US1704384A - Casting magnesium and alloy thereof - Google Patents

Casting magnesium and alloy thereof Download PDF

Info

Publication number
US1704384A
US1704384A US81304A US8130426A US1704384A US 1704384 A US1704384 A US 1704384A US 81304 A US81304 A US 81304A US 8130426 A US8130426 A US 8130426A US 1704384 A US1704384 A US 1704384A
Authority
US
United States
Prior art keywords
mold
casting
metal
cavity
core
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 - Lifetime
Application number
US81304A
Inventor
John A Gann
John E Hoy
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.)
Dow Chemical Co
Original Assignee
Dow Chemical Co
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 Dow Chemical Co filed Critical Dow Chemical Co
Priority to US81304A priority Critical patent/US1704384A/en
Application granted granted Critical
Publication of US1704384A publication Critical patent/US1704384A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D15/00Casting using a mould or core of which a part significant to the process is of high thermal conductivity, e.g. chill casting; Moulds or accessories specially adapted therefor
    • B22D15/02Casting using a mould or core of which a part significant to the process is of high thermal conductivity, e.g. chill casting; Moulds or accessories specially adapted therefor of cylinders, pistons, bearing shells or like thin-walled objects
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S164/00Metal founding
    • Y10S164/08Piston

Description

March 5, 1929. J. A. GANN ET AL 1,704,384
CASTING MAGNESIUM AND ALLOY THEREOF Filed Jan. 14, 1926 I Nl 'ENTOR Patented Mar. 5, 19253.l
JOHN A. GANN AND' JOHN E. HOY, OF MIDLAND, MICHIGAN, ASSIQNOBS T0 TH PATENT oFFlcE.
CHEMICAL COMPANY, OF MIDLAND, MICHIGAN, A CORPORATIN 0F MICHIG CASTING MAGNESIUM AND ALLOY Trimmer.
Application led January 14,` 1926. Serial No. 81,304.
While the present improvements relate. more particularly to the casting of magnesium and so-called light metal alloys 1n which magnesium is the predominant constituent, it will be understood that the improved method and apparatus involved are equally adaptable for the casting of any similar prevent the cast article from bein'g prop-l erly finished when removed from the mold, a certain loss of metal, due to oxidation, is 1n# evitable, and of course the cleaner the casting, the more easily may the finishing operation be carried out;
It has heretofore been proposed to overcome these difficulties specifically in casting magnesium and alloys containing the same by dusting the mold prior to casting the metal with sulphur or equivalent material capable of giving off in contact with the 'molten' metal a vapor which is more easily oxidizable than magnesium. This procedure, however, has the objection that it is obviously difHcult correctly to gauge the amount of sulphur or equivalent material thus used, and particularly if an excess' is applied to the surface either of the mold proper or the core, so much vapor may be generated that some of 1t becomes entrapped during the period that the metal 1s solidifying, the result being blow-holes or surface shrinks in the casting. Furthermore, the sulphur or equivalent material has to be applied or dusted onto the mold each time a fresh casting is poured and -1n any case the method in question is obviouslylnot applicable wherea metal mold is employed, because of the non-porous character `of the latter. Y.
By the present improved construction of mold we make it possible to supply to the mold cavity an inert or reducing gas, specically sulphur dioxide, vin an amountl suf- .the offset 4 in the mold w ficient to displace the air normally filling a continuous supply of such inert or reducing gas while a succession of castingsis being poured in the same mold.
To the accomplishment of the foregoing and related ends, the invention, then, consists of the steps and means hereinafter fully describedand particularly pointed out in the claims, the annexed drawing and the following description setting forth in detail certain means and one mode of carryin out the invention,` such disclosed means an mode illustrating, however, -but one of various ways in which the principle ofthe invention may be used.
In said annexed draw-ing:-
The single figure there appearing is a central vertical section through a mold con. structed and arranged to carry out our improved method.
The mold thus illustrated is specifically designed for casting a iston for an internal combustion engine or ike hollow article of general cylindrical form. The mold part 1 will preferably be of metal, e. g. cast iron, as is commonly used in foundries at vthe present time for casting light metal pistons, but such mold may be made of sand, if desof sired. Such permanent mold has a cavity 2 adapted to volatilize by the heat of the mold and give ofl' an inert gas that is heavier than air or that may be ignitedand give off such a gas. The core 6, which may be either of sand or of collapsible metal parts, is of course separable from themold l and is formed with an enlargement 7 at its upper end ada ted to fit the enlarged portion 3 of the mol cavity, the shoulder 8 between such enlargement and the core plroper resting on en the parts areproperly assembled. y
'When thus 5 in place, such shoulder will seal off .the chamber 5 save for a slit-like vent opening or openings 41() which are so narrow that molten metal will solidify bein which the casting is to be formed.
In operat-ion, atte;` the mold part 1 has,
beenpreliminarily warmed up, the gas producing material hereinbefore referred to is placed in the chamber 5,'or a small quantity of sulphur is-strewn around in such chamber and ignited. Then as the core 6A is put in place, the gas generated from such material is trapped and forced out through the vent l() into the cavity 2, expelling the air through the gate opening 12 and spnue 11. When this has been accomplished, the moltenl metal is then poured into the mold in the usual manner. The material 13 in the chamber can be replenished from time to time in the case where a permanent mold part 1 is used. As an example of a material that will generate a suitable inert gas as a result of the heat derived from the mold, para dichlor-benzol may be named, although this material has the disadvantage that the gases generated are more obnoxious than the sulphur dioxide formed by burning sulphur, as"also naphthalene, carbon tetrachloride, and fuel oil. In no case, however, does the material used thus to generate the neutral or reducing gas 'come into direct contact with the surfaces There is, accordingly, no danver of-an excessive amount oflsuch gas being generated with resultant formation .of blow-holes or surface shrinks.
Other modes of applying the principle vo our invention may be employed instead of the one explained, change being made as regards the means and the steps herein dis- I dizable metal, the combination .of separable moldparts', one of said parts having'a chamber normally open to the atmosphere wherein y a non-oxidizing as may be generated, and
`the other partfbem-g adapted, when in position for eastingrto' seal oil?` such chamber save for a vent into the-. i`no1d cavity.
2. In apparatus for casting a readilymxidizable metal, the combination of a separable mold and core, said mold having a chamber substantially encircling the `cavity vtherein and normally open to' the atmosphere and said core having a portion to seal olf such chamber save for a communicating vent.
'3. In apparatus for casting a readily oxidizablc metal, the combination of a separable mold and core,said mold having a chamber substantially encircling the cavity therein and normally open to the atmospbereand said'core .having a portion arranged, when said core is in position for cast-ing, to seal -otf such chamber save for a slit-like vent, the latter being so narrow that molten metal will solidify before lowing therethrough into such chamber.
4. Inapparatus for casting pistons and other .articles of general cylindrical shape from a readily oxidizable metal, the combination of a separable mold and core, said mold having a cavity conforming to the exterior shape of the article to be cast and an.
enlargedspace continuous with the upper end of such cavity, whereby a lateral offset is provided substantially encircling such cavity, with a depression in such offset adapted to receive and contain a gas-generating material, and said core having a lat-eral shoulder fitted to such enlarged space in said mold to seal oft' such depression@ save for, a slit-likevent opening into .the mold cavity.
5. In apparatus. for casting -pistons and other articles of general cylindrical shape from a readily oxidizable metal, theconibination of a separable mold and core, said mold having a cavity conforming to the ex terior shape of the article to be cast and an enlarged space continuous with the upper end of such cavity, whereby a lateral o'set is. provided substantially encircling such cavity, with a depression' in such offset adapted to receive and contain a gas-generat-l ing material, and said core having a lateral shoulder Vfitted to such enlarged space in said-mold to seal Voil` such depression save' foi` a slit-like vent opening into the mold cavit so narrow that molten metal will solidly before flowing therethrough.
Signed by us this 7th day of J anuary, 1926-.
*JOHN AQ GANN. JOHN E. Hor.
US81304A 1926-01-14 1926-01-14 Casting magnesium and alloy thereof Expired - Lifetime US1704384A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US81304A US1704384A (en) 1926-01-14 1926-01-14 Casting magnesium and alloy thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US81304A US1704384A (en) 1926-01-14 1926-01-14 Casting magnesium and alloy thereof

Publications (1)

Publication Number Publication Date
US1704384A true US1704384A (en) 1929-03-05

Family

ID=22163330

Family Applications (1)

Application Number Title Priority Date Filing Date
US81304A Expired - Lifetime US1704384A (en) 1926-01-14 1926-01-14 Casting magnesium and alloy thereof

Country Status (1)

Country Link
US (1) US1704384A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2893084A (en) * 1953-10-16 1959-07-07 Sulzer Ag Casting mold and method of casting carbon-containing alloys

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2893084A (en) * 1953-10-16 1959-07-07 Sulzer Ag Casting mold and method of casting carbon-containing alloys

Similar Documents

Publication Publication Date Title
US4240492A (en) Process of forming multi piece vaporizable pattern for foundry castings
EP0092690A1 (en) Molding core for casting engine cylinder block
US2752653A (en) Method of and dies for forming hollow expendable patterns for casting
DE2453584A1 (en) PRECISION MOLDING PROCESS
US3259949A (en) Casting method
US1704384A (en) Casting magnesium and alloy thereof
US3724531A (en) Mold for casting single crystal articles
US2081304A (en) Sectional mold
US3041688A (en) Shell mold for investment castings and method of making same
US1543657A (en) Mold
JPS63183744A (en) Production of porous casting
US1772490A (en) Casting magnesium and alloys therefor
US1492694A (en) Double coating for permanent molds
US3404724A (en) Method of casting in a shell molding
US1401577A (en) Art of molding
US1833128A (en) Chill for sand molds
US2832112A (en) Shell mold casting and method
US1570802A (en) Means for preventing adherence of cast metal to the mold
JPS597460A (en) Precision casting method
US2135537A (en) Method of casting
US1189391A (en) Art of casting metal.
JPS5545556A (en) Casting method
US1525547A (en) Motor valve and method for making the same
SU49074A1 (en) Method of casting steel inserts with lead bronze
US1518271A (en) Process of making permanent metal molds from a permanent master positive mold