priority to CN201410172292.7A priority Critical patent/CN104107879A/en
Publication of CN104107879A publication Critical patent/CN104107879A/en
Pending legal-status Critical Current

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Abstract

The invention relates to the field of precise casting of fusible patterns, and especially relates to a solution scheme of core breakage and leakage defects caused by insufficient ceramic core strength. A ceramic core secondary reinforcement method comprises the following steps: 1, secondary roasting of a de-waxed die shell with a ceramic core: heating from normal temperature to 900DEG C under a heating rate of 4-5DEG C/min, carrying out heat insulation for 1-2h, heating from 900DEG C to 1200DEG C under a heating rate of 3-4DEG C/min, carrying out heat insulation for 3-4h, cooling with a furnace to below 200DEG C, and discharging the obtained die shell from the furnace; and 2, secondary reinforcement on the secondary-roasted die shell with the ceramic: slowly dumping an ethyl silicate hydrolysate into the roasted die shell from the sprue cup of the die shell until the level of the ethyl silicate hydrolysate reaches the sprue cup, immersing for 20-40min, dumping out the ethyl silicate hydrolysate, naturally drying, and chemically hardening to obtain a die shell to be cast.

Description

Ceramic core secondary hardening method
Technical field
The present invention relates to precision-investment casting field, particularly relate to the solution of the disconnected leakage core defect causing because of ceramic core undercapacity.
Background technology
The intensity of ceramic core is the principal element that affects ceramic core performance.For making ceramic core can bear impact, the pressure of wax material in compacting wax-pattern, dewaxing, formwork roasting and casting process, the various external active forces such as the impact of molten metal, pressure, ceramic core need to carry out intensive treatment, traditional ceramic core high and low temperature reinforcement process, for the problems such as disconnected leakage core that solve smallclothes ceramic core, it is respond well.But for the ceramic core of large-scale blade, by its method, can not be satisfied with production requirement completely, the disconnected core problem of leaking still often occurs.Particularly, when the large hollow blade of production inner chamber especially complexity, because the elevated temperature strength of ceramic core is not enough, and the situation that causes foundry goods to be scrapped is many especially.
Summary of the invention
(1) goal of the invention
The object of the invention is by the ceramic core in formwork after dewaxing, to carry out secondary hardening further to improve ceramic core elevated temperature strength, reduces and even eliminate disconnected, the leakage core problem of foundry goods.
(2) invention technical scheme
The sintering when manufacturing ceramic core of the secondary hardening is here crossed once.Ceramic core secondary hardening method, this method comprises the following steps:
The first step, formwork after dewaxing with ceramic core is carried out to after baking, roasting technique is as follows: with the heating rate of 4-5 per minute ℃, from normal temperature, rise to 900 ℃, insulation 1-2 hour, with the heating rate of 3-4 per minute ℃, from 900 ℃, rise to 1200 ℃ again, insulation 3-4 hour, finally cools to 200 ℃ with the furnace and comes out of the stove below.
Second step, the formwork with ceramic core after after baking is carried out to secondary hardening, reinforcement process is as follows: silicate hydrolyzate liquid is slowly poured in the formwork after roasting from the cup of formwork, until flood to cup place, soak after 20~40 minutes, silicate hydrolyzate liquid is poured out, after natural drying and chemicosolidifying, it is to be cast that formwork gets final product etc. again.
(3) beneficial effect
The inventive method operating process is simple, and can effectively improve the elevated temperature strength of ceramic core, reduces disconnected generation of leaking core defect, and casting qualified rate is significantly improved, and has saved production cost, has produced huge economic benefit.
Accompanying drawing explanation
Fig. 1 is the artwork of this method.
The specific embodiment
Further illustrate by the following examples method of the present invention
Embodiment 1
The II level guide vane of certain machine of take is example.Implementation process is as follows: ceramic core secondary hardening method, and this method comprises the following steps:
The first step, formwork after dewaxing with ceramic core is carried out to after baking, roasting technique is as follows: with the heating rates of 4 ℃ per minute, from normal temperature, rise to 900 ℃, be incubated 1 hour, with the heating rate of 3 ℃ per minute, from 900 ℃, rise to 1200 ℃ again, be incubated 3 hours, finally cool to 200 ℃ with the furnace and come out of the stove below.
Second step, the formwork with ceramic core after after baking is carried out to secondary hardening, reinforcement process is as follows: silicate hydrolyzate liquid is slowly poured in the formwork after roasting from the cup of formwork, until flood to cup place, soak after 20 minutes, silicate hydrolyzate liquid is poured out, after natural drying and chemicosolidifying, it is to be cast that formwork gets final product etc. again.
Embodiment 2
The I level guide vane of certain machine of take is example.Implementation process is as follows:
Ceramic core secondary hardening method, this method comprises the following steps:
The first step, formwork after dewaxing with ceramic core is carried out to after baking, roasting technique is as follows: with the heating rates of 4.5 ℃ per minute, from normal temperature, rise to 900 ℃, be incubated 1.5 hours, with the heating rate of 3.5 ℃ per minute, from 900 ℃, rise to 1200 ℃ again, be incubated 3.5 hours, finally cool to 200 ℃ with the furnace and come out of the stove below.
Second step, the formwork with ceramic core after after baking is carried out to secondary hardening, reinforcement process is as follows: silicate hydrolyzate liquid is slowly poured in the formwork after roasting from the cup of formwork, until flood to cup place, soak after 30 minutes, silicate hydrolyzate liquid is poured out, after natural drying and chemicosolidifying, it is to be cast that formwork gets final product etc. again.

Claims (1)

1. ceramic core secondary hardening method, is characterized in that, this method comprises the following steps:
The first step, formwork after dewaxing with ceramic core is carried out to after baking, roasting technique is as follows: with the heating rate of 4-5 per minute ℃, from normal temperature, rise to 900 ℃, insulation 1-2 hour, with the heating rate of 3-4 per minute ℃, from 900 ℃, rise to 1200 ℃ again, insulation 3-4 hour, finally cools to 200 ℃ with the furnace and comes out of the stove below;
Second step, the formwork with ceramic core after after baking is carried out to secondary hardening, reinforcement process is as follows: silicate hydrolyzate liquid is slowly poured in the formwork after roasting from the cup of formwork, until flood to cup place, soak after 20~40 minutes, silicate hydrolyzate liquid is poured out, after natural drying and chemicosolidifying, it is to be cast that formwork gets final product etc. again.
CN201410172292.7A 2014-04-25 2014-04-25 Ceramic secondary reinforcement method Pending CN104107879A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410172292.7A CN104107879A (en) 2014-04-25 2014-04-25 Ceramic secondary reinforcement method

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Application Number Priority Date Filing Date Title
CN201410172292.7A CN104107879A (en) 2014-04-25 2014-04-25 Ceramic secondary reinforcement method

Publications (1)

Publication Number Publication Date
CN104107879A true CN104107879A (en) 2014-10-22

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CN (1) CN104107879A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104959536A (en) * 2015-07-31 2015-10-07 南昌航空大学 Preparation method of easy-to-clear aluminum chloride hardened water glass shell mold for investment casting
CN106363131A (en) * 2016-09-21 2017-02-01 上海万泽精密铸造有限公司 Modification method for ceramic shell surface layer for titanium alloy casting
CN107900286A (en) * 2017-12-04 2018-04-13 东方电气集团东方汽轮机有限公司 A kind of fused quartz ceramic shell preparation method
CN114273612A (en) * 2021-12-27 2022-04-05 江苏永瀚特种合金技术股份有限公司 Preparation method of ceramic core for refining surface grains of inner cavity of high-temperature alloy casting
CN114700465A (en) * 2022-03-02 2022-07-05 中国电建集团郑州泵业有限公司 Roasting method for final-stage guide vane investment casting formwork of double-casing pump

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CN101734910A (en) * 2009-12-04 2010-06-16 沈阳黎明航空发动机(集团)有限责任公司 Method for preparing porous alumina ceramic core
CN102491779A (en) * 2011-12-16 2012-06-13 沈阳黎明航空发动机(集团)有限责任公司 Method for improving poriness of alumina ceramic mold core
CN103265296A (en) * 2013-05-13 2013-08-28 沈阳黎明航空发动机(集团)有限责任公司 Method for reducing thermal deformation silicon-based ceramic core

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CN1807344A (en) * 2006-02-09 2006-07-26 沈阳黎明航空发动机(集团)有限责任公司 Hollow cast ceramic core and its preparation method
CN101734910A (en) * 2009-12-04 2010-06-16 沈阳黎明航空发动机(集团)有限责任公司 Method for preparing porous alumina ceramic core
CN102491779A (en) * 2011-12-16 2012-06-13 沈阳黎明航空发动机(集团)有限责任公司 Method for improving poriness of alumina ceramic mold core
CN103265296A (en) * 2013-05-13 2013-08-28 沈阳黎明航空发动机(集团)有限责任公司 Method for reducing thermal deformation silicon-based ceramic core

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104959536A (en) * 2015-07-31 2015-10-07 南昌航空大学 Preparation method of easy-to-clear aluminum chloride hardened water glass shell mold for investment casting
CN106363131A (en) * 2016-09-21 2017-02-01 上海万泽精密铸造有限公司 Modification method for ceramic shell surface layer for titanium alloy casting
CN107900286A (en) * 2017-12-04 2018-04-13 东方电气集团东方汽轮机有限公司 A kind of fused quartz ceramic shell preparation method
CN107900286B (en) * 2017-12-04 2019-05-17 东方电气集团东方汽轮机有限公司 A kind of fused quartz ceramic shell preparation method
CN114273612A (en) * 2021-12-27 2022-04-05 江苏永瀚特种合金技术股份有限公司 Preparation method of ceramic core for refining surface grains of inner cavity of high-temperature alloy casting
CN114273612B (en) * 2021-12-27 2023-09-05 江苏永瀚特种合金技术股份有限公司 Preparation method of ceramic core for refining grains on inner cavity surface of superalloy casting
CN114700465A (en) * 2022-03-02 2022-07-05 中国电建集团郑州泵业有限公司 Roasting method for final-stage guide vane investment casting formwork of double-casing pump

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Application publication date: 20141022