Patent Application
20240018630
The present invention relates to wear and corrosion resistant alloy compositions and, in particular, to alloy compositions exhibiting enhancements to ductility and processing capabilities.
Stellite alloys offer a desirable balance of mechanical wear resistance and corrosion resistance. Stellite alloys are generally cobalt-based with additions of chromium, carbon, tungsten and/or molybdenum. The lower carbon alloys can find application in cavitation, sliding wear or moderate galling, while the higher carbon alloys are usually selected for abrasion, severe galling, or low angle erosion. In addition to the Stellite family, Tribaloy alloy compositions have also been developed for applications in which extreme wear is combined with high temperatures and corrosive environments. Tribaloy alloys can be cobalt-based or nickel-based, depending on end use. Wear resistant Stellite and Tribaloy alloys are often formed with various hard phases such, as carbides and intermetallic compounds. Such hard phases can render the alloys brittle and prone to cracking and/or other failure mechanisms. Alloy brittleness can also lead to processing issues, including degradation during application by thermal spray, welding or casting.
In view of the foregoing disadvantages, alloy compositions and associated articles are described herein which, in some embodiments, exhibit enhancements to ductility and processing capabilities without significant sacrifices to hardness, wear resistance, and/or corrosion resistance. An alloy, in some embodiments, comprises 0-40 wt. % nickel, 14-20 wt. % chromium, 24-35 wt. % molybdenum, 0-15 wt. % iron, 0-1.5 wt. % manganese, 0.01-0.1 wt. % carbon, 0-15 wt. % tungsten, 0.5-5.5 wt. % silicon and the balance cobalt, wherein the alloy has a configurational entropy greater than 1.5R, where R is the universal gas constant. In some embodiments, the configurational entropy is up to 1.7R. In another aspect, an alloy comprises 0-40 wt. % nickel, 14-20 wt. % chromium, 24-35 wt. % molybdenum, 0-15 wt. % iron, 0-1.5 wt. % manganese, 0.01-0.1 wt. % carbon, 0-15 wt. % tungsten, 0.5-5.5 wt. % silicon and the balance cobalt, wherein the alloy has a magnetic permeability (μ) less than 1.005.
In another aspect, articles comprising alloys described herein are provided. In some embodiments, an article comprises one or more regions formed of an alloy comprising a cobalt rich solid solution matrix phase and intermetallic precipitates dispersed in the matrix phase, the intermetallic precipitates having a discontinuous dendritic microstructure, wherein the alloy comprises 0-40 wt. % nickel, 14-20 wt. % chromium, 24-35 wt. % molybdenum, 0-15 wt. % iron, 0-1.5 wt. % manganese, 0.01-0.1 wt. % carbon, 0-15 wt. % tungsten, 0.5-5.5 wt. % silicon, and the balance cobalt. The intermetallic precipitates, in some embodiments, comprise Laves phases.
These and other embodiments are further described in the following detailed description.
Embodiments described herein can be understood more readily by reference to the following detailed description and examples and their previous and following descriptions. Elements, apparatus and methods described herein, however, are not limited to the specific embodiments presented in the detailed description and examples. It should be recognized that these embodiments are merely illustrative of the principles of the present invention. Numerous modifications and adaptations will be readily apparent to those of skill in the art without departing from the spirit and scope of the invention.
In one aspect, an alloy comprises 0-40 wt. % nickel, 14-20 wt. % chromium, 24-35 wt. % molybdenum, 0-15 wt. % iron, 0-1.5 wt. % manganese, 0.01-0.1 wt. % carbon, 0-15 wt. % tungsten, 0.5-5.5 wt. % silicon, and the balance cobalt, wherein the alloy has a configurational entropy greater than 1.5R, where R is the universal gas constant. In some embodiments, the configurational entropy is up to 1.7R. Configuration entropy of the alloy composition can be determined according to the following equation:
where R is the universal gas constant and xi is the molar concentration of the ith alloying element which satisfies:
Moreover, in some embodiments, the alloy composition has a magnetic permeability (μ) less than 1.005. Magnetic permeability of the alloy composition, for example, can range from 1.000-1.003. Magnetic permeability is measured according to ASTM A342-Standard Test Methods for Permeability of Weakly Magnetic Materials.
In another aspect, an alloy comprises 0-40 wt. % nickel, 14-20 wt. % chromium, 24-35 wt. % molybdenum, 0-15 wt. % iron, 0-1.5 wt. % manganese, 0.01-0.1 wt. % carbon, 0-15 wt. % tungsten, 0.5-5.5 wt. % silicon, and the balance cobalt, wherein the alloy has a magnetic permeability GO less than 1.005.
In some embodiments of alloy compositions described herein, cobalt and/or nickel are each present in an amount of 15-40 wt. %. Accordingly, the alloy compositions may be cobalt-based or nickel-based. Nickel, for example, can be present in an amount of 20-40 wt. % or 22-35 wt %. Additionally, molybdenum can be present in the alloy compositions in an amount of 25-33 wt. % or 29-33 wt. %, in some embodiments.
Table I provides alloys having composition and properties described herein.
Any of the alloy compositions provided in Table 1 may also exhibit a magnetic permeability less than 1.005, including 1-1.003.
In another aspect, articles comprising alloys described herein are provided. In some embodiments, an article comprises one or more regions formed of an alloy comprising a cobalt rich solid solution matrix phase and intermetallic precipitates dispersed in the matrix phase, the intermetallic precipitates having a discontinuous dendritic microstructure, wherein the alloy comprises 0-40 wt. % nickel, 14-20 wt. % chromium, 24-35 wt. % molybdenum, 0-15 wt. % iron, 0-1.5 wt. % manganese, 0.01-0.1 wt. % carbon, 0-15 wt. % tungsten, 0.5-5.5 wt. % silicon, and the balance cobalt. In some embodiments, the alloy composition of the article can have a composition selected from Table I above. Moreover, alloy of the article can exhibit configurational entropy and/or magnetic permeability having a value described in Section I above.
The intermetallic precipitates, in some embodiments, comprise Laves phases.
In some embodiments, the intermetallic precipitates are present in the alloy in an amount 50 vol. % or less. The intermetallic precipitates, for example, can be present in an amount of 30-50 vol. % or 40-48 vol. %. Additionally, the cobalt-rich solid solution matrix is face centered cubic (fcc). In some embodiments, the alloy is 30-90 vol. % fcc. The alloy may also exhibit hexagonal crystalline phases, including hexagonal close packed (hcp) phases. In some embodiments, a ratio of fcc to hcp in the alloy is greater than 2. In some embodiments, alloys having composition described herein, including the alloy compositions in Table I, can exhibit a CoMo3Si phase. Depending on specific composition, alloys described herein may exhibit one or more of the phases in Table II.
In some embodiments, the one or more alloy regions of the article are exterior surfaces of the article. Alloys described herein can be applied as coatings via various techniques, including weld overlay via plasma transferred arc (PTA). One or multiple layers of alloy coating can be applied to an article for wear and/or corrosion resistance. Alloy compositions described herein can also be cast. In some embodiments, the entire article can be formed of the alloy composition.
Alloy forming one or more regions of an article can have hardness (HRC) of at least 55, in some embodiments. The alloy can also maintain desirable hardness at high temperatures.
In addition to hardness, alloy described herein forming one or more regions of an article can exhibit desirable wear characteristics.
Alloys having composition and microstructure described herein exhibit desirable adhesive wear resistance.
Alloys having composition and microstructure described herein also provide higher ductility and better processing relative to brittle alloys such as T-800. Alloys described herein do not crack or are resistant to cracking when applied to substrate by various techniques, including PTA and casting.
Various embodiments of the invention have been described in fulfillment of the various objects of the invention. It should be recognized that these embodiments are merely illustrative of the principles of the present invention. Numerous modifications and adaptations thereof will be readily apparent to those skilled in the art without departing from the spirit and scope of the invention.
