Patent Grant
10787726
The present invention is directed to ductile iron composition, articles including the ductile iron compositions, and processes of forming ductile iron. More specifically, the present invention is directed to a solid solution strengthened ductile iron having increased toughness and wear resistance.
Due to their wear resistance, strength, toughness, castability and machinability, ductile iron (cast nodular iron) alloys have also been used to produce a variety of wind turbine, gas turbine and mining components. The strength of cast iron has been improved remarkably by the development of spheroidal graphite cast iron, i.e. ductile cast iron, but its ductility and impact resistance are still behind those of the steel, making steel the desirable material for a variety of components, including gearbox components. To improve the mechanical properties of ductile iron, attempts at refining of the graphite nodules of the alloying of special elements have been made, but not succeeded yet in obtaining sufficient results. In addition, these compositions and processes may have such disadvantages as complicated or energy intensive processing.
In an exemplary embodiment of the present disclosure, a ductile iron composition including by weight:
In another embodiment of the present disclosure, a method of forming a ductile iron component. The method includes forming a melt of a charge alloy, nodularizing the melt with a nodularizing alloy, inoculating the melt with an inoculation alloy to nucleate graphite nodules and form a ductile iron component and includes a ductile iron composition comprising, by weight:
Other features and advantages of the present invention will be apparent from the following more detailed description of the preferred embodiment, taken in conjunction with the accompanying drawings which illustrate, by way of example, the principles of the invention.
Provided is an exemplary ductile iron composition and a process of forming the ductile iron component having a plurality of predetermined properties. Embodiments of the present disclosure, in comparison to methods and products not utilizing one or more features disclosed herein, increased toughness, increased wear resistance or combinations thereof. The desirable wear resistance of the materials according to the present disclosure are particularly suitable for wind turbine, gas turbine and mining components, such as gear components, toes on buckets, crushers and other suitable components
The terms “first,” “second”, and the like, herein do not denote any order, quantity, or importance, but rather are used to distinguish one element from another, and the terms “a” and “an” herein do not denote a limitation of quantity, but rather denote the presence of at least one of the referenced item. The suffix “(s)” as used herein is intended to include both the singular and the plural of the term that it modifies, thereby including one or more of that term (e.g., the metal(s) includes one or more metals). Ranges disclosed herein are inclusive and independently combinable (e.g., ranges of “up to about 25%, or, more specifically, about 5% to about 20%”, is inclusive of the endpoints and all intermediate values of the ranges of “about 5% to about 25%,” etc.).
The modifier “about” used in connection with a quantity is inclusive of the stated value and has the meaning dictated by the context, (e.g., includes the degree of error associated with measurement of the particular quantity). For example, a quantitative value indicated as being about a number may vary by about +/−10%.
In one embodiment, the disclosure includes a process for the production of a wide variety of components from ductile iron compositions. Other non-limiting examples include gas turbine, wind turbine, automotive or oil and gas components, such as shafts, gears, axles, and various other components used in the energy, automotive, railroad, construction, mining and agricultural industries. Other components may include gearbox components, ring gears, planetary gears, and mining equipment. Such components are well known in the art and therefore require no further description.
Ductile iron composition, according to embodiments of the present disclosure, contain, by weight, about 3.4% to about 4.0% silicon, about 3.0% to about 3.5% carbon, about 0.5% to about 1.0% chromium, about 0.02% to about 0.05% molybdenum, up to about 0.01% sulfur, up to about 0.5% manganese, and balance iron and incidental impurities. As known in the art, the level for carbon is necessary for graphite formation and castability considerations. The role of silicon is generally to promote the formation of graphite instead of metastable iron carbide during solidification. The carbon content separates as spheroidal graphite during solidification, primarily as the result of the presence of silicon. The spheroidal graphite imparts such desirable properties as high strength and toughness for which ductile iron alloys are known. In addition, in the composition according to the present disclosure chromium and molybdenum act as primary carbide formers (e.g., M6C and M7C3 type carbides). In one embodiment, the composition is devoid of nickel.
In a further embodiment, the ductile iron composition includes about 3.5% to about 3.9% silicon, about 3.1% to about 3.4% carbon, about 0.6% to about 0.9% chromium, about 0.03% to about 0.04% molybdenum, up to about 0.01% sulfur, up to about 0.4% manganese, and balance iron and incidental impurities.
In a further embodiment, the ductile iron composition includes about 3.6% to about 3.8% silicon, about 3.25% to about 3.35% carbon, about 0.7% to about 0.8% chromium, about 0.03% to about 0.04% molybdenum, up to about 0.01% sulfur, up to about 0.3% manganese, and balance iron and incidental impurities.
The ductile iron composition, according to the present disclosure, includes graphite nodules having varied spherical geometries. The microstructure of the ductile iron composition includes a substantially ferritic structure containing less than 5 areal % pearlite or less than 15 areal % pearlite. In certain embodiments of the disclosure, the mechanical properties vary based upon thickness of the component. For example, components having wall thicknesses of equal to or less than 2 inches include less than 5 areal % or less than 2 areal % or less than 1 areal % pearlite. Components having wall thicknesses of equal to or less than 4 inches include less than 15 areal % or less than 10 areal % or less than 7.5 areal % pearlite. The microstructure of the ductile iron composition includes carbide volumetric percentage between about 5% and about 20% or between about 5% and about 15% or about 10%. In one embodiment, the nodule density for highly spherical and substantially spherical graphite nodules is greater than 100 per mm2 or greater than 125 per mm2 or 150 per mm2. An exemplary microstructure is shown in
The ductile iron composition, according to the present disclosure, is formed treating a charge material with a specific composition to nodularize and inoculate the charge composition. The method includes forming a melt of a charge material. The charge material is any suitable material for forming the melt. Suitable mixtures for the charge material include a composition having 20-40% in-house return, 30-50% pig iron, 10-20% steel scrap. The composition is selected to result in the desired alloy composition after nodularization and inoculation. After the melt is formed, the charge composition is nodularized with a nodularizing composition. Nodularizing includes contacting the charge material with a nodularizing composition. The nodularizing composition is a material that nodularizes graphite within the ductile iron composition to form graphite nodules.
In one embodiment, the nodularizing composition comprises, by weight, from about 1.0% to about 1.4% of the charge alloy and nodularizing composition. In one embodiment, the nodularizing composition includes two portions, including a first portion and a second portion. In this embodiment, the first portion comprises, by weight, about 0.2 to about 2.0% Al, about 0.2 to about 2.0% Ca, about 0.2 to about 2.0% rare earth elements, 2.0 to about 4.0% Mg and balance essentially FeSi. The second portion of the nodularizing composition includes, by weight, of the first portion about 0.2 to about 2.0% Al, about 0.2 to about 2.0% Ca, less than about 0.1% rare earth elements, 2.0 to about 4.0% Mg and balance essentially FeSi.
To form the ductile iron composition, according to the present disclosure, the composition is inoculated. Inoculation is accomplished by contacting an inoculating composition with the charge material. Inoculation may occur at various stages of the process. For example, inoculating may be done in the furnace, in the ladle, at other stages in the formation process or in combination of these points in the process. Inoculating the charge material with the inoculating composition nucleates the graphite nodules and assists in the formation of a higher nodule density with desired nodule geometry. One composition suitable for use as an inoculating composition includes a ferrosilicon composition comprising, by weight, of the composition about 0.2 to about 2.0% Al, about 0.2 to about 2.0% Ca, and about 1.0 to about 2.0% Ce.
The ductile iron composition, according to the present disclosure, after nodularization and inoculation, is cast using casting techniques known in the art for casting.
The ductile iron composition may be heat treated to induce formation of carbides. In one embodiment, the ductile composition is heat treated at a temperature between about 1350° F. and 1425° F., to form a microstructure as shown in
While the invention has been described with reference to a preferred embodiment, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this invention, but that the invention will include all embodiments falling within the scope of the appended claims.
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| Number | Date | Country | |
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