Patent Application
20150129093
1. Field of the Technology
The present disclosure relates to methods for thermomechanically processing metal alloys.
2. Description of the Background of the Technology
When a metal alloy workpiece such as, for example, an ingot, a bar, or a billet, is thermomechanically processed (i.e., hot worked), the surfaces of the workpiece cool faster than the interior of the workpiece. A specific example of this phenomenon occurs when a bar of a metal alloy is heated and then forged using a radial forging press or an open die press forge. During the hot forging, the grain structure of the metal alloy deforms due to the action of the dies. If the temperature of the metal alloy during deformation is lower than the alloy's recrystallization temperature, the alloy will not recrystallize, resulting in a grain structure composed of elongated unrecrystallized grains. If, instead, the temperature of the alloy during deformation is greater than or equal to the recrystallization temperature of the alloy, the alloy will recrystallize into an equiaxed structure.
Since metal alloy workpieces typically are heated to temperatures greater than the alloy's recrystallization temperature before hot forging, the interior portion of the workpiece, which does not cool as fast as the workpiece surfaces, usually exhibits a fully recrystallized structure on hot forging. However, the surfaces of the workpiece can exhibit a mixture of unrecrystallized grains and fully recrystallized grains due to the lower temperatures at the surfaces resulting from relatively rapid cooling. Representative of this phenomenon,
Prior attempts to eliminate unrecrystallized grains in the surface region of a thermomechanically processed metal alloy workpiece, such as a forged bar, for example, have proven unsatisfactory. For example, excessive growth of grains in the interior portion of alloy workpieces has occurred during treatments to eliminate surface region unrecrystallized grains. Extra large grains also can make ultrasonic inspection of metal alloys difficult. Excessive grain growth in interior portions also can reduce fatigue strength of an alloy workpiece to unacceptable levels. In addition, attempts to eliminate unrecrystallized grains in the surface region of a thermomechanically processed alloy workpiece have resulted in the precipitation of deleterious intermetallic precipitates such as, for example, sigma-phase (σ-phase). The presence of such precipitates can decrease corrosion resistance.
It would be advantageous to develop methods for thermomechanically processing metal alloy workpieces in a way that minimizes or eliminates unrecrystallized grains in a surface region of the workpiece. It would also be advantageous to develop methods for thermomechanically processing metal alloy workpieces so as to provide an equiaxed recrystallized grain structure through the cross-section of the workpiece, and wherein the cross-section is substantially free of deleterious intermetallic precipitates, while limiting the average grain size of the equiaxed grain structure.
According to one non-limiting aspect of the present disclosure, a method of processing a metal alloy comprises heating a metal alloy to a temperature in a working temperature range. The working temperature range is from the recrystallization temperature of the metal alloy to a temperature just below the incipient melting temperature of the metal alloy. The metal alloy is then worked at a temperature in the working temperature range. After working the metal alloy, a surface region of the metal alloy is heated to a temperature in a working temperature range. The surface region of the metal alloy is maintained within the working temperature range for a period of time sufficient to recrystallize the surface region of the metal alloy, and to minimize grain growth in the internal region of the metal alloy. The metal alloy is cooled from the working temperature range to a temperature and at a cooling rate that minimize grain growth in the metal alloy.
According to another aspect of the present disclosure, a non-limiting embodiment of a method of processing a superaustenitic stainless steel alloy comprises heating a superaustenitic stainless steel alloy to a temperature in an intermetallic phase dissolution temperature range. The intermetallic phase dissolution temperature range may be from the solvus temperature of the intermetallic phase to just below the incipient melting temperature of the superaustenitic stainless steel alloy. In a non-limiting embodiment, the intermetallic phase is the sigma-phase (σ-phase), comprised of Fe—Cr—Ni intermetallic compounds. The superaustenitic stainless steel alloy is maintained in the intermetallic phase dissolution temperature range for a time sufficient to dissolve the intermetallic phase and minimize grain growth in the superaustenitic stainless steel alloy. Subsequently, the superaustenitic stainless steel alloy is worked at a temperature in the working temperature range from just above the apex temperature of the time-temperature-transformation curve for the intermetallic phase of the superaustenitic stainless steel alloy, to just below the incipient melting temperature of the superaustenitic stainless steel alloy. Subsequent to working, a surface region of the superaustenitic stainless steel alloy is heated to a temperature in an annealing temperature range, wherein the annealing temperature range is from a temperature just above the apex temperature of the time-temperature-transformation curve for the intermetallic phase of the alloy to just below the incipient melting temperature of the alloy The temperature of the superaustenitic stainless steel alloy does not cool to intersect the time-temperature-transformation curve during the time period from working the alloy to heating at least a surface region of the alloy to a temperature in the annealing temperature range. The surface region of the superaustenitic stainless steel alloy is maintained in the annealing temperature range for a time sufficient to recrystallize the surface region, and minimize grain growth in the superaustenitic stainless steel alloy. The alloy is cooled to a temperature and at a cooling rate that inhibit formation of the intermetallic precipitate of the superaustenitic stainless steel alloy, and minimize grain growth.
According to another non-limiting aspect of the present disclosure, a hot worked superaustenitic stainless steel alloy comprises, in weight percent based on total alloy weight, up to 0.2 carbon, up to 20 manganese, 0.1 to 1.0 silicon, 14.0 to 28.0 chromium, 15.0 to 38.0 nickel, 2.0 to 9.0 molybdenum, 0.1 to 3.0 copper, 0.08 to 0.9 nitrogen, 0.1 to 5.0 tungsten, 0.5 to 5.0 cobalt, up to 1.0 titanium, up to 0.05 boron, up to 0.05 phosphorus, up to 0.05 sulfur, iron, and incidental impurities. The superaustenitic stainless steel alloy includes an equiaxed recrystallized grain structure through a cross-section of the alloy, and an average grain size in a range of ASTM 00 to ASTM 3. The equiaxed recrystallized grain structure of the hot worked superaustenitic stainless steel alloy is substantially free of an intermetallic sigma-phase precipitate.
The features and advantages of methods, alloys, and articles described herein may be better understood by reference to the accompanying drawings in which:
The reader will appreciate the foregoing details, as well as others, upon considering the following detailed description of certain non-limiting embodiments according to the present disclosure.
It is to be understood that certain descriptions of the embodiments described herein have been simplified to illustrate only those steps, elements, features, and/or aspects that are relevant to a clear understanding of the disclosed embodiments, while eliminating, for purposes of clarity, other steps, elements, features, and/or aspects. Persons having ordinary skill in the art, upon considering the present description of the disclosed embodiments, will recognize that other steps, elements, and/or features may be desirable in a particular implementation or application of the disclosed embodiments. However, because such other steps, elements, and/or features may be readily ascertained and implemented by persons having ordinary skill in the art upon considering the present description of the disclosed embodiments, and are therefore not necessary for a complete understanding of the disclosed embodiments, a description of such steps, elements, and/or features is not provided herein. As such, it is to be understood that the description set forth herein is merely exemplary and illustrative of the disclosed embodiments and is not intended to limit the scope of the invention as defined solely by the claims.
Also, any numerical range recited herein is intended to include all sub-ranges subsumed therein. For example, a range of “1 to 10” is intended to include all sub-ranges between (and including) the recited minimum value of 1 and the recited maximum value of 10, that is, having a minimum value equal to or greater than 1 and a maximum value of equal to or less than 10. Any maximum numerical limitation recited herein is intended to include all lower numerical limitations subsumed therein and any minimum numerical limitation recited herein is intended to include all higher numerical limitations subsumed therein. Accordingly, Applicants reserve the right to amend the present disclosure, including the claims, to expressly recite any sub-range subsumed within the ranges expressly recited herein. All such ranges are intended to be inherently disclosed herein such that amending to expressly recite any such sub-ranges would comply with the requirements of 35 U.S.C. §112, first paragraph, and 35 U.S.C. §132(a).
The grammatical articles “one”, “a”, “an”, and “the”, if and as used herein, are intended to include “at least one” or “one or more”, unless otherwise indicated. Thus, the articles are used herein to refer to one or more than one (i.e., to at least one) of the grammatical objects of the article. By way of example, “a component” means one or more components, and thus, possibly, more than one component is contemplated and may be employed or used in an implementation of the described embodiments.
Any patent, publication, or other disclosure material that is said to be incorporated, in whole or in part, by reference herein is incorporated herein only to the extent that the incorporated material does not conflict with existing definitions, statements, or other disclosure material set forth in this disclosure. As such, and to the extent necessary, the disclosure as set forth herein supersedes any conflicting material incorporated herein by reference. Any material, or portion thereof, that is said to be incorporated by reference herein, but which conflicts with existing definitions, statements, or other disclosure material set forth herein is only incorporated to the extent that no conflict arises between that incorporated material and the existing disclosure material.
The present disclosure includes descriptions of various embodiments. It is to be understood that all embodiments described herein are exemplary, illustrative, and non-limiting. Thus, the invention is not limited by the description of the various exemplary, illustrative, and non-limiting embodiments. Rather, the invention is defined solely by the claims, which may be amended to recite any features expressly or inherently described in or otherwise expressly or inherently supported by the present disclosure.
It is possible to eliminate unrecrystallized surface grains in a hot worked metal alloy bar or other workpiece by performing an anneal heat treatment whereby the alloy is heated to an annealing temperature exceeding the recrystallization temperature of the alloy and held at temperature until recrystallization is complete. However, superaustenitic stainless steel alloys and certain other austenitic stainless steel alloys are susceptible to the formation of a deleterious intermetallic precipitate, such as a sigma-phase precipitate, when processed in this way. Heating larger size bars and other large mill forms of these alloys to an annealing temperature, for example, can cause the deleterious intermetallic compounds to precipitate, particularly in a center region of the mill forms. Therefore, annealing times and temperatures must be selected not only to recrystallize surface region grains, but also to solution any intermetallic compounds. To ensure that intermetallic compounds are solutioned through the entire cross-section of a large bar, for example, it may be necessary to hold the bar at the elevated temperature for a significant time. Bar diameter is a factor in determining the minimum necessary holding time to adequately solution deleterious intermetallic compounds, but minimum holding times can be as long as one to four hours, or longer. In non-limiting embodiments, minimum holding times are 2 hours, greater than 2 hours, 3 hours, 4 hours, or 5 hours. While it may be possible to select a temperature and holding time that both solutions intermetallic compounds and recrystallizes surface region unrecrystallized grains, holding at the solution temperature for long periods may also allow grains to grow to unacceptably large dimensions. For example, the macrostructure of a radial forged bar of ATI Datalloy HP™ superaustenitic stainless steel alloy that was annealed at a high temperature (2150° F.) for a long period is illustrated in
ATI Datalloy HP™ alloy is generally described in, for example, U.S. patent application Ser. No. 13/331,135, which is incorporated by reference herein in its entirety. The measured chemistry of the ATI Datalloy HP™ superaustenitic stainless steel alloy bar shown in
Referring to
Once heated to a temperature within the working temperature range, the metal alloy is worked 14 within the working temperature range. In a non-limiting embodiment, working the metal alloy within the working temperature range results in recrystallization of the grains of at least an internal region of the metal alloy. Because the surface region of the metal alloy tends to cool faster due to, for example, cooling from contact with the working dies, grains in the surface region of the metal alloy may cool below the working temperature range and may not recrystallize during working. In various non-limiting embodiments herein, a “surface region” of a metal alloy or metal alloy workpiece refers to a region from the surface to a depth of 0.001 inch, 0.01 inch, 0.1 inch, or 1 inch or greater into the interior of the alloy or workpiece. It will be understood that the depth of a surface region that does not recrystallize during working 14 depends on multiple factors, such as, for example, the composition of the metal alloy, the temperature of the alloy on commencement of working, the diameter or thickness of the alloy, the temperature of the working dies, and the like. The depth of a surface region that does not recrystallize during working is easily determined by a skilled practitioner without undue experimentation and, as such, the surface region that does not recrystallize during any particular non-limiting embodiment of the method of the present disclosure need not to be discussed further herein.
Because a surface region may not recrystallize during working, subsequent to working the metal alloy, and prior to any intentional cooling of the alloy, at least the surface region of the alloy is heated 18 to a temperature in the working temperature range. Optionally, after working 14 the metal alloy, the alloy is transferred 16 to a heating apparatus. In various non-limiting embodiments, the heating apparatus comprises at least one of a furnace, a flame heating station, an induction heating station, or any other suitable heating apparatus known to a person having ordinary skill in the art. It will be recognized that a heating apparatus may be in place at the working station, or dies, rolls, or any other hot working apparatus at the working station may be heated to minimize cooling of the contacted surface region of the alloy during working.
After at least the surface region of the metal alloy is heated 18 to within the working temperature range, the temperature of the surface region is maintained 20 in the working temperature range for a period of time sufficient to recrystallize the surface region of the metal alloy, so that the entire cross-section of the metal alloy is recrystallized. As applied to superaustenitic stainless steel alloys and austenitic alloys, the temperature of the superaustenitic stainless steel alloy or austenitic stainless steel alloy does not cool to intersect the time-temperature-transformation curve during the time period from working 14 the alloy to heating 18 at least a surface region of the alloy to a temperature in the annealing temperature range. This prevents deleterious intermetallic phases, such as, for example, sigma phase, from precipitating in the superaustenitic stainless steel alloy or austenitic alloy. This limitation is explained further below. In certain non-limiting embodiments of the methods according to the present disclosure applied to superaustenitic stainless steel alloys and other austenitic stainless steel alloys, the period of time during which the temperature of the heated surface region is maintained 20 within the annealing temperature range is a time sufficient to recrystallize grains in the surface region and dissolve any deleterious intermetallic precipitate phases.
After maintaining 20 the metal alloy in the working temperature range to recrystallize the surface region of the alloy, the alloy is cooled 22. In certain non-limiting embodiments, the metal alloy may be cooled to ambient temperature. In certain non-limiting embodiments, the metal alloy may be cooled from the working temperature range at a cooling rate and to a temperature sufficient to minimize grain growth in the metal alloy. In a non-limiting embodiment, a cooling rate during the cooling step is in the range of 0.3 Fahrenheit degrees per minute to 10 Fahrenheit degrees per minute. Exemplary methods of cooling according to the present disclosure include, but are not limited to, quenching (such as, for example, water quenching and oil quenching), forced air cooling, and air cooling. It will be recognized that a cooling rate that minimizes grain growth in the metal alloy will be dependent on many factors including, but not limited to, the composition of the metal alloy, the starting working temperature, and the diameter or thickness of the metal alloy. The combination of the steps of heating 18 at least a surface region of the metal alloy to the working temperature range and maintaining 20 the surface region within the working temperature range for a period of time to recrystallize the surface region may be referred to herein as “flash annealing”.
As used herein in connection with the present methods, the term “metal alloy” encompasses materials that include a base or predominant metal element, one or more intentional alloying additions, and incidental impurities. As used herein, “metal alloy” includes “commercially pure” materials and other materials consisting of a metal element and incidental impurities. The present method may be applied to any suitable metal alloy. According to a non-limiting embodiment, the method according to the present disclosure may be carried out on a metal alloy selected from a superaustenitic stainless steel alloy, an austenitic stainless steel alloy, a titanium alloy, a commercially pure titanium, a nickel alloy, a nickel-base superalloy, and a cobalt alloy. In a non-limiting embodiment, the metal alloy comprises an austenitic material. In a non-limiting embodiment, the metal alloy comprises one of a superaustenitic stainless steel alloy and an austenitic stainless steel alloy. In another non-limiting embodiment, the metal alloy comprises a superaustenitic stainless steel alloy. In certain non-limiting embodiments, an alloy processed by a method of the present disclosure is selected from the following alloys: ATI Datalloy HP™ alloy (UNS unassigned); ATI Datalloy 2® ESR alloy (UNS unassigned); Alloy 25-6HN (UNS N08367); Alloy 600 (UNS N06600); Hastelloy®G-2™ alloy (UNS N06975); Alloy 625 (UNS N06625); Alloy 800 (UNS N08800); Alloy 800H (UNS N08810), Alloy 800AT (UNS N08811); Alloy 825 (UNS N08825); Alloy G3 (UNS N06985); Alloy 2535 (UNS N08535); Alloy 2550 (UNS N06255); and Alloy 316L (UNS S31603).
ATI Datalloy 2® ESR alloy is available from ATI Allvac, Monroe, N.C. USA, and is generally described in International Patent Application Publication No. WO 99/23267, which is incorporated by reference herein in its entirety. ATI Datalloy 2® ESR alloy has the following nominal chemical composition, in weight percent based on total alloy weight: 0.03 carbon; 0.30 silicon; 15.1 manganese; 15.3 chromium; 2.1 molybdenum; 2.3 nickel; 0.4 nitrogen; and balance iron and incidental impurities. In general ATI Datalloy 2® alloy comprises in percent by weight based on total alloy weight: up to 0.05 carbon; up to 1.0 silicon; 10 to 20 manganese; 13.5 to 18.0 chromium; 1.0 to 4.0 nickel; 1.5 to 3.5 molybdenum; 0.2 to 0.4 nitrogen; iron; and incidental impurities.
Superaustenitic stainless steel alloys do not fit the classic definition of stainless steel because iron constitutes less than 50 weight percent of superaustenitic stainless steel alloys. Compared with conventional austenitic stainless steels, superaustenitic stainless steel alloys exhibit superior resistance to pitting and crevice corrosion in environments containing halides.
The step of working a metal alloy at an elevated temperature according to the present method may be conducted using any of known technique. As used herein, the terms “forming”, “forging”, and “radial forging” refer to thermomechanical processing (“TMP”), which also may be referred to herein as “thermomechanical working” or simply as “working”. As used herein, unless otherwise specified, “working” refers to “hot working”. “Hot working”, as used herein, refers to a controlled mechanical operation for shaping a metal alloy at temperatures at or above the recrystallization temperature of the metal alloy. Thermomechanical working encompasses a number of metal alloy forming processes combining controlled heating and deformation to obtain a synergistic effect, such as improvement in strength, without loss of toughness. See, for example, ASM Materials Engineering Dictionary, J. R. Davis, ed., ASM International (1992), p. 480.
In various non-limiting embodiments of the method 10 according to the present disclosure, and with reference to
In certain non-limiting embodiments of methods according to the present disclosure, and again referring to
In certain non-limiting embodiments of methods according to the present disclosure, and again referring to
Additionally, in non-limiting embodiments of the present methods applied to superaustenitic stainless steel alloys and austenitic stainless steel alloys, the alloy preferably is worked 14, the surface region heated 18, and the alloy maintained 20 at temperatures within the working temperature range that are sufficiently high to keep intermetallic phases that are detrimental to mechanical or physical properties of the alloys in solid solution, or to dissolve any precipitated intermetallic phases into solid solution during these steps. In a non-limiting embodiment, keeping the intermetallic phases in solid solution comprises preventing the temperature of the superaustenitic stainless steel alloy and austenitic stainless steel alloy from cooling to intersect the time-temperature-transformation curve during the time period of working the alloy to heating at least a surface region of the alloy to a temperature in the annealing temperature range. This is further explained below. In certain non-limiting embodiments of methods according to the present disclosure applied to superaustenitic stainless steel alloys and austenitic stainless steel alloys, the period of time during which the temperature of the heated surface region is maintained 20 within the working temperature range is a time sufficient to recrystallize grains in the surface region, dissolve any deleterious intermetallic precipitate phases that may have precipitated during the working 14 step due to unintentional cooling of the surface region during working 14, and minimize grain growth in the alloy. It will be recognized that the length of such a time period depends on factors including the composition of the metal alloy and the dimensions (e.g., diameter or thickness) of the metal alloy form. In certain non-limiting embodiments, the surface region of the metal alloy may be maintained 20 within the working temperature range for a period of time in a range of 1 minute to 2 hours, 5 minutes to 60 minutes, or 10 minutes to 30 minutes.
In certain non-limiting embodiments of the methods according to the present disclosure wherein the metal alloy is one of a superaustenitic stainless steel alloy and an austenitic stainless steel alloy, heating 12 comprises heating to a working temperature range from the solvus temperature of the intermetallic precipitate phase to just below the incipient melting temperature of the metal alloy. In certain non-limiting embodiments of the methods according to the present disclosure wherein the metal alloy is one of a superaustenitic stainless steel alloy and an austenitic stainless steel alloy, the working temperature range during the step of working 14 the metal alloy is from a temperature just below a solvus temperature of an intermetallic sigma-phase precipitate of the metal alloy to a temperature just below the incipient melting temperature of the metal alloy.
Without intending to be bound to any particular theory, it is believed that the intermetallic precipitates principally form in austenitic stainless steel alloys and superaustenitic stainless steel alloys because the precipitation kinetics are sufficiently rapid to permit precipitation to occur in the alloy as the temperature of any portion of the alloy cools to a temperature at or below the temperature of the nose, or apex, of the isothermal transformation curve of the alloy for the precipitation of a particular intermetallic phase.
When methods according to the present disclosure are conducted on austenitic stainless steel alloys or on superaustenitic stainless steel alloys, the step of cooling 22 the metal alloy may comprise cooling at a rate sufficient to inhibit precipitation of an intermetallic sigma-phase precipitate in the metal alloy. In a non-limiting embodiment, a cooling rate is in the range of 0.3 Fahrenheit degrees per minute to 10 Fahrenheit degrees per minute. Exemplary methods of cooling according to the present disclosure include, but are not limited to, quenching, such as, for example water quenching and oil quenching, forced air cooling, and air cooling.
Specific examples of austenitic materials that may be processed using methods according to the present disclosure include, but are not limited to: ATI Datalloy HP™ alloy (UNS unassigned); ATI Datalloy 2® ESR alloy (UNS unassigned); Alloy 25-6HN (UNS N08367); Alloy 600 (UNS N06600); Hastelloy®G-2™ alloy (UNS N06975); Alloy 625 (UNS N06625); Alloy 800 (UNS N08800); Alloy 800H (UNS N08810), Alloy 800AT (UNS N08811); Alloy 825 (UNS N08825); Alloy G3 (UNS N06985); Alloy 2550 (UNS N06255); Alloy 2535 (UNS N08535); and Alloy 316L (UNS S31603).
Referring now to
Method 50 comprises heating 52 a superaustenitic stainless steel alloy, for example, to a temperature in an intermetallic phase precipitate dissolution temperature range from the solvus temperature of the intermetallic phase precipitate in the superaustenitic stainless steel alloy to a temperature just below the incipient melting temperature of the superaustenitic stainless steel alloy. In a specific non-limiting method embodiment for Datalloy HP™ alloy, the intermetallic precipitate dissolution temperature range is from greater than 1900° F. to 2150° F. In a non-limiting embodiment, the intermetallic phase is the sigma-phase (σ-phase), which is comprised of Fe—Cr—Ni intermetallic compounds.
The superaustenitic stainless steel is maintained 53 in the intermetallic phase precipitate dissolution temperature range for a time sufficient to dissolve the intermetallic phase precipitates, and to minimize grain growth in the superaustenitic stainless steel alloy. In non-limiting embodiments, a superaustenitic stainless steel alloy or an austenitic stainless steel alloy may be maintained in the intermetallic phase precipitate dissolution temperature range for a period of time in a range of 1 minute to 2 hours, 5 minutes to 60 minutes, or 10 minutes to 30 minutes. It will be recognized that the minimum time required to maintain 53 a superaustenitic stainless steel alloy or austenitic stainless steel alloy in the intermetallic phase precipitate dissolution temperature range to dissolve the intermetallic phase precipitate depends on factors including, for example, the composition of the alloy, the thickness of the workpiece, and the particular temperature in the intermetallic phase precipitate dissolution temperature range that is applied. It will be understood that a person of ordinary skill, on considering the present disclosure, could determine the minimum time required for dissolution of the intermetallic phase without undue experimentation.
After the maintaining step 53, the superaustenitic stainless steel alloy is worked 54 at a temperature in a working temperature range from just above the apex temperature of the TTT curve for the intermetallic phase precipitate of the alloy to just below the incipient melting temperature of the alloy.
Because the surface region may not recrystallize during working 54, subsequent to working the superaustenitic stainless steel alloy, and prior to any intentional cooling of the alloy, at least a surface region of the superaustenitic stainless steel alloy is heated 58 to a temperature in an annealing temperature range. In a non-limiting embodiment, the annealing temperature range is from a temperature just above the apex temperature (see, for example,
Optionally, after working 54 the superaustenitic stainless steel alloy, the superaustenitic stainless steel alloy may be transferred 56 to a heating apparatus. In various non-limiting embodiments, the heating apparatus comprises at least one of a furnace, a flame heating station, an induction heating station, or any other suitable heating apparatus known to a person having ordinary skill in the art. For example, a heating apparatus may be in place at the working station, or the dies, rolls, or any hot working apparatus at the working station may be heated to minimize unintentional cooling of the contacted surface region of the metal alloy.
Subsequent to working 54, a surface region of the alloy is heated 58 to a temperature in an annealing temperature range. In the heating 58 step, the annealing temperature range is from a temperature just above the apex temperature (see, for example,
In a non-limiting embodiment, with reference to
Again referring to
Another aspect of the present disclosure is directed to certain metal alloy mill products. Certain metal alloy mill products according to the present disclosure comprise or consist of a metal alloy that has been processed by any of the methods according to the present disclosure, and that has not been processed to remove an unrecrystallized surface region by grinding or another mechanical material removal technique. In certain non-limiting embodiments, a metal alloy mill product according to the present disclosure comprises or consists of an austenitic stainless steel alloy or a superaustenitic stainless steel alloy that has been processed by any of the methods according to the present disclosure. In certain non-limiting embodiments, the grain structure of the metal alloy of the metal alloy mill product comprises an equiaxed recrystallized grain structure through a cross-section of the metal alloy, and an average grain size of the metal alloy is in an ASTM grain size number range of 00 to 3, or 00 to 2, or 00 to 1, as measured according to ASTM Designation E112-12. In a non-limiting embodiment, the equiaxed recrystallized grain structure of the metal alloy is substantially free of an intermetallic sigma-phase precipitate.
According to certain non-limiting embodiments, a metal alloy mill product according to the present invention comprises or consists of a superaustenitic stainless steel alloy or an austenitic stainless steel alloy having an equiaxed recrystallized grain structure throughout a cross-section of the mill product, wherein an average grain size of the alloy is in an ASTM grain size number range of 00 to 3, or 00 to 2, or 00 to 1, or 3 to 4, or an ASTM grain size number greater than 4, as measured according to ASTM Designation E112-12. In a non-limiting embodiment, the equiaxed recrystallized grain structure of the alloy is substantially free of an intermetallic sigma-phase precipitate.
Examples of metal alloys that may be included in a metal alloy mill product according to this disclosure include, but are not limited to, any of ATI Datalloy HP™ alloy (UNS unassigned); ATI Datalloy 2® ESR alloy (UNS unassigned); Alloy 25-6HN (UNS N08367); Alloy 600 (UNS N06600);®G-2™ (UNS N06975); Alloy 625 (UNS N06625); Alloy 800 (UNS N08800); Alloy 800H (UNS N08810), Alloy 800AT (UNS N08811); Alloy 825 (UNS N08825); Alloy G3 (UNS N06985); Alloy 2535 (UNS N08535); Alloy 2550 (UNS N06255); Alloy 2535 (UNS N08535); and Alloy 316L (UNS S31603).
Concerning various aspects of this disclosure, it is anticipated that the grain size of metal alloy bars or other metal alloy mill products made according to various non-limiting embodiments of methods of the present disclosure may be adjusted by altering temperatures used in the various method steps. For example, and without limitation, the grain size of a center region of a metal alloy bar or other form may be reduced by lowering the temperature at which the metal alloy is worked in the method. A possible method for achieving grain size reduction includes heating a worked metal alloy form to a temperature sufficiently high to dissolve any deleterious intermetallic precipitates formed during prior processing steps. For example, in the case of Datalloy HP™ alloy, the alloy may be heated to a temperature of about 2100° F., which is a temperature greater than the sigma-phase solvus temperature of the alloy. The sigma-solvus temperature of superaustenitic stainless steels that may be processed as described herein typically is in the range of 1600° F. to 1800° F. The alloy may then be immediately cooled to a working temperature of, for example, about 2050° F. for Datalloy HP™ alloy, without letting the temperature fall below the temperature of the apex of the TTT diagram for the sigma-phase. The alloy may be hot worked, for example, by radial forging, to a desired diameter, followed by immediate transfer to a furnace to permit recrystallization of the unrecrystallized surface grains, without letting the time for processing between the solvus temperature and the temperature of the apex of the TTT diagram exceed the time to the TTT apex, or without letting the temperature cool below the apex of the TTT diagram for the sigma-phase during this period, or so that the temperature of the superaustenitic stainless steel alloy does not cool to intersect the time-temperature-transformation curve during the time period of working the alloy to heating at least a surface region of the alloy to a temperature in the annealing temperature range. The alloy may then be cooled from the recrystallization step to a temperature and at a cooling rate that inhibit formation of deleterious intermetallic precipitates in the alloy. A sufficiently rapid cooling rate may be achieved, for example, by water quenching the alloy.
The examples that follow are intended to further describe certain non-limiting embodiments, without restricting the scope of the present invention. Persons having ordinary skill in the art will appreciate that variations of the following examples are possible within the scope of the invention, which is defined solely by the claims.
A 20 inch diameter ingot of Datalloy HP™ alloy, available from ATI Allvac, was prepared using a conventional melting technique combining argon oxygen decarburization and electroslag remelting steps. The ingot had the following measured chemistry, in weight percent based on total alloy weight: 0.007 carbon; 4.38 manganese; 0.015 phosphorus; less than 0.0003 sulfur; 0.272 silicon; 21.7 chromium; 30.11 nickel; 5.23 molybdenum; 1.17 copper; balance iron and unmeasured incidental impurities. The ingot was homogenized at 2200° F. and upset and drawn with multiple reheats on an open die press forge to a 12.5 inch diameter billet. The forged billet was further processed by the following steps which may be followed by reference to
A 20 inch diameter ingot of Datalloy HP™ alloy, available from ATI Allvac, was prepared using a conventional melting technique combining argon oxygen decarburization and electroslag remelting steps. The ingot had the following measured chemistry, in weight percent based on total alloy weight: 0.006 carbon; 4.39 manganese; 0.015 phosphorus; 0.0004 sulfur; 0.272 silicon; 21.65 chromium; 30.01 nickel; 5.24 molybdenum; 1.17 copper; balance iron and unmeasured incidental impurities. The ingot was homogenized at 2200° F. and upset and drawn with multiple reheats on an open die press forge to a 12.5 inch diameter billet. The billet was subjected to the following process steps, which may be followed by reference to
A 20 inch diameter ingot of ATI Allvac AL-6XN® austenitic stainless steel alloy (UNS N08367) is prepared using a conventional melting technique combining argon oxygen decarburization and electroslag remelting steps. The ingot has the following measured chemistry, in weight percent based on total alloy weight: 0.02 carbon; 0.30 manganese; 0.020 phosphorus; 0.001 sulfur; 0.35 silicon; 21.8 chromium; 25.3 nickel; 6.7 molybdenum; 0.24 nitrogen; 0.2 copper; balance iron and other incidental impurities. The following process steps may be better understood with reference to
A 20 inch diameter ingot of Grade 316L (UNS S31603) austenitic stainless steel alloy is prepared using a conventional melting technique combining argon oxygen decarburization and electroslag remelting steps. The ingot has the following measured chemistry, in weight percent based on total alloy weight: 0.02 carbon; 17.3 chromium; 12.5 nickel; 2.5 molybdenum; 1.5 manganese; 0.5 silicon, 0.035 phosphorus; 0.01 sulfur; balance iron and other incidental impurities. The following process steps may be better understood by reference to
A 20 inch diameter ingot of Alloy 2535 (UNS N08535), available from ATI Allvac, is prepared using a conventional melting technique combining argon oxygen decarburization and electroslag remelting steps. The ingot is homogenized at 2200° F. and upset and drawn with multiple reheats on an open die press forge to a 12.5 inch diameter billet. The 12.5 inch diameter billet is heated (see, for example,
A 20 inch diameter ingot of Alloy 2550 (UNS N06255), available from ATI Allvac, is prepared using a conventional melting technique combining argon oxygen decarburization and electroslag remelting steps. The ingot is homogenized at 2200° F. and upset and drawn with multiple reheats on an open die press forge to a 12.5 inch diameter billet. The 12.5 inch diameter billet is heated (see, for example,
It will be understood that the present description illustrates those aspects of the invention relevant to a clear understanding of the invention. Certain aspects that would be apparent to those of ordinary skill in the art and that, therefore, would not facilitate a better understanding of the invention have not been presented in order to simplify the present description. Although only a limited number of embodiments of the present invention are necessarily described herein, one of ordinary skill in the art will, upon considering the foregoing description, recognize that many modifications and variations of the invention may be employed. All such variations and modifications of the invention are intended to be covered by the foregoing description and the following claims.
