CN107427906A - For producing the arenaceous shell casting method of the part used in automobile and aviation field - Google Patents

For producing the arenaceous shell casting method of the part used in automobile and aviation field Download PDF

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Publication number
CN107427906A
CN107427906A CN201680019693.6A CN201680019693A CN107427906A CN 107427906 A CN107427906 A CN 107427906A CN 201680019693 A CN201680019693 A CN 201680019693A CN 107427906 A CN107427906 A CN 107427906A
Authority
CN
China
Prior art keywords
shell
casting method
automobile
producing
arenaceous shell
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
CN201680019693.6A
Other languages
Chinese (zh)
Inventor
埃米尔·托马斯·迪塞里奥
纪尧姆·马勒布
莱昂内尔·迪佩雷
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.)
Saint Jean Industries SAS
Original Assignee
Saint Jean Industries SAS
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 Saint Jean Industries SAS filed Critical Saint Jean Industries SAS
Publication of CN107427906A publication Critical patent/CN107427906A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/02Sand moulds or like moulds for shaped castings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D27/00Treating the metal in the mould while it is molten or ductile ; Pressure or vacuum casting
    • B22D27/04Influencing the temperature of the metal, e.g. by heating or cooling the mould
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21JFORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
    • B21J5/00Methods for forging, hammering, or pressing; Special equipment or accessories therefor
    • B21J5/002Hybrid process, e.g. forging following casting

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Mold Materials And Core Materials (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)
  • Forging (AREA)
  • Powder Metallurgy (AREA)
  • Body Structure For Vehicles (AREA)

Abstract

The present invention relates to a kind of arenaceous shell casting method for being used to produce the part used in automobile and aviation field, wherein, metal or alloy is poured into shell to produce part;The shell is forced and rapidly cooled down;And the part is removed.

Description

For producing the arenaceous shell casting method of the part used in automobile and aviation field
The present invention relates to the alloy of casting technology field, particularly aluminium, magnesium, copper or other similar materials.
More particularly, it relates to a kind of arenaceous shell casting method, for producing the portion used in automobile and aviation field Part.
Arenaceous shell casting method be well known to a person skilled in the art.
Including the use of the sand for being pre-coated with thermosetting resin, it is contacted with being heated to the mould plate of about 200 DEG C of temperature for it, Hardened on several millimeters of layer, form shell.Each shell corresponds to half module, is then polymerized, then glued.
In various arenaceous shell casting methods, it can mention and (polishing, hot tank, ice chest, warm up case, no cabinet etc.).
The casting method has some advantages, wherein the possibility for producing extremely complex geometry is may be mentioned that, And difference in functionality is integrated into the possibility on considered part, such as the exhaust manifold in the cylinder head of motor vehicles. It should be noted that other advantages, such as the weight saving of the part obtained.In addition, this method needs Low investment, and can Reduce the quantity of process operation.
On the contrary, considering low-down freezing rate, the part obtained by the arenaceous shell casting method has answers some With not always gratifying mechanical property in field.
Therefore, when these parts do not need good mechanical property, shell cast method will be particularly suitable for manufacturing The part of complicated geometry.
It will be apparent, however, that not only the geometry of part becomes to become increasingly complex, and the machinery of these parts Characteristic must reach high level, to meet code requirement.
From the point of view of prior art and such case, it is therefore important that arenaceous shell casting method can be improved, that can obtain The part with extremely complex geometry with good mechanical properties.
In order to overcome this problem, according to the present invention, arenaceous shell casting method is had been designed that, according to this method, In one embodiment:
- metal or alloy is poured into produce part in shell,
- the shell is forced and rapidly cooled down,
- realize the part decoring operation.
This method has in automobile and aviation field particularly advantageously to be applied, and for producing extremely complex part, is needed Mechanical property that will be very good.Arenaceous shell in known manner according to be suitable for the part to be obtained property (hot tank, ice chest, Warm case, 3D printing etc.) method manufacture.According to the characteristic for the part to be obtained, the thickness of shell is also suitable for quiet to reach metal Optimal compromise between Voltage force and interface resistance.
As noted, after casting metal or alloy, such as by quenching, by comprising the metal or the alloy still Arenaceous shell cooling in liquid or solidifying phase.In known manner, the quenching can pass through water, oil, air or any other Allow the means of this cooling.Quick and compulsory cooling means that housing is quenched when alloy is still liquid.As non- Restricted example, hardening heat are less than 100 DEG C.
Both operations of cast and cooling have two-fold advantage, the advantage, on the one hand, by establishing heat during quenching Gradient makes it possible to the orientation of solidification front, and on the other hand, increases freezing rate, and the therefore part of increase gained Mechanical property.
Then, the part simply needs to be subjected to conventional decoring operation, and the decoring can be chemical, hot or mechanical 's.
According to a further embodiment of the method according to the invention, it is no longer most that metal or alloy, which is poured into shell to produce, Back part, but preform.Obviously, therefore the profile of shell is suitable.Then, as previously noted, shell to force and Rapid mode is cooled, and realizes the operation of the decoring of preform.
According to the present invention casting method embodiment in, as be based on brand COBAPRESS known to method, make it is pre- into Shape base is subjected to the punching press and and forging operation of combination.Teaching of the COBAPRESS methods based on such as patent EP 0119365.
According to the characteristic of the present invention, the arenaceous shell casting method makes it possible to obtain than the arenaceous shell casting side according to prior art The much better mechanical property of mechanical property that method obtains, such as the following test result institute carried out with the metal or alloy of same type Show.
According to the shell moulded casting method of prior art:
SDAS:60-70μm
Rp0.2=200-220MPa
Rm=240-260MPa
A%=1-2%
According to the shell moulded casting method of the present invention:
SDAS:30-35μm
Rp0.2=220-260MPa
Rm=290-310MPa
A%=6-8%
Formula, wherein, SDAS corresponds to interdendritic gap, and Rp corresponds to elastic limit, and Rm corresponds to mechanical resistance, with And A% corresponds to elongation.
Can be seen that this method from the characteristic of the method according to the invention will be poured into arenaceous shell so that can be had There is the advantages of part of complex geometric shapes, decline with weight, process operation is reduced, while needs small investment, and is had Superperformance is combined, as shown in above-mentioned contrast test.It should also be noted that the application of COBAPRESS methods makes it possible to greatly Amount reduces porosity and skin effect.

Claims (2)

1. a kind of arenaceous shell casting method, for producing the part used in automobile and aviation field, wherein:
Metal or alloy is poured into the shell to produce part;
The shell is forced and rapidly cooled down;
Realize the operation of the decoring of the part.
2. a kind of arenaceous shell casting method, for producing the part used in automobile and aviation field, wherein:
Metal or alloy is poured into the shell to produce preform;
The shell is forced and rapidly cooled down;
Realize the operation of the decoring of the preform;
The preform is set to be subjected to the punching press and forging operation of combination.
CN201680019693.6A 2015-04-01 2016-03-16 For producing the arenaceous shell casting method of the part used in automobile and aviation field Pending CN107427906A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1552788 2015-04-01
FR1552788A FR3034332A1 (en) 2015-04-01 2015-04-01 PROCESS FOR SANDING CARAPLE MOLDING FOR THE PRODUCTION OF A PART IN THE AUTOMOTIVE AND AERONAUTICS FIELD
PCT/FR2016/050579 WO2016156692A1 (en) 2015-04-01 2016-03-16 Sand shell-moulding method for the production of a part for use in the automotive and aeronautics fields

Publications (1)

Publication Number Publication Date
CN107427906A true CN107427906A (en) 2017-12-01

Family

ID=53274664

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201680019693.6A Pending CN107427906A (en) 2015-04-01 2016-03-16 For producing the arenaceous shell casting method of the part used in automobile and aviation field

Country Status (10)

Country Link
US (1) US20180369906A1 (en)
EP (1) EP3277451A1 (en)
JP (1) JP2018516761A (en)
KR (1) KR20170132771A (en)
CN (1) CN107427906A (en)
CA (1) CA2981374A1 (en)
FR (1) FR3034332A1 (en)
MA (1) MA41836A (en)
MX (1) MX2017012495A (en)
WO (1) WO2016156692A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11958105B2 (en) 2022-03-09 2024-04-16 Honda Motor Co., Ltd. Rapid solidification of molded products

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4222429A (en) * 1979-06-05 1980-09-16 Foundry Management, Inc. Foundry process including heat treating of produced castings in formation sand
JPS57202943A (en) * 1981-06-05 1982-12-13 Kubota Ltd Manufacture of casting mold
CA1165967A (en) * 1980-08-29 1984-04-24 Anton Alt Process for casting metals, using sand-moulds in the form of shells
JPH02280956A (en) * 1989-04-21 1990-11-16 Kobe Steel Ltd Lost wax casting method
CN103286279A (en) * 2013-07-03 2013-09-11 韶关市富迪精密铸造有限公司 Novel casting technique of semitrailer brake drum
FR2995235A1 (en) * 2012-09-11 2014-03-14 Snecma FOUNDRY MODEL
FR3000910A1 (en) * 2013-01-17 2014-07-18 Snecma PROCESS FOR MANUFACTURING A PIECE BY LOST WAX FOUNDRY AND DIRECTED COOLING

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3373281D1 (en) * 1983-03-14 1987-10-08 Serio Thomas Di Method of producing pieces of aluminium or aluminium alloy
JP3008759B2 (en) * 1992-12-18 2000-02-14 株式会社リケンキャステック Hollow camshaft with oil hole in chill surface and its manufacturing method
US6622774B2 (en) * 2001-12-06 2003-09-23 Hamilton Sundstrand Corporation Rapid solidification investment casting

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4222429A (en) * 1979-06-05 1980-09-16 Foundry Management, Inc. Foundry process including heat treating of produced castings in formation sand
CA1165967A (en) * 1980-08-29 1984-04-24 Anton Alt Process for casting metals, using sand-moulds in the form of shells
JPS57202943A (en) * 1981-06-05 1982-12-13 Kubota Ltd Manufacture of casting mold
JPH02280956A (en) * 1989-04-21 1990-11-16 Kobe Steel Ltd Lost wax casting method
FR2995235A1 (en) * 2012-09-11 2014-03-14 Snecma FOUNDRY MODEL
FR3000910A1 (en) * 2013-01-17 2014-07-18 Snecma PROCESS FOR MANUFACTURING A PIECE BY LOST WAX FOUNDRY AND DIRECTED COOLING
CN103286279A (en) * 2013-07-03 2013-09-11 韶关市富迪精密铸造有限公司 Novel casting technique of semitrailer brake drum

Also Published As

Publication number Publication date
MA41836A (en) 2018-02-06
WO2016156692A1 (en) 2016-10-06
KR20170132771A (en) 2017-12-04
EP3277451A1 (en) 2018-02-07
MX2017012495A (en) 2018-07-06
FR3034332A1 (en) 2016-10-07
JP2018516761A (en) 2018-06-28
CA2981374A1 (en) 2016-10-06
US20180369906A1 (en) 2018-12-27

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Application publication date: 20171201

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