EP2671959A1 - Nickel-chromium-molybdenum-vanadium alloy and turbine component - Google Patents

Nickel-chromium-molybdenum-vanadium alloy and turbine component Download PDF

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Publication number
EP2671959A1
EP2671959A1 EP13170181.5A EP13170181A EP2671959A1 EP 2671959 A1 EP2671959 A1 EP 2671959A1 EP 13170181 A EP13170181 A EP 13170181A EP 2671959 A1 EP2671959 A1 EP 2671959A1
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Prior art keywords
concentration
present
nicrmov
alloy
weight
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EP13170181.5A
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German (de)
French (fr)
Inventor
David Bruce KNORR
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General Electric Co
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General Electric Co
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/10Metals, alloys or intermetallic compounds
    • F05D2300/13Refractory metals, i.e. Ti, V, Cr, Zr, Nb, Mo, Hf, Ta, W

Definitions

  • the present invention is directed to alloys and components comprising alloys. More specifically, the present invention is directed to Nickel-Chromium-Molybdenum-Vanadium (NiCrMoV) alloys.
  • NiCrMoV Nickel-Chromium-Molybdenum-Vanadium
  • steam turbine plants can include a high pressure steam turbine, an intermediate pressure steam turbine, and a low pressure steam turbine.
  • Each steam turbine is formed of materials appropriate to withstand operating conditions, pressure, temperature, flow rate, etc., for that particular turbine.
  • Each turbine can include a rotor and a casing jacket.
  • the rotor includes a rotatably mounted turbine shaft that includes blades. When heated and pressurized steam flows through the flow space between the casing jacket and the rotor, the turbine shaft is set in rotation as energy is transferred from the steam to the rotor.
  • the low pressure steam turbine can include low pressure rotor forgings that operate for long periods of time at temperatures in excess of 600°F. Alloys of NiCrMoV formed by conventional steel making processes and used at temperatures above 600°F undesirably require special cooling otherwise an undesirable increase in the ductile to brittle transition temperature occurs.
  • NiCrMoV alloys capable of handling these high temperatures require extensive steelmaking processing to reduce the content of deleterious impurities, for example, having manganese at a concentration of less than about 0.06% and phosphorus at a concentration of less than about 0.005%. These alloys are referred to as superclean. These superclean alloys can incur a high manufacturing cost and/or are not capable of being produced by conventional steel making processes.
  • a NiCrMoV alloy includes, by weight, between about 0.06% and about 0.12% manganese, at least about 3.40% nickel, between about 0.24% and about 0.30% carbon, up to about 0.60% molybdenum, up to about 0.15% vanadium, up to about 2.00% chromium, up to about 0.012% phosphorus, up to about 0.007% sulfur, up to about 0.10% silicon, up to about 0.002% antimony, up to about 0.008% arsenic, up to about 0.012% tin, and up to about 0.015% aluminum.
  • a NiCrMoV alloy includes, by weight, between about 0.06% and about 0.12% manganese, at least about 3.40% nickel, between about 0.22% and about 0.30% carbon, up to about 0.60% molybdenum, up to about 0.15% vanadium, up to about 2.00% chromium, up to about 0.012% phosphorus, up to about 0.007% sulfur, up to about 0.10% silicon, up to about 0.002% antimony, up to about 0.008% arsenic, up to about 0.012% tin, and up to about 0.015% aluminum.
  • the phosphorus is present at a concentration of at least about 0.007%
  • the sulfur is present at a concentration of at least about 0.006%
  • the silicon is present at a concentration of at least about 0.05%, or a combination thereof.
  • a NiCrMoV alloy in another exemplary embodiment, includes nickel, chromium, molybdenum, vanadium, and manganese, the manganese being at a concentration of, by weight, at least about 0.06%.
  • the NiCrMoV alloy is resistant to embrittlement at temperatures above 371°C (700°F).
  • NiCrMoV alloy and turbine component Provided is an exemplary NiCrMoV alloy and turbine component.
  • Embodiments of the present disclosure increase resistance to embrittlement, permit use of NiCrMoV alloys at higher temperatures (for example, in excess of 600°F and especially at 700°F and higher, such as above 725°F or above 750°F), extend the operational use of non-superclean NiCrMoV alloys above 600°F, permit production/fabrication of NiCrMoV alloys that are not superclean alloys without requiring special cooling provisions, limit an increase in the ductile to brittle transition temperature to 60% of what a comparable conventional alloy would experience, reduce costs of production/fabrication (for example, by about 25%), increase operational efficiency of turbine systems, or combinations thereof.
  • the NiCrMoV alloy is a portion or all of any suitable component.
  • the NiCrMoV alloy is in a turbine component, for example, in a power generation system, such as, a steam turbine and/or steam turbine system, a gas turbine and/or gas turbine system, or any other suitable system.
  • the turbine component is a low pressure rotor of a steam turbine in a steam turbine system.
  • the NiCrMoV alloy and/or the turbine component is/are formed by any suitable fabrication process(es).
  • the fabrication process is a conventional steel-making process and/or is not a superclean process, where the superclean process requires much longer times to refine the steel thereby removing impurities, such as, manganese, sulfur, and/or phosphorus.
  • the turbine component includes the NiCrMoV alloy and the NiCrMoV alloy has a composition of, by weight, between about 0.06% and about 0.12% manganese, at least about 3.40% nickel, between about 0.24% and about 0.30% carbon, up to about 0.60% molybdenum, up to about 0.15% vanadium, up to about 2.00% chromium, up to about 0.012% phosphorus, up to about 0.007% sulfur, up to about 0.10% silicon, up to about 0.002% antimony, up to about 0.008% arsenic, up to about 0.012% tin, and up to about 0.015% aluminum.
  • the phosphorus is present at a concentration of at least about 0.007%
  • the sulfur is present at a concentration of at least about 0.006%
  • the silicon is present at a concentration of at least about 0.05%, or a combination thereof.
  • the NiCrMoV alloy includes a balance of iron and incidental impurities.
  • the NiCrMoV alloy includes, by weight, at least about 0.06% manganese, the NiCrMoV alloy being resistant to embrittlement, for example, at temperatures of between about 700°F and about 750°F, between about 700°F and about 725°F, between about 725°F and about 750°F, above about 700°F, above about 725°F, about 700°F, about 725°F, about 750°F, or any suitable combination, sub-combination, range, or sub-range thereof.
  • the NiCrMoV alloy limits the amount of manganese permitting the NiCrMoV alloy to be resistant to embrittlement and retain sufficient manganese to combine with the deleterious sulfur impurity.
  • Suitable amounts of manganese include, by weight, between about 0.06% and about 0.09% manganese, between about 0.09% and about 0.12%, between about 0.08% and about 0.10%, about 0.06%, about 0.08%, about 0.10%, about 0.12%, or any suitable combination, sub-combination, range, or sub-range thereof.
  • the phosphorus is present in the NiCrMoV alloy at a concentration of, by weight, between about 0.010% and about 0.012%, between about 0.007% and about 0.010%, between about 0.008% and about 0.011%, about 0.007%, about 0.008%, about 0.009%, about 0.010%, about 0.011%, about 0.012%, or any suitable combination, sub-combination, range, or sub-range thereof.
  • the sulfur is present in the NiCrMoV alloy at a concentration of, by weight, about 0.006%, about 0.007%, or any suitable combination, sub-combination, range, or sub-range thereof.
  • the silicon is present in the NiCrMoV alloy at a concentration of, by weight, between about 0.05% and about 0.08%, between about 0.08% and about 0.10%, between about 0.07% and about 0.08%, about 0.05%, about 0.07%, about 0.08%, about 0.10%, or any suitable combination, sub-combination, range, or sub-range thereof.
  • the carbon is present in the NiCrMoV alloy at a concentration of, by weight, between about 0.22% and about 0.30%, between about 0.24% and about 0.26%, between about 0.22% and about 0.26%, between about 0.22% and about 0.24%, between about 0.24% and about 0.26%, between about 0.26% and about 0.30%, between about 0.28% and about 0.30%, up to about 0.30%, about 0.22%, about 0.24%, about 0.26%, about 0.28%, about 0.30%, or any suitable combination, sub-combination, range, or sub-range thereof.
  • the molybdenum is present in the NiCrMoV alloy at a concentration of, by weight, between about 0.35% and about 0.50%, between about 0.35% and about 0.40%, between about 0.45% and about 0.50%, between about 0.45% and about 0.60%, between about 0.50% and about 0.60%, between about 0.55% and about 0.60%, about 0.35%, about 0.40%, about 0.45%, about 0.50%, about 0.55%, about 0.60%, or any suitable combination, sub-combination, range, or sub-range thereof.
  • the vanadium is present in the NiCrMoV alloy at a concentration of, by weight, between about 0.10% and about 0.15%, between about 0.05% and about 0.10%, between about 0.09% and about 0.13%, between about 0.10% and about 0.12%, about 0.05%, about 0.07%, about 0.08%, about 0.09%, about 0.10%, about 0.11%, about 0.12%, about 0.13%, about 0.14%, about 0.15%, or any suitable combination, sub-combination, range, or sub-range thereof.
  • the chromium is present in the NiCrMoV alloy at a concentration of, by weight, between about 1.70% and about 2.00%, between about 1.50% and about 1.80%, between about 1.80% and about 2.00%, between about 1.70% and about 1.80%, between about 1.50% and about 1.70%, between about 1.50% and about 1.60%, about 1.50%, about 1.70%, about 1.80%, about 2.00%, or any suitable combination, sub-combination, range, or sub-range thereof.
  • the nickel is present in the NiCrMoV alloy at a concentration of, by weight, between about 3.40% and about 3.80%, between about 3.40% and about 3.70%, between about 3.40% and about 3.60%, between about 3.70% and about 4.00%, between about 3.80% and about 4.00%, between about 3.90% and about 4.00%, between about 3.70% and about 3.80%, or any suitable combination, sub-combination, range, or sub-range thereof.
  • the NiCrMoV alloy includes a concentration of, by weight, up to about 0.012% tin, up to about 0.010% tin, up to about 0.005% tin, between about 0.001% and about 0.012% tin, between about 0.008% and about 0.012% tin, between about 0.001% and about 0.010% tin, between about 0.008% and about 0.010% tin, about 0.001% tin, about 0.005% tin, about 0.010% tin, about 0.012% tin, or any suitable combination, sub-combination, range, or sub-range thereof.
  • the NiCrMoV alloy includes a concentration of, by weight, up to about 0.015% aluminum, up to about 0.010% aluminum, up to about 0.005% aluminum, between about 0.001% and about 0.015% aluminum, between about 0.008% and about 0.015% aluminum, between about 0.012% and about 0.015% aluminum, between about 0.001% and about 0.010% aluminum, between about 0.008% and about 0.010% aluminum, about 0.001% aluminum, about 0.005% aluminum, about 0.010% aluminum, about 0.015% aluminum, or any suitable combination, sub-combination, range, or sub-range thereof.
  • the NiCrMoV alloy includes a concentration of, by weight, up to about 0.002% antimony, up to about 0.001% antimony, about 0.002% antimony, or about 0.001% antimony, or any suitable combination, sub-combination, range, or sub-range thereof.
  • the NiCrMoV alloy includes up to about 0.008% arsenic, up to about 0.006% arsenic, up to about 0.004% arsenic, up to about 0.002% arsenic, between about 0.001% and about 0.008% arsenic, between about 0.003% and about 0.008% arsenic, between about 0.005% and about 0.008% arsenic, between about 0.007% and about 0.008% arsenic, between about 0.003% and about 0.006% arsenic, between about 0.002% and about 0.007% arsenic, or any suitable combination, sub-combination, range, or sub-range thereof.
  • the NiCrMoV alloy includes oxygen, as either dissolved oxygen or in oxides, at a concentration of, by weight, up to about 0.0075%, up to about 0.0050%, up to about 0.0030%, up to about 0.0010%, between about 0.0010% and about 0.0075%, between about 0.0030% and about 0.0075%, between about 0.0010% and about 0.0030%, about 0.0010%, about 0.0030%, about 0.0075%, or any suitable combination, sub-combination, range, or sub-range thereof.
  • the NiCrMoV alloy is substantially devoid of certain impurities and/or trace elements.
  • the NiCrMoV alloy is substantially devoid of or completely devoid of tungsten, cobalt, and/or niobium.
  • the NiCrMoV alloy includes trace amounts or more of tungsten, cobalt, and/or niobium.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

A NiCrMoV alloy and a turbine component are disclosed. The NiCrMoV alloy includes at least about 0.06%, at least about 3.40% nickel, between about 0.22% and about 0.30% carbon, up to about 0.60% molybdenum, up to about 0.15% vanadium, up to about 2.00% chromium, up to about 0.012% phosphorus, up to about 0.007% sulfur, up to about 0.10% silicon, up to about 0.002% antimony, up to about 0.008% arsenic, up to about 0.012% tin, and up to about 0.015% aluminum and/or is resistant to embrittlement at temperatures above 371°C (700°F).

Description

    FIELD OF THE INVENTION
  • The present invention is directed to alloys and components comprising alloys. More specifically, the present invention is directed to Nickel-Chromium-Molybdenum-Vanadium (NiCrMoV) alloys.
  • BACKGROUND OF THE INVENTION
  • In general, steam turbine plants can include a high pressure steam turbine, an intermediate pressure steam turbine, and a low pressure steam turbine. Each steam turbine is formed of materials appropriate to withstand operating conditions, pressure, temperature, flow rate, etc., for that particular turbine. Each turbine can include a rotor and a casing jacket. The rotor includes a rotatably mounted turbine shaft that includes blades. When heated and pressurized steam flows through the flow space between the casing jacket and the rotor, the turbine shaft is set in rotation as energy is transferred from the steam to the rotor.
  • Recently, steam turbine plant designs directed toward a larger capacity and a higher efficiency have been designed that include steam turbines that operate at higher temperatures and/or for longer periods. For example, the low pressure steam turbine can include low pressure rotor forgings that operate for long periods of time at temperatures in excess of 600°F. Alloys of NiCrMoV formed by conventional steel making processes and used at temperatures above 600°F undesirably require special cooling otherwise an undesirable increase in the ductile to brittle transition temperature occurs.
  • NiCrMoV alloys capable of handling these high temperatures require extensive steelmaking processing to reduce the content of deleterious impurities, for example, having manganese at a concentration of less than about 0.06% and phosphorus at a concentration of less than about 0.005%. These alloys are referred to as superclean. These superclean alloys can incur a high manufacturing cost and/or are not capable of being produced by conventional steel making processes.
  • An alloy and turbine component having an alloy that do not suffer from one or more of the above drawbacks would be desirable in the art.
  • BRIEF DESCRIPTION OF THE INVENTION
  • In an exemplary embodiment, a NiCrMoV alloy includes, by weight, between about 0.06% and about 0.12% manganese, at least about 3.40% nickel, between about 0.24% and about 0.30% carbon, up to about 0.60% molybdenum, up to about 0.15% vanadium, up to about 2.00% chromium, up to about 0.012% phosphorus, up to about 0.007% sulfur, up to about 0.10% silicon, up to about 0.002% antimony, up to about 0.008% arsenic, up to about 0.012% tin, and up to about 0.015% aluminum.
  • In an exemplary embodiment, a NiCrMoV alloy includes, by weight, between about 0.06% and about 0.12% manganese, at least about 3.40% nickel, between about 0.22% and about 0.30% carbon, up to about 0.60% molybdenum, up to about 0.15% vanadium, up to about 2.00% chromium, up to about 0.012% phosphorus, up to about 0.007% sulfur, up to about 0.10% silicon, up to about 0.002% antimony, up to about 0.008% arsenic, up to about 0.012% tin, and up to about 0.015% aluminum. The phosphorus is present at a concentration of at least about 0.007%, the sulfur is present at a concentration of at least about 0.006%, the silicon is present at a concentration of at least about 0.05%, or a combination thereof.
  • In another exemplary embodiment, a NiCrMoV alloy includes nickel, chromium, molybdenum, vanadium, and manganese, the manganese being at a concentration of, by weight, at least about 0.06%. The NiCrMoV alloy is resistant to embrittlement at temperatures above 371°C (700°F).
  • Other features and advantages of the present invention will be apparent from the following more detailed description of the preferred embodiment, by way of example, the principles of the invention.
  • DETAILED DESCRIPTION OF THE INVENTION
  • Provided is an exemplary NiCrMoV alloy and turbine component. Embodiments of the present disclosure increase resistance to embrittlement, permit use of NiCrMoV alloys at higher temperatures (for example, in excess of 600°F and especially at 700°F and higher, such as above 725°F or above 750°F), extend the operational use of non-superclean NiCrMoV alloys above 600°F, permit production/fabrication of NiCrMoV alloys that are not superclean alloys without requiring special cooling provisions, limit an increase in the ductile to brittle transition temperature to 60% of what a comparable conventional alloy would experience, reduce costs of production/fabrication (for example, by about 25%), increase operational efficiency of turbine systems, or combinations thereof.
  • The NiCrMoV alloy is a portion or all of any suitable component. In one embodiment, the NiCrMoV alloy is in a turbine component, for example, in a power generation system, such as, a steam turbine and/or steam turbine system, a gas turbine and/or gas turbine system, or any other suitable system. In one embodiment, the turbine component is a low pressure rotor of a steam turbine in a steam turbine system.
  • The NiCrMoV alloy and/or the turbine component is/are formed by any suitable fabrication process(es). In one embodiment, the fabrication process is a conventional steel-making process and/or is not a superclean process, where the superclean process requires much longer times to refine the steel thereby removing impurities, such as, manganese, sulfur, and/or phosphorus.
  • In one embodiment, the turbine component includes the NiCrMoV alloy and the NiCrMoV alloy has a composition of, by weight, between about 0.06% and about 0.12% manganese, at least about 3.40% nickel, between about 0.24% and about 0.30% carbon, up to about 0.60% molybdenum, up to about 0.15% vanadium, up to about 2.00% chromium, up to about 0.012% phosphorus, up to about 0.007% sulfur, up to about 0.10% silicon, up to about 0.002% antimony, up to about 0.008% arsenic, up to about 0.012% tin, and up to about 0.015% aluminum. In one embodiment, the phosphorus is present at a concentration of at least about 0.007%, the sulfur is present at a concentration of at least about 0.006%, the silicon is present at a concentration of at least about 0.05%, or a combination thereof. In a further embodiment, the NiCrMoV alloy includes a balance of iron and incidental impurities.
  • Additionally or alternatively, in one embodiment, the NiCrMoV alloy includes, by weight, at least about 0.06% manganese, the NiCrMoV alloy being resistant to embrittlement, for example, at temperatures of between about 700°F and about 750°F, between about 700°F and about 725°F, between about 725°F and about 750°F, above about 700°F, above about 725°F, about 700°F, about 725°F, about 750°F, or any suitable combination, sub-combination, range, or sub-range thereof.
  • In one embodiment, the NiCrMoV alloy limits the amount of manganese permitting the NiCrMoV alloy to be resistant to embrittlement and retain sufficient manganese to combine with the deleterious sulfur impurity. Suitable amounts of manganese include, by weight, between about 0.06% and about 0.09% manganese, between about 0.09% and about 0.12%, between about 0.08% and about 0.10%, about 0.06%, about 0.08%, about 0.10%, about 0.12%, or any suitable combination, sub-combination, range, or sub-range thereof.
  • In one embodiment, the phosphorus is present in the NiCrMoV alloy at a concentration of, by weight, between about 0.010% and about 0.012%, between about 0.007% and about 0.010%, between about 0.008% and about 0.011%, about 0.007%, about 0.008%, about 0.009%, about 0.010%, about 0.011%, about 0.012%, or any suitable combination, sub-combination, range, or sub-range thereof.
  • In one embodiment, the sulfur is present in the NiCrMoV alloy at a concentration of, by weight, about 0.006%, about 0.007%, or any suitable combination, sub-combination, range, or sub-range thereof.
  • In one embodiment, the silicon is present in the NiCrMoV alloy at a concentration of, by weight, between about 0.05% and about 0.08%, between about 0.08% and about 0.10%, between about 0.07% and about 0.08%, about 0.05%, about 0.07%, about 0.08%, about 0.10%, or any suitable combination, sub-combination, range, or sub-range thereof.
  • In one embodiment, the carbon is present in the NiCrMoV alloy at a concentration of, by weight, between about 0.22% and about 0.30%, between about 0.24% and about 0.26%, between about 0.22% and about 0.26%, between about 0.22% and about 0.24%, between about 0.24% and about 0.26%, between about 0.26% and about 0.30%, between about 0.28% and about 0.30%, up to about 0.30%, about 0.22%, about 0.24%, about 0.26%, about 0.28%, about 0.30%, or any suitable combination, sub-combination, range, or sub-range thereof.
  • In one embodiment, the molybdenum is present in the NiCrMoV alloy at a concentration of, by weight, between about 0.35% and about 0.50%, between about 0.35% and about 0.40%, between about 0.45% and about 0.50%, between about 0.45% and about 0.60%, between about 0.50% and about 0.60%, between about 0.55% and about 0.60%, about 0.35%, about 0.40%, about 0.45%, about 0.50%, about 0.55%, about 0.60%, or any suitable combination, sub-combination, range, or sub-range thereof.
  • In one embodiment, the vanadium is present in the NiCrMoV alloy at a concentration of, by weight, between about 0.10% and about 0.15%, between about 0.05% and about 0.10%, between about 0.09% and about 0.13%, between about 0.10% and about 0.12%, about 0.05%, about 0.07%, about 0.08%, about 0.09%, about 0.10%, about 0.11%, about 0.12%, about 0.13%, about 0.14%, about 0.15%, or any suitable combination, sub-combination, range, or sub-range thereof.
  • In one embodiment, the chromium is present in the NiCrMoV alloy at a concentration of, by weight, between about 1.70% and about 2.00%, between about 1.50% and about 1.80%, between about 1.80% and about 2.00%, between about 1.70% and about 1.80%, between about 1.50% and about 1.70%, between about 1.50% and about 1.60%, about 1.50%, about 1.70%, about 1.80%, about 2.00%, or any suitable combination, sub-combination, range, or sub-range thereof.
  • In one embodiment, the nickel is present in the NiCrMoV alloy at a concentration of, by weight, between about 3.40% and about 3.80%, between about 3.40% and about 3.70%, between about 3.40% and about 3.60%, between about 3.70% and about 4.00%, between about 3.80% and about 4.00%, between about 3.90% and about 4.00%, between about 3.70% and about 3.80%, or any suitable combination, sub-combination, range, or sub-range thereof.
  • In one embodiment, the NiCrMoV alloy includes a concentration of, by weight, up to about 0.012% tin, up to about 0.010% tin, up to about 0.005% tin, between about 0.001% and about 0.012% tin, between about 0.008% and about 0.012% tin, between about 0.001% and about 0.010% tin, between about 0.008% and about 0.010% tin, about 0.001% tin, about 0.005% tin, about 0.010% tin, about 0.012% tin, or any suitable combination, sub-combination, range, or sub-range thereof.
  • In one embodiment, the NiCrMoV alloy includes a concentration of, by weight, up to about 0.015% aluminum, up to about 0.010% aluminum, up to about 0.005% aluminum, between about 0.001% and about 0.015% aluminum, between about 0.008% and about 0.015% aluminum, between about 0.012% and about 0.015% aluminum, between about 0.001% and about 0.010% aluminum, between about 0.008% and about 0.010% aluminum, about 0.001% aluminum, about 0.005% aluminum, about 0.010% aluminum, about 0.015% aluminum, or any suitable combination, sub-combination, range, or sub-range thereof.
  • In one embodiment, the NiCrMoV alloy includes a concentration of, by weight, up to about 0.002% antimony, up to about 0.001% antimony, about 0.002% antimony, or about 0.001% antimony, or any suitable combination, sub-combination, range, or sub-range thereof.
  • In one embodiment, the NiCrMoV alloy includes up to about 0.008% arsenic, up to about 0.006% arsenic, up to about 0.004% arsenic, up to about 0.002% arsenic, between about 0.001% and about 0.008% arsenic, between about 0.003% and about 0.008% arsenic, between about 0.005% and about 0.008% arsenic, between about 0.007% and about 0.008% arsenic, between about 0.003% and about 0.006% arsenic, between about 0.002% and about 0.007% arsenic, or any suitable combination, sub-combination, range, or sub-range thereof.
  • In one embodiment, the NiCrMoV alloy includes oxygen, as either dissolved oxygen or in oxides, at a concentration of, by weight, up to about 0.0075%, up to about 0.0050%, up to about 0.0030%, up to about 0.0010%, between about 0.0010% and about 0.0075%, between about 0.0030% and about 0.0075%, between about 0.0010% and about 0.0030%, about 0.0010%, about 0.0030%, about 0.0075%, or any suitable combination, sub-combination, range, or sub-range thereof.
  • In one embodiment, the NiCrMoV alloy is substantially devoid of certain impurities and/or trace elements. For example, in one embodiment, the NiCrMoV alloy is substantially devoid of or completely devoid of tungsten, cobalt, and/or niobium. Alternatively, in one embodiment, the NiCrMoV alloy includes trace amounts or more of tungsten, cobalt, and/or niobium.
  • 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.

Claims (15)

  1. A NiCrMoV alloy, comprising, by weight:
    between about 0.06% and about 0.12% manganese, at least about 3.40% nickel; between about 0.24% and about 0.30% carbon, up to about 0.60% molybdenum, up to about 0.15% vanadium, up to about 2.00% chromium, up to about 0.012% phosphorus, up to about 0.007% sulfur, up to about 0.10% silicon, up to about 0.002% antimony, up to about 0.008% arsenic, up to about 0.012% tin, and up to about 0.015% aluminum.
  2. The NiCrMoV alloy of claim 1, further comprising a balance of iron and incidental impurities.
  3. The NiCrMoV alloy of claim 1 or claim 2, wherein the phosphorus is present at a concentration of at least about 0.007%, the sulfur is present at a concentration of at least about 0.006%, the silicon is present at a concentration of at least about 0.05%, or a combination thereof.
  4. The NiCrMoV alloy of any preceding claim, wherein the phosphorus is present at a concentration of at least about 0.007%.
  5. The NiCrMoV alloy of any preceding claim, wherein the sulfur is present at a concentration of at least about 0.006%.
  6. The NiCrMoV alloy of any preceding claim, wherein the silicon is present at a concentration of at least about 0.05%.
  7. The NiCrMoV alloy of any preceding claim, wherein the manganese is present at a concentration of, by weight, at least about 0.06%.
  8. The NiCrMoV alloy of any preceding claim, wherein the molybdenum is present at a concentration of, by weight, at least about 0.35%.
  9. The NiCrMoV alloy of any preceding claim, wherein the vanadium is present at a concentration of, by weight, at least about 0.05%.
  10. The NiCrMoV alloy of any preceding claim, wherein the chromium is present at a concentration of, by weight, at least about 1.50%.
  11. The NiCrMoV alloy of any preceding claim, wherein the nickel is present at a concentration of, by weight, up to about 4.00% nickel.
  12. The NiCrMoV alloy of any preceding claim, wherein the NiCrMoV alloy is resistant to embrittlement at temperatures above 700°F.
  13. The NiCrMoV alloy of any preceding claim, wherein oxygen is present at a concentration, by weight, of up to about 0.0075%.
  14. A turbine component including the alloy of any preceding claim.
  15. A NiCrMoV alloy, comprising, by weight:
    between about 0.06% and about 0.12% manganese, at least about 3.40% nickel; between about 0.22% and about 0.30% carbon, up to about 0.60% molybdenum, up to about 0.15% vanadium, up to about 2.00% chromium, up to about 0.012% phosphorus, up to about 0.007% sulfur, up to about 0.10% silicon, up to about 0.002% antimony, up to about 0.008% arsenic, up to about 0.012% tin, and up to about 0.015% aluminum;
    wherein the phosphorus is present at a concentration of at least about 0.007%, the sulfur is present at a concentration of at least about 0.006%, the silicon is present at a concentration of at least about 0.05%, or a combination thereof.
EP13170181.5A 2012-06-04 2013-05-31 Nickel-chromium-molybdenum-vanadium alloy and turbine component Withdrawn EP2671959A1 (en)

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Families Citing this family (2)

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Publication number Priority date Publication date Assignee Title
CN104878321B (en) * 2015-04-21 2017-01-04 中信重工机械股份有限公司 A kind of smelting process of 25Cr2Ni4MoV rotor steel
CN111705269A (en) * 2020-07-09 2020-09-25 河南中原特钢装备制造有限公司 Low-silicon steel 27NiCrMoV15-6 and smelting continuous casting production process thereof

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0225425A2 (en) * 1985-11-06 1987-06-16 Kabushiki Kaisha Kobe Seiko Sho Low alloy steel having good stress corrosion cracking resistance
JPH0234724A (en) * 1988-07-22 1990-02-05 Toshiba Corp Manufacture of turbine rotor
JPH08120400A (en) * 1994-10-25 1996-05-14 Japan Steel Works Ltd:The Steel for ultrahigh pressure vessel and method of manufacturing the same
EP0759499A1 (en) * 1995-08-21 1997-02-26 Hitachi, Ltd. Steam-turbine power plant and steam turbine
JPH10317105A (en) * 1997-05-20 1998-12-02 Hitachi Ltd High-strength steel, steam turbine long blade and steam turbine
EP1067206A2 (en) * 1999-07-09 2001-01-10 Hitachi, Ltd. Steam turbine blade, and steam turbine and steam turbine power plant using the same

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61190049A (en) * 1985-02-18 1986-08-23 Hitachi Ltd Low alloy steel
JPH0219446A (en) * 1988-07-05 1990-01-23 Toshiba Corp Turbine rotor
US5741374A (en) * 1997-05-14 1998-04-21 Crs Holdings, Inc. High strength, ductile, Co-Fe-C soft magnetic alloy
US6574966B2 (en) * 2000-06-08 2003-06-10 Hitachi, Ltd. Gas turbine for power generation
AT414341B (en) * 2003-11-07 2010-12-15 Boehler Edelstahl Gmbh & Co Kg STEEL FOR CHEMICALS - PLANTS - COMPONENTS
JP2006170006A (en) * 2004-12-14 2006-06-29 Toshiba Corp Steam turbine power generation system and low-pressure turbine rotor
DE102006025241A1 (en) * 2006-05-29 2007-12-06 Rheinmetall Waffe Munition Gmbh Method for producing forged steel for highly stressed weapons, tube blanks and a weapon equipped therewith
KR20100033421A (en) * 2008-08-11 2010-03-29 미츠비시 쥬고교 가부시키가이샤 Rotor for low pressure turbine
JP2011042812A (en) * 2009-08-19 2011-03-03 Japan Casting & Forging Corp Method for manufacturing forged steel article superior in toughness
US8523519B2 (en) * 2009-09-24 2013-09-03 General Energy Company Steam turbine rotor and alloy therefor
CN102234744B (en) * 2010-04-23 2013-06-26 宝山钢铁股份有限公司 Ultra-pure alloy and method for manufacturing turbine rotor forging by using same

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0225425A2 (en) * 1985-11-06 1987-06-16 Kabushiki Kaisha Kobe Seiko Sho Low alloy steel having good stress corrosion cracking resistance
JPH0234724A (en) * 1988-07-22 1990-02-05 Toshiba Corp Manufacture of turbine rotor
JPH08120400A (en) * 1994-10-25 1996-05-14 Japan Steel Works Ltd:The Steel for ultrahigh pressure vessel and method of manufacturing the same
EP0759499A1 (en) * 1995-08-21 1997-02-26 Hitachi, Ltd. Steam-turbine power plant and steam turbine
JPH10317105A (en) * 1997-05-20 1998-12-02 Hitachi Ltd High-strength steel, steam turbine long blade and steam turbine
EP1067206A2 (en) * 1999-07-09 2001-01-10 Hitachi, Ltd. Steam turbine blade, and steam turbine and steam turbine power plant using the same

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