US3147111A - Article of aluminum-base alloy - Google Patents
Article of aluminum-base alloy Download PDFInfo
- Publication number
- US3147111A US3147111A US155165A US15516561A US3147111A US 3147111 A US3147111 A US 3147111A US 155165 A US155165 A US 155165A US 15516561 A US15516561 A US 15516561A US 3147111 A US3147111 A US 3147111A
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- United States
- Prior art keywords
- aluminum
- base alloy
- atomized
- alloy
- particles
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- 229910045601 alloy Inorganic materials 0.000 title claims description 47
- 239000000956 alloy Substances 0.000 title claims description 47
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 49
- 229910052782 aluminium Inorganic materials 0.000 claims description 44
- 239000008188 pellet Substances 0.000 claims description 26
- 229910000765 intermetallic Inorganic materials 0.000 claims description 18
- 239000002245 particle Substances 0.000 claims description 17
- 239000007787 solid Substances 0.000 claims description 15
- 239000000203 mixture Substances 0.000 claims description 6
- 229910052751 metal Inorganic materials 0.000 description 21
- 239000002184 metal Substances 0.000 description 21
- 239000000470 constituent Substances 0.000 description 9
- 238000000034 method Methods 0.000 description 9
- 150000002739 metals Chemical class 0.000 description 8
- 239000011159 matrix material Substances 0.000 description 7
- 238000005275 alloying Methods 0.000 description 6
- 230000008901 benefit Effects 0.000 description 5
- 239000006185 dispersion Substances 0.000 description 5
- 238000005728 strengthening Methods 0.000 description 4
- 229910015999 BaAl Inorganic materials 0.000 description 3
- -1 boron Chemical class 0.000 description 3
- 238000001125 extrusion Methods 0.000 description 3
- 238000010438 heat treatment Methods 0.000 description 3
- 238000004881 precipitation hardening Methods 0.000 description 3
- 238000002360 preparation method Methods 0.000 description 3
- 230000009467 reduction Effects 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- KDLHZDBZIXYQEI-UHFFFAOYSA-N Palladium Chemical compound [Pd] KDLHZDBZIXYQEI-UHFFFAOYSA-N 0.000 description 2
- ATUOYWHBWRKTHZ-UHFFFAOYSA-N Propane Chemical compound CCC ATUOYWHBWRKTHZ-UHFFFAOYSA-N 0.000 description 2
- 229910003668 SrAl Inorganic materials 0.000 description 2
- 230000002411 adverse Effects 0.000 description 2
- 230000002776 aggregation Effects 0.000 description 2
- 229910052788 barium Inorganic materials 0.000 description 2
- DSAJWYNOEDNPEQ-UHFFFAOYSA-N barium atom Chemical compound [Ba] DSAJWYNOEDNPEQ-UHFFFAOYSA-N 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 239000011261 inert gas Substances 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 230000000704 physical effect Effects 0.000 description 2
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 description 2
- 238000007712 rapid solidification Methods 0.000 description 2
- 239000006104 solid solution Substances 0.000 description 2
- 238000007711 solidification Methods 0.000 description 2
- 230000008023 solidification Effects 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- 238000005482 strain hardening Methods 0.000 description 2
- ZSLUVFAKFWKJRC-IGMARMGPSA-N 232Th Chemical compound [232Th] ZSLUVFAKFWKJRC-IGMARMGPSA-N 0.000 description 1
- 229910018137 Al-Zn Inorganic materials 0.000 description 1
- 229910016570 AlCu Inorganic materials 0.000 description 1
- 229910000789 Aluminium-silicon alloy Inorganic materials 0.000 description 1
- 229910018573 Al—Zn Inorganic materials 0.000 description 1
- 229910016015 BaAl4 Inorganic materials 0.000 description 1
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 1
- 239000004215 Carbon black (E152) Substances 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- OTMSDBZUPAUEDD-UHFFFAOYSA-N Ethane Chemical compound CC OTMSDBZUPAUEDD-UHFFFAOYSA-N 0.000 description 1
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- 229910017706 MgZn Inorganic materials 0.000 description 1
- 229910001122 Mischmetal Inorganic materials 0.000 description 1
- 101100123718 Neurospora crassa (strain ATCC 24698 / 74-OR23-1A / CBS 708.71 / DSM 1257 / FGSC 987) pda-1 gene Proteins 0.000 description 1
- 229910021122 PdAl3 Inorganic materials 0.000 description 1
- BUGBHKTXTAQXES-UHFFFAOYSA-N Selenium Chemical compound [Se] BUGBHKTXTAQXES-UHFFFAOYSA-N 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 1
- 229910052776 Thorium Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 229910052770 Uranium Inorganic materials 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 238000007792 addition Methods 0.000 description 1
- 238000005054 agglomeration Methods 0.000 description 1
- 238000004220 aggregation Methods 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 229910052787 antimony Inorganic materials 0.000 description 1
- WATWJIUSRGPENY-UHFFFAOYSA-N antimony atom Chemical compound [Sb] WATWJIUSRGPENY-UHFFFAOYSA-N 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 238000000889 atomisation Methods 0.000 description 1
- 238000009835 boiling Methods 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- 239000001273 butane Substances 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- 239000011575 calcium Substances 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000012611 container material Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 239000000112 cooling gas Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 239000012467 final product Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 1
- 229910052737 gold Inorganic materials 0.000 description 1
- 239000010931 gold Substances 0.000 description 1
- 231100001261 hazardous Toxicity 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- 229930195733 hydrocarbon Natural products 0.000 description 1
- 150000002430 hydrocarbons Chemical class 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 125000004435 hydrogen atom Chemical class [H]* 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 229910052744 lithium Inorganic materials 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 239000002923 metal particle Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- IJDNQMDRQITEOD-UHFFFAOYSA-N n-butane Chemical compound CCCC IJDNQMDRQITEOD-UHFFFAOYSA-N 0.000 description 1
- OFBQJSOFQDEBGM-UHFFFAOYSA-N n-pentane Natural products CCCCC OFBQJSOFQDEBGM-UHFFFAOYSA-N 0.000 description 1
- 229910052763 palladium Inorganic materials 0.000 description 1
- 238000013031 physical testing Methods 0.000 description 1
- 229910052697 platinum Inorganic materials 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 239000001294 propane Substances 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 229910052761 rare earth metal Inorganic materials 0.000 description 1
- 150000002910 rare earth metals Chemical class 0.000 description 1
- 238000011084 recovery Methods 0.000 description 1
- 238000001953 recrystallisation Methods 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 229910052711 selenium Inorganic materials 0.000 description 1
- 239000011669 selenium Substances 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 229910052709 silver Inorganic materials 0.000 description 1
- 239000004332 silver Substances 0.000 description 1
- 229910052712 strontium Inorganic materials 0.000 description 1
- CIOAGBVUUVVLOB-UHFFFAOYSA-N strontium atom Chemical compound [Sr] CIOAGBVUUVVLOB-UHFFFAOYSA-N 0.000 description 1
- 229910052714 tellurium Inorganic materials 0.000 description 1
- PORWMNRCUJJQNO-UHFFFAOYSA-N tellurium atom Chemical compound [Te] PORWMNRCUJJQNO-UHFFFAOYSA-N 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- DNYWZCXLKNTFFI-UHFFFAOYSA-N uranium Chemical compound [U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U][U] DNYWZCXLKNTFFI-UHFFFAOYSA-N 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/04—Making non-ferrous alloys by powder metallurgy
- C22C1/0408—Light metal alloys
- C22C1/0416—Aluminium-based alloys
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S75/00—Specialized metallurgical processes, compositions for use therein, consolidated metal powder compositions, and loose metal particulate mixtures
- Y10S75/956—Producing particles containing a dispersed phase
Definitions
- the invention relates to die-expressed articles of aluminum-based alloy. It more particularly concerns an improved method of producing die-expressed articles of dispersion-hardened aluminum-base alloys whereby good mechanical properties are attained which are not appreciably lowered by exposure to elevated temperatures.
- high strength aluminum-base alloys have been prepared by alloying aluminum with one or more suitable constituents which are capable of forming solid solutions with aluminum. Such alloys are often further treated, as by solution and precipitation, heat treating and cold-working, to increase yield and tensile strength.
- solution and precipitation heat treating and cold-working
- the eiiectiveness of solid solution strengthening and precipitation hardening is limited and further the benefits of cold-working and aging are soon lost because recovery, recrystallization and overaging take place upon heating the alloys to even rather moderate temperatures.
- fine aluminum powder having a thin oxide coating has been die-expressed to produce an extrude in which aluminum oxideis widely and finely dispersed in an aluminum metal matrix.
- a further object is to provide an improved method of preparing an aluminum-base alloy which has superior mechanical and physical properties but is still readily formable into useful shapes.
- a still further object of the invention is to provide an improved aluminum-base alloy having superior mechanical and physical properties which are not appreciably decreased by exposure to elevated temperatures.
- This invention is predicated on the discovery that, by preparing an aluminum-base alloy containing aluminum and one or more constituents which are each miscible with aluminum in the molten state but substantially insoluble in solidified aluminum and by rapid solidification of said alloy, for example, into a mass of atomized particles, heating, compacting and then die-expressing the solidified metal to form an extrude or die-expressed article, the so-obtained article exhibits exceptionally desirable mechanical properties;
- solidified aluminum is extended in meaning to include solidified aluminum-base alloy.
- an aluminum-base alloy containing at least 70 percent of aluminum is prepared by alloying, according to well known methods, aluminum and one or more constituent metals having the hereinafter defined specific properties.
- An essential constituent metal must have suflicient solubility in molten aluminum at reasonable alloying temperatures, for example 650 to 900 C., to avoid the necessity of employing high temperatures at which aluminum readily attacks container materials, but a solid solubility in aluminum and aluminum-base alloy of less than 0.1 atomic percent.
- metals, such as boron which exhibit the requisite low solid solubility in solidified aluminum but which are difiicult to alloy in effective amount in molten aluminum is undesirable in the practice of the invention.
- the solid solubility in aluminum those elements which on cooling form an intermetallic compound with aluminum, and which are insoluble in solid aluminum are employed.
- the insoluble phase must remain suspended in the rapidly cooled and solidified aluminum.
- the molten alloy exhibit a narrow solidification range so that size of the intermetallic compound particles is minimized.
- the intermetallic particles dispersed in the solid aluminum have a maximum diameter of about 0.0001 inch or less, preferably'as small as about 0.00005 inch or less since the smaller the particle size the more the improvement in properties that results. A few particles having larger diameters can be tolerated but they should be kept to a minimum to avoid adversely affecting the properties of the final product.
- Suitable metal constituents that may be used singly or in combination in the practice of the invention include gold, barium, rare earth metals, palladium, platinum, antimony, selenium, strontium, tellurium, thorium and uranium, the pertinent propertles of wh1ch are listed m Table I.
- the alloy to be used is brought to the molten state in any convenient manner in preparation for rapid solidification. Temperatures in the order of 25 to 50 centigrade degrees above the melting point of the alloy are desirable although other temperatures may be used at which the alloy is in the molten state. It is preferable to use the lower temperature of a molten state not only so as to reduce the degree of hazard involved in handling the molten alloy but also to reduce the amount of heat which must be removed to permit the molten alloy to return to the solid state. It is highly desirable for reasons hereinafter more fully discussed that the solidification of the atomized alloy take place quickly in order to minimize aggregation or crystal growth of intermetallic compounds which are insoluble in solidified aluminum.
- the alloy while in the molten state may be subjected to a dispersion and chilling operation whereby the metal is obtained in atomized form, that is, in the form of fine individually frozen discrete pellets.
- atomization may be performed and any one of them may be used.
- a convenient method appears to be directing a jet of an inert cooling gas against an unconfined stream of the molten alloy as described in U.S. Patent No. 2,630,623.
- a freely falling stream of the molten metal may be broken into droplets and solidified by impinging upon the stream an inert gas such as a hydrocarbon gas (e.g., methane, ethane, propane, butane, etc.), argon, helium, hydrogen, the inert gas having a boiling temperature below the melting point of the molten metal.
- a hydrocarbon gas e.g., methane, ethane, propane, butane, etc.
- argon e.g., argon, helium, hydrogen
- the inert gas having a boiling temperature below the melting point of the molten metal.
- a wide range of pellet sizes although small, usually results from the atomizing operation.
- the atomized product comprises more or less spherical pellets for the most part ranging in size from about mesh to smaller than 325 mesh.
- a preferred range of pellet sizes is from about 325 mesh to about 140 mesh because of the outstanding properties achieved. However, very good properties are
- pellets exhibit very desirable mechanical properties and may be used as pellets, per se, for example, to reinforce other metals, as a load support, etc. or may be further fabricated, as by extrusion, rolling, and the like.
- each pellet of the aluminum-base alloy there is imparted to each pellet of the aluminum-base alloy a special heterogeneous microstructure essential in achieving the objects of this invention.
- This structure is characterized
- the amount of reduction in the cross-sectional dimensions of the compact effected by the extrusion or dieexpression is subject to wide variations and may be from about 5 to 1 to as much as 200 to l or more (i.e., from about 80 percent to over 99 percent reduction in crosssectional area).
- the so-produced extrude having a uniform dispersion of finely-divided intermetallic compounds exhibits enhanced properties at both room and elevated temperatures and is less adversely affected by fabrication or heat treatment at high temperatures.
- Example 1 a quantity of each of the aluminum-base alloys listed in Table II in atomized form was provided.
- the atomized pellets contained a uniform dispersion of intermetallic compound in which the intermetallic compound had an average diameter of about 0.00005 inch, substantially none of the intermetallic compound having a diameter greater than 0.0001 inch.
- the quantity of atomized material was charged into a cylindrical container 3 inches in internal diameter, the container being at 400 C. The charge had a depth of about 6 inches and was compacted at 400 C. in the container to a compact about 4 inches long.
- the compact was then die-expressed at the same temperature at the rate of 5 feet per minute into a strip having a rectangular cross section 1 /4 inches by /1t; inch, tie reduction in area being about 90:1.
- the so-obtained die-expressed articles were subjected to physical testing at 24 C., 315 C. and 427 C. The results of the tests are listed in Table II.
- an aluminum metal matrix having uniformly dispersed therethrough a discontinuous phase made up of very fine crystallites of an intermetallic compound thereof with aluminum.
- the intermetallic compound is present in an amount totaling by volume from about 0.5 to 20 percent of the alloy and preferably from 3 to 15 percent.
- the rapidly solidified metal is heated in preparation for compacting and dieexpression.
- Compacting and die-expression may be carried out in conventional apparatus designed for the extrusion of aluminum-base alloy.
- a suitable method and apparatus for carrying out the die-expression of pelletized light metal, such as aluminum, is described in US. Patent No. 2,630,623.
- the temperature to which the metal is heated is within the conventional plastic deformation temperature range for aluminum-base alloys, usually between about 250 C. and 500 C. but always below that tempcrtaure which affects the dispersion through agglomeration.
- a preferred range is about 315 to 427 C.
- the as-atomized aluminum-base alloy may be heated in bulk to the desired temperature merely by placing it in a suitable metal vessel in a heated oven. Or, it is possible to charge the heated container of a die-expressing apparatus with as-atomized metal and proceed with the operation of the apparatus to efiect die-expression with substantially no destruction of the as-atomized microstructure of the alloy.
- an aluminumbase alloy is prepared by making suitable additions to aluminum of a metal constituent, which forms an insoluble phase therewith as described hereinabove as well as one or more metals which increase the strength of aluminum in a well known conventional manner such as by solution hardening. It has thus been found that the benefits of dispersion hardening may be combined with the benefits of increasing the strength of the matrix about the finely dispersed crystallites of solid insoluble phase.
- Metals which may be added variously to increase the matrix strength include:
- Weight percent Use of combinations of the above-listed elements in amount in which the metals are incompatible by virtue of mutual insolubility in molten aluminum whereby a precipitate is formed which settles from the melt, or in amounts which otherwise fail to increase matrix strength, is of no advantage in the practice of the invention. While simple binary or ternary combinations of the above-listed matrix strengthening constituents are believed to be compatible, it is within the skill of the metallurgist to check desired alloying combinations for incompatibility such as insolubility in molten aluminum.
- any conventional aluminum-base alloy system may be employed, such as AlMg, AlCu, AlMn, AlSi, Al-Zn, Al--MgZn, or AlSiCu, in combination with one or more of the previously mentioned metals which form a solid insoluble phase in solidified aluminum.
- Such composite alloys that is, those including dispersion hardening, as Well as conventional strengthening alloying metals, are atomized, compacted, and extruded as described hereinabove.
- Atomized pellets comprising from 0.5 to 20% by volume of particles of solid insoluble aluminum intermetallic compound and the balance aluminum-base alloy; said particles having maximum diameters of 0.0001 inch and being intimately and uniformly dispersed throughout said aluminum-base alloy; said aluminum intermetallic compound being selected from the group consisting of AuAlz, BaAl CeAl PdA1 PtA13, Se Al SI'A14, TeAl ThAl UAl and mixtures thereof; said atomized pellets comprising at least about 70% of aluminum; and said atomized pellets having diameters smaller than about mesh.
- Atomized pellets comprising from 3 to by volume of particles of solid insoluble aluminum intermetallic compound and the balance aluminum-base alloy; said particles having maximum diameters of 0.0001 inch and being intimately and uniformly dispersed throughout said aluminum-base alloy; said aluminum intermetallic compound being selected from the group consisting of AuAl BaAl CeAl PdAl PtAl SbAl, Se Al SrAl TeAl 6 ThAl UAL, and mixtures thereof; said atomized pellets comprising at least about of aluminum; and said atomized pellets having diameters smaller than about 10 mesh.
- Atomized pellets consisting essentially of from 0.5 to 20% by volume of particles of solid insoluble aluminum intermetallic compound, and the balance aluminumbase alloy containing at least one matrix strengthening alloying constituent selected from the group consisting of silver, calcium, chromium, copper, lithium, magnesium, manganese, silicon, titanium, zinc; said particles having maximum diameters of 0.0001 inch and being intimately and uniformly dispersed throughout said aluminum-base alloy; said aluminum intermetallic compound being selected from the group consisting of AuAl BaAl CeAl PdAl PtAl SbAl, Se Al SrAl TeAl ThAl UAl and mixtures thereof; said atomized pellets comprising at least about 70% of aluminum; and said atomized pellets having diameters smaller than about 10 mesh.
- Atomized pellets consisting essentially of from 0.5 to 20% by volume of solid insoluble ThAl particles and the balance aluminum-base alloy; said ThAl particles having maximum diameters of 0.0001 inch and being intimately and uniformly dispersed throughout said aluminum-base alloy; said atomized pellets comprising at least about 70% of aluminum; and said atomized pellets having diameters smaller than about 10 mesh.
- Atomized pellets of aluminum-base alloy comprising at least about 70% aluminum and from 0.5 to 20% by volume of solid insoluble AuAl particles intimately and uniformly dispersed throughout said aluminum, said AuAl particles having a maximum diameter of 0.0001 inch, said atomized pellets having diameters smaller than about 10 mesh.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Powder Metallurgy (AREA)
- Manufacture Of Metal Powder And Suspensions Thereof (AREA)
Description
United States Patent Deiaware No Drawing. Filed Nov. 27, 1961, Ser. No. 155,165 5 Claims. (Cl. 75-1225) The invention relates to die-expressed articles of aluminum-based alloy. It more particularly concerns an improved method of producing die-expressed articles of dispersion-hardened aluminum-base alloys whereby good mechanical properties are attained which are not appreciably lowered by exposure to elevated temperatures.
This application is a continuation-impart of a priorfiled application, Serial No. 810,258, filed May 1, 1959, now abandoned.
Heretofore high strength aluminum-base alloys have been prepared by alloying aluminum with one or more suitable constituents which are capable of forming solid solutions with aluminum. Such alloys are often further treated, as by solution and precipitation, heat treating and cold-working, to increase yield and tensile strength. However, at elevated temperatures the eiiectiveness of solid solution strengthening and precipitation hardening is limited and further the benefits of cold-working and aging are soon lost because recovery, recrystallization and overaging take place upon heating the alloys to even rather moderate temperatures. In other attempts to produce high strength aluminum-base alloys, fine aluminum powder having a thin oxide coating has been die-expressed to produce an extrude in which aluminum oxideis widely and finely dispersed in an aluminum metal matrix. While so-tormed extrudes exhibit good mechanical properties, they tend to be quite brittle and difiicult to form even at elevated temperatures. In addition, extremely fine aluminum powder is required to provide sufliciently wide dispersion of the oxide in the extrude as the oxide is present only as a surface coating on the so-particulated metal particles. The preparation of aluminum powder of sulficient fineness is not only expensive but the fine powder is hazardous to handle.
It is therefore an object of the invention to provide an improved method of forming an aluminum-base alloy having superior physical and mechanical properties at elevated temperatures. A further object is to provide an improved method of preparing an aluminum-base alloy which has superior mechanical and physical properties but is still readily formable into useful shapes.
A still further object of the invention is to provide an improved aluminum-base alloy having superior mechanical and physical properties which are not appreciably decreased by exposure to elevated temperatures.
These and other objects and advantages of the invention will bemore fully understood on becoming familiar with the following description and the appended claims.
This invention is predicated on the discovery that, by preparing an aluminum-base alloy containing aluminum and one or more constituents which are each miscible with aluminum in the molten state but substantially insoluble in solidified aluminum and by rapid solidification of said alloy, for example, into a mass of atomized particles, heating, compacting and then die-expressing the solidified metal to form an extrude or die-expressed article, the so-obtained article exhibits exceptionally desirable mechanical properties; For purposes of the specification and claims the term solidified aluminum is extended in meaning to include solidified aluminum-base alloy.
In carrying out the invention, an aluminum-base alloy containing at least 70 percent of aluminum is prepared by alloying, according to well known methods, aluminum and one or more constituent metals having the hereinafter defined specific properties. An essential constituent metal must have suflicient solubility in molten aluminum at reasonable alloying temperatures, for example 650 to 900 C., to avoid the necessity of employing high temperatures at which aluminum readily attacks container materials, but a solid solubility in aluminum and aluminum-base alloy of less than 0.1 atomic percent. The use of metals, such as boron, which exhibit the requisite low solid solubility in solidified aluminum but which are difiicult to alloy in effective amount in molten aluminum is undesirable in the practice of the invention. As to the solid solubility in aluminum, those elements which on cooling form an intermetallic compound with aluminum, and which are insoluble in solid aluminum are employed. The insoluble phase must remain suspended in the rapidly cooled and solidified aluminum. It is further desirable that the molten alloy exhibit a narrow solidification range so that size of the intermetallic compound particles is minimized. It is desired that the intermetallic particles dispersed in the solid aluminum have a maximum diameter of about 0.0001 inch or less, preferably'as small as about 0.00005 inch or less since the smaller the particle size the more the improvement in properties that results. A few particles having larger diameters can be tolerated but they should be kept to a minimum to avoid adversely affecting the properties of the final product. Suitable metal constituents that may be used singly or in combination in the practice of the invention include gold, barium, rare earth metals, palladium, platinum, antimony, selenium, strontium, tellurium, thorium and uranium, the pertinent propertles of wh1ch are listed m Table I.
TABLE I Wt. percent Liquid of constit- Solid solubility Solidus l'nteruent to Metal solubility in A1 at temperametallic form 10% constituent inAl, Wt. 800 0., ture of A] compound by volume percent Wt. Binary, formed of interpereent C. with Al metallic compound (estimated) 1 30 642 AuAlz 20 nil 10 652 BaAl4 10 0. 05 20 638 CeA14 l0 nil 50 615 PdAl3 8 nil 40 639 PtA]a 12 0. 1 10 057 SbAl l. 18 nil 22 648 SeaAl-z 15 nil nil 53 621 20 0. 01 30 632 18 nil 20 640 15 1 Similar to barium.
The alloy to be used is brought to the molten state in any convenient manner in preparation for rapid solidification. Temperatures in the order of 25 to 50 centigrade degrees above the melting point of the alloy are desirable although other temperatures may be used at which the alloy is in the molten state. It is preferable to use the lower temperature of a molten state not only so as to reduce the degree of hazard involved in handling the molten alloy but also to reduce the amount of heat which must be removed to permit the molten alloy to return to the solid state. It is highly desirable for reasons hereinafter more fully discussed that the solidification of the atomized alloy take place quickly in order to minimize aggregation or crystal growth of intermetallic compounds which are insoluble in solidified aluminum.
The alloy while in the molten state may be subjected to a dispersion and chilling operation whereby the metal is obtained in atomized form, that is, in the form of fine individually frozen discrete pellets. There are various ways in which atomization may be performed and any one of them may be used. A convenient method appears to be directing a jet of an inert cooling gas against an unconfined stream of the molten alloy as described in U.S. Patent No. 2,630,623.
For example, a freely falling stream of the molten metal may be broken into droplets and solidified by impinging upon the stream an inert gas such as a hydrocarbon gas (e.g., methane, ethane, propane, butane, etc.), argon, helium, hydrogen, the inert gas having a boiling temperature below the melting point of the molten metal. A wide range of pellet sizes, although small, usually results from the atomizing operation. The atomized product comprises more or less spherical pellets for the most part ranging in size from about mesh to smaller than 325 mesh. A preferred range of pellet sizes is from about 325 mesh to about 140 mesh because of the outstanding properties achieved. However, very good properties are achieved with pellet sizes predominating in the 30 to 60 mesh range.
These pellets exhibit very desirable mechanical properties and may be used as pellets, per se, for example, to reinforce other metals, as a load support, etc. or may be further fabricated, as by extrusion, rolling, and the like.
Of course, other methods of rapidly quenching appropriate alloy compositions, as well as other methods of atomizing aluminum may be employed.
As a result of the atomizing operation, there is imparted to each pellet of the aluminum-base alloy a special heterogeneous microstructure essential in achieving the objects of this invention. This structure is characterized The amount of reduction in the cross-sectional dimensions of the compact effected by the extrusion or dieexpression is subject to wide variations and may be from about 5 to 1 to as much as 200 to l or more (i.e., from about 80 percent to over 99 percent reduction in crosssectional area).
The so-produced extrude having a uniform dispersion of finely-divided intermetallic compounds exhibits enhanced properties at both room and elevated temperatures and is less adversely affected by fabrication or heat treatment at high temperatures.
Example In accordance with the invention, a quantity of each of the aluminum-base alloys listed in Table II in atomized form was provided. In each instance, the atomized pellets contained a uniform dispersion of intermetallic compound in which the intermetallic compound had an average diameter of about 0.00005 inch, substantially none of the intermetallic compound having a diameter greater than 0.0001 inch. In each case the quantity of atomized material was charged into a cylindrical container 3 inches in internal diameter, the container being at 400 C. The charge had a depth of about 6 inches and was compacted at 400 C. in the container to a compact about 4 inches long. The compact was then die-expressed at the same temperature at the rate of 5 feet per minute into a strip having a rectangular cross section 1 /4 inches by /1t; inch, tie reduction in area being about 90:1. The so-obtained die-expressed articles were subjected to physical testing at 24 C., 315 C. and 427 C. The results of the tests are listed in Table II.
TABLE II Composition Properties at 24 0. Properties at Properties at Run No.
Per- Per- Per- Per- Per- Per- Percent cent cent cent cent TYS CYS TS cent TYS TS cent TYS TS Th Ba MM Al E E E MM=Misch Metal.
by an aluminum metal matrix having uniformly dispersed therethrough a discontinuous phase made up of very fine crystallites of an intermetallic compound thereof with aluminum. The intermetallic compound is present in an amount totaling by volume from about 0.5 to 20 percent of the alloy and preferably from 3 to 15 percent.
In the next step of the method, the rapidly solidified metal is heated in preparation for compacting and dieexpression. Compacting and die-expression may be carried out in conventional apparatus designed for the extrusion of aluminum-base alloy. A suitable method and apparatus for carrying out the die-expression of pelletized light metal, such as aluminum, is described in US. Patent No. 2,630,623. The temperature to which the metal is heated is within the conventional plastic deformation temperature range for aluminum-base alloys, usually between about 250 C. and 500 C. but always below that tempcrtaure which affects the dispersion through agglomeration. A preferred range is about 315 to 427 C.
It has been found that the as-atomized aluminum-base alloy may be heated in bulk to the desired temperature merely by placing it in a suitable metal vessel in a heated oven. Or, it is possible to charge the heated container of a die-expressing apparatus with as-atomized metal and proceed with the operation of the apparatus to efiect die-expression with substantially no destruction of the as-atomized microstructure of the alloy.
In another embodiment of the invention, an aluminumbase alloy is prepared by making suitable additions to aluminum of a metal constituent, which forms an insoluble phase therewith as described hereinabove as well as one or more metals which increase the strength of aluminum in a well known conventional manner such as by solution hardening. It has thus been found that the benefits of dispersion hardening may be combined with the benefits of increasing the strength of the matrix about the finely dispersed crystallites of solid insoluble phase. Metals which may be added variously to increase the matrix strength include:
Weight percent Use of combinations of the above-listed elements in amount in which the metals are incompatible by virtue of mutual insolubility in molten aluminum whereby a precipitate is formed which settles from the melt, or in amounts which otherwise fail to increase matrix strength, is of no advantage in the practice of the invention. While simple binary or ternary combinations of the above-listed matrix strengthening constituents are believed to be compatible, it is within the skill of the metallurgist to check desired alloying combinations for incompatibility such as insolubility in molten aluminum. In general, any conventional aluminum-base alloy system may be employed, such as AlMg, AlCu, AlMn, AlSi, Al-Zn, Al--MgZn, or AlSiCu, in combination with one or more of the previously mentioned metals which form a solid insoluble phase in solidified aluminum.
Such composite alloys, that is, those including dispersion hardening, as Well as conventional strengthening alloying metals, are atomized, compacted, and extruded as described hereinabove.
Various modifications may be made in the present invention Without departing from the spirit or scope thereof and it is to be understood that I limit myself only as defined in the appended claims.
What is claimed is:
1. Atomized pellets comprising from 0.5 to 20% by volume of particles of solid insoluble aluminum intermetallic compound and the balance aluminum-base alloy; said particles having maximum diameters of 0.0001 inch and being intimately and uniformly dispersed throughout said aluminum-base alloy; said aluminum intermetallic compound being selected from the group consisting of AuAlz, BaAl CeAl PdA1 PtA13, Se Al SI'A14, TeAl ThAl UAl and mixtures thereof; said atomized pellets comprising at least about 70% of aluminum; and said atomized pellets having diameters smaller than about mesh.
2. Atomized pellets comprising from 3 to by volume of particles of solid insoluble aluminum intermetallic compound and the balance aluminum-base alloy; said particles having maximum diameters of 0.0001 inch and being intimately and uniformly dispersed throughout said aluminum-base alloy; said aluminum intermetallic compound being selected from the group consisting of AuAl BaAl CeAl PdAl PtAl SbAl, Se Al SrAl TeAl 6 ThAl UAL, and mixtures thereof; said atomized pellets comprising at least about of aluminum; and said atomized pellets having diameters smaller than about 10 mesh.
3. Atomized pellets consisting essentially of from 0.5 to 20% by volume of particles of solid insoluble aluminum intermetallic compound, and the balance aluminumbase alloy containing at least one matrix strengthening alloying constituent selected from the group consisting of silver, calcium, chromium, copper, lithium, magnesium, manganese, silicon, titanium, zinc; said particles having maximum diameters of 0.0001 inch and being intimately and uniformly dispersed throughout said aluminum-base alloy; said aluminum intermetallic compound being selected from the group consisting of AuAl BaAl CeAl PdAl PtAl SbAl, Se Al SrAl TeAl ThAl UAl and mixtures thereof; said atomized pellets comprising at least about 70% of aluminum; and said atomized pellets having diameters smaller than about 10 mesh.
4. Atomized pellets consisting essentially of from 0.5 to 20% by volume of solid insoluble ThAl particles and the balance aluminum-base alloy; said ThAl particles having maximum diameters of 0.0001 inch and being intimately and uniformly dispersed throughout said aluminum-base alloy; said atomized pellets comprising at least about 70% of aluminum; and said atomized pellets having diameters smaller than about 10 mesh.
5. Atomized pellets of aluminum-base alloy comprising at least about 70% aluminum and from 0.5 to 20% by volume of solid insoluble AuAl particles intimately and uniformly dispersed throughout said aluminum, said AuAl particles having a maximum diameter of 0.0001 inch, said atomized pellets having diameters smaller than about 10 mesh.
References Cited in the file of this patent UNITED STATES PATENTS 2,056,604 Guertler Oct. 6, 1936 2,087,269 Stroup July 20, 1937 2,659,131 Leontis et al Nov. 19, 1953 2,950,188 Picklesimer et a1. Aug. 23, 1960 2,966,736 Towner et al. Jan. 3, 1961
Claims (1)
1. ATOMIZED PELLETS COMPRISING FROM 0.5 TO 20% BY VOLUME OF PARTICLES OF SOLID INSOLUBLE ALUMINUM INTERMETALLIC COMPOUND AND THE BALANCE ALUMINUM-BASE ALLOY; SAID PARTICLES HAVING MAXIMUM DIAMETERS OF 0.0001 INCH AND BEING INTIMELY AND UNIFORMLY DISPERSED THROUGHOUT SAID ALUMINUM-BASE ALLOY; SAID ALUMINUM INTERMETALLIC COMPOUND BEING SELECTED FROM THE GROUP CONSISTING OF AUAL2, BAA,4, CEAL4, PDAL3, PTAL3, SBAL, SE3AL2, SRAL4, TEAL3, THAL3, UAL4 AND MIXTURES THEREOF; SAID ATOMIZED PELLETS COMPRISING AT LEST ABOUT 70% OF ALUMINUM; AND SAID ATOMIZED PELLETS HAVING DIAMETERS SMALLER THAN ABOUT 10 MESH.
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| US155165A US3147111A (en) | 1961-11-27 | 1961-11-27 | Article of aluminum-base alloy |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
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| FR2607522A1 (en) * | 1986-12-02 | 1988-06-03 | Cegedur | PROCESS FOR INCREASING THE RECRYSTALLIZATION TEMPERATURE OF ALUMINUM AND ITS ALLOYS |
| US20050011591A1 (en) * | 2002-06-13 | 2005-01-20 | Murty Gollapudi S. | Metal matrix composites with intermettalic reinforcements |
| WO2015036959A3 (en) * | 2013-09-12 | 2015-08-06 | Cima Nanotech Israel Ltd. | Process for producing a metal nanoparticle composition |
| WO2020173909A1 (en) | 2019-02-26 | 2020-09-03 | Umicore Ag & Co. Kg | Catalyst materials comprising nanoparticles on a carrier and methods for their production |
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| US2056604A (en) * | 1934-07-19 | 1936-10-06 | Degussa | Aluminum alloy |
| US2087269A (en) * | 1936-04-29 | 1937-07-20 | Aluminum Co Of America | Aluminum-calcium alloys |
| US2659131A (en) * | 1950-08-16 | 1953-11-17 | Dow Chemical Co | Composite alloy |
| US2950188A (en) * | 1957-09-10 | 1960-08-23 | Marion L Picklesimer | Method of suppressing ual4 formation in u-al alloys |
| US2966736A (en) * | 1958-03-27 | 1961-01-03 | Aluminum Co Of America | Aluminum base alloy powder product |
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| US2056604A (en) * | 1934-07-19 | 1936-10-06 | Degussa | Aluminum alloy |
| US2087269A (en) * | 1936-04-29 | 1937-07-20 | Aluminum Co Of America | Aluminum-calcium alloys |
| US2659131A (en) * | 1950-08-16 | 1953-11-17 | Dow Chemical Co | Composite alloy |
| US2950188A (en) * | 1957-09-10 | 1960-08-23 | Marion L Picklesimer | Method of suppressing ual4 formation in u-al alloys |
| US2966736A (en) * | 1958-03-27 | 1961-01-03 | Aluminum Co Of America | Aluminum base alloy powder product |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
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| FR2607522A1 (en) * | 1986-12-02 | 1988-06-03 | Cegedur | PROCESS FOR INCREASING THE RECRYSTALLIZATION TEMPERATURE OF ALUMINUM AND ITS ALLOYS |
| EP0273838A3 (en) * | 1986-12-02 | 1988-07-20 | Cegedur Societe De Transformation De L'aluminium Pechiney | Process to increase the recrystillization temperature of aluminium and its alloys |
| US20050011591A1 (en) * | 2002-06-13 | 2005-01-20 | Murty Gollapudi S. | Metal matrix composites with intermettalic reinforcements |
| US7794520B2 (en) * | 2002-06-13 | 2010-09-14 | Touchstone Research Laboratory, Ltd. | Metal matrix composites with intermetallic reinforcements |
| WO2015036959A3 (en) * | 2013-09-12 | 2015-08-06 | Cima Nanotech Israel Ltd. | Process for producing a metal nanoparticle composition |
| WO2020173909A1 (en) | 2019-02-26 | 2020-09-03 | Umicore Ag & Co. Kg | Catalyst materials comprising nanoparticles on a carrier and methods for their production |
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