US1156093A - White-metal casting and the method of making same. - Google Patents

White-metal casting and the method of making same. Download PDF

Info

Publication number
US1156093A
US1156093A US84619714A US1914846197A US1156093A US 1156093 A US1156093 A US 1156093A US 84619714 A US84619714 A US 84619714A US 1914846197 A US1914846197 A US 1914846197A US 1156093 A US1156093 A US 1156093A
Authority
US
United States
Prior art keywords
casting
copper
castings
white
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 - Lifetime
Application number
US84619714A
Inventor
Charles Pack
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.)
DOEHLER DIE CASTING CO
Original Assignee
DOEHLER DIE CASTING 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 DOEHLER DIE CASTING CO filed Critical DOEHLER DIE CASTING CO
Priority to US84619714A priority Critical patent/US1156093A/en
Application granted granted Critical
Publication of US1156093A publication Critical patent/US1156093A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/02Alloys based on aluminium with silicon as the next major constituent
    • 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
    • Y10S148/00Metal treatment
    • Y10S148/902Metal treatment having portions of differing metallurgical properties or characteristics

Definitions

  • the invention relates to a white metal casting and the method by which said casting is made, and more particularly to a cast .ing made from an aluminum alloy.
  • a tough, sound casting of an aluminum alloy maybe made in metal molds by bringing the solidifying point nearer the eutectic point of the alloy through an increase in the percentage of copper over that which is generally recognized as being the highest percentage which can be successfully used in commercial castings, and by maintaining conditions throughout the casting process which will result in the chilling of the casting.
  • a casting made in accordance with my improved process or method has sufficiently high tensile strength; is free from cracks, and has a hard chilled superficial stratum imparting to the casting good wearing properties.
  • the invention consists primarily in a method of making finished white metal castings consisting in alloying from 80 to 91 per cent. of aluminum with from 20 to 9 per cent. of copper and delivering the molten alloy to a metallic mold maintained at a temperature below the fusing point of the alloy; and in the casting produced by this process; all as hereinafter set forth and described and more particularly pointed out Spe'cification of Letters Patent, Patented Oct, 12, 1915, Application filed June 19, 1914. Serial No; $46,197.
  • the alloy containing the highest percentage of copper which I have-been able to use successfully has been I composed of 20 parts of copper and 80 parts of aluminum.
  • the metal alloys which I employ are therefore richer. in copper than the alloy which is ordinarily recognized as being the the size and character of the casting to be i most desirable for commercial castings, and while theoretically an aluminum alloy containing from 20 to 9 per cent. of copper would be too brittle for commercial castings,
  • a finished, pressure die cast white metal casting composed of an alloy of from 80 to 91 parts of aluminum and from 20 to 9 parts of copper having a chilled outer stratum or surface.

Description

CHARLES PACK, OF NEW YORK, N. Y., ASSIGNOR TO DOEHLER DIE CASTIN COMPANY,
. v A CORPORATION OF NEW YORK.
WHITE-METAL CASTING AND THE METHOD OF MAKING SAME.-
1,156,993. No Drawing.
To all w/wm it may concern Be it known that I, CHARLES PACK, a citizen of the United States, residing at the borough of Brooklyn, city of New York,
lfi
county of Kings, and State of New York, have invented certain new and useful Improvements in White-Metal Castings and the Method of Making Same, of which the following is a specification.
The invention relates to a white metal casting and the method by which said casting is made, and more particularly to a cast .ing made from an aluminum alloy.
Heretofore in the art of making castings of aluminum alloys by. what is known as the pressure die casting process, great difiiculty has been encountered due in partto the high fusing point of'aluminum and of the ordinary commercial aluminum alloys; in part to the difficulties in producing a machinecapable of casting such alloys, and in part due to the high shrinkage of the alloy in the molds which resulted in the formation of superficial or deep-seated cracks in the finished castings.
I have discovered that a tough, sound casting of an aluminum alloy maybe made in metal molds by bringing the solidifying point nearer the eutectic point of the alloy through an increase in the percentage of copper over that which is generally recognized as being the highest percentage which can be successfully used in commercial castings, and by maintaining conditions throughout the casting process which will result in the chilling of the casting. I have discovered that a casting made in accordance with my improved process or method has sufficiently high tensile strength; is free from cracks, and has a hard chilled superficial stratum imparting to the casting good wearing properties.
The invention consists primarily in a method of making finished white metal castings consisting in alloying from 80 to 91 per cent. of aluminum with from 20 to 9 per cent. of copper and delivering the molten alloy to a metallic mold maintained at a temperature below the fusing point of the alloy; and in the casting produced by this process; all as hereinafter set forth and described and more particularly pointed out Spe'cification of Letters Patent, Patented Oct, 12, 1915, Application filed June 19, 1914. Serial No; $46,197.
tions of these metals varying accordingto the percentage of copper with castings.
larger in dimensions and more complicated in their configuration. The alloy containing the highest percentage of copper which I have-been able to use successfully has been I composed of 20 parts of copper and 80 parts of aluminum.
The metal alloys which I employ are therefore richer. in copper than the alloy which is ordinarily recognized as being the the size and character of the casting to be i most desirable for commercial castings, and while theoretically an aluminum alloy containing from 20 to 9 per cent. of copper would be too brittle for commercial castings,
nevertheless, I have found that if this alloy is cast under certain conditions, the commercial castings not only are lacking in that brittleness which would make them undesirable, if cast in sand, but-the quality of the castings is much superior v to castings of aluminum alloys containing a lower percentage of co dper. This I attribute to the fact that the solidifying point of the alloy is brought nearer the eutectic point by the use of a higher percentage of copper thus permitting casting at lower temperatures and reducing the shrinkage of the casting in the mold. Furthermore, by casting alloys composed of copper and aluminum, in which the percentage of the aluminum will range from 80 to 91 per cent. in metal molds maintained at a temperature below the eutectic point of the alloy, a chilled casting is secured and by reason of the reduced shrinkage of the metal, this casting is sound or without cracks. Furthermore, a rapid chillsolidification shrinkage so as to avoid excessive contraction of the" metal while in the in my method are readily handled in charging the mold, and that they flow readily in pouring. These conditions practically adapt an alloy of this characterto the production of finished castings or castings made to a fixed dimension or size. As l have heretofore stated in larger and more complicated castings, I increase the proportion of copper.
Inasmuch as by my experiments I have determined that the percentage of copper may be varied from 9 to 20 per cent., it is not my intention to limit the invention of any specific percentage of. copper, except that no less than 9 per cent. of copper shall be used and no more than 20 per cent, my invention contemplating the use of copper in proportions between these two limits.
Having described the invention what I claim as new and desire to have protected bv Letters Patent is 1. The herein described method of producing finished white metal castings consist-v ing in alloying from S0 to 91 parts of aluminum with from 20 to 9 parts of copper, and pouring the molten alloy in a metallic mold maintained at a temperature below the fusmes es ing point of the alloy, whereby the surface of the casting is chilled, and drawing the casting from the mold immediately following the solidification shrinkage whereby excessive contraction of the casting in the mold 1 is avoided.
2. Ihe herein described method of producing finished white metal castings consisting in alloying from 80 to 91 parts of aluminum drawing the casting from the mold immediately following the solidification shrinkage whereby excessive contraction of the casting.
in the mold is avoided.
3. A finished, pressure die cast white metal casting composed of an alloy of from 80 to 91 parts of aluminum and from 20 to 9 parts of copper having a chilled outer stratum or surface.
In witness whereof I hereunto afiix my signature in the presence of two subscribing witnesses this 10th day of June, 1914.
CHARLES PACK.
Witnesses C; CLAmse FRANCK, JUDITH PARDEE.
US84619714A 1914-06-19 1914-06-19 White-metal casting and the method of making same. Expired - Lifetime US1156093A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US84619714A US1156093A (en) 1914-06-19 1914-06-19 White-metal casting and the method of making same.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US84619714A US1156093A (en) 1914-06-19 1914-06-19 White-metal casting and the method of making same.

Publications (1)

Publication Number Publication Date
US1156093A true US1156093A (en) 1915-10-12

Family

ID=3224151

Family Applications (1)

Application Number Title Priority Date Filing Date
US84619714A Expired - Lifetime US1156093A (en) 1914-06-19 1914-06-19 White-metal casting and the method of making same.

Country Status (1)

Country Link
US (1) US1156093A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2572064A (en) * 1948-11-22 1951-10-23 Solar Aircraft Co Method of controlling shrinkage of castings
US2615199A (en) * 1945-05-15 1952-10-28 Welding Engineers Material treating apparatus
US3283376A (en) * 1962-02-23 1966-11-08 Hockin John Method of investment casting of ball bearings
US4090872A (en) * 1976-12-29 1978-05-23 The United States Of America As Represented By The Secretary Of The Air Force Aluminum base brazing alloy

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2615199A (en) * 1945-05-15 1952-10-28 Welding Engineers Material treating apparatus
US2572064A (en) * 1948-11-22 1951-10-23 Solar Aircraft Co Method of controlling shrinkage of castings
US3283376A (en) * 1962-02-23 1966-11-08 Hockin John Method of investment casting of ball bearings
US4090872A (en) * 1976-12-29 1978-05-23 The United States Of America As Represented By The Secretary Of The Air Force Aluminum base brazing alloy

Similar Documents

Publication Publication Date Title
US20200232069A1 (en) Aluminum alloy and die casting method
US1156093A (en) White-metal casting and the method of making same.
US2185348A (en) Aluminum base alloy
JPS59232649A (en) Metallic mold for molding plastic
US2280170A (en) Aluminum alloy
US927495A (en) Art of producing from foundry-iron a product having cutting and other properties of high-grade tool and high-speed steel.
US2795501A (en) Copper base alloys
US2280174A (en) Aluminum alloy
US1227174A (en) Aluminum alloy and in articles made therefrom.
US1166167A (en) Forming castings.
US2007008A (en) Copper zinc alloy containing silicon and iron
US1932843A (en) Aluminum alloys
US1932838A (en) Aluminum alloys
US2280169A (en) Aluminum alloy
US3744997A (en) Metallurgical grain refinement process
US2098081A (en) Aluminum alloy
US1932840A (en) Aluminum alloys
US1997494A (en) Aluminum-base alloy
US2280171A (en) Aluminum alloy
US2280177A (en) Aluminum alloy
US2280172A (en) Aluminum alloy
US1932844A (en) Aluminum alloys
US1572459A (en) Making castings of aluminum-silicon alloys
US1932841A (en) Aluminum alloys
US1671408A (en) Alloy