US3847679A - Directional eutectoid composites by solid-state up-transformation - Google Patents
Directional eutectoid composites by solid-state up-transformation Download PDFInfo
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- US3847679A US3847679A US00416255A US41625573A US3847679A US 3847679 A US3847679 A US 3847679A US 00416255 A US00416255 A US 00416255A US 41625573 A US41625573 A US 41625573A US 3847679 A US3847679 A US 3847679A
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- 239000007790 solid phase Substances 0.000 claims abstract description 23
- 239000000835 fiber Substances 0.000 claims abstract description 9
- 238000000354 decomposition reaction Methods 0.000 claims description 16
- RZJQYRCNDBMIAG-UHFFFAOYSA-N [Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Zn].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn] Chemical compound [Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Cu].[Zn].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Ag].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn] RZJQYRCNDBMIAG-UHFFFAOYSA-N 0.000 claims description 8
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910000809 Alumel Inorganic materials 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229910002514 Co–Co Inorganic materials 0.000 description 1
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 1
- 229910015372 FeAl Inorganic materials 0.000 description 1
- 229910017108 Fe—Fe Inorganic materials 0.000 description 1
- GRYLNZFGIOXLOG-UHFFFAOYSA-N Nitric acid Chemical compound O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 0.000 description 1
- 241001486234 Sciota Species 0.000 description 1
- 229910010169 TiCr Inorganic materials 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
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Classifications
-
- C—CHEMISTRY; METALLURGY
- C30—CRYSTAL GROWTH
- C30B—SINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
- C30B3/00—Unidirectional demixing of eutectoid materials
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C47/00—Making alloys containing metallic or non-metallic fibres or filaments
- C22C47/08—Making alloys containing metallic or non-metallic fibres or filaments by contacting the fibres or filaments with molten metal, e.g. by infiltrating the fibres or filaments placed in a mould
Definitions
- ABSTRACT A eutectoid type alloy is heated to a temperature above its eutectoid temperature to form the high temperature single solid phase which is then quenched to retain it at about room temperature.
- the quenched single phase solid is heated unidirectionally through a thermal gradient at a velocity of transformation which on reaching transformation temperature directionally transforms it into an aligned composite of at least two phases with one of the phases aligned in the form of substantially uniform lamellae, fibers or rods substantially parallel to each other and to the thermal gradient.
- the transformation temperature is a minimum of 20C below that of the nonnal down-temperature technique at the same velocity in a certain velocity of transformation range resulting in significantly finer microstructures.
- the present invention relates generally to the art of directional control of eutectoid decomposition of metal alloys, and particularly, it relates to producing directional composites of eutectoid type alloys, i.e., alloys with one phase aligned in a matrix of a second or other phases.
- the art has disclosed the directional transformation of eutectic and eutectoid alloys to produce aligned composite structures. These transformations were accomplished by 'moving the alloy sample down a temperature gradient, i.e. moving the sample from a hot zone to a cold zone at a certain rate. Specifically, in eutectoid systems the transfonnation occurs by cooling from the high temperature single phase solid through the temperature at which decomposition into at least two solid phases occurs.
- this normal down temperature-transformation technique as a means of producing aligned structures of eutectoids has two major limitations.
- alloys only'slightly off the exact eutectoid composition contain pro-eutectoid particles that destroy the alignment of the structure. This sensitivity to composition appears to be significantly greater than in the competitive process of directional eutectic solidification.
- pro-eutectoid particles it is meant herein those portions of the alloy which do not undergo a eutectoid reaction.
- the aligned phase in the resulting composite is at least 10 percent finer in size than that attained by the down temperature transformationtechnique. Also, with decreasing temperatures of transformation in the present process the aligned phase is correspondingly finer in size.
- the present process uses an alloy which undergoes a eutectoid decomposition. Specifically, it is an alloy which forms a single solid phase at an elevated temperature, sometimes referred to as the high temperature single phase, and which, when cooled through a eutectoid or decomposition temperature, decomposes to form at least two solid phases.
- an alloy is of a eutectoid composition or a composition close thereto and the range that the composition may vary from the eutectoid composition is determinable empirically for the particular alloy. Specifically, for most of the alloys in the present process such range usually varies up to about 10 percent by weight from the eutectoid composition.
- Such alloys are Fe-Fe C, FeAl-FeAl Cu-Cu Al Cu- Cu In ,Co-Co Si, l-If-HfCr Ti-TiCr Zr-ZtCr and Niln-Ni In
- the solid alloy preferably in the form of an ingot, is heated to a temperature above its eutectoid temperature to form the high temperature single solid phase.
- the formation of this high temperature single solid phase is determinable empirically by standard metallographic techniques. Also, the eutectoid temperature for a particular alloy is usually available in the literature.
- the single phase alloy is then rapidly quenched to retain it at about room temperature.
- a number of conventional methods can be used to carry out the quenching such as, for example, a water quench. Generally, quenching is carried out at a rate in the range of about 200C per second to 400C per second.
- the quenched single phase alloy is a metastable high temperature structure.
- the quenched solid alloy can be directionally aligned by a number of conventional methods which allow passage of the quenched single phase solid through a thermal gradient in a single direction at a fixed velocity of transformation to the transformation temperature.
- the thermal gradient can be moved relative to the quenched solid.
- the apparatus is comprised of a heated vertical mold provided with a cooling system at its lower'end, means for maintaining the desired thermal gradient and means for pulling the quenched solid through the thermal gradient at the desired fixed velocity of transformation.
- the rate that the aligned composite is cooled, once it is formed, is not critical.
- the geometry of the aligned phase in the aligned composite depends upon the specific composition of the alloy and the velocity at which it is transformed.
- the aligned phase may be in the form of lame]- lae, rods or fibers. The slower the velocity of transformation, the lower is the temperature of transformation and the finer is the resulting aligned phase in the composite structure.
- the quenched single phase solid alloy is heated unidirectionally through a thermal gradient which achieves eutectoid decomposition. This is determinable empirically and depends largely on the particular alloy composition. In the present process, the thermal gradient usually ranges from 50C per cm. to about l,OOOC per cm. For practical purposes the lowest thermal gradient which achieves decomposition or transformation of the quenched solid is preferred.
- the velocity of transformation is determinable empirically and depends largely on the particular alloy composition. Ordinarily, a certain minimum to maximum velocity range will achieve transformation of the quenched alloy into an aligned solid composite. Within the velocity of transformation range, the temperature of transformation increases with increasing velocity. Specifically, fixing of the velocity of transformation also fixes the temperature of transformation in a given system. In the present invention the temperature of transformation is at least 30C below the eutectoid temperature of the alloy, and it is a minimum of 20C below the decomposition or transformation temperature of the normal down temperature technique at equivalent velocities in the range from the minimum up to 75 percent of the maximum velocity of transformation.
- the temperature of transformation is at least 50C below that of the decomposition or transformation temperature of the conventional down temperature transformation technique at the same velocity.
- the temperature of transformation increases, and at a velocity above75 percent of the maximum velocity of transformation in the present process, the difference between the present transformation temperature and that of the decomposition temperature of the conventional down temperature transformation technique is less than 20C and at the maximum velocity of transformation in the present process, the difference in such temperatures is zero.
- the quenched single phase solid alloy is cold-worked to increase the driving force for the transformation, thereby increasing the obtainable transformation rates.
- the alloy can be worked at room temperature by methods such as rolling and swaging.
- the degree of cold-working to achieve a significant increase in the transformation rate is determinable empirically.
- the rate of transformation can be increased by at least 10 percent by such cold-working and such rate of transformation is at least 10 percent higher than that possible by the normal down temperaturetransformation technique.
- EXAMPLE A number of samples of Cu-l 1.8 wt.% Al alloys are prepared. This alloy undergoes a eutectoid reaction wherein the high temperature solid B-phase decomposes into two solid phases at a temperature of 565C.
- Each alloy sample preferably made from elements of 99.99percent purity, is formed into a rod 0.175 in. in diameter.
- Each rod is heated in an atmosphere in which it is substantially inert, such as argon, to a temperature above the eutectoid temperature to convert it to the high temperature single solid B-phase for example to 800C for at least about one hour.
- Each sample can then be rapidly quenched by immersing it in 25C water, which is at a rate of about 400C per second, to retain this high temperature solid phase at room temperature.
- the quenched sample is placed in a graphite crucible, for example, 5 in. long with 0.250 in. outer diameter and 0.035 in. walls and can be directionally decomposed in a suitable apparatus where each is driven at constant velocity through a temperature gradient of preferably 300C/cm.
- each quenched sample is pulled under a substantially inert atmosphere such as flowing argon in, for example, a vertical, platinumwound furnace and the aligned or transformed portion of the sample can be cooled by driving the crucible upwards through a A inch hole in a water-cooled copper toroid.
- An insulated chromel-alumel thermocouple can be imbedded in the center of a sample and moved with the sample during pulling and alignment to determine the temperature of transformation, i.e. the temperature at which the quenched sample directionally decomposes to produce an aligned two phase solid composite.
- the samples'driven in the range of 7 X 10 cm/sec. to 8 X 10 cm/sec. will form aligned composites at temperatures of transformation ranging from about 505C to about 515C.
- the resulting aligned sampled can be polished for metallographic examination by thinning selected regions for transmission electron microscopy using a cooled solution of 50 percent conc. nitric acid, 50 percent 'alcohol.
- the aligned composites are of a substantially uniform microstructure composed of one phase in the form of lamellae substantially parallel to each other grown substantially parallel to the thermal gradient and passing through a matrix of the second phase. At lower temperatures of transformation the lamellae are significantly finer than at higher temperatures of transformation.
- a process for producing a solid composite of at least two different metal phases with one phase in the form of substantially uniform parallel lamellae, rods or fibers passing through a matrix of the second or other phases which comprises providing an alloy which forms at an elevated temperature a single solid phase that decomposes eutectoidally when cooled through a eutectoid temperature to form at least two solid phases, said alloy having a decomposition temperature varying with velocity of motion down a temperature gradient, heating said alloy to a temperature above its eutectoid temperature to form said single solid phase, quenching the resulting single solid phase alloy to retain said phase at about room temperature, unidirectionally raising the temperature of the resulting quenched single solid phase alloy through a thermal gradient of at least 50C per cm.
- transformation temperature being a minimum of C below said decomposition temperature when said velocities are equivalent in the range from a minimum velocity up to percent of the maximum velocity of transformation to produce said aligned solid composite.
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- Manufacture Of Alloys Or Alloy Compounds (AREA)
Abstract
A eutectoid type alloy is heated to a temperature above its eutectoid temperature to form the high temperature single solid phase which is then quenched to retain it at about room temperature. The quenched single phase solid is heated unidirectionally through a thermal gradient at a velocity of transformation which on reaching transformation temperature directionally transforms it into an aligned composite of at least two phases with one of the phases aligned in the form of substantially uniform lamellae, fibers or rods substantially parallel to each other and to the thermal gradient. The transformation temperature is a minimum of 20*C below that of the normal down-temperature technique at the same velocity in a certain velocity of transformation range resulting in significantly finer microstructures.
Description
United States Patent [1 1 Livingston 1451 Nov. 12, 1974 [75] lnventor: James D. Livingston, Scotia, NY.
[73] Assignee: General Electric Company,
Schenectady, NY.
[22] Filed: Nov. 15, 1973 [21] Appl. No.: 416,255
52 US. (:1 148/2, 148/3, 75/129, 75/135 [51] Int. Cl. C22c 19/00, C22c 39/20 [58] Field of Search 148/2, 3, 4, 134, 135; 75/135, 129
[56] References Cited UNITED STATES PATENTS 3,552,953 1 1971 Lemkey et ill. 75/171 3,635,769 l/l972 Shaw 75/171 X 3,671,223 6/1972 Chumpsen et al..., 75/135 X 3,677,835 7/1972 Tien et a1 75/135 X 3,783,033 l/l974 Tarshis 75/170 X Primary E.\'aminerL. Dewayne Rutledge Assistant ExaminerArthur J. Steiner Attorney, Agent, or Firm-Jane M. Binkowski; Joseph T..Cohen; Jerome C. Squillaro [57] ABSTRACT A eutectoid type alloy is heated to a temperature above its eutectoid temperature to form the high temperature single solid phase which is then quenched to retain it at about room temperature. The quenched single phase solid is heated unidirectionally through a thermal gradient at a velocity of transformation which on reaching transformation temperature directionally transforms it into an aligned composite of at least two phases with one of the phases aligned in the form of substantially uniform lamellae, fibers or rods substantially parallel to each other and to the thermal gradient. The transformation temperature is a minimum of 20C below that of the nonnal down-temperature technique at the same velocity in a certain velocity of transformation range resulting in significantly finer microstructures.
2 Claims, No Drawings I nvention s ed hcreinw s mad i the course of, or under, a contract with the Naval Air Systems Command.
The present invention relates generally to the art of directional control of eutectoid decomposition of metal alloys, and particularly, it relates to producing directional composites of eutectoid type alloys, i.e., alloys with one phase aligned in a matrix of a second or other phases.
The art has disclosed the directional transformation of eutectic and eutectoid alloys to produce aligned composite structures. These transformations were accomplished by 'moving the alloy sample down a temperature gradient, i.e. moving the sample from a hot zone to a cold zone at a certain rate. Specifically, in eutectoid systems the transfonnation occurs by cooling from the high temperature single phase solid through the temperature at which decomposition into at least two solid phases occurs. However, this normal down temperature-transformation technique as a means of producing aligned structures of eutectoids has two major limitations. First the decomposition temperature is high which is not only inconvenient but also leads to a minimum attainable laminar spacing which is too coarse to provide the necessary properties for a number of applications. Second, alloys only'slightly off the exact eutectoid composition contain pro-eutectoid particles that destroy the alignment of the structure. This sensitivity to composition appears to be significantly greater than in the competitive process of directional eutectic solidification. By pro-eutectoid particles it is meant herein those portions of the alloy which do not undergo a eutectoid reaction.
,ature-to form at least two solid phases, said alloy having a decomposition temperature which varies with velocity of motion down a temperature gradient, heating said alloy to a temperature above the said eutectoid temperature to form said single solid phase, quenching the resulting single solid phase alloy to retain said phase at about room temperature, unidirectionally raising the temperature of the resulting quenched single solid phase alloy through a thermal gradient of at least.50C per cm. at a velocity which on reaching transformation temperature directionally transforms said quenched solid to produce an aligned solid composite of at least two phases wherein one of said phases is aligned in the form of lamellae, fibers or rods substantially parallel to each other and to the thermal gradient, said aligned phase being substantially uniform in size and passing through a matrix of the second or other phases, said transformation temperature being a minimum of C- below said decomposition temperature when said velocities are equivalent in the range from a minimum velocity up t o- 7 5 percent of the maximum velocity of 2 transformation to produce said aligned solid composlte. .1..-
Since the transformation temperature in the present process is at least 20C below that of the transformation or decomposition temperature of the normal down temperature transformation technique, the aligned phase in the resulting composite is at least 10 percent finer in size than that attained by the down temperature transformationtechnique. Also, with decreasing temperatures of transformation in the present process the aligned phase is correspondingly finer in size.
The present process uses an alloy which undergoes a eutectoid decomposition. Specifically, it is an alloy which forms a single solid phase at an elevated temperature, sometimes referred to as the high temperature single phase, and which, when cooled through a eutectoid or decomposition temperature, decomposes to form at least two solid phases. In the present process such an alloy is of a eutectoid composition or a composition close thereto and the range that the composition may vary from the eutectoid composition is determinable empirically for the particular alloy. Specifically, for most of the alloys in the present process such range usually varies up to about 10 percent by weight from the eutectoid composition. Representative of such alloys are Fe-Fe C, FeAl-FeAl Cu-Cu Al Cu- Cu In ,Co-Co Si, l-If-HfCr Ti-TiCr Zr-ZtCr and Niln-Ni In In carrying out the present process the solid alloy, preferably in the form of an ingot, is heated to a temperature above its eutectoid temperature to form the high temperature single solid phase. The formation of this high temperature single solid phase is determinable empirically by standard metallographic techniques. Also, the eutectoid temperature for a particular alloy is usually available in the literature.
The single phase alloy is then rapidly quenched to retain it at about room temperature. A number of conventional methods can be used to carry out the quenching such as, for example, a water quench. Generally, quenching is carried out at a rate in the range of about 200C per second to 400C per second. The quenched single phase alloy is a metastable high temperature structure.
The quenched solid alloy can be directionally aligned by a number of conventional methods which allow passage of the quenched single phase solid through a thermal gradient in a single direction at a fixed velocity of transformation to the transformation temperature. Alternatively, the thermal gradient can be moved relative to the quenched solid. Generally, the apparatus is comprised of a heated vertical mold provided with a cooling system at its lower'end, means for maintaining the desired thermal gradient and means for pulling the quenched solid through the thermal gradient at the desired fixed velocity of transformation. The rate that the aligned composite is cooled, once it is formed, is not critical. The geometry of the aligned phase in the aligned composite depends upon the specific composition of the alloy and the velocity at which it is transformed. The aligned phase may be in the form of lame]- lae, rods or fibers. The slower the velocity of transformation, the lower is the temperature of transformation and the finer is the resulting aligned phase in the composite structure.
In carrying out the present process, the quenched single phase solid alloy is heated unidirectionally through a thermal gradient which achieves eutectoid decomposition. This is determinable empirically and depends largely on the particular alloy composition. In the present process, the thermal gradient usually ranges from 50C per cm. to about l,OOOC per cm. For practical purposes the lowest thermal gradient which achieves decomposition or transformation of the quenched solid is preferred.
The velocity of transformation is determinable empirically and depends largely on the particular alloy composition. Ordinarily, a certain minimum to maximum velocity range will achieve transformation of the quenched alloy into an aligned solid composite. Within the velocity of transformation range, the temperature of transformation increases with increasing velocity. Specifically, fixing of the velocity of transformation also fixes the temperature of transformation in a given system. In the present invention the temperature of transformation is at least 30C below the eutectoid temperature of the alloy, and it is a minimum of 20C below the decomposition or transformation temperature of the normal down temperature technique at equivalent velocities in the range from the minimum up to 75 percent of the maximum velocity of transformation. Specifically, at the minimum velocity of transformation in the present process, the temperature of transformation is at least 50C below that of the decomposition or transformation temperature of the conventional down temperature transformation technique at the same velocity. However, with increasing velocity the temperature of transformation increases, and at a velocity above75 percent of the maximum velocity of transformation in the present process, the difference between the present transformation temperature and that of the decomposition temperature of the conventional down temperature transformation technique is less than 20C and at the maximum velocity of transformation in the present process, the difference in such temperatures is zero.
In one embodiment of the present invention the quenched single phase solid alloy is cold-worked to increase the driving force for the transformation, thereby increasing the obtainable transformation rates. For example, the alloy can be worked at room temperature by methods such as rolling and swaging. The degree of cold-working to achieve a significant increase in the transformation rate is determinable empirically. Specifically, the rate of transformation can be increased by at least 10 percent by such cold-working and such rate of transformation is at least 10 percent higher than that possible by the normal down temperaturetransformation technique. The invention is further illustrated by the following example.
EXAMPLE A number of samples of Cu-l 1.8 wt.% Al alloys are prepared. This alloy undergoes a eutectoid reaction wherein the high temperature solid B-phase decomposes into two solid phases at a temperature of 565C.
Each alloy sample, preferably made from elements of 99.99percent purity, is formed into a rod 0.175 in. in diameter. Each rod is heated in an atmosphere in which it is substantially inert, such as argon, to a temperature above the eutectoid temperature to convert it to the high temperature single solid B-phase for example to 800C for at least about one hour. Each sample can then be rapidly quenched by immersing it in 25C water, which is at a rate of about 400C per second, to retain this high temperature solid phase at room temperature.
To carry out the directional transformation the quenched sample is placed in a graphite crucible, for example, 5 in. long with 0.250 in. outer diameter and 0.035 in. walls and can be directionally decomposed in a suitable apparatus where each is driven at constant velocity through a temperature gradient of preferably 300C/cm. Specifically, each quenched sample is pulled under a substantially inert atmosphere such as flowing argon in, for example, a vertical, platinumwound furnace and the aligned or transformed portion of the sample can be cooled by driving the crucible upwards through a A inch hole in a water-cooled copper toroid.
An insulated chromel-alumel thermocouple can be imbedded in the center of a sample and moved with the sample during pulling and alignment to determine the temperature of transformation, i.e. the temperature at which the quenched sample directionally decomposes to produce an aligned two phase solid composite. The samples'driven in the range of 7 X 10 cm/sec. to 8 X 10 cm/sec. will form aligned composites at temperatures of transformation ranging from about 505C to about 515C.
The resulting aligned sampled can be polished for metallographic examination by thinning selected regions for transmission electron microscopy using a cooled solution of 50 percent conc. nitric acid, 50 percent 'alcohol.
The aligned composites are of a substantially uniform microstructure composed of one phase in the form of lamellae substantially parallel to each other grown substantially parallel to the thermal gradient and passing through a matrix of the second phase. At lower temperatures of transformation the lamellae are significantly finer than at higher temperatures of transformation.
In copending US. Pat. application, Ser. No. 416,254 (RD7064) entitled Directional Composites By Solid- State Up-Transformation filed of even date herewith in the name of James D. Livingston and assigned to the assignee hereof there is disclosed a process of heating a cellular precipitation type alloy to a temperature above its solvus temperature to form the high temperature single soild phase, quenching the single solid phase to retain it at about room temperature, heating the quenched single phase solid unidirectionally through a thermal gradient at a velocity of transformation which on reaching transformation temperature directionally transforms it into an aligned composite of at least two phases with one of the phases aligned in the form of substantially uniform lamellae, fibers or rods substantially paiallel to each other and to the thermal gradient.
What is claimed is:
l. A process for producing a solid composite of at least two different metal phases with one phase in the form of substantially uniform parallel lamellae, rods or fibers passing through a matrix of the second or other phases which comprises providing an alloy which forms at an elevated temperature a single solid phase that decomposes eutectoidally when cooled through a eutectoid temperature to form at least two solid phases, said alloy having a decomposition temperature varying with velocity of motion down a temperature gradient, heating said alloy to a temperature above its eutectoid temperature to form said single solid phase, quenching the resulting single solid phase alloy to retain said phase at about room temperature, unidirectionally raising the temperature of the resulting quenched single solid phase alloy through a thermal gradient of at least 50C per cm. at a velocity of transformation which on reaching transformation temperature directionally transforms said quenched solid to produce an aligned solid composite of at least two phases wherein one of said phases is aligned in the form of substantially uniform lamellae, fibers or rods substantially parallel to each other and to the thermal gradient, said transformation temperature being a minimum of C below said decomposition temperature when said velocities are equivalent in the range from a minimum velocity up to percent of the maximum velocity of transformation to produce said aligned solid composite.
2. A process for producing an aligned composite according to claim 1 wherein prior to said unidirectional raising of the temperature said quenched single phase solid is cold-worked in an amount sufficient to raise the maximum velocity of transformation by at least 10 percent.
Claims (2)
1. A PROCESS FOR PRODUCING A SOLID COMPOSITE OF AT LEAST TWO DIFFERENT METAL PHASES WITH ONE PHASE IN THE FORM OF SUBSTANTIALLY UNIFORM PARALLEL LAMELLAE, RODS OR FIBERS PASSING THROUGH A MATRIX OF THE SECOND OR OTHER PHASES WHICH COMPRISES PROVIDING AN ALLOY WHICH FORMS AT AN ELEVATED TEMPERATURE A SINGLE SOLID PHASE THAT DECOMPOSES EUTECTOIDALLY WHEN COOLED THROUGH A EUTECTOID TEMPERATURE TO FORM AT LEAST TWO SOLID WITH VELOCITY OF MOLTION DOWN A TEMPERATURE GRADIENT, HEATING WITH VELOCITY OF MOTION DOWN A TEMPERATURE GRADIENT, HEATING SAID ALLOY TO A TEMPERATURE ABOVE ITS EUTECTOID TEMPERATURE TO FORM SAID SINGLE SOLID PHASE, QUENCHING THE RESULTING SINGLE SOLID PHASE ALLOY TO RETAIN SAID PHASE AT ABOUT ROOM TEMPERATURE, UNIDIRECTIONALLY RAISING THE TEMPERATURE OF THE RESULTING QUENCHED SINGLE SOLID PHASE ALLOY THROUGH A THERMAL GRADIENT OF AT LEAST 50*C PER CM. AT A VELOCITTY OF TRANSFORMATION WHICH ON REACHING TRANSFORMATION TEMPERATURE DIRECTIONALLY TRANSFORMS SAID QUENCHED SOLID TO PRODUCE AN ALIGNED SOLID COMPOSITE OF AT LEAST TWO PHASES WHEREIN ONE OF SAID PHASES IS ALIGNED IN THE FORM OF SUBSTANTIALLY UNIFORM LAMELLAE, FIBERS OR RODS SUBSTANTIALLY PARALLEL TO EACH OTHER AND TO THETHERMAL GRADIENT, SAID TRANSFORMATION TEMPERATURE BEING A MINIMUM OF 20*C BELOW SAID DECOMPOSITION TEMPERATURE WHEN SAID VELOCITIES ARE EQUIVALENT IN THE RANGE FROM A MINIMUM VELOCITY U TO 75 PERCENT OF THE MAXIMUM VELOCITY OF TRANSFORMATION TO PRODUCE SAID ALIGNED SOLID COMPOSITE.
2. A process for producing an aligned composite according to claim 1 wherein prior to said unidirectional raising of the temperature said quenched single phase solid is cold-worked in an amount sufficient to raise the maximum velocity of transformation by at least 10 percent.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US00416255A US3847679A (en) | 1973-11-15 | 1973-11-15 | Directional eutectoid composites by solid-state up-transformation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US00416255A US3847679A (en) | 1973-11-15 | 1973-11-15 | Directional eutectoid composites by solid-state up-transformation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3847679A true US3847679A (en) | 1974-11-12 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US00416255A Expired - Lifetime US3847679A (en) | 1973-11-15 | 1973-11-15 | Directional eutectoid composites by solid-state up-transformation |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3847679A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4029500A (en) * | 1975-03-11 | 1977-06-14 | Nasa | Method of growing composites of the type exhibiting the Soret effect |
| US4441939A (en) * | 1981-11-06 | 1984-04-10 | United Technologies Corporation | M7 C3 Reinforced iron base superalloys |
| EP0158844A1 (en) * | 1984-03-19 | 1985-10-23 | Inco Alloys International, Inc. | Promoting directional grain growth in objects |
| FR2599759A1 (en) * | 1986-06-09 | 1987-12-11 | Gen Electric | SINGLE CRYSTAL ALLOYS REINFORCED BY DISPERSION |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3552953A (en) * | 1969-01-10 | 1971-01-05 | United Aircraft Corp | Cobalt-chromium base alloy and articles produced therefrom |
| US3635769A (en) * | 1969-08-21 | 1972-01-18 | Westinghouse Electric Corp | Nickel-chromium eutectic alloy |
| US3671223A (en) * | 1969-12-10 | 1972-06-20 | United Aircraft Corp | Anisotropic polyphase structure of multivariant eutectic composition |
| US3677835A (en) * | 1970-10-16 | 1972-07-18 | United Aircraft Corp | Homogeneous nickel-base superalloy castings |
| US3783033A (en) * | 1973-01-17 | 1974-01-01 | Gen Electric | Rapid solidification to improve the oxidation resistance of directionally solidified eutectic alloys |
-
1973
- 1973-11-15 US US00416255A patent/US3847679A/en not_active Expired - Lifetime
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3552953A (en) * | 1969-01-10 | 1971-01-05 | United Aircraft Corp | Cobalt-chromium base alloy and articles produced therefrom |
| US3635769A (en) * | 1969-08-21 | 1972-01-18 | Westinghouse Electric Corp | Nickel-chromium eutectic alloy |
| US3671223A (en) * | 1969-12-10 | 1972-06-20 | United Aircraft Corp | Anisotropic polyphase structure of multivariant eutectic composition |
| US3677835A (en) * | 1970-10-16 | 1972-07-18 | United Aircraft Corp | Homogeneous nickel-base superalloy castings |
| US3783033A (en) * | 1973-01-17 | 1974-01-01 | Gen Electric | Rapid solidification to improve the oxidation resistance of directionally solidified eutectic alloys |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4029500A (en) * | 1975-03-11 | 1977-06-14 | Nasa | Method of growing composites of the type exhibiting the Soret effect |
| US4441939A (en) * | 1981-11-06 | 1984-04-10 | United Technologies Corporation | M7 C3 Reinforced iron base superalloys |
| EP0158844A1 (en) * | 1984-03-19 | 1985-10-23 | Inco Alloys International, Inc. | Promoting directional grain growth in objects |
| US4921549A (en) * | 1984-03-19 | 1990-05-01 | Inco Alloys International, Inc. | Promoting directional grain growth in objects |
| FR2599759A1 (en) * | 1986-06-09 | 1987-12-11 | Gen Electric | SINGLE CRYSTAL ALLOYS REINFORCED BY DISPERSION |
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