US856392A - Aluminium alloy. - Google Patents

Aluminium alloy. Download PDF

Info

Publication number
US856392A
US856392A US35198507A US1907351985A US856392A US 856392 A US856392 A US 856392A US 35198507 A US35198507 A US 35198507A US 1907351985 A US1907351985 A US 1907351985A US 856392 A US856392 A US 856392A
Authority
US
United States
Prior art keywords
aluminium
aluminium alloy
alloy
copper
proportions
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
US35198507A
Inventor
Alexandre Chambaud
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 US35198507A priority Critical patent/US856392A/en
Application granted granted Critical
Publication of US856392A publication Critical patent/US856392A/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
    • C22C21/10Alloys based on aluminium with zinc as the next major constituent

Definitions

  • the object of this invention is a new aluminium alloy and the process employed in its manufacture.
  • the new metal is a white silvery compound, of which the density does not exceed 2,7. Very elastic malleable and ductile, and more tenacious than copper, this metal beats out, embosses, hammers, bends, wiredraws, and welds very easily. It can be worked without the use of special tools.
  • This alloy furthermore possesses reat tensile strength and is not substantial y oxidizable in air or water. It is particularly useful in cases where 1t is exposed to the action of seawater, which 1t has been found to success- I fully resist. In addition the new metal is not seriously attacked by any acid with the exception of hydrochloric acid.
  • the following process is employed; about 20% of the aluminium to be employed is first melted down in a suitable bath and when the temperature has reached about 750 C. the copper is added 3 when the fusion of this last metal is complete the zinc is added and afterward the iron. After the complete fusion of this mixture the remaining 80% of the aluminium is added.
  • the fluid mass is then withdrawn from the fire and the magnesium is incorporated with it.
  • aluminium alloy having the following proportions. Aluminium about 99,020%, iron 0,310%, zinc 0,010%, magnesium 0,041%, copper 0,610%, substantially as described.

Description

'tions of its constituent materials.
UNITED STATES PATENT OFFICE.
ALUMINIUM ALLOY.
No. 856,392. Specification of Letters Patent. Patented June 1 1, 1907.
Application filed January 12, 1.907. Serial No. 351,985.
To a'ZZ whom it may concern:
Be it known that I, ALEXANDRE CHAM- BAUD, residing in Paris, France, 9 Rue St. Georges, have invented certain new and useful Improvements Relating to Aluminium Alloys.
The object of this invention is a new aluminium alloy and the process employed in its manufacture.
Numerous alloys of aluminium are already known but the alloy which is the subject of this invention is distinguished from those hitherto obtained by the nature and propor- These proportions are of considerable importance in that they give to the alloy particular and eminently characteristic qualities which are indicated below. The proportions of its constituent elements are as follows :--Aluminium 9'9,020%, iron 0,310%, zinc 0.010%, magnesium 0,041%, copper 0,610%. The remaining 0,009% is comprised of the silica which is found in the aluminium.
The above proportions have appeared to give the best practical result, but the right is reserved to modify these proportions within certain measures without exceeding the limits of the invention. a
The new metal is a white silvery compound, of which the density does not exceed 2,7. Very elastic malleable and ductile, and more tenacious than copper, this metal beats out, embosses, hammers, bends, wiredraws, and welds very easily. It can be worked without the use of special tools. This alloy furthermore possesses reat tensile strength and is not substantial y oxidizable in air or water. It is particularly useful in cases where 1t is exposed to the action of seawater, which 1t has been found to success- I fully resist. In addition the new metal is not seriously attacked by any acid with the exception of hydrochloric acid.
To obtain the metal, the following process is employed; about 20% of the aluminium to be employed is first melted down in a suitable bath and when the temperature has reached about 750 C. the copper is added 3 when the fusion of this last metal is complete the zinc is added and afterward the iron. After the complete fusion of this mixture the remaining 80% of the aluminium is added.
The fluid mass is then withdrawn from the fire and the magnesium is incorporated with it.
Having now particularly described and ascertained the nature of my said invention and in what manner the same is to be performed, I declare that what I claim is:
l 1. An aluminium alloy having the following proportions. Aluminium about 99,020%, iron 0,310%, zinc 0,010%, magnesium 0,041%, copper 0,610%, substantially as described.
2. The process of manufacture of aluminium alloy consisting in first melting about 20% of the aluminium to be employed and when the temperature has reached about 750 C. in addin copper and when the fusion of this last metal is complete in adding zinc and afterward iron and after the complete fusion of this mixture, in adding the remaining 80% of the aluminium and finally in incorporating magnesium when the fluid mass is withdrawn from the fire as substantially described.
ALEXANDRE CHAMBAUD.
Witnesses:
LOUIS TAILFER, FRANooIs DU BOISROUVRAY.
US35198507A 1907-01-12 1907-01-12 Aluminium alloy. Expired - Lifetime US856392A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US35198507A US856392A (en) 1907-01-12 1907-01-12 Aluminium alloy.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US35198507A US856392A (en) 1907-01-12 1907-01-12 Aluminium alloy.

Publications (1)

Publication Number Publication Date
US856392A true US856392A (en) 1907-06-11

Family

ID=2924847

Family Applications (1)

Application Number Title Priority Date Filing Date
US35198507A Expired - Lifetime US856392A (en) 1907-01-12 1907-01-12 Aluminium alloy.

Country Status (1)

Country Link
US (1) US856392A (en)

Similar Documents

Publication Publication Date Title
US856392A (en) Aluminium alloy.
US3759758A (en) High strength aluminum casting alloy
US1907219A (en) High strength hot working copper nickel zinc alloy
US2121194A (en) Welding rod
US3249429A (en) Tantalum brazing alloy
US1933390A (en) Copper zinc silicon alloys
US1224362A (en) Aluminum-calcium alloy and process of making the same.
US2371531A (en) Magnesium base alloy
US1239785A (en) Soldering compound.
US2075014A (en) Copper silicon alloys
US2075004A (en) Copper-silicon-zinc-tin-lead alloy
US2157149A (en) Copper base alloy
US652833A (en) Alloy and process of making same.
US2153978A (en) Cupro-nickel alloys
US2279712A (en) Magnesium base alloy
US1457289A (en) Copper and zinc alloy
US2052139A (en) Fabricated structure and method of making the same
US2221255A (en) Magnesium base alloy
US2231940A (en) Alloy
US1104369A (en) Aluminum alloy.
US2270190A (en) Magnesium base alloy
US3507032A (en) Method of improving the stress corrosion resistance of a susceptible aluminum alloy
US2189834A (en) Aluminum alloy
US2230969A (en) Alloys
US1007548A (en) Aluminium bronze.