US1555959A - Light alloy and process of manufacture of the same - Google Patents

Light alloy and process of manufacture of the same Download PDF

Info

Publication number
US1555959A
US1555959A US697395A US69739524A US1555959A US 1555959 A US1555959 A US 1555959A US 697395 A US697395 A US 697395A US 69739524 A US69739524 A US 69739524A US 1555959 A US1555959 A US 1555959A
Authority
US
United States
Prior art keywords
alloy
manufacture
magnesium
copper
aluminium
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
US697395A
Inventor
Fresneau Andre Angelo
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to US697395A priority Critical patent/US1555959A/en
Application granted granted Critical
Publication of US1555959A publication Critical patent/US1555959A/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
    • C22C21/12Alloys based on aluminium with copper as the next major constituent

Definitions

  • My invention has. for its object a light alloy formed of aluminium, copper, nickel, zinc and magnesium and having approximately the following percentage composition:
  • the melted alloy is well stirred, and is then deoxidized by adding 2 percent of baryta.
  • the resulting alloy is remarkably light, its density being in fact about 2.9, but at the same time it possesses great strength.
  • a metal alloy the composition whereof is substantially: aluminium 93.3, copper 3.4, nickel 1, zinc 1.8 and magnesium 0.5.

Description

Patented Qct. 6, 1925.
UNITED STATES PATENT OFFICE.
ANDRE ANGELO rnnsmu, or AUBERVILLIERS, FRANCE.
LIGHT A LLOY AND PROCESS OF MANUFACTURE OF THE SAME.
NqDrawing.
To all whom it may concern:
Be it known that I, ANDRE ANGELO FRESNEAU, citizen of the French Republic,
residing at Aubervilliers,- Seine, in the zinc, magnesiuln and manganese, and the Y alloy composed of aluminium, copper, nickel and magnesium. These light alloys have in all cases a great strength, this being variable according as the metal is rolled, drawn, cast or forged.
My invention has. for its object a light alloy formed of aluminium, copper, nickel, zinc and magnesium and having approximately the following percentage composition:
Aluminium 93.32 Copper 3. 4 -Nickel- 1.0 Zinc 1.78 Magnesium O. 5
For the manufacture of the said alloy I proceed as follows: I first prepare a ternary alloy composed of:
Copper 54.5 Nickie-1 16.5 Zinc 29.0
The melted alloy is well stirred, and is then deoxidized by adding 2 percent of baryta.
I then take 6.5 kilograms of the melted and deoxidized alloy and pour the same into a crucible containing 100 kilograms of aluminium in fusion. The mixture is well stirred, and after about 5 minutes I add 500 grams of magnesium. I then add, while continuing the stirring, 2 kilograms of caustic soda which has been previously dried at a red heat. The soda renders the alumina soluble and the bath is thus made fluid; the latter is skimmed olf and is then ready for casting, which is carried out at about 7 00 C., this temperature being variable by some 15 either way.
The resulting alloy is remarkably light, its density being in fact about 2.9, but at the same time it possesses great strength.
Application filed Marchfi, 1924. Serial No. 697,395.
After 1% hours thermic treatment at about 530 (3., followed by a rapid immer- I sion in Water at about 25 (within 5- more or less) to obtain a complete cooling, and a subsequent tempering in boiling Water at 100, my alloy has the following tensile strength:
.17 to 19 kgs. per m/m for cast metal, 45 to 5'.) kgs. per m/m for drawn metal, 42' to 48 kgs. per m/m for rolled metal, 46 to 52 kgs. per m/m for forged metal.
The corresponding elongations are:
8 to 11 per cent for cast metal, 17 to 22 h per cent for, drawn metal, 17 to 22 per cent for rolled metal, 16 to 22 per cent for forged metal. a
It should also be observed that the heating and cooling curves for the said alloy show no particular features nor critical points.
Obviously, I may vary the proportions of the constituent metals of the said alloy to a-slight degree, without departing from the scope of the invention.
Having. now described my invention, what I claim as new and desire to secure by Letters Patent is:
1. A metal alloy the composition whereof is substantially: aluminium 93.3, copper 3.4, nickel 1, zinc 1.8 and magnesium 0.5.
2. The process of manufacture of a metal alloy containing aluminium, copper, nickel, zinc and magnesium which consists inpreparing a ternary alloy containing the whole amount of copper, nickel and zinc, pouring said melted ternary alloy into the melted mass of aluminium and then adding the desired quantity of magnesium.
3. The process of-manufacture of a metal alloy containing aluminium, copper, nickel, zincjand magnesium which consists in preparing a ternary alloy containing the whole amount of copper, nickel and zinc, pouring said melted ternary alloy into the melted mass of aluminium, then adding the desired quantity of magnesium, addingsubsequently anhydrous caustic soda and skimming the slag oil the bath. I
4. The process of manufacture of a metal alloy the composition whereof is substantially: aluminium 93.3, copper 3.4, nickel 1, zinc 1.8 and magnesium, which consists in preparing a ternary'alloy containing the whole amount of copper, nickel and zinc, pouring said melted ternary alloy into the melted mass of aluminium, then adding the corresponding quantity of magnesium and baryta to said ternary alloy'for deoxidi zing casting the alloy thus obtained at a temperthe same, pouring said deoxidized ternary 10 ature substantially equal to 700 C. alloy into' the melted mass of aluminium 5. The process of manufacture of a metal and then adding the desired quantity of 5 alloy containing aluminium, copper, nickel, magnesium zinc and magnesium which consists in pre- I11 est p y lI IBQf I have Signed my paring a ternary alloy containing the whole name thls speclficatlonamount of copper, nickel and zinc, adding ANDRE ANGELO FRESNEAU.
US697395A 1924-03-06 1924-03-06 Light alloy and process of manufacture of the same Expired - Lifetime US1555959A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US697395A US1555959A (en) 1924-03-06 1924-03-06 Light alloy and process of manufacture of the same

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US697395A US1555959A (en) 1924-03-06 1924-03-06 Light alloy and process of manufacture of the same

Publications (1)

Publication Number Publication Date
US1555959A true US1555959A (en) 1925-10-06

Family

ID=24800978

Family Applications (1)

Application Number Title Priority Date Filing Date
US697395A Expired - Lifetime US1555959A (en) 1924-03-06 1924-03-06 Light alloy and process of manufacture of the same

Country Status (1)

Country Link
US (1) US1555959A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6368427B1 (en) 1999-09-10 2002-04-09 Geoffrey K. Sigworth Method for grain refinement of high strength aluminum casting alloys
US6645321B2 (en) 1999-09-10 2003-11-11 Geoffrey K. Sigworth Method for grain refinement of high strength aluminum casting alloys

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6368427B1 (en) 1999-09-10 2002-04-09 Geoffrey K. Sigworth Method for grain refinement of high strength aluminum casting alloys
US6645321B2 (en) 1999-09-10 2003-11-11 Geoffrey K. Sigworth Method for grain refinement of high strength aluminum casting alloys

Similar Documents

Publication Publication Date Title
US4239535A (en) Magnesium alloys
NZ205764A (en) Aluminium alloys containing lithium,magnesium and zinc and uses thereof
US1558066A (en) Method of making light metal alloys
US1555959A (en) Light alloy and process of manufacture of the same
US2578098A (en) Aluminum base alloy
US2085697A (en) Method for treating aluminum and aluminum alloys
US2031486A (en) Process for the production of alloys of the alkaline earth metals with lead or other metals
US3355281A (en) Method for modifying the physical properties of aluminum casting alloys
US1387900A (en) Alloy
US1352322A (en) Metallic alloy and method of making same
US1490696A (en) Zinc alloy
US1261987A (en) Method of making aluminum-alloy articles.
US1792944A (en) Copper-silicon alloy
US2098081A (en) Aluminum alloy
US1412280A (en) Aluinum alloy
US1848816A (en) Robert s
US2086604A (en) Copper-titanium-silicon alloys
US1227174A (en) Aluminum alloy and in articles made therefrom.
US2214432A (en) Aluminum alloy containing copper, iron, and columbium
US2185453A (en) Method of heat treating magnesium base alloys
US1937934A (en) Metallurgical process
US2060919A (en) Nonferrous metal
US1960916A (en) Aluminium alloy
US1707753A (en) Malleable iron alloy
US2148151A (en) Copper alloy