MANUFACTURING OF A STABLE CARBIDE-CONTAINING ALUMINIUM ALLOY BY MECHANICAL ALLOYING

Abstract: Aluminum-base alloys and a method of preparing aluminum-base alloys by mechanical alloying in the presence of a carbidiferous processing aid wherein a strong carbide former such as titanium is included so as to produce carbides in the final alloy more thermally stable at temperatures in excess of 100°C than Al₄C₃.

Description: The present invention is concerned with the use of aluminium-base alloys at temperatures in excess of 100°C. PRIOR ART AND PROBLEM High strength aluminum-base alloys i.e., alloys containing greater than 50% by weight aluminum have been made by mechanical alloying techniques which alloys have useful mechanical characteristics at room temperature. These alloys depend in part for strength on age hardened and/or work hardened internal structures and, in part, on the formation, in-situ, of a fine dispersion of aluminum carbide (A1₄C₃) and aluminum oxide by reaction of aluminum with the break-down products of a carbon-containing processing aid (e.g., stearic acid) used in the mechanical alloying process. On exposure to temperatures above about about 100°C, age-hardened structures and/or work hardened tend to soften and at higher temperatures the dispersion of A1₄C₃ in the alloy tends to coarsen, thus lessening the contribution of carbide to the strength of the alloy. In consequence, aluminum-base alloys of the prior art as produced by mechanical alloying are not generally suitable for use in the temperature range of 100°C to 480°C. The present invention has for its object, the provision and production of mechanically alloyed, aluminum-base alloys suitable for use in this temperature range. EP-O 147 769 describes an aluminum-base alloy that is dispersion strengthened by, inter alia, a carbide. The alloy, which is formed by mechanical alloying of a powder, can also contain iron and when it does so, Co, Ni, Cr, Mn, Ce, Ti, Zr and Mo may also be added to improve formability or workability of the powder. The specification contains no indication of how carbide coarsening can be avoided. GENERAL DESCRIPTION OF THE INVENTION Broadly, the present invention is based on the finding that by including in the mechanical alloying charge for an aluminum-base alloy, a material in microfine dipersion or readily transformable to a microfine dispersion which comprises or contains an element from the group of titanium, niobium, zirconium and vanadium, along with aluminum and other alloying elements, then when such a charge is mechanically alloyed in the presence of a carbon-containing processing aid, an alloy containing aluminum carbide is produced that is resistant to coarsening at temperatures above 100°C and even above 370°C. The present invention covers the use of such an alloy at temperatures in excess of about 100°C without coarsening of the aluminum carbide as defined in claims 1 to 6. The present invention also relates to a process for producing such an alloy that is substantially free of iron, as defined in claims 7 to 10 For purposes of this specification and claims the term "mechanical alloying" is employed to mean a process in which a charge of powder ingredients is subjected to impacts by an impacting medium so as to cause a multiplicity of particle weldings and fracturing until the charge is converted to an essentially uniform powder product. While attritors and horizontal ball mills are most often used for mechanical alloying, for purposes of the invention the particular apparatus used is immaterial. The product of mechanical alloying is thereafter compressed, sintered and worked as disclosed hereinafter. Again for purposes of the present specification and claims, the term "microfine dispersion" means a dispersion having particle sizes significantly below 5 micrometers (µm) average particle size and more preferably below about 1 µm in particle size. Additions of Ti, Nb, Zr and V (hereinafter called the 'addition elements') to the mechanical alloying charge can thus be in the form of dust or fume size particles of elements or compounds or alloys of the above elements or in the form of larger size, brittle materials (e.g., intermetallic compounds) which are readily broken down by mechanical impact in the mechanical alloying process to particles less than 1 µm or, more preferably, less than 0.8 µm in average dimension. Carbon-containing processing aids useful in mechanical alloying of aluminum-base alloys include stearic acid, methanol, graphite, oxalic acid, etc. It is advantageous to employ in the mechanical alloying charge a powder of a brittle intermetallic compound containing the addition element. Examples of such brittle, intermetallic compounds are VAl₃, TiAl₃, ZrAl₃ , NbAl₃, FeTi, Fe 0.85 Mn 0.15 Ti, Ti₂Ni, Ti₅Si₃, Zr₂Si and TiFe₂. It is also advantageous to employ the addition elements in the form of rapidly solidified particulates of alloys of the elements and other metals. Such particulates may have the characteristics of amorphous "glassy" alloys or supersaturated solid solution alloys or may contain almost microscopically indistinguishable crystallites of a solid phase or phases normally existing at or just below the liquidus of the particular alloy system employed. Powder charges in accordance with the present invention are all processed by mechanical alloying. This technique can be a high energy milling process, which is described in U.S. patents 3,591,362, 3,740,210 and 3,816,080 (among others). Briefly, the aluminum-base alloy is prepared by subjecting a powder charge to dry, high energy milling in the presence of a grinding medium, e.g., balls, and a process control agent, under conditions sufficient to comminute the powder particles of the charge, and through a combination of comminution and welding actions caused repeatedly by the milling, to create new, dense, composite particles containing fragments of the initial powder material intimately associated and uniformly interdispersed. Milling is done in a protective atmosphere, e.g., under an argon or nitrogen blanket, thereby facilitating oxygen control since virtually the only sources of oxygen are the starting powders and the process control agent. The process control agent is a weld-controlling amount of a carbon-contributing agent. The formation of dispersion strengthened mechanically alloyed aluminum is given in detail in U.S. Patents No. 3,740,210 and 3,816,080, mentioned above. Suitably the powder is prepared in an attritor using a ball-to-powder weight ratio of 15:1 to 60:1. Preferably process control agents are methanol, stearic acid or graphite. Carbon from these organic compounds and/or graphite is incorporated in the powder and contributes to the dispersoid content. The addition elements should be present in the charge at least in an amount approximately that stoichiometrically equivalent to about one half of the carbon entering the charge and up to about 200% or more in excess of the stoichiometric equivalent of the carbon entering the charge. Generally it is possible to charge all ingredients into a mill along with processing aid and carry out mechanical alloying in a single continuous operation. On occasion it is advantageous to mechanically alloy an aluminum-rich fraction of the mill charge for a significant amount of time prior to introducing into the mill harder ingredients of the charge. Unless extreme, commercially unrealistic precautions are taken, the alloys of the present invention produced by the process of the present invention contain oxygen in the form of stable metal oxides, e.g. Al₂O₃. This oxygen is derived from oxide present on the powder particles introduced into the mechanical alloying apparatus, from the atmosphere present in the apparatus during mechanical alloying and, usually, from the processing aid used. While in theory it may be possible to supply metal, e.g. aluminum, powder free of oxide film and mechanically alloy such powder in an atmosphere totally devoid of oxygen, e.g. an atmosphere of argon with an oxygen-free processing aid, e.g. pure graphite or an alkane, carrying out such a process on an industrial scale would be impractical unless the ultimate consumers were willing to pay extraordinary high prices for low-oxygen alloys. In the ordinary course of events it is possible to minimize the amount of oxygen included in the mechanically alloyed alloys of the invention by utilizing starting aluminum powder of relatively large, regular particle size, controlling the mill atmosphere to largely exclude oxygen and externally derived carbon oxides and water vapor and by using a processing aid containing a low amount of oxygen, e.g. stearic acid. Specifically stearic acid contains about 11% by weight oxygen. Accordingly use of about 2% by weight (of metal) of stearic acid as a processing aid will contribute about 0.23% of oxygen to the metal being mechanically alloyed. In alloys of the invention, oxygen in an amount up to about 1% or even higher is not necessarily bad. Accordingly when it is desired to have oxygen contents on the high side one may very well select a processing aid such as oxalic acid which, as the monohydrate, contains about 64% oxygen. The carbon content of the alloys of the present invention is derived primarily or exclusively from the processing aid. Use of 2% stearic acid as a processing aid will contribute about 1.4% carbon to a mechanically alloyed charge. However a portion of this carbon may not report in the product alloy because of the formation of carbon oxides which may escape from the milling means. After mechanical alloying is complete and before the dispersion strengthened mechanically alloyed product is consolidated it must be degassed and compacted. Degassing and compacting are effected under vacuum and generally carried out at a temperature in the range of about 480°C (895°F) up to just below incipient liquification of the alloy. The degassing temperature should be higher than any temperature to be subsequently experienced by the alloy. Degassing is preferably carried out, for example, at a temperature in the range of from about 480°C (900°F) up to 545°C (1015°F) and more preferably above 500°C (930°F). Pressing is carried out at a temperature in the range of about 545°C (1015°F) to about 480°C (895°F). In a preferred embodiment the degassing and compaction are carried out by vacuum hot pressing (VHP). However, other techniques may be used. For example, the degassed powder may be upset under vacuum in an extrusion press. To enable powder to be extruded to substantially full density, compaction should be such that the porosity is isolated thereby avoiding internal contamination of the billet by the extrusion lubricant. This is achieved by carrying out compaction to at least about 95% of full density. Preferably the powders are compacted to 99% of full density and higher, that is, to substantially full density. The resultant compaction products formed in the degassing and compaction step or steps are then consolidated. Consolidation is carried out by extrusion. The extrusion of the material not only is necessary to insure full density in the alloy, but also to break up surface oxide on the particles. The extrusion temperature may be of significance in that control within a narrow temperature established for each alloy may optimize mechanical characteristics . Lubrication practice and the exact die-type equipment used for extrusion can also be of significance to mechanical characteristics. Hot compaction and hot consolidation each alone or together with heating cycles serve to totally sinter bond the product of mechanical alloying and together provide a body of substantially full density. After extrusion, billets can be forged. If necessary, the billets may be machined to remove surface imperfections. Following forging and before or after any finishing operations the alloy can be age-hardened if it is amenable to age-hardening. Those skilled in the art will appreciate that alloys of the invention may be used in the extruded condition as well as in the forged condition. Thus heat treatment, if any, is carried out after the last appropriate working operation. In practicing the present invention, it is advantageous to use titanium as the addition element added to the mechanical alloying charge. Titanium is highly advantageous in that it has a relatively low density. Vanadium is a second choice based principally on density. It is to be appreciated that when an oxygen-containing process control agent such as stearic acid is used in the mechanical alloying operation, carbon monoxide, water vapor and carbon dioxide will exist in the mill atmosphere as breakdown products of the process control agent. Under such circumstances, titanium will compete with aluminum as an oxide former and therefor the amount of titanium available in the alloy will be less than if graphite or an oxygen-poor hydrocarbon is used as process control agent. In order to give those skilled in the art a further appreciation of the advantage of the present invention, the following examples are given. EXAMPLES Compositions to be prepared by mechanical alloying in percent by weight as set forth in Table I. Alloy No. Al Mg% Li% Si% Addition Material Amount of Addition Material (%) Processing Aid 1 Bal - - - Ti 1.5 Methanol 2 Bal - - - V 1.8 Same 3 Bal - - - Nb 3.0 Same 4 Bal - - - Zr 2.4 Same 5 Bal - - - Ti 4.0 Stearic Acid 6 Bal - 2.6 - Ti 2.5 Stearic Acid 7 Bal - 1.9 - FeTi 5.5 Same Alloy No. Al Mg% Li% Si% Addition Material Amount of Addition Material (%) Processing Aid 8 Bal 4 - - Al₃Ti 6.8 Same 9 Bal 4 1.5 - Al₃ Ti 6.8 Same 10 Bal 4 1.5 - FeTi 5.0 Same 11 Bal 4 1.5 0.5 Al₃Ti 20 Graphite and Stearic Acid 12 Bal 2 2 - FeTi 7.6 Graphite and Stearic Acid 13 Bal 2 2 - Ti₅Si₃ 3.4 Stearic Acid The amount of processing aid is generally between 1% and 2% by weight. After mechanical alloying, the charges of the foregoing Table are degassed, compacted and extruded as disclosed hereinbefore to provide product which contains a refractory oxide. Additional compositions to be prepared by mechanical alloying using between about 1% and 2% of processing aid as set forth in Table I are presented in Table II. Alloy Cr Mn Ti Fe Cu Ni V Si Al 14 7 - 1.8 - - - - - Bal 15 7 - - - - - 2.5 - Bal 16 - 5 2.5 - - - - - Bal 17 - 5 2.0 - - 5 - - Bal 18 - 2.5 1.6 - 6 - 0.1 - Bal 19 - - 2.0 7.5 - - - - Bal 20 2.0 - 1.6 7.5 - - - - Bal 21 - 5.0 3.8 - - - - - Bal 22 - - 1.6 7.5 - - - - Bal 23 - 2 2.5 1 - 6 - - Bal Precursors of the compositions of Table II are made by melting aluminum together with any one or more of chromium, molybdenum, tungsten, manganese, titanium, iron, cobalt, nickel and vanadium (i.e., elements having a low diffusion rate in solid aluminum at temperatures above about 300°C) together with copper and silicon, if any, to form a uniform molten composition and atomizing the molten metal to form alloy powder. This step is taught in any one or more of U.S. patents No. 2,966,731, 2,966,732, 2,966,733, 2,966,734, 2,966,735,2,966,736 and 2,967,351. The atomized powder thus formed is then subjected to mechanical alloying in the presence of a carbon-containing processing aid. The resultant mechanically alloyed powder is then compacted, sintered and worked to the desired configuration as described hereinbefore. After mechanical alloying, the charges of the foregoing Table are degassed, compacted and extruded as disclosed hereinbefore. Supplementing or in part substituting the addition elements is the addition of a rare earth element or elements to high temperature aluminum-base alloys. Thus it is within the contemplation of the present invention to incorporate in a mechanical alloying charge for a high temperature aluminum-base alloy about 0.01 to about 0.2% by weight of one or more metals of the rare earth group. The metal is advantageously yttrium or lanthanum or a commercially available mixture of rare earth metals such as mischmetal, cerium-free mischmetal or lanthanum-free mischmetal. Illustrative compositions in percent by weight are set forth in Table III. Alloy A (%) B (%) C (%) D (%) Mg 4 4 4 2 Li 1.5 1.5 1.75 2 Si 0.5 0.5 - - Rare Earth 0.1 0.1 0.1 0.15 Addition Element - (Ti) 5.0 (V) 5.5 (Ti) 5.5 Al Bal E Bal E Bal E Bal E

Claims: Use of a sintered and worked aluminium-base alloy containing aluminium carbide at temperatures in excess of about 100°C without coarsening the aluminium carbide, which alloy is produced by a process comprising including in a mechanical alloying charge for an aluminum-base alloy a material having a particle size of less than 5µm or in a form readily convertible to a material having a particle size of less than 5µm under mechanical alloying conditions and containing an element from the group of titanium, vanadium, niobium and zirconium, mechanically alloying said charge in the presence of a carbon-containing processing aid and thereafter compressing and hot working the thus produced mechanically alloyed product to substantially full density. A use as in claim 1 wherein said element is titanium. A use as claimed in claim 1 or claim 2, wherein additionally there is included in the mechanical alloying charge at least one element chosen from chromium, molybdenum, tungsten, manganese, titanium, iron, cobalt, nickel and vanadium. A use as claimed in any one of claims 1 to 3, wherein additionally there is included in the mechanical alloying charge 0.01 to 0.2% by weight of one or more rare earth elements. A use as claimed in any one of claims 1 to 4, wherein the material included in the mechanical alloying charge has a particle size of less than 1 µm or is convertible into a material having a particle size of less than 1 µm under mechanical alloying conditions. A use as claimed in any one of claims 1 to 5, which includes forming the alloy into a billet. A process for producing sintered and worked aluminum-base alloy to be used at temperatures in excess of about 100°C comprising including in a mechanical alloying charge for an aluminum-base alloy a material having a particle size of less than 5 µm or in a form readily convertible to a material having a particle size of less than 5 µm under mechanical alloying conditions and containing an element from the group of titanium, vanadium, niobium, and zirconium, but said charge including substantially no iron, mechanically alloying said charge in the presence of a carbon-containing processing aid and thereafter compressing and hot working the thus produced mechanically alloyed product to substantially full density. A process as claimed in claim 7, wherein additionally there is included in the mechanical alloying charge at least one element chosen from chromium, molybdenum, tungsten, manganese, titanium, cobalt, nickel and vanadium. A process as claimed in any one of claims 7 and 8, wherein additionally there is included in the mechanical alloying charge 0.01 to 0.2% by weight of one or more rare earth elements. A process as claimed in any one of claims 7 to 9, wherein the material included in the mechanical alloying charge has a particle size of less than 1 µm or is convertible into a material having a particle size of less than 1 µm under mechanical alloying conditions.

Inventors: BENN, RAYMOND CHRISTOPHER, GILMAN, PAUL SANDFORD, JATKAR, ARUN DINKAR
Applicants: INCO ALLOYS INTERNATIONAL, INC.
Application year: 1987
Main classification: C22C1
IPC codes: C22C21, C22C32, C22C1