Patent Application
20140238556
This present disclosure is directed at a new type of warm formable advanced high strength steel (AHSS). This steel can be warm formed due to its unique structure which allows it to develop relatively high strength without the need for austenitizing and quenching.
Existing hot forming steels are variations of martensitic grades produced by various trade names including USIBOR™, DUXTIBOR™, etc. This class of materials can develop high strength commonly in the 1200 to 1600 MPa range with limited ductility of 5 to 8%. In the as-produced condition, these grades of steel are in their annealed soft conditions and consist of mainly ferrite plus cementite and thus exhibit low tensile strength. To produce high strength parts, the steel must then be heated up to its austenitizing temperature (i.e. A3), which depending on the chemistry is typically in the range of 850 to 1000° C. After an appropriate hold time to form a single phase solid solution of austenite, the steel is then deformed to produce a part which can be a wide variety of structural and non-structural components. After deformation, the part is held to ensure the shape is maintained and then quenched in oil or water depending on the thickness of the part formed and the specific hardenability of the steel alloy. Often small additions of boron typically up to 0.05 wt % are used to increase the hardenability of the steel which means that it opens up the process window for martensite formation. Upon proper quenching, the steel part then forms a martensitic structure which is strong and brittle. Subsequent heat treating is commonly done to produce tempered martensite which results in an improvement of ductility through sacrificing some of the strength levels.
The present disclosure is directed at steel alloys which may be wormed formed (treated at temperatures of 200° C. to 850° C. for time period of 1.0 second to 1 hour either by direct heating or induction heating). The elemental composition ranges (atomic percent) include: Fe present at 48.0 to 81.0, B at 2.0-8.0, Si at 4.0 to 14.0 and at least one austenite stabilizer (element that stabilizes austenite formation) comprising one or more of Cu, Mn and Ni, where the Cu is present at 0.1-6.0 atomic percent, Mn is present at 0.1-21.0 atomic percent and Ni is present at 0.1-16.0 atomic percent. Optionally, one may include Cr at a level of up to 32.0 atomic percent. Other optional elements such as C, Al, Ti, V, Nb, Mo, Zr, W and Pd may be present at up to 10.0 atomic percent. Impurities known/expected to be present include Nb, Ti, S, O, N, P, W, Co, Sn, which may present at levels up to 10.0 atomic percent. The alloys herein that are suitable for warm forming include the Class 1, Class 2 and Class 3 Steels described herein. Steel alloys of the present disclosure with application to centrifugal casting provide unique property combinations in wide ranges of strength and ductility depending on the aforementioned class of steel due to new enabling structure types facilitated by new enabling mechanisms.
The new class of warm forming steel does not need to be austenitized due to a much different metallurgy and enabling metallurgical transformations (i.e. not austenite to martensite). In
As shown in
To further explain these differences, a model phase diagram for the warm forming alloys is provided in
The new type of steel produced herein may include any of the Class 1, Class 2 or Class 3 Steel Alloys noted herein that are warm formed, but preferably include warm forming of the Class 2 or Class 3 Steel Alloys. These Class 1, Class 2 and Class 3 Steel structure is stable to high temperatures and could be hot formed at conventional temperatures known for hot forming processes with typical hot forming ductility from 30 to 120%. However, the Class 1, Class 2 and Class 3 Steels herein exhibit relatively high strength and ductility at room temperature and maintains its high ductility at warm temperatures (i.e. 200 to 850°). Thus, it is applicable for cold deformation through a variety of methods including cold rolling, stamping, roll forming, hydroforming etc. Furthermore, the Class 1, Class 2 and Class 3 steel can now be treated by a warm forming process. In warm forming, the aforementioned steels are now heated up to a temperature range which is less than hot forming, typically 200 to 850° C., and for a time period of 1.0 seconds to 1 hour via direct heating (e.g. furnace heating) and/or induction heating. This temperature range is enabling for manufacturing for a number of key factors which will be described subsequently. In short, warm forming may now reduce cost while producing new functionality through minimizing or avoiding springback issues found in cold forming steels.
Steels are protected from corrosion through a process generally called galvanization which provides an anodic sacrificial coating to protect the surface of the steel from corrosion. There are various methods of applying the zinc or zinc alloy to the surface including conventional galvanization, hot dip galvanization, galvannealing etc. All of these processes share the same feature with zinc being bonded to different extents to the surface of steel. For hot forming this is a problem, since zinc exhibits a low melting point of 419° C. Thus, during hot forming of conventional martensitic/press formable steels, the zinc coating melts and vaporizes off, thus leaving the resulting steel part vulnerable to corrosive attack. While efforts are being done to produce thicker initial layers of zinc and/or to shorten the cycle time of hot forming to limit high temperature exposure, the results have been ineffective, resulting in costly post part forming coating steps to restore the anodic surface. Through warm forming at temperatures below the melting point of zinc (i.e. ˜200 to ˜419° C.), the problem of zinc loss can be minimized or entirely avoided. Thus the new NanoModal steels processed through warm forming creates new functionality through the ability to pre-coat with conventional galvanization processes and then maintaining this protective coating in the finished warm deformed part.
Conventional hot forming lines utilize conveyor type continuous ovens which allow the hot formed parts to be feed in a continuous manner reaching their targeted austenitizing temperature prior to hot deformation. The length of these continuous gas fired ovens can be upwards of 50 meters and if any issue occurs during the hot forming operation, all of the parts moving through the long furnace are generally scrapped since during subsequent re-heating their metallurgical structure will be deleteriously non-recoverably affected. By heating up to lower temperature for warm forming, the length of this continuous oven used will be needed to be much less thus, requiring less infrastructure, lower amounts of scrapped parts, and especially lower energy cost. This ultimately results in lower cost parts thus, enabling the technology for a wider range of applications.
A cost factor limiting hot forming is the scale/oxide removal which forms during the elevated temperature exposure and then needs to be removed through existing shot/grit blasting processes. The oxidation occurs due to the elevated temperature exposure necessary to austenitize existing materials. Furthermore, the process does not lend itself to inert gas atmospheres because after hot forming, the parts must be quenched in a liquid medium to form martensite, thus creating additional oxidation. With the new class of Warm Forming steels, the temperature of deformation will be much lower which limits/prevents the oxidation typical for high temperature exposure. Additionally, since the Warm Forming steels do not need to be quenched and they exhibit an insensitive response to cooling rates in the solid state, the warm formed parts may be able to be processed while remaining in an inert atmosphere to prevent or minimize oxidation. This then is expected to result in a part which does not need to go through the expensive grit/shot blasting processes since scale formation is avoided.
Existing hot forming steels need to be quenched from their high temperature austenitizing temperatures in order to form the martensitic structure that provides high strength. During quenching into oil, water, salt water brines, etc. part distortion and/or cracking can occur which can create higher rates of scraps. Additionally, since the formation of the martensitic structure is highly cooling rate dependent, some areas of insufficient cooling may occur for example when a vapor barrier is created from the liquid medium. This results in lower strength levels in certain areas creating a limiting strength debit which while accounted for in the part design often results in higher gauge thicknesses and higher weight parts than necessary in order to overcome local strength variations. The new class of NanoModal Warm Forming Steels does not need to be water quenched and do not need to be heated up to the high temperatures found in conventional austenitizing. Thus, strict dimensional control is possible due to the lack of quench distortion. This results in a lower scrap rate and reduced cost enabling the technology.
Due to the fact that existing martensitic steels need to be austenitized at high temperatures, hot deformed, and then quenched in a liquid medium, the resulting part is distorted from the original blank dimensions. Due to the presence of distortion, especially during quenching, the final details (i.e. final trimming, hole incorporation, etc.) in the part cannot be pre-shaped in the starting blanks. Thus, expensive laser trimming or mechanical re-striking in a post stamping operation is needed which requires expensive dies that need regular maintenance to handle the extremely strong material resulting from the hot forming needed as a final post finishing process to put in the final holes and trim to the final part dimensions. Through warm forming, there is a lot less temperature range resulting in a lot less thermal expansion and this along with the lack of the need to quench, means that the Warm Forming Steels offer previously unknown design and process capability. Thus, the starting blanks can be fully or partially preformed with holes and trimmed appropriately prior to warm forming, thus creating new functionality and eliminating the final costly laser trimming processing inherent to existing hot forming processes.
The non-stainless steel alloys herein are such that they are capable of formation of what is described herein as Class 1 Steel, Class 2 Steel or Class 3 Steel which are preferably crystalline (non-glassy) with identifiable crystalline grain size morphology. The ability of the alloys to form Class 1, Class 2 or Class 3 Steels herein is described in detail herein. However, it is useful to first consider a description of the general features of Class 1, Class 2 and Class 3 Steels, which is now provided below.
The formation of Class 1 Steel herein is illustrated in
The Modal Structure of Class 1 Steel will therefore initially indicate, when cooled from the melt, the following grain sizes: (1) matrix grain size of 500 nm to 20,000 nm containing austenite and/or ferrite; (2) boride grain size of 25 nm to 500 nm (i.e. non-metallic grains such as M2B where M is the metal and is covalently bonded to B). The boride grains may also preferably be “pinning” type phases which is reference to the feature that the matrix grains will effectively be stabilized by the pinning phases which resist coarsening at elevated temperature. Note that the metal boride grains have been identified as exhibiting the M2B stoichiometry but other stoichiometries are possible and may provide pinning including M3B, MB (M1B1), M23B6, and M7B3.
The Modal Structure of Class 1 Steel may be subjected to thermomechanical deformation and/or heat treatment, resulting in some variation in properties, but the Modal Structure may be maintained.
When the Class 1 Steel noted above is exposed to a mechanical stress, the observed stress versus strain diagram is illustrated in
Reference to the hexagonal phases may be understood as a dihexagonal pyramidal class hexagonal phase with a P63mc space group (#186) and/or a ditrigonal dipyramidal class with a hexagonal P6bar2C space group (#190). In addition, the mechanical properties of such second type structure of the Class 1 Steel are such that the tensile strength is observed to fall in the range of 700 MPa to 1400 MPa, with an elongation of 10-50%. Furthermore, the second type structure of the Class 1 Steel is such that it exhibits a strain hardening coefficient from 0.1 to 0.4 that is nearly flat after undergoing the indicated yield. The strain hardening coefficient is reference to the n-value in the formula σ=Kεn, where σ represents the applied stress on the material, ε is the strain and K is the strength coefficient. The value of the strain hardening exponent n lies between 0 and 1. A value of 0 means that the alloy is a perfectly plastic solid (i.e. the material undergoes non-reversible changes to applied force), while a value of 1 represents a 100% elastic solid (i.e. the material undergoes reversible changes to an applied force).
Table 1A below provides a comparison and performance summary for Class 1 Steel herein.
The formation of Class 2 Steel herein is illustrated in
As shown therein, Structure #1 is initially formed in which Modal Structure is the result of starting with a liquid melt of the alloy and solidifying by cooling, which provides nucleation and growth of particular phases having particular grain sizes. Grain size herein may again be understood as the size of a single crystal of a specific particular phase preferably identifiable by methods such as scanning electron microscopy or transmission electron microscopy. Accordingly, Structure #1 of the Class 2 Steel may be preferably achieved by processing through either laboratory scale procedures and/or through industrial scale methods such as powder atomization or alloy casting.
The Modal Structure of Class 2 Steel will therefore initially indicate, when cooled from the melt, the following grain sizes: (1) matrix grain size of 500 nm to 20,000 nm containing austenite and/or ferrite; (2) boride grain size of 25 nm to 500 nm (i.e. non-metallic grains such as M2B where M is the metal and is covalently bonded to B). The boride grains may also preferably be “pinning” type phases which are referenced to the feature that the matrix grains will effectively be stabilized by the pinning phases which resist coarsening at elevated temperature. Note that the metal boride grains have been identified as exhibiting the M2B stoichiometry but other stoichiometries are possible and may provide pinning including M3B, MB (M1B1), M23B6, and M7B3 and which are unaffected by Mechanisms #1 or #2 noted above). Reference to grain size is again to be understood as the size of a single crystal of a specific particular phase preferably identifiable by methods such as scanning electron microscopy or transmission electron microscopy. Furthermore, Structure #1 of Class 2 steel herein includes austenite and/or ferrite along with such boride phases.
In
Characteristic of the Static Nanophase Refinement Mechanism #1 in Class 2 steel, the micron scale austenite phase (gamma-Fe) which was noted as falling in the range of 500 nm to 20,000 nm is partially or completely transformed into new phases (e.g. ferrite or alpha-Fe). The volume fraction of ferrite (alpha-iron) initially present in the Modal Structure (Structure 1) of Class 2 steel is 0 to 45%. The volume fraction of ferrite (alpha-iron) in Structure #2 as a result of Static Nanophase Refinement Mechanism #2 is typically from 20 to 80%. The static transformation preferably occurs during elevated temperature heat treatment and thus involves a unique refinement mechanism since grain coarsening rather than grain refinement is the conventional material response at elevated temperature.
Accordingly, grain coarsening does not occur with the alloys of Class 2 Steel herein during the Static Nanophase Refinement mechanism. Structure #2 is uniquely able to transform to Structure #3 during Dynamic Nanophase Strengthening and as a result Structure #3 is formed and indicates tensile strength values in the range from 800 to 1800 MPa with 5 to 40% total elongation.
Depending on alloy chemistries, nano-scale precipitates can form during Static Nanophase Refinement and the subsequent thermal process in some of the non-stainless high-strength steels. The nano-precipitates are in the range of 1 nm to 200 nm, with the majority (>50%) of these phases 10˜20 nm in size, which are much smaller than the boride pinning phase formed in Structure #1 for retarding matrix grain coarsening. Also, during Static Nanophase Refinement, the boride grain sizes grow larger to a range from 200 to 2500 nm in size.
Expanding upon the above, in the case of the alloys herein that provide Class 2 Steel, when such alloys exceed their yield point, plastic deformation at constant stress occurs followed by a dynamic phase transformation leading toward the creation of Structure #3. More specifically, after enough strain is induced, an inflection point occurs where the slope of the stress versus strain curve changes and increases (
With further straining during Dynamic Nanophase Strengthening, the strength continues to increase but with a gradual decrease in strain hardening coefficient value up to nearly failure. Some strain softening occurs but only near the breaking point which may be due to reductions in localized cross sectional area at necking. Note that the strengthening transformation that occurs at the material straining under the stress generally defines Mechanism #2 as a dynamic process, leading to Structure #3. By dynamic, it is meant that the process may occur through the application of a stress which exceeds the yield point of the material. The tensile properties that can be achieved for alloys that achieve Structure 3 include tensile strength values in the range from 800 to 1800 MPa and 5 to 40% total elongation. The level of tensile properties achieved is also dependent on the amount of transformation occurring as the strain increases corresponding to the characteristic stress strain curve for a Class 2 steel.
Thus, depending on the level of transformation, tunable yield strength may also now be developed in Class 2 Steel herein depending on the level of deformation and in Structure #3 the yield strength can ultimately vary from 400 MPa to 1700 MPa. That is, conventional steels outside the scope of the alloys here exhibit only relatively low levels of strain hardening, thus their yield strengths can be varied only over small ranges (e.g., 100 to 200 MPa) depending on the prior deformation history. In Class 2 steels herein, the yield strength can be varied over a wide range (e.g. 400 to 1700 MPa) as applied to Structure #2 transformation into Structure #3, allowing tunable variations to enable both the designer and end users in a variety of applications, and utilize Structure #3 in various applications such as crash management in automobile body structures.
With regards to this dynamic mechanism, new and/or additional precipitation phase or phases are observed that indicates identifiable grain sizes of 1 nm to 200 nm. In addition, there is the further identification in said precipitation phase a dihexagonal pyramidal class hexagonal phase with a P63mc space group (#186), a ditrigonal dipyramidal class with a hexagonal P6bar2C space group (#190), and/or a M3Si cubic phase with a Fm3m space group (#225). Accordingly, the dynamic transformation can occur partially or completely and results in the formation of a microstructure with novel nanoscale/near nanoscale phases providing relatively high strength in the material. That is, Structure #3 may be understood as a microstructure having matrix grains sized generally from 100 nm to 2000 nm which are pinned by boride phases which are in the range of 200 to 2500 nm and with precipitate phases which are in the range of 1 nm to 200 nm. The initial formation of the above referenced precipitation phase with grain sizes of 1 nm to 200 nm starts at Static Nanophase Refinement and continues during Dynamic Nanophase Strengthening leading to Structure 3 formation. The volume fraction of the precipitation phase with grain size from 1 nm to 200 nm in Structure 2 increases in Structure 3 and assists with the identified strengthening mechanism. It should also be noted that in Structure 3, the level of gamma-iron is optional and may be eliminated depending on the specific alloy chemistry and austenite stability.
Note that dynamic recrystallization is a known process but differs from Mechanism #2 (
Table 1B below provides a comparison of the structure and performance features of Class 2 Steel herein.
Class 3 steel is associated with formation of a High Strength Lamellae Nanomodal Structure through a multi-step process as now described herein.
In order to achieve a tensile response involving high strength with adequate ductility in non-stainless carbon-free steel alloys, a preferred seven-step process is now disclosed and shown in
Structure #1 involving the formation of the Modal Structures (i.e. bi, tri, and higher order) may be achieved in the alloys with the referenced chemistries in this application by processing through the laboratory scale as shown and/or through industrial scale methods involving chill surface processing such as twin roll casting or thin slab casting. The Modal Structure of Class 3 Steel will therefore initially indicate, when cooled from the melt, the following grain sizes: (1) matrix grain size of 500 nm to 20,000 nm containing ferrite or alpha-Fe (required) and optionally austenite or gamma-Fe; and (2) boride grain size of 100 nm to 2500 nm (i.e. non-metallic grains such as M2B where M is the metal and is covalently bonded to B); (3) yield strengths of 350 to 1000 MPa; (4) tensile strengths of 400 to 1200 MPa; and total elongation of 0-3.0%. It will also indicate dendritic growth morphology of the matrix grains. The boride grains may also preferably be “pinning” type phases which is reference to the feature that the matrix grains will effectively be stabilized by the pinning phases which resist coarsening at elevated temperature. Note that the metal boride grains have been identified as exhibiting the M2B stoichiometry but other stoichiometries are possible and may provide pinning including M3B, MB (M1B1), M23B6, and M7B3 and which are unaffected by Mechanism #1, #2 or #3 noted above). Reference to grain size is again to be understood as the size of a single crystal of a specific particular phase preferably identifiable by methods such as scanning electron microscopy or transmission electron microscopy. Accordingly, Structure #1 of Class 3 steel herein includes ferrite along with such boride phases.
Structure #2 involves the formation of the Modal Lath Phase Structure with uniformly distributed precipitates from Modal Structure (Structure 1) with dendritic morphology though Mechanism #1. Lath phase structure may be generally understood as a structure composed from plate-shaped crystal grains. Reference to “dendritic morphology” may be understood as tree-like and reference to “plate shaped” may be understood as sheet like. Lath structure formation preferably occurs at elevated temperature (e.g. at temperatures of 700° C. to 1200° C.) through plate-like crystal grain formation with: (1) lath structural grain sizes typically from 100 to 10,000 nm; (2) boride grain size of 100 nm to 2,500 nm; (3) yield strengths of 350 MPa to 1400 MPa; (4) tensile strengths of 350 MPa to 1600 MPa; (5) elongation of 0-12%. Structure #2 also contains alpha-Fe and gamma-Fe remains optional.
A second phase of boride precipitates with a size typically from 100 to 1000 nm may be found distributed in the lath matrix as isolated particles. The second phase of boride precipitates may be understood as non-metallic grains of different stoichiometry (M2B, M3B, MB (M1B1), M23B6, and M7B3) where M is the metal and is covalently bonded to Boron. These boride precipitates are distinguished from the boride grains in Structure #1 with little or no change in size.
Structure #3 (Lamellae Nanomodal Structure) involves the formation of the lamellae morphology as a result of static transformation of ferrite into one or several phases through Mechanism #2 identified as Lamellae Nanophase Creation. Static transformation is a decomposition of the parent phase into new phase or several new phases due to alloying elements distribution by diffusion during elevated temperature heat treatment, which may preferably occur in the temperature range from 700° C. to 1200° C. Lamellae (or layered) structure is composed of alternating layers of two phases whereby individual lamellae exist within a colony connected in three dimensions. In Class 3 alloys, Lamellae Nanomodal Structure contains: (1) lamellas of 100 nm to 1000 nm wide with a thickness in the range of 100 nm to 10,000 nm and with a length of 0.1 to 5 microns; (2) boride grains of 100 nm to 2500 nm of different stoichiometry (M2B, M3B, MB (M1B1), M23B6, and M7B3) where M is the metal and is covalently bonded to Boron, (3) precipitation grains of 1 nm to 100 nm; (4) yield strength of 350 MPa to 1400 MPa. The Lamellae Nanomodal Structure continues to contain alpha-Fe and gamma-Fe remains optional.
Lamellae Nanomodal Structure (Structure #3) transforms into Structure #4 through Dynamic Nanophase Strengthening (Mechanism #3, exposure to mechanical stress) during plastic deformation (i.e. exceeding the yield stress for the material) displaying relatively high tensile strengths in the range of 1000 MPa to 2000 MPa. In
The strengthening during deformation is related to phase transformation that occurs as the material strains under stress and defines Mechanism #3 as a dynamic process. For the alloy to display high strength at the level described in this application, lamellae structure is preferably formed prior to deformation. Specific to this mechanism, the micron scale austenite phase is transformed into new phases with reductions in microstructural feature scales generally down to the nanoscale regime. Some fraction of austenite may initially form in some Class 3 alloys during casting and then may remain present in Structure #1 and Structure #2. During straining when stress is applied, new or additional phases are formed with nanograins typically in a range from 1 to 100 nm.
In the post-deformed Structure #4 (High Strength Lamellae Nanomodal Structure), the ferrite grains contain alternating layers with nanostructure composed from new phases formed during deformation. Depending on the specific chemistry and the stability of the austenite, some austenite may be additionally present. In contrast with layers in Structure #3 where each layer represents a single or just few grains, in Structure #4, a large number of nanograins of different phases are present as a result of Dynamic Nanophase Strengthening. Since nanoscale phase formation occurs during alloy deformation, it represents a stress induced transformation and defined as a dynamic process. Nanoscale phase precipitations during deformation are responsible for extensive strain hardening of the alloys. The dynamic transformation can occur partially or completely and results in the formation of a microstructure with novel nanoscale/near nanoscale phases specified as High Strength Lamellae Nanomodal Structure (Structure #4) that provides high strength in the material. Thus the Structure #4 can be formed with various levels of strengthening depending on specific chemistry and the amount of strengthening achieved by Mechanism #3.
Table 1C below provides a comparison of the structure and performance features of Class 3 Steel herein.
In the new alloys, melting occurs in one or multiple stages with initial melting from ˜1000° C. depending on alloy chemistry and final melting temperature might be up to ˜1500° C. Variations in melting behavior reflect a complex phase formation at chill surface processing of the alloys depending on their chemistry. The density of the alloys varies from 7.2 g/cm3 to 8.2 g/cm3. The mechanical characteristic values in the alloys from each Class will depend on alloy chemistry and processing/treatment condition. For Class 1 Steels, the ultimate tensile strength values may vary from 700 to 1500 MPa with tensile elongation from 5 to 40%. The yield stress is in a range from 400 to 1300 MPa. For Class 2 Steels, the ultimate tensile strength values may vary from 800 to 1800 MPa with tensile elongation from 5 to 40%. The yield stress is in a range from 400 to 1700 MPa. For Class 3 Steels, the ultimate tensile strength values may vary from 1000 to 2000 MPa with tensile elongation from 0.5 to 15%. The yield stress is in a range from 500 to 1800 MPa. Additional classes of steel are anticipated with possible yield strengths, tensile strengths, and elongation values outside of the limits listed above.
The chemical composition of the alloys studied is shown in Table 2 which provides the preferred atomic ratios utilized. These chemistries have been studied by using material processing through sheet casting in a Pressure Vacuum Caster (PVC). Using high purity elements or ferroadditives and other readily commercially available constituents, 35 g alloy feedstocks of the targeted alloys were weighed out according to the atomic ratios provided in Table 2. The feedstock material was then placed into the copper hearth of an arc-melting system. The feedstock was arc-melted into an ingot using high purity argon as a shielding gas. The ingots were flipped several times and re-melted to ensure homogeneity. After mixing, the ingots were then cast in the form of a finger approximately 12 mm wide by 30 mm long and 8 mm thick. The resulting fingers were then placed in a PVC chamber, melted using RF induction and then ejected onto a copper die designed for casting 3 by 4 inches sheets with thickness of 1.8 mm. An example of the cast plate is shown in
The atomic percent of Fe present may therefore be 48.0, 48.1, 48.2, 48.3, 48.4, 48.5, 48.6, 48.7, 48.8, 48.9, 49.0, 49.1, 49.2, 49.3, 49.4, 49.5, 49.6, 49.7, 49.8, 49.9, 50.0, 50.1, 50.2, 50.3, 50.4, 50.5, 50.6, 50.7, 50.8, 50.9, 51.0, 51.1, 51.2, 51.3, 51.4, 51.5, 51.6, 51.7, 51.8, 51.9, 52.0, 52.1, 52.2, 52.3, 52.4, 52.5, 52.6, 52.7, 52.8, 52.9, 53.0, 53.1, 53.2, 53.3, 53.4, 53.5, 53.6, 53.7, 54.8, 53.9, 53.0 53.1, 53.2, 53.3, 53.4, 53.5, 53.6, 53.7, 53.8, 53.9, 54.0, 54.1, 54.2, 54.3, 54.4, 54.5, 54.6, 54.7, 54.8, 54.9, 55.0, 55.1, 55.2, 55.3, 55.4, 55.5, 55.6, 55.7, 55.8, 55.9, 56.0, 56.1, 56.2, 56.3, 56.4, 56.5, 56.6, 56.7, 56.8, 56.9 57.0, 57.1, 57.2, 57.3, 57.4, 57.5, 57.6, 57.7, 57.8, 57.9, 58.0, 58.1, 58.2, 58.3, 58.4, 58.5, 58.6, 58.7, 58.8, 58.9, 59.0, 59.1, 59.2, 59.3, 59.4, 59.5, 59.6, 59.7, 59.8, 59.9, 60.0, 60.1, 60.2, 60.3, 60.4, 60.5, 60.6, 60.7, 60.8, 60.9 61.0, 61.1, 61.2, 61.3, 61.4, 61.5, 61.6, 61.7, 61.8, 61.9, 62.0, 62.1, 62.2, 62.3, 62.4, 62.5, 62.6, 62.7, 62.8, 62.9, 63.0, 63.1, 63.2, 63.3, 63.4, 63.5, 63.6, 63.7, 63.8, 63.9, 64.0, 64.1, 64.2, 64.3, 64.4, 64.5, 64.6, 64.7, 64.8, 64.9, 65.0, 65.1, 65.2, 65.3, 65.4, 65.5, 65.6, 65.7, 65.8, 65.9, 66.0, 66.1, 66.2, 66.3, 66.4, 66.5, 66.6, 66.7, 66.8, 66.9, 67.0, 67.1, 67.2, 67.3, 67.4, 67.5, 67.6, 67.7, 67.8, 67.9, 68.0, 68.1, 68.2, 68.3, 68.4, 68.5, 68.6, 68.7, 68.8, 68.9, 69.0, 69.1, 69.2, 69.3, 69.4, 69.5, 69.6, 69.7, 69.8, 69.9, 70.0, 70.1, 70.2, 70.3, 70.4, 70.5, 70.6, 70.7, 70.8, 70.9, 71.0, 71.1, 71.2, 71.3, 71.4, 71.5, 71.6, 71.7, 71.8, 71.9, 72.0, 72.1, 72.2, 72.3, 72.4, 72.5, 72.6, 72.7, 72.8, 72.9, 73.0, 73.1, 73.2, 73.3, 73.4, 73.5, 73.6, 73.7, 73.8, 73.9, 74.0, 74.1, 74.2, 74.3, 74.4, 74.5, 74.6, 74.7, 74.8, 74.9, 75.0, 75.1, 75.2, 75.3, 75.4, 75.5, 75.6, 75.7, 75.8, 75.9, 76.0, 76.1, 76.2, 76.3, 76.4, 76.5, 76.6, 76.7, 76.8, 76.9, 77.0, 77.1, 77.2, 77.3, 77.4, 77.5, 77.6, 77.7, 77.8, 77.9, 78.0, 78.1, 78.2, 78.3, 78.4, 78.5, 78.6, 78.7, 78.8, 78.9, 79, 79.1, 79.2, 79.3, 79.4, 79.5, 79.6, 79.7, 79.8, 79.9, 80.0, 80.1, 80.2, 80.3, 80.4, 80.5, 80.6, 80.7, 80.8, 80.9, 81.0.
The atomic percent of B may therefore be 2.0, 2.1, 2.2, 2.3, 2.4, 2.5, 2.6 2.7, 2.8, 2.9 3.0, 3.1, 3.2, 3.3, 3.4, 3.5, 3.6, 3.7, 3.8, 3.9, 4.0, 4.1, 4.2, 4.3, 4.4, 4.5, 4.6, 4.7, 4.8, 4.9, 5.0, 5.1, 5.2, 5.3, 5.4, 5.5, 5.6, 5.7, 5.8, 5.9, 6.0, 6.1, 6.2, 6.3, 6.4, 6.5, 6.6, 6.7, 6.8, 6.9, 7.0, 7.1, 7.2, 7.3, 7.4, 7.5, 7.6, 7.7, 7.8, 7.9, 8.0.
The atomic percent of Si may therefore be 4.0, 4.1, 4.2, 4.3, 4.4, 4.5, 4.6, 4.7, 4.8, 4.9, 5.0, 5.1, 5.2, 5.3, 5.4, 5.5, 5.6, 5.7, 5.8, 5.9, 6.0, 6.1, 6.2, 6.3, 6.4, 6.5, 6.6, 6.7, 6.8, 6.9, 7.0, 7.1, 7.2, 7.3, 7.4, 7.5, 7.6, 7.7, 7.8, 7.9, 8.0, 8.1, 8.2, 8.3, 8.4, 8.5, 8.6, 8.7, 8.8, 8.9, 9.0, 9.1, 9.2, 9.3, 9.4, 9.5, 9.6, 9.7, 9.8, 9.9, 10.0, 10.1, 10.2, 10.3, 10.4, 10.5, 10.6, 10.7, 10.8, 10.9, 11.0, 11.1, 11.2, 11.3, 11.4, 11.5, 11.6, 11.7, 11.8, 11.9, 12.0, 12.1, 12.2, 12.3, 12.4, 12.5, 12.6, 12.7, 12.8, 12.9, 13.0, 13.1, 13.2, 13.3, 13.4, 13.5, 13.6, 13.7, 13.8, 13.9, 14.0.
The atomic percent of Cu may therefore be 0.1, 0.2, 0.3, 0.4, 0.5, 0.6, 0.7, 0.8, 0.9, 1.0, 1.1, 1.2, 1.3, 1.4, 1.5, 1.6, 1.7, 1.8, 1.9, 2.0, 2.1, 2.2, 2.3, 2.4, 2.5, 2.6 2.7, 2.8, 2.9 3.0, 3.1, 3.2, 3.3, 3.4, 3.5, 3.6, 3.7, 3.8, 3.9, 4.0, 4.1, 4.2, 4.3, 4.4, 4.5, 4.6, 4.7, 4.8, 4.9, 5.0, 5.1, 5.2, 5.3, 5.4, 5.5, 5.6, 5.7, 5.8, 5.9, 6.0.
The atomic ratio of Mn may therefore be 0.1, 0.2, 0.3, 0.4, 0.5, 0.6, 0.7, 0.8, 0.9 1.0, 1.1, 1.2, 1.3, 1.4, 1.5, 1.6, 1.7, 1.8, 1.9, 2.0, 2.1, 2.2, 2.3, 2.4, 2.5, 2.6, 2.7, 2.8, 2.9, 3.0, 3.1, 3.2, 3.3, 3.4, 3.5, 3.6, 3.7, 3.8, 3.9, 4.0, 4.1, 4.2, 4.3, 4.4, 4.5, 4.6, 4.7, 4.8, 4.9, 5.0, 5.1, 5.2, 5.3, 5.4, 5.5, 5.6, 5.7, 5.8, 5.9, 6.0, 6.1, 6.2, 6.3, 6.4, 6.5, 6.6, 6.7, 6.8, 6.9, 7.0, 7.1, 7.2, 7.3, 7.4, 7.5, 7.6, 7.7, 7.8, 7.9, 8.0, 8.1, 8.2, 8.3, 8.4, 8.5, 8.6, 8.7, 8.8, 8.9, 9.0, 9.1, 9.2, 9.3, 9.4, 9.5, 9.6, 9.7, 9.8, 9.9, 10.0, 10.1, 10.2, 10.3, 10.4, 10.5, 10.6, 10.7, 10.8, 10.9, 11.0, 11.1, 11.2, 11.3, 11.4, 11.5, 11.6, 11.7, 11.8, 11.9, 12.0, 12.1, 12.2, 12.3, 12.4, 12.5, 12.6, 12.7, 12.8, 12.9, 13.0, 13.1, 13.2, 13.3, 13.4, 13.5, 13.6, 13.7, 13.8, 13.9, 14.0, 14.1, 14.2, 14.3, 14.4, 14.5, 14.6, 14.7, 14.8, 14.9, 15.0, 15.1, 15.2, 15.3, 15.4, 15.5, 15.6, 15.7, 15.8, 15.9, 16.0, 16.1, 16.2, 16.3, 16.4, 16.5, 16.6, 16.7, 16.8, 16.9, 17.0, 17.1, 17.2, 17.3, 17.4, 17.5, 17.6, 17.7, 17.8, 17.9, 18.0, 18.1, 18.2, 18.3, 18.4, 18.5, 18.6, 18.7, 18.8, 18.9, 19.0, 19.1, 19.2, 19.3, 19.4, 19.5, 19.6, 19.7, 19.8, 19.9, 20.0, 20.1, 20.2, 20.3, 20.4, 20.5, 20.6, 20.7, 20.8, 20.9, 21.0.
The atomic ratio of Ni may therefore be 0.1, 0.2, 0.3, 0.4, 0.5, 0.6, 0.7, 0.8, 0.9, 1.0, 1.1, 1.2, 1.3, 1.4, 1.5, 1.6, 1.7, 1.8, 1.9, 2.0, 2.1, 2.2, 2.3, 2.4, 2.5, 2.6 2.7, 2.8, 2.9 3.0, 3.1, 3.2, 3.3, 3.4, 3.5, 3.6, 3.7, 3.8, 3.9, 4.0, 4.1, 4.2, 4.3, 4.4, 4.5, 4.6, 4.7, 4.8, 4.9, 5.0, 5.1, 5.2, 5.3, 5.4, 5.5, 5.6, 5.7, 5.8, 5.9, 6.0, 6.1, 6.2, 6.3, 6.4, 6.5, 6.6, 6.7, 6.8, 6.9, 7.0, 7.1, 7.2, 7.3, 7.4, 7.5, 7.6, 7.7, 7.8, 7.9, 8.0, 8.1, 8.2, 8.3, 8.4, 8.5, 8.6, 8.7, 8.8, 8.9, 9.0, 9.1, 9.2, 9.3, 9.4, 9.5, 9.6, 9.7, 9.8, 9.9, 10.0, 10.1, 10.2, 10.3, 10.4, 10.5, 10.6, 10.7, 10.8, 10.9, 11.0, 11.1, 11.2, 11.3, 11.4, 11.5, 11.6, 11.7, 11.8, 11.9, 12.0, 12.1, 12.2, 12.3, 12.4, 12.5, 12.6, 12.7, 12.8, 12.9, 13.0, 13.1, 13.2, 13.3, 13.4, 13.5, 13.6, 13.7, 13.8, 13.9, 14.0, 14.1, 14.2, 14.3, 14.4, 14.5, 14.6, 14.7, 14.8, 14.9, 15.0, 15.1, 15.2, 15.3, 15.4, 15.5, 15.6, 15.7, 15.8, 15.9, 16.0.
The atomic ratio of Cr as an optional element, if present, may therefore be 0.1, 0.2, 0.3, 0.4, 0.5, 0.6, 0.7, 0.8, 0.9, 1.0, 1.1, 1.2, 1.3, 1.4, 1.5, 1.6, 1.7, 1.8, 1.9, 2.0, 2.1, 2.2, 2.3, 2.4, 2.5, 2.6, 2.7, 2.8, 2.9, 3.0, 3.1, 3.2, 3.3, 3.4, 3.5, 3.6, 3.7, 3.8, 3.9, 4.0, 4.1, 4.2, 4.3, 4.4, 4.5, 4.6, 4.7, 4.8, 4.9, 5.0, 5.1, 5.2, 5.3, 5.4, 5.5, 5.6, 5.7, 5.8, 5.9, 6.0, 6.1, 6.2, 6.3, 6.4, 6.5, 6.6, 6.7, 6.8, 6.9, 7.0, 7.1, 7.2, 7.3, 7.4, 7., 7.6, 7.7, 7.8, 7.9, 8.0, 8.1, 8.2, 8.3, 8.4, 8.5, 8.6, 8.7, 8.8, 8.9, 9.0, 9.1, 9.2, 9.3, 9.4, 9.5, 9.6, 9.7, 9.8, 9.9, 10.0, 10.1, 10.2, 10.3, 10.4, 10.5, 10.6, 10.7, 10.8, 10.9, 11.0, 11.1, 11.2, 11.3, 11.4, 11.5, 11.6, 11.7, 11.8, 11.9, 12.0, 12.1, 12.2, 12.3, 12.4, 12.5, 12.6, 12.7, 12.8, 12.9, 13.0, 13.1, 13.2, 13.3, 13.4, 13.5, 13.6, 13.7, 13.8, 13.9, 14.0, 14.1, 14.2, 14.3, 14.4, 14.5, 14.6, 14.7, 14.8, 14.9, 15.0, 15.1, 15.2, 15.3, 15.4, 15.5, 15.6, 15.7, 15.8, 15.9, 16.0, 16.1, 16.2, 16.3, 16.4, 16.5, 16.6, 16.7, 16.8, 16.9, 17.0, 17.1, 17.2, 17.3, 17.4, 17.5, 17.6, 17.7, 17.8, 17.9, 18.0, 18.1, 18.2, 18.3, 18.4, 18.5, 18.6, 18.7, 18.8, 18.9, 19.0, 19.1, 19.2, 19.3, 19.4, 19.5, 19.6, 19.7, 19.8, 19.9, 20.0, 20.1, 20.2, 20.3, 20.4, 20.5, 20.6, 20.7, 20.8, 20.9, 21.0, 21.1, 21.2, 21.3, 21.4, 21.5, 21.6, 21.7, 21.8, 21.9, 22.0, 22.1, 22.2, 22.3, 22.4, 22.5, 22.6, 22.7, 22.8, 22.9, 23.0, 23.1, 23.2, 23.3, 23.4, 23.5, 23.6, 23.7, 23.8, 23.9, 24.0, 24.1, 24.2, 24.3, 24.4, 24.5, 24.6, 24.7, 24.8, 24.9, 25.0, 25.1, 25.2, 25.3, 25.4, 25.5, 25.6, 25.7, 25.8, 25.9, 26.0, 26.1, 26.2, 26.3, 26.4, 26.5, 26.6, 26.7, 26.8, 26.9, 27, 27.1, 27.2, 27.3, 27.4, 27.5, 27.6, 27.7, 27.8, 27.9, 28.0, 28.1, 28.2, 28.3, 28.4, 28.5, 28.6, 28.7, 28.8, 28.9, 29.0, 29.1, 29.2, 29.3, 29.4, 29.5, 29.6, 29.7, 29.8, 29.9, 30.0, 30.1, 30.2, 30.3, 30.4, 30.5, 30.6, 30.7, 30.8, 30.9, 31.0, 31.1, 31.2, 31.3, 31.4, 31.5, 31.6, 31.7, 31.8, 31.9, 32.0.
The study was performed to evaluate warm formability of the alloys described in this application at elevated temperatures. In a case of plate production by Twin Roll Casting or Thin Slab Casting, utilized alloys should have good formability to be processed by hot rolling as a step at production process. Moreover, hot forming ability is a critical feature of the high strength alloys in terms of their usage for part production with different configuration by such methods as hot pressing, hot stamping, etc.
Using ferroadditives and other readily commercially available constituents, 35 g commercial purity (CP) feedstocks for Alloy 82 representing Class 2 steel were weighed out according to the atomic ratio provided in Table 2. The feedstock material was then placed into the copper hearth of an arc-melting system. The feedstock was arc-melted into an ingot using high purity argon as a shielding gas. The ingots were flipped several times and re-melted to ensure homogeneity. The resulting ingots were then placed in a PVC chamber, melted using RF induction and then ejected onto a copper die designed for casting a 3×4 inches plates with thickness of 1.8 mm.
Resultant plate from the Alloy 82 was subjected to a HIP cycle at 1150° C. using an American Isostatic Press Model 645 machine with a molybdenum furnace with furnace chamber size of 4 inch diameter by 5 inch height. The plates were heated at 10° C./min until the target temperature and were exposed to an isostatic pressure of 30 ksi for 1 hour. Heat treatment at 850° C. for 1 hour was applied after HIP cycle. Tensile specimens with a gage length of 12 mm and a width of 3 mm were cut from the treated plate.
The tensile measurements were done with testing parameters listed in Table 3 at temperatures specified in Table 4. The NanoSteel R&D specimen geometry (shown in
Using ferroadditives and other readily commercially available constituents, 35 g commercial purity (CP) feedstocks for Alloy 213 representing Class 2 steel were weighed out according to the atomic ratio provided in Table 2. The feedstock material was then placed into the copper hearth of an arc-melting system. The feedstock was arc-melted into an ingot using high purity argon as a shielding gas. The ingots were flipped several times and re-melted to ensure homogeneity. The resulting ingots were then placed in a PVC chamber, melted using RF induction and then ejected onto a copper die designed for casting a 3×4 inches plates with thickness of 1.8 mm.
Resultant plate from the Alloy 213 was subjected to a HIP cycle at 1125° C. using an American Isostatic Press Model 645 machine with a molybdenum furnace with furnace chamber size of 4 inch diameter by 5 inch height. The plates were heated at 10° C./min until the target temperature and were exposed to an isostatic pressure of 30 ksi for 1 hour. Tensile specimens with NanoSteel R&D specimen geometry (
The tensile measurements were done with testing parameters listed in Table 6 at temperatures specified in Table 7. In Table 8, a summary of the tensile test results including total tensile elongation (strain), yield stress, and ultimate tensile strength are shown for the treated plate from Alloy 213. Room temperature tensile property ranges for the same alloy after the same treatments are listed for comparison. As can be seen, this alloy shows high ductility up to 74% when tested at 700° C. demonstrating high warm forming ability. Temperature dependence of yield stress and tensile elongation is illustrated on
The study was performed to evaluate warm formability of the alloys described in this application at elevated temperatures. In a case of plate production by Twin Roll Casting or Thin Slab Casting, utilized alloys should have good formability to be processed by hot rolling as a step at production process. Moreover, hot forming ability is a critical feature of the high strength alloys in terms of their usage for part production with different configuration by such methods as hot pressing, hot stamping, etc.
Using high purity elements, 35 g alloy feedstocks of the Alloy 36 representing Class 3 steel were weighed out according to the atomic ratios provided in Table 2. The feedstock material was then placed into the copper hearth of an arc-melting system. The feedstock was arc-melted into an ingot using high purity argon as a shielding gas. The ingots were flipped several times and re-melted to ensure homogeneity. The resulting ingots were then placed in a PVC chamber, melted using RF induction and then ejected onto a copper die designed for casting a 3×4 inches plates with thickness of 1.8 mm.
Resultant plate from the Alloy 36 was subjected to a HIP cycle at 1100° C. using an American Isostatic Press Model 645 machine with a molybdenum furnace with furnace chamber size of 4 inch diameter by 5 inch height. The plates were heated at 10° C./min until the target temperature and were exposed to an isostatic pressure of 30 ksi for 1 hour. Heat treatment at 850° C. for 1 hour was applied after HIP cycle. Tensile specimens with NanoSteel R&D specimen geometry (
The tensile measurements were done at strain rate of 0.001 s−1 at 700° C. In Table 9, a summary of the tensile test results including total tensile elongation (strain), yield stress, and ultimate tensile strength are shown for the treated plate from Alloy 36. Room temperature tensile property ranges for the same alloy after the same treatments are listed for comparison. As can be seen, high strength alloys with ultimate strength up to 1650 MPa at room temperature show high ductility up to 88.5% when tested at 700° C. demonstrating high warm forming ability. Warm temperature ductility of the alloys strongly depends on alloy chemistry, thermal mechanical treatment parameters and testing temperature. An example of tested specimen is shown in
Alloy 82 was utilized for commercial sheet production by Thin Strip casting with in-line hot rolling that was done at ˜1050° C. to ˜9% reduction. The condition of the sheet material is not optimized (partial transformation into NanoModal structure due to low temperature and reduction at in-line rolling). Tensile specimens with NanoSteel R&D specimen geometry (
This application claims the benefit of U.S. Provisional Application Ser. No. 61/768,131 filed Feb. 22, 2013.
| Number | Date | Country | |
|---|---|---|---|
| 61768131 | Feb 2013 | US |
