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Publication numberUS2966736 A
Publication typeGrant
Publication dateJan 3, 1961
Filing dateMar 27, 1958
Priority dateMar 27, 1958
Publication numberUS 2966736 A, US 2966736A, US-A-2966736, US2966736 A, US2966736A
InventorsRaymond J Towner, Jr John P Lyle
Original AssigneeAluminum Co Of America
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Aluminum base alloy powder product
US 2966736 A
Abstract  available in
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Claims  available in
Description  (OCR text may contain errors)

ALUMINUIVI BASE ALLOY POWDER PRODUCT Raymond J. Towner and John P. Lyle, In, New Kensington, Pa., assignors to Aluminum Company of America, Pittsburgh, Pa., a corporation of Pennsylvania No Drawing. Filed Mar. 27, 1 958, Ser. No. 724,232

'3 Claims. (Cl. 29-182) This invention relates to articles made from aluminum base alloy powders, and its is more particularly concerned with those products resulting from heating and working a compacted mass of atomized particles of an aluminum-zirconium base alloy.

Heretofore, compressed and sintered bodies of oxidecoated aluminum flake powders have been produced which possess unique strength properties at elevated temperatures. The particles of oxide distributed throughout the body appear to impart the unusual strength at elevated temperatures. The production of the oxide coated flakes is time consuming and consequently expensive. It has now been found, contrary to previous belief, that useful articles can be made from certain types of atomized aluminum alloy powders. As is well known, the automization process involves disintegrating a stream of molten metal with a jet of gas, such as compressed air, or by mechanical means. Very finely divided particles can be produced by this process which pass through a standard Tyler 100 mesh screen.

It is an object of this invention to provide articles having a high strength at elevated temperatures which are made from atomized particles of an aluminum base alloy containing zirconium as the principal added alloy component.

Another object is to provide such articles which do not require any preliminary thermal treatment to place them in condition for service at elevated temperatures.

Still another object is to provide an article made from atomized aluminum-zirconium alloy powder that does not depend upon the presence of oxide particles to impart strength at elevated temperatures.

These and other objects are achieved by atomizing a substantially iron-free aluminum base alloy containing not less than 70 percent by weight of aluminum and from 3.5 to 15% by weight of zirconium as the principal added alloy component and subsequently consolidating and working a mass of such atomized particles under the influence of heat and pressure. The resultant articles have a density closely approximating that of the alloy if cast; and in the worked condition they have a tensile strength of not less than 10,000 psi and a minimum yield strength of 9,000 psi. at 600 F. after a 100-hour exposure. These tensile and yield strength values are to be compared with those of some conventional Wrought heat treated aluminum base alloys that have been recommended for service at elevated temperatures. For example, a wrought aluminum base alloy nominally composed of aluminum, 12.2% silicon, 1.1% magnesium, 0.9% nickel and 0.9% copper in the solution heat-treated and age-hardened condition has a tensile strength of only 5,000 p.s.i. and a yield strength of 3,000 psi. after an exposure of 100 hours at 600 F. Under the same exposure conditions, a second well-known aluminum base alloy nominally consisting of aluminum, 4.5% copper, 1.5% magnesium and 0.6% manganese, when worked, solution heat treated and age hardened, has a tensile 2,966,736 rammed Jalll. 3, 1951 ice strength of 10,000 p.s.i. and a yield strength of 7,500 psi. The aluminum-zirconium powder products can be readily worked under the usual hot working conditions of temperature and pressure employed in fabricating conventional aluminum and aluminum base alloy articles. Furthermore, the hot-worked product can be cold worked to a limited extent, if desired. The fabricated alloy product can be placed in service without any preliminary thermal treatment. The strength of the wrought powder products at elevated temperatures is not influenced to any significant extent by the oxide film which coats the atomized particles.

The atomized alloy particles are preferably prepared by melting the alloy in the desired composition and projecting'it through a suitably designed nozzle with the aid of a compressed gas. The atomizing condition should be so adjusted that none or only a small proportion'of the particles are larger than mesh microns opening) and that the majority of the particles pass through a 200 mesh screen (74 microns opening). Articles produced in this manner generally have an irregular shape but for the most part are substantially equiaxed in dimensions and have an as-cast structure. The aluminum-zirconium constituent in the alloy is very finely divided as the result of the drastic chill associated with the atomization process. The surface of the particles are, of course, oxidized if the atomization has occurred in air orin some other oxidizing atmosphere, however, the oxide skin is very thin and the amount of oxide iritroduced ino the final product is too small to affect the properties thereof to any significant extent.

The zirconium content of the alloy should be between 3.5 and 15 by weight, as mentioned above, and prefer.- ably within the range of 5 to 10% to obtain the highest strength at elevated temperatures. If less than 3.5% is employed, the minimum strength is not achieved; and if more than 15% is present, the worked article has insuificient ductllity and may fracture under applied stresses. Zirconium is substantially insoluble in aluminum and whatever small proportion may be dissolved is too small to have any significant effect upon the properties of the atomized particles. It will, therefore, be appreciated that the matrix of the atomized particles consists of aluminum with a dispersion of finely divided aluminum-zirconium constituent distributed throughout the particle. The high strength at elevated temperatures appears to be controlled by the amount of the aluminum-zirconium constituent and the fineness of the dispersion.

The alloy may contain the usual impurities associated with aluminum, for example, silicon and iron. Generally, the silicon impurities should not exceed 1% and the iron content should not be more than about 1%. Other impurities, such as copper, may also be present in amount up to 1%. In view of the relatively small amount of iron impurity permitted in the alloy, the com position is referred to herein as being substantially ironfree.

For some purposes, it may be desirable to add one or more of the elements selected from the group composed of manganese, nickel, cobalt, chromium, vanadium, titanium, molybdenum and tungsten in amount of 0.1 to 10% by weight of each, the total not exceeding 10%. These elements act as hardeners and, like zirconium are substantially insoluble in the aluminum matrix. To obtain the properties attributable to the aluminum-zirconium constituents, the zirconium content in the alloy should exceed the total amount of any added hardener elements.

To make the wrought article from atomized powder, the powder may be initially formed into a compact that is subsequently worked or it may be charged directly to a compression chamber, such as an extrusion press cylinder, and be extruded therefrom after initial consolidation of the mass. The initial compact may be made by heating the powder to a temperature between 700 and 900 F. and applying a sufiicient pressure thereto for a long enough period of time to cause at least some Tensile specimens were cut from the extruded rod and tested without any preliminary thermal treatment, some at room temperature and others at 600 F. after a 100- hour exposure at that temperature. The composition of the alloys and the tensile strength at both room temperature and 600 F. are given in Table I below:

consolidation on the welding of the atomized particles. Pressures of 200 to 150,000 p.s.i. are satisfactory which are applied for varying periods of time from a minute or less to a few hours. Generally, a longer time is required where low pressures are employed. The compact may be left in the press cylinder and then extruded, or it may .be ejected, cooled, scalped, reheated to the hot working temperature and hot worked. In some cases it may be desirable to reheat the compact to temperatures as high as 1150 F. for hot working or to obtain adequate workability.

Where the powder is charged to a compression chamber, it may be initially heated to a temperature between 700 and 900 F. and introduced to the chamber or it may be charged cold and heated within the chamber. Alternatively, it may be heated to an intermediate temperature and brought to the desired temperature in the compression chamber. Where the powder is charged to a press cylinder, compacted and immediately extruded, it is generally convenient to compress the powder mass against a blind die and then substitute a die with the desired orifice therein. Although reference has been made to the extrusion of the powder mass, it is to be understood that it can be subjected to other types of hot working operations, such as rolling, forging or pressing, proyiding a suitable compact is initially produced. The hot working is preferably performed within the temperature range of 700 to 900 F.

Our invention is illustrated by the following examples wherein aluminum-zirconium atomized powders were consolidated and the product hot worked. The powders were of a fineness such that approximately 70%. passed through a 200 mesh screen and substantially all of the remainder passed through a 100 mesh screen. Each powder was charged to an extrusion press cylinder, preheated to 800 F. and compressed against the blind die under a pressure of 100,000 p.s.i. for a period of approximately one minute. In the course of charging and compressing the powder, the temperature of the compact reached 700 to 800 F. After the compact was thus formed, it was ejected from the cylinder, cooled, scalped, and reheated for hot working. These compacts were reheated to 850 F., inserted in an extrusion press cylinder heated to 800 F. and extruded to diameter rod.

It is apparent from the foregoing that the tensile and yield strengths of the alloys increase with an increase in the zirconium content. The tensile properties obtained at 600 F. are considerably higher than those of the two commercial aluminum base alloys referred to hereinabove. It is also significant that the high strengths at 603 F. were obtained without any preliminary thermal treatment of the worked powder product, such as solution heat treatment, which is a definite economic advantage.

Having thus described our invention and certain embodiments thereof, we claim:

1. A hot worked aluminum base alloy powder article free from aluminum oxide except as incidental impurity and having a maximum iron content of 1%, said hot worked alloy powder article being formed from atomized powder of alminum base alloy containing at least by weight of aluminum and from 3.5 to 15% by weight of zirconium as the essential component, the amount of said component exceeding the total of any hardening elements present in the alloy, said alloy being substantially free from elements which form a solid solution with aluminum, except as they occur as impurities, said hot worked article being characterized in the as-worked condition by tensile strength at 600 F. after a hour exposure of not less than 10,000 p.s.i. and yield strength not less than 9,000 p.s.i.

2. A hot worked aluminum base alloy powder article according to claim 1 wherein the zirconium content is 5 to 10% by weight.

3. A hot worked aluminum base alloy powder article according to claim 1 wherein the alloy also contains at least one hardening element selected from the group consisting of manganese, nickel, cobalt, chromium, vanadium, titanium, molybdenum and tungsten in amounts of 0.1 to 10% each, the total not exceeding 10% by weight, the zirconium content of said alloy exceeding the total amount of hardening elements added thereto.

References'Cited in the tile of this patent UNITED STATES PATENTS Notice of Adverse Decision In Interference N o. 92 and J. P. Lyle, Jr., Alumlnum base all oy powder product, final decision adverse to the patentees was rendered Jul y 9, 1963, as to claims 1 and 2. [Ofiieml Gazette September 3, 1963.]

in Interference ,634 involving Patent No. 2,966,736, R. J. Towner

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US2062329 *Apr 21, 1932Dec 1, 1936Aluminum Co Of AmericaThermal treatment of aluminum alloys containing copper
US2287251 *Jul 1, 1940Jun 23, 1942Jones William DavidManufacture of nonporous metal articles
US2809891 *Oct 12, 1954Oct 15, 1957Aluminum Co Of AmericaMethod of making articles from aluminous metal powder
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US3119684 *Nov 27, 1961Jan 28, 1964Dow Chemical CoArticle of magnesium-base alloy and method of making
US3119725 *Nov 27, 1961Jan 28, 1964Dow Chemical CoDie-expressed article of magnesium-base alloy and method of making
US3147110 *Nov 27, 1961Sep 1, 1964Dow Chemical CoDie-expressed article of aluminum-base alloy and method of making
US3147111 *Nov 27, 1961Sep 1, 1964Dow Chemical CoArticle of aluminum-base alloy
US3231344 *Dec 14, 1964Jan 25, 1966Brush Beryllium CoSintered intermetallic bodies composed of aluminum and niobium or tantalum
US3386820 *Jan 26, 1966Jun 4, 1968Olin MathiesonAluminum base alloy containing zirconium-chromium-manganese
US3388050 *Sep 7, 1965Jun 11, 1968Horizons IncAnodized aluminum alloy product
US3462248 *Jan 18, 1960Aug 19, 1969Kaiser Aluminium Chem CorpMetallurgy
US4715893 *Apr 4, 1984Dec 29, 1987Allied CorporationAluminum-iron-vanadium alloys having high strength at elevated temperatures
US4743317 *Jul 19, 1984May 10, 1988Allied CorporationAluminum-transition metal alloys having high strength at elevated temperatures
US4805686 *May 15, 1987Feb 21, 1989Allied-Signal Inc.An apparatus for forming aluminum-transition metal alloys having high strength at elevated temperatures
US5087301 *Dec 22, 1988Feb 11, 1992Angers Lynette MAlloys for high temperature applications
U.S. Classification75/249, 419/48, 419/28, 75/950, 420/552
International ClassificationC22C1/04
Cooperative ClassificationY10S75/95, C22C1/0416
European ClassificationC22C1/04B1