CN105728654A - Process for eliminating microporosity of surfaces of aluminum alloy castings - Google Patents

Process for eliminating microporosity of surfaces of aluminum alloy castings Download PDF

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Publication number
CN105728654A
CN105728654A CN201410755876.7A CN201410755876A CN105728654A CN 105728654 A CN105728654 A CN 105728654A CN 201410755876 A CN201410755876 A CN 201410755876A CN 105728654 A CN105728654 A CN 105728654A
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CN
China
Prior art keywords
microporosity
castings
aluminum alloy
cast
series
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.)
Pending
Application number
CN201410755876.7A
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Chinese (zh)
Inventor
刘俊英
蒲伟
朱淑惠
李增乐
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shaanxi Hongyuan Aviation Forging Co Ltd
Original Assignee
Shaanxi Hongyuan Aviation Forging Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Shaanxi Hongyuan Aviation Forging Co Ltd filed Critical Shaanxi Hongyuan Aviation Forging Co Ltd
Priority to CN201410755876.7A priority Critical patent/CN105728654A/en
Publication of CN105728654A publication Critical patent/CN105728654A/en
Pending legal-status Critical Current

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Abstract

The invention relates to a process for eliminating the microporosity of the surfaces of ZL2xx series of aluminum alloy castings. Because the ZL2xx series of aluminum alloy castings are produced under the normal investment casting technological conditions, the microporosity of the surfaces of the castings is serious, and the castings do not meet the aviation standard requirements and cannot pass fluorescent inspection. In order to control the microporosity of the surfaces of the ZL2xx series of aluminum alloy castings, eliminate the microporosity of the surfaces of the castings and meet the aviation standard requirements, the scattered pouring, cold shell pouring and forced cooling processes are adopted. Accordingly, the microporosity of the surfaces of the castings is eliminated, the requirements for application of the ZL2xx series of aluminum alloy castings are met, and a new approach is provided for controlling the microporosity of the surfaces of the ZL2xx series of aluminum alloy castings.

Description

A kind of process solving aluminium alloy castings surface microporosity
Technical field
The invention belongs to technique processing method technical field, particularly relate to the process of a kind of ZL2 ×× series alloys cast(ing) surface microporosity.
Background technology
Foundry goods microporosity is defined as on related data: the small hole formed between crystal grain in metal liquid solidification process.Being formed of microporosity is mainly relevant with the crystallization range of alloy and casting section thickness etc..The crystallization range of usual alloy is more wide, more easily forms mushy freezing, and last remaining part metals liquid is divided into numerous zonules by solid phase dendrite branch, produces small hole when causing molten metal crystallization between crystal grain.Aluminium alloy castings specifies have sand mould casting method and investment casting method to prepare in air standard, but the ZL2 ×× series alloys foundry goods that investment casting method produces is due to cast(ing) surface microporosity, foundry goods can not pass through to cause that foundry goods learies is big in fluoroscopy, especially more prominent more than showing on 10mm foundry goods at casting section thickness.
Summary of the invention
The technical problem to be solved is: provides and produces ZL2 ×× series alloys foundry goods under full form casting process, and cast(ing) surface, without microporosity, meets the foundry goods that air standard requires.
The technical scheme is that due to ZL2 ×× series alloys foundry goods, produce when normal full form casting process, cast(ing) surface microporosity is serious, does not meet air standard requirement, and fluoroscopy can not be passed through.Loosen to control ZL2 ×× series alloys cast(ing) surface so that cast(ing) surface, without microporosity, meets air standard requirement, take dispersion cast, the cast of cold shell, Constraint Cooling Technology, reach to eliminate the purpose of surface microporosity.Specifically include following steps:
The first step, dispersion cast: when pouring cast part, as much as possible arrange ingate, to reach dispersed metal liquid, reduces the heat local assault to formwork, eliminates the purpose of foundry goods hot-spot;
Second step, cold shell is poured into a mould, and is down to room temperature, pours into a mould after formwork roasting;
3rd, force cooling, after casting pouring, at once foundry goods thickness large part dried or blow CO2Gas, to reach the purpose of quickly cooling.
The invention has the beneficial effects as follows: by adopting full form casting process to produce ZL2 ×× series alloys foundry goods, it is met air standard requirement, surface is without the foundry goods of microporosity, and all reach requirement through multiple batches of checking, meet ZL2 ×× series alloys foundry goods instructions for use, control surface microporosity for ZL2 ×× series alloys foundry goods and provide a new approach.
Detailed description of the invention:
Below by instantiation, the present invention is described in further detail:
Certain housing design requires to be ZL201 Melt casting, and castings desire fluoroscopy, cast(ing) surface must not have microporosity.So have employed the dispersion of present invention cast, the cast of cold shell, Constraint Cooling Technology method produces.
Disperse ingate when casting moulding system designs, with dispersed metal liquid, made formwork is down to room temperature after 1020 DEG C of roastings, insulation > 1.5h to be cast;Melting ZL201 metal in 100Kg resistance furnace, comes out of the stove in 720 DEG C after molten metal fusing, refine, slag hitting totally, pours into foundry goods;Adopt rapidly compression air that foundry goods thickness large part is carried out pressure after cast and be cooled to less than 300 DEG C, continue to naturally cool to room temperature, shelling cleaning.In 49 foundry goods prepared through above-mentioned process, through fluoroscopy, it is satisfied by user's design, instructions for use.The successful implementation of this process program, provides new thinking and selection approach for solving ZL2 ×× series alloys cast(ing) surface microporosity.

Claims (1)

1. the process solving ZL2 ×× series alloys cast(ing) surface microporosity, it is characterised in that comprise the following steps:
The first step, dispersion cast: when pouring cast part, as much as possible arrange ingate, to reach dispersed metal liquid, reduces the heat local assault to formwork, eliminates the purpose of foundry goods hot-spot;
Second step, cold shell is poured into a mould, and is down to room temperature, pours into a mould after formwork roasting;
3rd, force cooling, after casting pouring, at once foundry goods thickness large part dried or blow CO2Gas, to reach to be quickly cooled to the purpose of less than 300 degree.
CN201410755876.7A 2014-12-10 2014-12-10 Process for eliminating microporosity of surfaces of aluminum alloy castings Pending CN105728654A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410755876.7A CN105728654A (en) 2014-12-10 2014-12-10 Process for eliminating microporosity of surfaces of aluminum alloy castings

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410755876.7A CN105728654A (en) 2014-12-10 2014-12-10 Process for eliminating microporosity of surfaces of aluminum alloy castings

Publications (1)

Publication Number Publication Date
CN105728654A true CN105728654A (en) 2016-07-06

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Country Status (1)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110961577A (en) * 2019-12-24 2020-04-07 陕西宏远航空锻造有限责任公司 Method for solving shrinkage porosity of investment casting aluminum alloy casting
CN111390155A (en) * 2020-04-30 2020-07-10 中国航发哈尔滨东安发动机有限公司 Investment casting solidification method and device

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Publication number Priority date Publication date Assignee Title
US5303764A (en) * 1990-03-27 1994-04-19 Atsugi Unisia Corporation Die for forming aluminum silicon alloy
JP2000343202A (en) * 1999-05-28 2000-12-12 Chuo Spring Co Ltd Manufacture of partial composite metal-based composite material, and its manufacturing device
CN101239385A (en) * 2008-03-18 2008-08-13 上海大学 Casting method capable of effectively improving quality of aluminum alloy casting parts
CN101590519A (en) * 2009-06-26 2009-12-02 宁波强盛机械模具有限公司 The pouring casting process of aluminum alloy air inlet manifold
CN201776424U (en) * 2010-08-04 2011-03-30 徐州徐航压铸有限公司 Forced cooling device of main oil gallery in die casting and molding of four-cylinder engine
CN102029377A (en) * 2010-12-08 2011-04-27 何丙军 Low-pressure casting die of aluminium alloy wheel and casting method thereof
CN203124711U (en) * 2012-12-20 2013-08-14 江苏凯特汽车部件有限公司 Low-pressure casting mold capable of reducing cavity shrinkage and loosening of aluminum alloy wheel spoke
CN103567387A (en) * 2013-11-08 2014-02-12 中国航空工业集团公司北京航空材料研究院 Integral gating system of certain airplane cabin door casting
CN103752809A (en) * 2014-01-07 2014-04-30 南通宏德机电有限公司 Method for eliminating aluminum alloy casting pore defects

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5303764A (en) * 1990-03-27 1994-04-19 Atsugi Unisia Corporation Die for forming aluminum silicon alloy
JP2000343202A (en) * 1999-05-28 2000-12-12 Chuo Spring Co Ltd Manufacture of partial composite metal-based composite material, and its manufacturing device
CN101239385A (en) * 2008-03-18 2008-08-13 上海大学 Casting method capable of effectively improving quality of aluminum alloy casting parts
CN101590519A (en) * 2009-06-26 2009-12-02 宁波强盛机械模具有限公司 The pouring casting process of aluminum alloy air inlet manifold
CN201776424U (en) * 2010-08-04 2011-03-30 徐州徐航压铸有限公司 Forced cooling device of main oil gallery in die casting and molding of four-cylinder engine
CN102029377A (en) * 2010-12-08 2011-04-27 何丙军 Low-pressure casting die of aluminium alloy wheel and casting method thereof
CN203124711U (en) * 2012-12-20 2013-08-14 江苏凯特汽车部件有限公司 Low-pressure casting mold capable of reducing cavity shrinkage and loosening of aluminum alloy wheel spoke
CN103567387A (en) * 2013-11-08 2014-02-12 中国航空工业集团公司北京航空材料研究院 Integral gating system of certain airplane cabin door casting
CN103752809A (en) * 2014-01-07 2014-04-30 南通宏德机电有限公司 Method for eliminating aluminum alloy casting pore defects

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Title
蒋文明: "铝(镁)合金真空低压消失模壳型铸造技术基础研究", 《中国博士学位论文全文数据库 工程科技Ⅰ辑》 *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110961577A (en) * 2019-12-24 2020-04-07 陕西宏远航空锻造有限责任公司 Method for solving shrinkage porosity of investment casting aluminum alloy casting
CN111390155A (en) * 2020-04-30 2020-07-10 中国航发哈尔滨东安发动机有限公司 Investment casting solidification method and device

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