Patent Application
20140290321
The present disclosure is directed to alloy ingots and other alloy workpieces, methods for processing the same and, in particular, methods for improving the hot workability of alloy ingots and other alloy workpieces by providing a surface coating thereon.
Various alloys may be characterized as being “crack sensitive”. Ingots and other workpieces composed of crack sensitive alloys may form cracks along their surfaces and/or edges during hot working operations. Forming articles from crack sensitive alloys may be problematic because, for example, cracks formed during forging or other hot working operations may need to be ground off or otherwise removed, increasing production time and expense, and reducing yield.
During certain hot working operations, such as forging and extrusion, dies apply a force to an alloy workpiece to deform the workpiece. The interaction between the die's surfaces and the alloy workpiece's surfaces may involve heat transfer, friction, and wear. One conventional technique for reducing surface and edge cracking during hot working is to enclose the alloy workpiece in a metal alloy can before hot working. With a cylindrical workpiece, for example, the inside diameter of the alloy can may be slightly larger than the outside diameter of the workpiece. The alloy workpiece may be inserted into the alloy can such that the alloy can loosely surrounds the workpiece, and the dies contact the outer surfaces of the alloy can. The alloy can thermally insulate and mechanically protect the enclosed workpiece, thereby eliminating or reducing the incidence of crack formation on the workpiece. The alloy can thermally insulates the alloy workpiece by action of the air gaps between the workpiece and the alloy can's inner surfaces and also by directly inhibiting the alloy workpiece from radiating heat to the environment.
An alloy workpiece canning operation may result in various disadvantages. For example, mechanical contact between dies and the alloy can's outer surfaces may break apart the alloy can. In one specific case, during upset-and-draw forging of a canned workpiece, the alloy may break apart during the draw operation. In such a case, the alloy workpiece may need to be re-canned between each upset-and-draw cycle of a multiple upset-and-draw forging operation, which increases process complexity and expense. Further, the alloy may impair an operator from visually monitoring the surface of a canned alloy workpiece for cracks and other work-induced defects.
Given the foregoing drawbacks, it would be advantageous to provide a more efficient and/or more cost-effective method of hot working crack sensitive alloys. More generally, it would be advantageous to provide a method for improving the hot workability of alloy ingots and other alloy workpieces.
According to certain non-limiting embodiments, methods for processing alloy ingots and other alloy workpieces are described.
A method in accordance with certain non-limiting embodiments comprises positioning a glass fiber fabric onto an alloy workpiece. The glass fiber fabric is heated to form an at least partially molten, adherent surface coating on at least a portion of the alloy workpiece. The alloy workpiece is hot worked.
A method in accordance with certain non-limiting embodiments comprises depositing a glass particle slurry onto an alloy workpiece. The deposited glass slurry is heated to form an at least partially molten, adherent surface coating on at least a portion of the alloy workpiece. The alloy workpiece is hot worked.
Further non-limiting embodiments according to the present disclosure are directed to alloy workpieces made or processed according to any of the methods of the present disclosure.
Still further non-limiting embodiments according to the present disclosure are directed to articles of manufacture made from or including alloy workpieces made or processed according to any of the methods of the present disclosure. Such article of manufacture include, for example, jet engine components, land based turbine components, valves, engine components, shafts, and fasteners.
The various non-limiting embodiments described herein may be better understood by considering the following description in conjunction with the accompanying drawing figures.
As generally used herein, the terms “consisting essentially of” and “consisting of” are embodied in the term “comprising”.
As generally used herein, the articles “one”, “a”, “an”, and “the” refer to “at least one” or “one or more”, unless otherwise indicated.
As generally used herein, the terms “including” and “having” mean “comprising”.
As generally used herein, the term “softening point” refers to the minimum temperature at which a particular glass material no longer behaves as a rigid solid and begins to sag under its own weight.
As generally used herein, the term “about” refers to an acceptable degree of error for the quantity measured, given the nature or precision of the measurement. Typical exemplary degrees of error may be within 20%, within 10%, or within 5% of a given value or range of values.
All numerical quantities stated herein are to be understood as being modified in all instances by the term “about” unless otherwise indicated. The numerical quantities disclosed herein are approximate and each numerical value is intended to mean both the recited value and a functionally equivalent range surrounding that value. At the very least, and not as an attempt to limit the application of the doctrine of equivalents to the scope of the claims, each numerical value should at least be construed in light of the number of reported significant digits and by applying ordinary rounding techniques. Notwithstanding the approximations of numerical quantities stated herein, the numerical quantities described in specific examples of actual measured values are reported as precisely as possible.
All numerical ranges stated herein include all sub-ranges subsumed therein. For example, ranges of “1 to 10” and “between 1 and 10” are intended to include all sub-ranges between and including the recited minimum value of 1 and the recited maximum value of 10. Any maximum numerical limitation recited herein is intended to include all lower numerical limitations. Any minimum numerical limitation recited herein is intended to include all higher numerical limitations.
In the following description, certain details are set forth to provide a thorough understanding of various non-limiting embodiments of the articles and methods described herein. One of ordinary skill in the art will understand that the non-limiting embodiments described herein may be practiced without these details. In other instances, well-known structures and methods associated with the articles and methods may not be shown or described in detail to avoid unnecessarily obscuring descriptions of the non-limiting embodiments described herein.
This disclosure describes various features, aspects, and advantages of various non-limiting embodiments of articles and methods. It is understood, however, that this disclosure embraces numerous alternative embodiments that may be accomplished by combining any of the various features, aspects, and advantages of the various non-limiting embodiments described herein in any combination or sub-combination that one of ordinary skill in the art may find useful.
During hot working operations, such as, for example, forging operations and extrusion operations, a force may be applied to an alloy ingot or other alloy workpiece at a temperature greater than ambient temperature, such as above the recrystallization temperature of the workpiece, to plastically deform the workpiece. The temperature of an alloy ingot or other alloy workpiece undergoing the working operation may be greater than the temperature of the dies or other structures used to mechanically apply force to the surfaces of the workpiece. The workpiece may form temperature gradients due to cooling of its surface by heat loss to ambient air and the thermal gradient off-set between its surfaces and the contacting dies or other structures. The temperature gradients may contribute to surface cracking of the workpiece during hot working. Surface cracking is especially problematic in situations in which the alloy ingots or other alloy workpieces are formed from crack sensitive alloys.
According to certain non-limiting embodiments, the alloy workpiece may comprise a crack sensitive alloy. For example, various nickel base alloys, iron base alloys, nickel-iron base alloys, titanium base alloys, titanium-nickel base alloys, cobalt base alloys, and superalloys, such as nickel base superalloys, may be crack sensitive, especially during hot working operations. An alloy ingot or other alloy workpiece may be formed from such crack sensitive alloys and superalloys. For example, a crack sensitive alloy workpiece may be formed from alloys or superalloys selected from, but not limited to, Alloy 718 (UNS No. N07718), Alloy 720 (UNS No. N07720), Rene 41™ alloy (UNS No. N07041), Rene 88™ alloy, Waspaloy® alloy (UNS No. N07001), and Inconel® 100 alloy. Although the methods described herein are advantageous for use in connection with crack sensitive alloys, it will be understood that the methods also are generally applicable to any alloy, including, for example, alloys characterized by a relatively low ductility at hot working temperatures, alloys hot worked at temperatures from 1000° F. to 2200° F., and alloys not generally prone to cracking. As used herein, the term “alloy” includes conventional alloys and superalloys. As is understood by those having ordinary skill in the art, superalloys exhibit relatively good surface stability, corrosion and oxidation resistance, high strength, and high creep resistance at high temperatures. In various non-limiting embodiments, the alloy workpiece may comprise or be selected from an ingot, a billet, a bar, a plate, a tube, a sintered pre-form, and the like.
An alloy ingot or other alloy workpiece may be formed using, for example, conventional metallurgy techniques or powder metallurgy techniques. For example, in various non-limiting embodiments, an alloy ingot or other alloy workpiece may be formed by a combination of vacuum induction melting (VIM) and vacuum arc remelting (VAR), known as a VIM-VAR operation. In various non-limiting embodiments, an alloy workpiece may be formed by a triple melting technique, in which an electroslag remelting (ESR) operation is performed intermediate a VIM operation and a VAR operation, providing a VIM-ESR-VAR (i.e., triple melt) sequence. In other non-limiting embodiments, an alloy workpiece may be formed using a powder metallurgy operation involving atomization of molten alloy and the collection and consolidation of the resulting metallurgical powders into an alloy workpiece.
In certain non-limiting embodiments, an alloy ingot or other alloy workpiece may be formed using a spray forming operation. For example, VIM may be used to prepare a base alloy composition from a feedstock. An ESR operation may optionally be used after VIM. Molten alloy may be extracted from a VIM or ESR melt pool and atomized to form molten droplets. The molten alloy may be extracted from a melt pool using a cold wall induction guide (CIG), for example. The molten alloy droplets may be deposited using a spray forming operation to form a solidified alloy workpiece.
In certain non-limiting embodiments, an alloy ingot or other alloy workpiece may be formed using hot isostatic pressing (HIP). HIP generally refers to the isostatic application of a high pressure and high temperature gas, such as, for example, argon, to compact and consolidate powder material into a monolithic preform. The powder may be separated from the high pressure and high temperature gas by a hermetically sealed container, which functions as a pressure barrier between the gas and the powder being compacted and consolidated. The hermetically sealed container may plastically deform to compact the powder, and the elevated temperatures may effectively sinter the individual powder particles together to form a monolithic preform. A uniform compaction pressure may be applied throughout the powder, and a homogeneous density distribution may be achieved in the preform. For example, a near-equiatomic nickel-titanium alloy powder may be loaded into a metallic container, such as, for example, a steel can, and outgassed to remove adsorbed moisture and entrapped gas. The container containing the near-equiatomic nickel-titanium alloy powder may be hermetically sealed under vacuum, such as, for example, by welding. The sealed container may then be HIP'ed at a temperature and under a pressure sufficient to achieve full densification of the nickel-titanium alloy powder in the container, thereby forming a fully-densified near-equiatomic nickel-titanium alloy preform.
According to certain non-limiting embodiments, a method of processing an alloy ingot or other alloy workpiece may generally comprise depositing an inorganic material onto at least a portion of an alloy workpiece and heating the inorganic material to form a surface coating on the workpiece that reduces heat loss from the workpiece. The inorganic material may comprise one or more of a thermally insulating material comprising, for example, a material selected from a fiber, a particle, and a tape. The inorganic material may comprise, for example, one or more of aluminum oxide, calcium oxide, magnesium oxide, silicon dioxide, zirconium oxide, sodium oxide, lithium oxide, potassium oxide, boron oxide, and the like. The inorganic material may have a melting point or softening point of 500° F. or higher, such as, for example, 500° F. to 2500° F. and 1000° F. to 2200° F. The method may comprise, for example, depositing the inorganic material onto at least a portion of the surface of the alloy workpiece and heating the inorganic material to form a surface coating on the workpiece and reduce heat loss from the workpiece. In various non-limiting embodiments, heating the inorganic material includes heating the inorganic material to a forging temperature, such as 1000° F. to 2200° F. The composition and form of the inorganic material may be selected to form a viscous surface coating at the forging temperature. The surface coating may adhere to the surface of the alloy workpiece. The surface coating may be characterized as an adherent surface coating. In addition to eliminating or reducing surface cracking, the surface coating according to the present disclosure also may lubricate surfaces of the alloy ingot or other alloy workpiece during hot working operations.
Referring to
In certain non-limiting embodiments, the inorganic fibers may comprise glass fibers. The glass fibers may comprise continuous fibers and/or discontinuous fibers. Discontinuous fibers may be made, for example, by cutting or chopping continuous fibers. The glass fibers may comprise, for example, one or more of SiO2, Al2O3, and MgO. The glass fibers may comprise, for example, magnesium aluminosilicate fibers. The glass fibers may comprise, for example, magnesium aluminosilicate fibers selected from the group consisting of E-glass fibers, S-glass-fibers, S2-glass fibers, and R-glass fibers. E-glass fibers may comprise one or more of SiO2, Al2O3, B2O3, CaO, MgO, and other oxides. S-glass fibers and S2-glass fibers may comprise one or more of SiO2, Al2O3, MgO. R-glass fibers may comprise one or more of SiO2, Al2O3, CaO, and MgO. In certain non-limiting embodiments, the inorganic fibers may comprise refractory ceramic fibers. The refractory ceramic fibers may be amorphous and comprise one or more of SiO2, Al2O3, and ZrO2.
According to certain non-limiting embodiments, a plurality of the glass fibers may comprise one or more of a bundle, a strip or tow, a fabric, and a board. As generally used herein the term “fabric” refers to materials that may be woven, knitted, felted, fused, or non-woven materials, or that otherwise are constructed of fibers. The fabric may comprise a binder to hold the plurality of fibers together. In certain non-limiting embodiments, the fabric may comprise a yarn, a blanket, a mat, a paper, a felt, and the like. In certain non-limiting embodiments, the glass fibers may comprise a glass blanket. The glass blanket may comprise, for example, E-glass fibers. Exemplary glass blankets comprising E-glass fibers useful in embodiments according to the present disclosure include, but are not limited to, fibers commercially available from Anchor Industrial Sales, Inc. (Kernersville, N.C.) under the trade designation “Style 412” and “Style 412B” having a thickness of 0.062 inches, E-glass fibers having a weight of 24 oz./yd2, and a temperature rating of 1000° F. The glass fabric may comprise, for example, a fiberglass blanket, such as, for example, an E-glass blanket. The fabric may have any suitable width and length to cover at least a portion of the workpiece. The width and length of the fabric may vary according to the size and/or shape of the workpiece. The thicknesses of the fabric may vary according to the thermal conductivity of the fabric. In certain non-limiting embodiments, the fabric may have a thickness from 1-25 mm, such as 5-20 mm or 8-16 mm.
According to certain non-limiting embodiments, the inorganic particles may comprise glass particles. The glass particles may be referred to as “frits” or “fillers”. The glass particles may comprise, for example, one or more of aluminum oxide, calcium oxide, magnesium oxide, silicon dioxide, zirconium oxide, sodium and sodium oxide, lithium oxide, potassium oxide, boron oxide, and the like. In certain non-limiting embodiments, the glass particles, for example, may be free from lead or comprise only trace levels of lead. In certain embodiments, the glass particles may have a metal hot-working range of 1400-2300° F., such as, for example, 1400-1850° F., 1850-2050° F., 1850-2100° F., or 1900-2300° F. Exemplary glass particles useful in embodiments according to the present disclosure include materials commercially available from Advance Technical Products (Cincinnati, Ohio) under the trade designations “Oxylub-327”, “Oxylub-811”, “Oxylub-709”, and “Oxylub-921”.
According to certain non-limiting embodiments, the inorganic tape may comprise a glass tape. In certain embodiments, the glass tape may comprise a glass backing and an adhesive. The glass backing may comprise, for example, one or more of aluminum oxide, calcium oxide, magnesium oxide, silicon dioxide, zirconium oxide, sodium and sodium oxide, lithium oxide, potassium oxide, boron oxide, and the like. The glass backing may comprise a glass fiber, such as a glass yarn, a glass fabric, and a glass cloth. The glass backing may comprise a glass filament. In various non-limiting embodiments, the glass tape may comprise a fiberglass filament reinforced packing tape. In various non-limiting embodiments, the glass tape may comprise an adhesive tape including a glass cloth backing or a tape impregnated with glass yarn or filament. In various non-limiting embodiments, the glass tape may comprise a polypropylene backing reinforced with continuous glass yarn. In various non-limiting embodiments, the glass tape may have characteristics including: an adhesion to steel of about 55 oz./in. width (60 N/100 mm width) according to ASTM Test Method D-3330; a tensile strength of about 300 lbs./in. width (5250 N/100 mm width) according to ASTM Test Method D-3759; an elongation at break of about 4.5% according to ASTM Test Method D-3759; and/or a total thickness of about 6.0 mil (0.15 mm) according to ASTM Test Method D-3652. Exemplary glass tapes useful in embodiments according to the present disclosure are commercially available from 3M Company (St. Paul, Minn.) under the trade designation SCOTCH® Filament Tape 893.
According to certain non-limiting embodiments, a method of processing an alloy ingot or other alloy workpiece in a way that reduces thermal cracking during hot working may generally comprise disposing a glass fabric onto at least a portion of a surface of the workpiece. In certain non-limiting embodiments, the fabric may be disposed onto a substantial portion of the surface of the workpiece. The surface of an alloy workpiece may comprise, for example, a circumferential surface and two lateral surfaces disposed at each end of the circumferential surface. In certain non-limiting embodiments, the fabric may be disposed onto a substantial portion of a circumferential surface of a cylindrical alloy workpiece. In certain non-limiting embodiments, the fabric may be disposed onto the circumferential surface of the cylindrical workpiece and at least one lateral surface of the cylindrical workpiece. In at least one non-limiting embodiment, a glass blanket may be disposed onto at least a portion of a circumferential surface of a cylindrical alloy workpiece and at least one lateral surface of the cylindrical workpiece. In certain non-limiting embodiments, more than one glass fabric, such as two, three, or more, may each be disposed onto at least a portion of a surface of a cylindrical workpiece and/or at least one lateral surface of the cylindrical workpiece. The fabric may be disposed by transversely wrapping the fabric around the circumferential surface of the workpiece, for example. A person having ordinary skill in the art will understand that in certain non-limiting embodiments the glass fabric may be secured to the workpiece using adhesives and/or mechanical fasteners such as, for example, glass tape and bale wire.
In certain non-limiting embodiments, a method of processing an alloy ingot or other alloy workpiece so as to reduce thermal cracking during hot working may comprise repeating the step of disposing a glass fabric onto at least a portion of the surface of the workpiece. For example, the fabric may be wrapped around the workpiece at least one time, two times, three times, four times, or more than four times. In certain non-limiting embodiments, the fabric may be wrapped around the workpiece until a predetermined thickness is achieved. Alternatively, more than one glass fabric may be disposed onto at least a portion of a circumferential surface of a cylindrical workpiece and at least one of each lateral surface of the cylindrical workpiece until a predetermined thickness is achieved. For example, the predetermined thickness may be from 1 mm to 50 mm, such as 10 mm to 40 mm. In at least one non-limiting embodiment, the method may comprise disposing a first glass fabric onto at least a portion of the surface of the workpiece and a second glass fabric onto at least one of the first glass fabric and at least a portion of the surface of the workpiece. The first glass fabric and the second glass fabric may comprise the same or different inorganic materials. For example, the first glass fabric may comprise a first E-glass blanket and the second glass fabric may comprise a second E-glass fabric. In one non-limiting embodiment, the first glass fabric may comprise an E-glass blanket and the second glass fabric may comprise a ceramic blanket, such as, for example, a KAOWOOL blanket, which is a material produced from alumina-silica fire clay.
According to certain non-limiting embodiments, a method of processing a workpiece to reduce thermal cracking may generally comprise depositing glass particles onto at least a portion of the surface of the workpiece. In certain non-limiting embodiments, the particles may be deposited onto a substantial portion of the surface of the workpiece. In certain non-limiting embodiments, the particles may be deposited onto the circumferential surface of a cylindrical workpiece and/or at least one lateral surface of the cylindrical workpiece. Depositing the particles onto a surface of the workpiece may comprise, for example, one or more of rolling, dipping, spraying, brushing, and sprinkling. The method may comprise heating the workpiece to a predetermined temperature prior to depositing the particles. For example, a workpiece may be heated to a forging temperature, such as 1000° F. to 2000° F., and 1500° F., and rolled in a bed of glass particles to deposit the glass particles on a surface of the workpiece.
According to certain non-limiting embodiments, a method of processing an alloy ingot or other alloy workpiece to reduce thermal cracking may generally comprise disposing a glass tape onto at least a portion of the surface of the workpiece. In certain non-limiting embodiments, the tape may be disposed onto a substantial portion of the surface of the workpiece. In certain non-limiting embodiments, the tape may be disposed onto a circumferential surface of a cylindrical workpiece and/or at least one lateral surface of the workpiece. Disposing the tape onto a surface of the workpiece may comprise, for example, one or more of wrapping and taping. In various non-limiting embodiments, for example, the tape may be disposed by transversely wrapping the tape around the circumferential surface of the workpiece. In certain non-limiting embodiments, the tape may be disposed onto a surface by adhering the tape onto the surface of the workpiece. In certain non-limiting embodiments, the tape may be disposed onto at least a portion of a surface of a cylindrical alloy workpiece and/or at least a portion of a glass blanket.
In certain non-limiting embodiments, a method of processing an alloy ingot or other alloy workpiece to reduce thermal cracking may comprise repeating one or more times the step of disposing a glass tape onto at least a portion of the surface of the workpiece. For example, the tape may be wrapped around the workpiece at least one time, two times, three times, four times, or more than four times. In at least one non-limiting embodiment, the method may comprise wrapping a first glass tape onto at least a portion of a surface of the workpiece and wrapping a second glass tape onto at least one of the first glass tape and at least a portion of an un-taped surface of the workpiece. In at least one non-limiting embodiment, the method may comprise taping a first glass tape to at least a portion of the surface of the workpiece and a second glass tape to at least one of the first glass tape and at least a portion of the un-taped surface of the workpiece. The first glass tape and the second glass tape may comprise the same or different inorganic materials. In certain non-limiting embodiments, the tape may be disposed on the alloy workpiece until a predetermined thickness is achieved. Alternatively, more than one glass tape may be disposed onto at least a portion of a circumferential surface of a cylindrical alloy ingot or other alloy workpiece and at least one of each lateral surface of the cylindrical workpiece until a predetermined thickness is achieved. The predetermined thickness may be, for example, from less than 1 mm to 50 mm, such as 10 mm to 40 mm.
According to certain non-limiting embodiments, the glass material provided on the alloy workpiece may form a viscous surface coating on the workpiece when the glass material is heated. The workpiece comprising the glass material thereon may be heated in a furnace. The composition of the glass material may be selected to form a viscous surface coating at the forging temperature. For example, the oxides comprising the glass material may be selected to provide a glass material having a melting point or softening point at a predetermined temperature, such as a forging temperature. In another example, the form of the glass material, i.e., a fiber, a particle, a tape, and any combinations thereof, may be selected to form a viscous surface coating at a predetermined temperature, such as, a forging temperature. A glass fabric provided on a surface of the workpiece may form a viscous surface coating on the workpiece when the glass material is heated, for example, in a furnace at a temperature from 1900° F. to 2100° F. Glass particles provided on a surface of the workpiece may form a viscous surface coating on the workpiece when the glass material is heated, for example, in a furnace at a temperature from 1450° F. to 1550° F. A glass tape provided on a surface of the workpiece may form a viscous surface coating on the workpiece when the glass material is heated, for example, in a furnace at a temperature from 1900° F. to 2100° F.
According to certain non-limiting embodiments, a surface coating provided on a surface of an alloy ingot or other alloy workpiece may be characterized as an adherent surface coating. The viscous surface coating may form an adherent surface coating when the surface coating is cooled. For example, the viscous surface coating may form an adherent surface coating when the workpiece comprising the surface coating is removed from the furnace. A surface coating may be characterized as being “adherent” when the surface coating does not immediately flow off of a workpiece surface. For example, in various non-limiting embodiments, a surface coating may be considered “adherent” when the coating does not immediately flow off the surface when the alloy ingot or other alloy workpiece is removed from the furnace. In another example, in various non-limiting embodiments, a surface coating on a circumferential surface of an alloy workpiece having a longitudinal axis and a circumferential surface may be considered “adherent” when the coating does not immediately flow off the circumferential surface when the workpiece is disposed so that the longitudinal axis is vertically oriented, such as, for example, at 45° to 135° relative to a horizontal surface. A surface coating may be characterized as a “non-adherent” surface coating when the surface coating immediately flows off of the surface of the workpiece when the workpiece is removed from the furnace.
The temperature range over which alloys may be hot worked may take into account the temperature at which cracks initiate in the alloy and the composition and form of the inorganic material. At a given starting temperature for a hot working operation, some alloys may be effectively hot worked over a larger temperature range than other alloys because of differences in the temperature at which cracks initiate in the alloy. For alloys having a relatively small hot working temperature range (i.e., the difference between the lowest temperature at which the alloy may be hot worked and the temperature at which cracks initiate), the thickness of the inorganic material may be relatively greater to inhibit or prevent the underlying workpiece from cooling to a brittle temperature range in which cracks initiate. Likewise, for alloys having a relatively large hot working temperature range, the thickness of the inorganic material may be relatively smaller to inhibit or prevent the underlying alloy ingot or other alloy workpiece from cooling to a brittle temperature range in which cracks initiate.
According to certain non-limiting embodiments, a method of processing an alloy ingot or other alloy workpiece to reduce thermal cracking may generally comprise heating the inorganic material to form a surface coating on the workpiece. Heating the inorganic material may comprise, for example, heating the inorganic material to a temperature from 500-2500° F., such as, for example, 500-1500° F., 1000-2000° F., 1500° F.-2000° F., or 2000-2500° F., to form the surface coating. In certain non-limiting embodiments, the inorganic fibers, such as glass blankets and glass tapes, may be heated to a temperature from 2000-2500° F. In certain non-limiting embodiments, the inorganic particles, such as glass particles, may be heated to a temperature from 1500-2000° F. In certain non-limiting embodiments, the temperature may be greater than the melting point of the inorganic material. In certain non-limiting embodiments, the temperature may be greater than the temperature rating of the inorganic material. In various non-limiting embodiments, the temperature may be greater than the melting point of the glass fabric, glass particle, and/or glass tape. In one non-limiting embodiment, the temperature may be greater than the melting point of the glass blanket. As understood by a person skilled in the art, inorganic materials may not have a specific melting point and may be characterized by a “softening point”. ASTM Test Method C338-93(2008), for example, provides a standard test method for determining the softening point of a glass. As such, in certain non-limiting embodiments, the inorganic material may be heated to a temperature that is at least the softening point of the inorganic material.
In certain non-limiting embodiments, the surface coating may be formed on at least a portion of the surface of the alloy workpiece. In certain non-limiting embodiments, the surface coating may be formed on a substantial portion of the surface of the workpiece. In certain non-limiting embodiments, the surface coating may completely cover the surface of the workpiece. In certain non-limiting embodiments, the surface coating may be formed on a circumferential surface of the alloy workpiece. In certain non-limiting embodiments, the surface coating may be formed on a circumferential surface of the workpiece and at least one lateral face of the workpiece. In certain non-limiting embodiments, the surface coating may be formed on a circumferential surface of the workpiece and each lateral face of the workpiece. In certain non-limiting embodiments, the surface coating may be formed on at least a portion of the surface of the workpiece free from the inorganic material. For example, the inorganic material may be deposited onto a portion of the surface of the workpiece. The inorganic material may melt when heated. The melted inorganic material may flow to a portion of the surface of the workpiece on which the inorganic material was not deposited.
The inorganic material may be deposited to a thickness sufficient to form a surface coating thereon when heated, wherein the surface coating insulates the underlying workpiece surface from the surface of a contacting die, thereby inhibiting or preventing the underlying workpiece surface from cooling to a temperature at which the underlying workpiece surface may more readily crack during hot working. In this manner, greater hot working temperatures may generally correlate with a preference for greater surface coating thicknesses. In certain non-limiting embodiments, the surface coating may have a thickness suitable to reduce heat loss from the workpiece. In certain non-limiting embodiments, the surface coating may have a thickness of 0.1 mm to 2 mm, such as, for example, 0.5 mm to 1.5 mm, and about 1 mm. Without intending to be bound to any particular theory, the surface coating may reduce heat loss of the alloy workpiece and/or increase slippage of the workpiece relative to the die or other contacting surfaces during hot working. The surface coating may act as a thermal barrier to heat loss from the workpiece through convection, conduction, and/or radiation. In certain non-limiting embodiments, the surface coating may reduce surface friction of the alloy workpiece and act as a lubricant, and thereby increase the slippage of the workpiece during a hot working operation, e.g., forging and extruding. In certain non-limiting embodiments, the inorganic material may be deposited to a thickness sufficient to lubricate the workpiece during hot working operations.
According to certain non-limiting embodiments, a method of processing an alloy ingot or other alloy workpiece to reduce thermal cracking may generally comprise cooling the workpiece including the surface coating. Cooling the workpiece may comprise cooling the surface coating. In certain non-limiting embodiments, cooling the workpiece may comprise air cooling the workpiece. In certain non-limiting embodiments, cooling the workpiece may comprise disposing a ceramic blanket, such as, for example, a KAOWOOL blanket, onto at least one of the surface coating and at least a portion of a surface of the workpiece. In certain non-limiting embodiments, the surface of the workpiece may be cooled to room temperature.
According to certain non-limiting embodiments, a method of processing an alloy ingot or other alloy workpiece to reduce thermal cracking may generally comprise removing at least one of at least a portion of the surface coating and/or remnants of the surface coating from the workpiece. In certain non-limiting embodiments, the method may comprise, after hot working, removing at least one of a portion of the surface coating and/or remnants of the surface coating from the product formed by hot working the workpiece. Removing the surface coating or remnants may comprise, for example, one or more of shot blasting, grinding, peeling, and turning. In certain non-limiting embodiments, peeling the hot worked workpiece may comprise lathe-turning.
After initial workpiece formation, but before depositing the inorganic material and/or subsequent to hot working of the alloy workpiece, a non-limiting method of processing an alloy ingot or other alloy workpiece to reduce thermal cracking may generally comprise heating the workpiece and/or conditioning the surface of the workpiece. In certain non-limiting embodiments, an alloy workpiece may be exposed to high temperatures to homogenize the alloy composition and microstructure of the workpiece. The high temperatures may be above the recrystallization temperature of the alloy but below the melting point temperature of the alloy. For example, the workpiece may be heated to a forging temperature, the inorganic material may be deposited thereon, and the workpiece may be reheated to form a surface coating thereon. The workpiece may be heated before depositing the inorganic material to reduce the furnace time necessary to bring the workpiece to temperature. An alloy workpiece may be surface conditioned, for example, by grinding and/or peeling the surface of the workpiece. A workpiece may also be sanded and/or buffed. Surface conditioning operations may be performed before and/or after any optional heat treatment steps, such as, for example, homogenization at high temperatures.
According to certain non-limiting embodiments, a method of processing an alloy ingot or other alloy workpiece to reduce thermal cracking may generally comprise hot working the workpiece. Hot working the workpiece may comprise applying a force to the workpiece to deform the workpiece. The force may be applied with, for example, dies and/or rolls. In certain non-limiting embodiments, hot working the workpiece may comprise hot working the workpiece at a temperature from 1500° F. to 2500° F. In certain non-limiting embodiments, hot working the workpiece may comprise a forging operation and/or an extrusion operation. For example, a workpiece having a surface coating deposited onto at least a region of a surface of the workpiece may be upset forged and/or draw forged. In various non-limiting embodiments, the method may comprise after forming a surface coating on the workpiece, hot working the workpiece by forging. In various non-limiting embodiments, the method may comprise after forming a surface coating on the workpiece, hot working the workpiece by forging at a temperature from 1500° F. to 2500° F. In various non-limiting embodiments, the method may comprise after forming a surface coating on the workpiece, hot working the workpiece by extruding. In various non-limiting embodiments, the method may comprise after forming a surface coating on the workpiece, hot working the workpiece by extruding at a temperature from 1500° F. to 2500° F.
An upset-and-draw forging operation may comprise one or more sequences of an upset forging operation and one or more sequences of a draw forging operation. During an upset operation, the end surfaces of a workpiece may be in contact with forging dies that apply force to the workpiece that compresses the length of the workpiece and increases the cross-section of the workpiece. During a draw operation, the side surfaces (e.g., the circumferential surface of a cylindrical workpiece) may be in contact with forging dies that apply force to the workpiece that compresses the cross-section of the workpiece and increases the length of the workpiece.
In various non-limiting embodiments, an alloy ingot or other alloy workpiece having a surface coating deposited onto at least a region of a surface of the workpiece may be subjected to one or more upset-and-draw forging operations. For example, in a triple upset-and-draw forging operation, a workpiece may be first upset forged and then draw forged. The upset and draw sequence may be repeated twice more for a total of three sequential upset and draw forging operations. In various non-limiting embodiments, a workpiece having a surface coating deposited onto at least a region of a surface of the workpiece may be subjected to one or more extrusion operations. For example, in an extrusion operation, a cylindrical workpiece may be forced through a circular die, thereby decreasing the diameter and increasing the length of the workpiece. Other hot working techniques will be apparent to those having ordinary skill, and the methods according to the present disclosure may be adapted for use with one or more of such other techniques without the need for undue experimentation.
In various non-limiting embodiments, the methods disclosed herein may be used to produce a wrought billet from an alloy ingot on the form of a cast, consolidated, or spray formed ingot. The forge conversion or extrusion conversion of an ingot to a billet or other worked article may produce a finer grain structure in the article as compared to the former workpiece. The methods and processes described herein may improve the yield of forged or extruded products (such as, for example, billets) from workpieces because the surface coating may reduce the incidence of surface cracking of the workpiece during the forging and/or extrusion operations. For example, it has been observed that a surface coating according to the present disclosure provided on at least a region of a surface of a workpiece may more readily tolerate the strain induced by working dies. It also has been observed that a surface coating according to the present disclosure provided onto at least a portion of a surface of an alloy workpiece may also more readily tolerate the temperature differential between the working dies and the workpiece during hot working. In this manner, it has been observed that a surface coating according to the present disclosure may exhibit zero or minor surface cracking while surface crack initiation is prevented or reduced in the underlying workpiece during working.
In various non-limiting embodiments, ingot or other workpieces of various alloys having a surface coating according to the present disclosure may be hot worked to form products that may be used to fabricate various articles. For example, the processes described herein may be used to form billets from a nickel base alloy, an iron base alloy, a nickel-iron base alloy, a titanium base alloy, a titanium-nickel base alloy, a cobalt base alloy, a nickel base superalloy, and other superalloys. Billets or other products formed from hot worked ingots or other alloy workpieces may be used to fabricate articles including, but not limited to, turbine components, such as, for example, disks and rings for turbine engines and various land-based turbines. Other articles fabricated from alloy ingots or other alloy workpieces processed according to various non-limiting embodiments described herein may include, but are not limited to, valves, engine components, shafts, and fasteners.
Alloy workpieces that may be processed according to the various embodiments herein may be in any suitable form. In particular non-limiting embodiments, for example, the alloy workpieces may comprise or be in the form of ingots, billets, bars, plates, tubes, sintered pre-forms, and the like.
The various non-limiting embodiments described herein may be better understood when read in conjunction with the following representative examples. The following examples are included for purposes of illustration and not limitation.
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An alloy workpiece in the form of a generally cylindrical uncoated ingot of 718Plus® alloy (UNS No. N07818) was hot forged from a diameter of 20 inches down to a diameter of 14 inches. The workpiece developed extensive surface cracks during the forging operation. The forged workpiece was turned down to 12 inches diameter to remove the surface cracks. The turned workpiece was then hot forged from 12 inches to 10 inches, and one end of the workpiece cracked extensively during forging. The workpiece was then surface conditioned by shot blasting and a first end of the workpiece was hot forged from 10 inches to 6 inches. An E-glass blanket was wrapped around and secured to the second end of the forged workpiece, and the workpiece was placed in a furnace at a temperature of 1950° F. and heated. The E-glass blanket formed a surface coating on the second end when heated.
An alloy workpiece in the form of a 1.5 inch diameter generally cylindrical titanium Ti-6Al-4V alloy (UNS No. R56400) ingot was heated in a furnace at a temperature of 1500° F. for 1.5 hours. The heated workpiece was rolled in glass particles comprising Oxylub-327 material (available from Advance Technical Products, Cincinnati, Ohio), which has a metal hot-working range of 1400-1850° F. The workpiece was then placed in the furnace for an additional 30 minutes, and the glass particles formed a surface coating on the workpiece during the heating operation. The coated workpiece was then forged three times in three independent directions.
All documents cited in herein are incorporated herein by reference unless otherwise indicated. The citation of any document is not to be construed as an admission that it is prior art with respect to the present invention. To the extent that any meaning or definition of a term in this document conflicts with any meaning or definition of the same term in a document incorporated by reference, the meaning or definition assigned to that term in this document shall govern.
While particular non-limiting embodiments of the present invention have been illustrated and described, it would be obvious to those skilled in the art that various other changes and modifications can be made without departing from the spirit and scope of the invention. It is therefore intended to cover in the appended claims all such changes and modifications that are within the scope of this invention.
This patent application is a continuation application and claims the benefit of the filing date under 35 U.S.C. §120 of co-pending U.S. patent application No. 13/007,692, filed on Jan. 17, 2011. The content of U.S. patent application Ser. No. 12/007,692 is incorporated-by-reference into this specification.
| Number | Date | Country | |
|---|---|---|---|
| Parent | 13007692 | Jan 2011 | US |
| Child | 14302479 | US |
