|Publication number||US2169441 A|
|Publication date||Aug 15, 1939|
|Filing date||Sep 23, 1937|
|Priority date||Jun 2, 1937|
|Publication number||US 2169441 A, US 2169441A, US-A-2169441, US2169441 A, US2169441A|
|Inventors||Winter Herbert, Fahrenhorst Wolfgang, Schmid Erich|
|Original Assignee||New Jersey Zinc Co|
|Export Citation||BiBTeX, EndNote, RefMan|
|Referenced by (7), Classifications (10)|
|External Links: USPTO, USPTO Assignment, Espacenet|
, Patented Aug. 15, 1939 UNITED STATES PATENT OFFICE WORKING ZINC ALLOYS Application September 23, 1937, Serial No. 165,322 In Germany June 2, 1937 4 Claims.
This invention relates to improvements in forming alloy metal objects and particularly to working zinc alloys containing from 10 to 20% aluminum to produce'an alloy object without im- 6 pairing the mechanical properties of the alloys.
Zinc generally is rolled at temperatures below 200 C. because its rollability is decreased at higher temperatures. The presence of other substances in the zinc generally decreases the rollability so that the rolling temperature must be increased in the case of zinc alloys. However, in practice, temperatures of 270 C. are not exceeded because this tends to bring about deterioration in the mechanical properties of the rolled alloys. Moreover, the temperature cannot be decreased below 180 C. on account of the high roll pressures then requisite. (A. Burkhardt, Technologie der Zinklegierungen, Berlin 1937, page 192.)
We have found, however, that aluminum-bearing zinc base alloys containing from 10 to 20% of aluminum can readily be rolled and otherwise worked at temperatures between 270 and 380 C.. and preferably at a temperature of about 340 C. Although the addition of aluminum generally decreases the rollability of zinc so far that at 25 medium temperatures only slight decreases in thickness are possible at each pass, it was unexpeetedly found that at temperatures about 270 C. the malleability of zinc-base alloys containing 10 to 20% of aluminum increased so suddenly and the work of deformation decreased so rapidly that in this range hot working is possible with heavy reductions at each pass. The mechanical properties of the resuting zinc alloy objects are not impaired by this method of treatment, but 3 instead are generally improved. Thus we have discovered that the malleability of an alloy consisting of 10 to 15% aluminum, 1.5 to 4% copper and .01 to .04% magnesium, the balance of the alloy being zinc having a purity of at least 99.98% (as described in co-pending United States application No. 159,711, filed August 18th, 1937, by Herbert Winter, and subsequently issued as United States Patent No. 2,102,869, on December 21, 1937) increases suddenly at temperatures above 270 C. and retains this increased mallea- -bility to. a temperature of about 380 C. At a temperature of 340 C. the malleability of this alloy is optimum.
Our invention, therefore, contemplates the improvement in the manufacture of zinc base objects which comprises working at a temperature ranging from 270 C. to 380 C., and preferably at 340 C. a zinc-base alloy containing from 10 55 to 20% aluminum, and more particularly an alloy consisting of 10 to 15% aluminum, 1.5 to 4% copper, .01 to .04 magnesium, the balance of the alloy being zinc having a purity of at least 99.98%. When such alloys are thus worked, there is no deterioration in their mechanical properties. On the contrary, the resulting metal objects possess high tensile and impact strengths, 6 improved machinability and high resistance to corrosion.
The curves A and B in the accompanying single figure illustrate the sudden increase in malleability of aluminum-bearing zinc base alloys that we have discovered. Two alloys A and B were subjected under constant load to difierent temperatures. In the figure the ordinates show the change of form suffered by the test rods under a compression of 7.5 kilograms per square millimeter. The change in form was measured in per cent decrease in the height of the pieces under compression. The abscissae in the figure show the temperature of deformation in degrees Centigrade. The compositions of the alloys investigated were as follows:
1. In the manufacture of zinc alloy objects, the improvement which comprises working at a temperature ranging from 270 to 380 C. an aluminum-bearing zinc base alloy containing from 10 to 20% aluminum.
2. In the manufacture of zinc alloy objects, the improvement which comprises working at a temperature of about 340 C. an aluminum-bear ing zinc base alloy containing from 10' to 20% aluminum.
3. In the manufacture of zinc alloy objects, the.improvement which comprises working .at a temperature ranging from 270 to 380 C. an alloyconsisting of 10 to 15% aluminum, 1.5 to 4% copper and 0.01 to 0.04% magnesium, the balance of the alloy being zinc having-a purity of at least 99.98%.
4. In the manufacture of a zinc alloy object, the improvement which comprises working at a temperature of about 340 C. an alloy consisting of 10 to 15% aluminumflfi to 4% copper, and 0.01 to 0.04 magnesium, the balance of the alloy being zinc having a purity of at least 99.98%.
HERBERT WINTER. WOLFGANG FAHRENHORBT.
|Citing Patent||Filing date||Publication date||Applicant||Title|
|US2516737 *||Jan 15, 1944||Jul 25, 1950||New Jersey Zinc Co||Hot-rolled binary zinc-titanium alloy|
|US3753791 *||Jan 4, 1971||Aug 21, 1973||Imp Smelting Corp Ltd||Heat-treatment of zinc/aluminium alloys|
|US3966505 *||Apr 30, 1975||Jun 29, 1976||Ball Corporation||High strength wrought zinc alloy|
|US3972743 *||Oct 20, 1975||Aug 3, 1976||Ball Corporation||High strength, stable zinc-aluminum alloy|
|US4599279 *||Oct 1, 1984||Jul 8, 1986||Ball Corporation||Zinc alloy for reducing copper-zinc diffusion|
|US6383657||Dec 18, 2000||May 7, 2002||Alltrista Zinc Products||Aluminum clad zinc bimetallic coin planchet|
|US20040173294 *||Mar 22, 2004||Sep 9, 2004||Grillo-Werke Ag||Use of zinc alloys|
|U.S. Classification||72/364, 148/441, 72/700|
|International Classification||C22F1/16, C22C18/04|
|Cooperative Classification||C22C18/04, C22F1/165, Y10S72/70|
|European Classification||C22F1/16B, C22C18/04|