CN100415908C - Solution treatment method for hypoeutectic cast aliuminium-silicon alloy heat treatment reinforcement - Google Patents

Solution treatment method for hypoeutectic cast aliuminium-silicon alloy heat treatment reinforcement Download PDF

Info

Publication number
CN100415908C
CN100415908C CNB2006100951996A CN200610095199A CN100415908C CN 100415908 C CN100415908 C CN 100415908C CN B2006100951996 A CNB2006100951996 A CN B2006100951996A CN 200610095199 A CN200610095199 A CN 200610095199A CN 100415908 C CN100415908 C CN 100415908C
Authority
CN
China
Prior art keywords
alloy
treatment
minutes
solution treatment
silicon 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.)
Expired - Fee Related
Application number
CNB2006100951996A
Other languages
Chinese (zh)
Other versions
CN1936040A (en
Inventor
杨明波
潘复生
汤爱涛
胡红军
代兵
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.)
Chongqing Institute of Technology
Original Assignee
Chongqing Institute of Technology
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 Chongqing Institute of Technology filed Critical Chongqing Institute of Technology
Priority to CNB2006100951996A priority Critical patent/CN100415908C/en
Publication of CN1936040A publication Critical patent/CN1936040A/en
Application granted granted Critical
Publication of CN100415908C publication Critical patent/CN100415908C/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Continuous Casting (AREA)

Abstract

The invention relates to a solution treatment method to intensify hypoeutectic casting aluminum-silicon alloy thermal treatment. It includes the following steps: after melting hypoeutectic casting aluminum-silicon alloy, heating to 720-740 degree centigrade, removing dross, taking metamorphism treatment to ternary alterative that is 3wt% of the total charge weight for 15-20 minutes, after that taking refining treatment by hexachloroethane and removing slag, standing for 5-10 minutes at 730-740 minutes, taking metal type gravity casting, after the temperature decreasing under solution treatment process temperature, keeping for 3-8 hours, and tempering into water. The invention effectively ensures vast supersaturation solid solubility in a short time and would bring great energy benefits.

Description

A kind of solid solution treatment method that is used for the hypoeutectic cast aluminium-silicon alloy heat treatment reinforcement
Technical field:
What the present invention relates to is a kind of cast Al-Si alloy heat treatment reinforcement method, belongs to class of metal materials and field of metallurgy.
Background technology:
Cast Al-Si alloy is as the important component part of aluminum alloy materials, because of it has that unit weight is little, intensity is high, cast form is good and series of advantages such as machining property is good, therefore be widely applied at present on Aeronautics and Astronautics, automobile and other conveying mechanicals, used this material can alleviate equipment self-weight, save energy greatly, reduce cost, raise the efficiency.But at present both at home and abroad the mechanical property of the cast Al-Si alloy of the existing trade mark still can not be equal to high-strength cast steel mutually at aspects such as specific tenacity and unit elongation, is difficult to satisfy current and conveying mechanical parts such as automobile, aircraft industrial expansion requirement from now on.Therefore, people just study cast Al-Si alloy from aspects such as alloying constituent optimization, purifying treatment, the rotten processing of refinement and thermal treatments, in the hope of improving its comprehensive mechanical property.And in improving the various technological measures of cast Al-Si alloy mechanical property, because thermal treatment can be brought into play the performance potential of alloy to greatest extent, therefore given both at home and abroad to pay close attention to widely and attention highly for the heat treatment reinforcement of cast Al-Si alloy always.
As everyone knows, the thermal treatment of cast Al-Si alloy generally comprises solution treatment and two operations of ageing treatment, therefore how wherein solution treatment is the basis of the follow-up ageing treatment of cast Al-Si alloy and crucial, obtains satisfied solution treatment effect by technology controlling and process and just seems particularly crucial for the heat treatment reinforcement of cast Al-Si alloy.At present, a large amount of research of having carried out for the solution treatment of cast Al-Si alloy both at home and abroad, and single-stage, twin-stage and different solid solution treatment process such as multistage have successively been developed, and set up relevant theory and engineering application technology standard, but these solid solution treatment processes of having developed all carry out reheating under the solid solution temperature condition behind the cast Al-Si alloy cool to room temperature.Owing to need reheat, clearly, problems such as these solid solution treatment processes that developed existence are heated and soaking time is long, energy consumption is big, in addition, technological factors such as the type of heating of also necessary strict control cast Al-Si alloy and rate of heating, it is improper because in case type of heating and rate of heating are selected, it is uneven to produce heating, be difficult to guarantee the homogeneity of alloy super saturated solid solution degree, cause the comprehensive mechanical property of alloy to be affected, thereby make the effect of solution treatment in the cast Al-Si alloy heat treatment reinforcement be difficult to perform to maximum limit.Therefore how to avoid the deficiency of the existing solid solution treatment process of cast Al-Si alloy, research and develop novel solid solution treatment method and just seem particularly important for bringing into play the strengthening effect of thermal treatment to greatest extent to cast Al-Si alloy.
Summary of the invention
The objective of the invention is to overcome the deficiency of existing cast Al-Si alloy solid solution treatment method, a kind of solid solution treatment method that is used for the hypoeutectic cast aluminium-silicon alloy heat treatment reinforcement is proposed, adopt this method both can save energy, shorten the solid solution soaking time and do not influence the heat treatment reinforcement effect, thereby help further to enlarge the application of heat treatment reinforcement in cast Al-Si alloy.
To achieve these goals, the present invention proposes a kind of solid solution treatment method that the castingprocesses and the heat treatment process of hypoeutectic cast aluminium-silicon alloy are organically combined, it is to be warmed up to 720~740 ℃ after hypoeutectic cast aluminium-silicon alloy is melted by composition proportion, drag for alloy liquid surface scum, between 750~780 ℃ the 3% ternary alterant (62%NaCl+25%NaF+13%KCl) that accounts for the alloy charging weight after the preheating is carried out 15~20 minutes rotten processing then, back hexachloroethane (C disposes 2Cl 6) carry out refining treatment, to skim then, left standstill 5~10 minutes at 730~740 ℃ the back of skimming, carry out metal mold gravity casting then, in castingprocesses, after the temperature of alloy drops to solid solution temperature below the solidus temperature,, take out in the entry of quenching fast then alloy insulation 3~8 hours.
As seen from Figure 1, hypoeutectic cast aluminium-silicon alloy tradition solid solution treatment method is behind the alloy casting cool to room temperature, and then reheats the solid solution temperature insulation regular hour, carries out shrend then.The solid content processing method that the present invention proposes then is to carry out solution treatment in the alloy casting process of cooling, promptly is incubated the regular hour immediately during the solid solution temperature below alloy temperature drops to solidus temperature, carries out shrend then, sees shown in Figure 2.Obviously, the solid solution treatment method that the present invention proposes, because castingprocesses and heat treatment process are organically combined, avoided original solid solution treatment method after the alloy graining cooling, to reheat this technological process, efficiently solved type of heating and the improper problem of bringing of heating rate control because of reheating; And because hypoeutectic cast aluminium-silicon alloy solidifies cooling and solution treatment is among the successive processes, make hypoeutectic cast aluminium-silicon alloy be in the higher state of temperature always, the diffusibility of inner atom is strong, some low melting point alloys are not also separated out mutually fully in addition, therefore can guarantee to obtain bigger super saturated solid solution degree degree in the short period of time, for follow-up ageing treatment has been established the good tissue basis.Simultaneously, the source benefit that brings than short solid solution soaking time also is very significant.
Description of drawings
Fig. 1 is the temperature-timing relationship synoptic diagram of traditional solid solution treatment method.
Fig. 2 is the temperature-timing relationship synoptic diagram of the solid solution treatment method that proposes of the present invention.
Embodiment:
Below by three concrete embodiment technical scheme of the present invention and effect are further elaborated.
Embodiment 1:
The ZL101 aluminum silicon alloy is warmed up to 720 ℃ after by the fusing of corresponding composition proportion, drag for alloy liquid surface scum, between 760 ℃ the 3% ternary alterant (62%NaCl+25%NaF+13%KCl) that accounts for the alloy charging weight after the preheating is carried out 20 minutes rotten processing then, back hexachloroethane (C disposes 2Cl 6) carry out refining treatment, to skim then, left standstill 5 minutes at 730 ℃ the back of skimming, carry out metal mold gravity casting then, in castingprocesses, after the temperature of alloy drops to 535 ℃ of solid solution temperatures below the alloy solidus temperature,, take out in the entry of quenching fast then alloy insulation 3 hours.After solution treatment is finished routinely aging treatment method (table 1) alloy is carried out ageing treatment.The alloy that adopts proposition method of the present invention to obtain is done the room temperature tensile performance test, the result is as shown in table 1, as can be seen from Table 1, compares with traditional method, adopt the present invention to propose method and can save 50% solution treatment cost, and the alloy at room temperature tensile property is suitable with traditional method.
Embodiment 2:
The ZL105 aluminum silicon alloy is warmed up to 720 ℃ after by the fusing of corresponding composition proportion, drag for alloy liquid surface scum, between 760 ℃ the 3% ternary alterant (62%NaCl+25%NaF+13%KCl) that accounts for the alloy charging weight after the preheating is carried out 20 minutes rotten processing then, back hexachloroethane (C disposes 2Cl 6) carry out refining treatment, to skim then, left standstill 5 minutes at 730 ℃ the back of skimming, carry out metal mold gravity casting then, in castingprocesses, after the temperature of alloy drops to 525 ℃ of solid solution temperatures below the alloy solidus temperature,, take out in the entry of quenching fast then alloy insulation 8 hours.After solution treatment is finished routinely aging treatment method (table 1) alloy is carried out ageing treatment.The alloy that adopts proposition method of the present invention to obtain is done the room temperature tensile performance test, the result is as shown in table 1, as can be seen from Table 1, compares with traditional method, adopt the present invention to propose method and can save 33% solution treatment cost, and the alloy at room temperature tensile property is suitable with traditional method.
Embodiment 3:
The ZL107 aluminum silicon alloy is warmed up to 720 ℃ after by the fusing of corresponding composition proportion, drag for alloy liquid surface scum, between 760 ℃ the 3% ternary alterant (62%NaCl+25%NaF+13%KCl) that accounts for the alloy charging weight after the preheating is carried out 20 minutes rotten processing then, back hexachloroethane (C disposes 2Cl 6) carry out refining treatment, to skim then, left standstill 5 minutes at 730 ℃ the back of skimming, carry out metal mold gravity casting then, in castingprocesses, after the temperature of alloy drops to 515 ℃ of solid solution temperatures below the alloy solidus temperature,, take out in the entry of quenching fast then alloy insulation 6 hours.After solution treatment is finished routinely aging treatment method (table 1) alloy is carried out ageing treatment.The alloy that adopts proposition method of the present invention to obtain is done the room temperature tensile performance test, the result is as shown in table 1, as can be seen from Table 1, compares with traditional method, adopt the present invention to propose method and can save 25% solution treatment cost, and the alloy at room temperature tensile property is suitable with traditional method.

Claims (1)

1. solid solution treatment method that is used for the hypoeutectic cast aluminium-silicon alloy heat treatment reinforcement, hypoeutectic cast aluminium-silicon alloy is warmed up to 720~740 ℃ by after the composition proportion fusing, drag for alloy liquid surface scum, between 750~780 ℃ the 3% ternary alterant 62%NaCl+25%NaF+13%KCl that accounts for the alloy charging weight after the preheating is carried out 15~20 minutes rotten processing then, back hexachloroethane C disposes 2Cl 6Carry out refining treatment, skim then, left standstill 5~10 minutes at 730~740 ℃ after skimming, carry out metal mold gravity casting then, in castingprocesses after the temperature of alloy drops to solid solution temperature below the alloy solidus temperature, with alloy insulation 3~8 hours, take out in the entry of quenching fast then.
CNB2006100951996A 2006-10-14 2006-10-14 Solution treatment method for hypoeutectic cast aliuminium-silicon alloy heat treatment reinforcement Expired - Fee Related CN100415908C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNB2006100951996A CN100415908C (en) 2006-10-14 2006-10-14 Solution treatment method for hypoeutectic cast aliuminium-silicon alloy heat treatment reinforcement

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNB2006100951996A CN100415908C (en) 2006-10-14 2006-10-14 Solution treatment method for hypoeutectic cast aliuminium-silicon alloy heat treatment reinforcement

Publications (2)

Publication Number Publication Date
CN1936040A CN1936040A (en) 2007-03-28
CN100415908C true CN100415908C (en) 2008-09-03

Family

ID=37953779

Family Applications (1)

Application Number Title Priority Date Filing Date
CNB2006100951996A Expired - Fee Related CN100415908C (en) 2006-10-14 2006-10-14 Solution treatment method for hypoeutectic cast aliuminium-silicon alloy heat treatment reinforcement

Country Status (1)

Country Link
CN (1) CN100415908C (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101629251B (en) * 2008-07-16 2011-06-22 贵州红林机械有限公司 Method for smelting high-silicon aluminum alloy
CN103060583A (en) * 2012-12-14 2013-04-24 安徽润鑫泰达智能系统工程有限公司 Method for refining hypo eutectic aluminum-silicon alloy structure
CN105728698A (en) * 2016-03-30 2016-07-06 山东省科学院新材料研究所 Method for refining solidification structure of aluminum silicon alloy

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1125263A (en) * 1995-06-26 1996-06-26 上海交通大学 Method for forming nascent silicon phase in hypoeutectic aluminiumsilicon alloy
JP2002346729A (en) * 2001-05-21 2002-12-04 Hitachi Metals Ltd HYPOEUTECTIC Al-Si ALLOY CASTING AND ITS PRODUCING METHOD
CN1405345A (en) * 2002-11-07 2003-03-26 上海交通大学 Method for treating refined grain of hypoeutectic aluminium-silicon alloy at melt temperature
US20040055724A1 (en) * 2002-09-20 2004-03-25 Spx Corporation Semi-solid metal casting process and product
US20040216857A1 (en) * 2003-05-01 2004-11-04 Deepak Saha Semi-solid metal casting process of hypoeutectic aluminum alloys

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1125263A (en) * 1995-06-26 1996-06-26 上海交通大学 Method for forming nascent silicon phase in hypoeutectic aluminiumsilicon alloy
JP2002346729A (en) * 2001-05-21 2002-12-04 Hitachi Metals Ltd HYPOEUTECTIC Al-Si ALLOY CASTING AND ITS PRODUCING METHOD
US20040055724A1 (en) * 2002-09-20 2004-03-25 Spx Corporation Semi-solid metal casting process and product
CN1405345A (en) * 2002-11-07 2003-03-26 上海交通大学 Method for treating refined grain of hypoeutectic aluminium-silicon alloy at melt temperature
US20040216857A1 (en) * 2003-05-01 2004-11-04 Deepak Saha Semi-solid metal casting process of hypoeutectic aluminum alloys

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
压力铸造对亚共晶Al-11Si-1.8Cu合金的组织细化作用. 杨明波,潘复生,彭晓东等.重庆大学学报(自然科学版),第28卷第1期. 2005
压力铸造对亚共晶Al-11Si-1.8Cu合金的组织细化作用. 杨明波,潘复生,彭晓东等.重庆大学学报(自然科学版),第28卷第1期. 2005 *

Also Published As

Publication number Publication date
CN1936040A (en) 2007-03-28

Similar Documents

Publication Publication Date Title
CN108823472B (en) High-strength and high-toughness Al-Zn-Mg-Cu aluminum alloy and heat treatment method thereof
CN103820689B (en) Be high-strength heat-resistant magnesium alloy and the preparation working method thereof of rare earth containing two
CN103882271B (en) A kind of high-strength high-elongation ratio Al-Mg-Si-Cu alloy material and preparation method thereof
CN102899540B (en) Super large specification aluminum alloy slab ingot and casting method
CN102943193B (en) Grain refinement machining process of hard aluminium alloy cast ingot
CN104357721A (en) 7050 aluminum alloy
CN105039817B (en) The preparation method and multicomponent heat-resistant magnesium alloy of a kind of multicomponent heat-resistant magnesium alloy
CN104651693A (en) Microscale Al-containing rare earth wrought magnesium alloy and preparation method thereof
CN103993208A (en) Al-Mg-Si-Cu-Mn-Er alloy material and preparation method thereof
CN109504884A (en) Polynary a small amount of high-strength plasticity magnesium alloy and its heavy reduction short flow process
CN107164669A (en) It is wrought aluminium alloy and preparation method thereof that a kind of easy processing, which reclaims 7,
CN104404326B (en) The heat top casting technique and 7A85 aluminium alloy cast ingots of a kind of 7A85 aluminium alloys
CN109022973A (en) A kind of deformed magnesium alloy material and its preparation process of middle high-strength and high-plasticity
CN106834822A (en) Fastening parts of automobiles high-strength aluminum alloy bar and preparation method thereof
CN103993209A (en) Rare earth Sc micro-alloyed Al-Mg-Si-Cu alloy and preparation method thereof
CN106282685A (en) A kind of high strength cast aluminum alloys and preparation method thereof
CN107841665A (en) A kind of high-strength/tenacity aluminum alloy sheet material of scandium containing rare earth and erbium and preparation method thereof
CN102304651B (en) Casting aluminum-silicon alloy and strengthening method thereof
CN101649405B (en) Al-Mg-Mn-Zr-Sr alloy and preparation method thereof
CN100415908C (en) Solution treatment method for hypoeutectic cast aliuminium-silicon alloy heat treatment reinforcement
CN104532028A (en) Hot top casting process of 7050 aluminum alloy and 7050 aluminum alloy ingot
CN104404415A (en) Preparation process of aviation aluminum alloy ingot and aluminum alloy ingot
CN104099505B (en) A kind of wrought magnesium alloy and preparation method thereof
CN101967614A (en) Homogenizing treatment method for strengthening Al-Zn-Mg-Cu series ultrahigh strength aluminum alloy
CN104451292A (en) 7A85 aluminum alloy

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
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20080903

Termination date: 20091116