Classifications

• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/001—Ferrous alloys, e.g. steel alloys containing N
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/002—Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/20—Ferrous alloys, e.g. steel alloys containing chromium with copper
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
  • C22C38/22—Ferrous alloys, e.g. steel alloys containing chromium with molybdenum or tungsten
• • C—CHEMISTRY; METALLURGY
  • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
  • C22C—ALLOYS
  • C22C38/00—Ferrous alloys, e.g. steel alloys
  • C22C38/60—Ferrous alloys, e.g. steel alloys containing lead, selenium, tellurium, or antimony, or more than 0.04% by weight of sulfur

Definitions

• This invention relates to martensitic stainless steel alloys, and in particular to a martensitic stainless steel alloy having a composition that is balanced to provide a unique combination of corrosion resistance, cold formability, machinability, and high strength.
• the balance of the alloy is essentially iron together with usual impurities.
• Nickel and copper are balanced such that the ratio Ni/Cu is less than 0.2, preferably not more than about 0.15, and better yet, not more than about 0.10.
• Carbon is present in this alloy because it benefits the high strength provided by the alloy. Carbon is also beneficial for the good phase balance of the alloy. For those reasons, the alloy contains at least about 0.10%, better yet at least about 0.15%, and preferably at least about 0.20% carbon. Too much carbon results in the excess formation of primary carbides in this alloy which adversely affect the corrosion resistance and the cold formability of the alloy. Therefore, the alloy contains not more than about 0.40% carbon, better yet not more than about 0.30% carbon, and preferably not more than about 0.25% carbon.
• Manganese is an element that is beneficial to the phase balance of this alloy because it promotes the formation of austenite and inhibits the formation of ferrite.
• the alloy contains up to about 2.0% manganese.
• the alloy contains at least about 0.01% manganese.
• sulfur is added to this alloy to benefit its machinability
• manganese sulfides can form which adversely affect the corrosion resistance provided by the alloy. Therefore, when more than about 0.005% sulfur is present in the alloy, manganese is restricted to not more than about 1.0% and preferably to not more than about 0.3%. Restricting the formation of manganese sulfides by keeping manganese at such low levels promotes the formation of chromium sulfides which benefit machinability, but do not adversely affect the corrosion resistance provided by this alloy.
• a small amount of sulfur can be present in this alloy to benefit the machinability of the alloy when desired or needed. Therefore, when good machinability is needed, the alloy contains at least about 0.005% sulfur and preferably at least about 0.007% sulfur. Too much sulfur adversely affects the hot workability and cold formability of the alloy. Also, as described above, sulfur combines with available manganese to form manganese sulfides which adversely affect the corrosion resistance of the alloy. Therefore, when present, sulfur is limited to not more than about 0.030%, better yet not more than about 0.020%, and preferably not more than about 0.015%. Selenium can be substituted for some or all of the sulfur on a 1:1 weight percent basis because selenium also benefits the machinability of this alloy.
• sulfur is preferably restricted to not more than 0.010%, better yet to not more than about 0.007%, and for best results, to not more than about 0.005%.
• Chromium is present in this alloy to benefit the corrosion resistance provided by the alloy. Accordingly, the alloy contains at least about 10% chromium, better yet at least about 11.5% chromium, and preferably at least about 13.0% chromium. Too much chromium results in the formation of ferrite in the alloy in an amount that adversely affects the corrosion resistance and hot workability of the alloy. Therefore, chromium is restricted to not more than about 15% chromium, better yet to not more than about 14.3% chromium, and preferably to not more than about 13.8% chromium in this alloy.
• This alloy contains at least about 0.75% molybdenum because it benefits the corrosion resistance of the alloy, particularly in chloride-containing environments.
• the alloy contains at least about 1.25% molybdenum and preferably at least about 1.75% molybdenum for that purpose.
• molybdenum promotes the formation of ferrite in the alloy and too much ferrite adversely affects the general corrosion resistance and the hot workability of the alloy. Therefore, the alloy contains not more than about 4.0% molybdenum, better yet not more than about 3.0% molybdenum, and preferably not more than about 2.5% molybdenum.
• Copper is present in this alloy to benefit the cold formability of the alloy. Copper also helps provide an acceptable phase balance in the alloy and contributes to the machinability of the alloy when sulfur is present.
• the advantages provided by copper are realized when the alloy contains at least about 1.5%. Preferably the alloy contains at least about 1.75% copper and better yet, at least about 2.0% copper. Too much copper can result in hot shortness in the alloy which adversely affects its hot workability. Therefore, copper is restricted to not more than about 4.0%, better yet to not more than about 3.5%, and preferably to not more than about 3.0% in this alloy.
• nickel can be present in this alloy to benefit the phase balance of the alloy.
• nickel is restricted to not more than about 0.35% and better yet to not more than about 0.25% because nickel increases the annealed strength of the alloy which adversely affects its cold formability.
• nickel and copper are balanced in this alloy such that the ratio of nickel to copper (Ni/Cu) is preferably less than 0.2, better yet, not more than about 0.15, and preferably, not more than about 0.10.
• This alloy contains at least about 0.02% nitrogen, better yet at least about 0.04% nitrogen, and preferably at least about 0.05% nitrogen because nitrogen contributes to the high strength provided by the alloy. Nitrogen also benefits the phase balance and the corrosion resistance provided by this alloy. Too much nitrogen in the alloy results in blowy ingots and adversely affects the cold formability and hot workability of the alloy. Therefore, nitrogen is restricted to not more than about 0.15%, better yet to not more than about 0.10% nitrogen, and preferably to not more than about 0.08% nitrogen.
• Silicon can be present in this alloy in an amount that is effective to deoxidize the alloy during melting. However, too much silicon promotes the formation of excess ferrite in the alloy which adversely affects the corrosion resistance and the hot workability of the alloy. Therefore, the alloy may contain up to about 2.0% silicon for use as a deoxidizer. However, silicon is preferably limited to not more than about 1.0%, and better yet to not more than about 0.75% in this alloy.
• the balance of the alloy is iron except for the usual impurities and additives found in similar grades of martensitic stainless steel alloys intended for the same or similar use or service.
• the alloy contains up to about 0.2% phosphorus, better yet up to about 0.1%, and preferably not more than about 0.05% phosphorus.
• the alloy contains up to about 0.20%, but preferably not more than about 0.10% vanadium. Up to about 0.10%, preferably not more than about 0.01% of niobium and tantalum combined can be present in this alloy.
• the alloy contains less than about 0.01% each of titanium, aluminum, and zirconium.
• the alloy may contain up to about 0.003% boron. Small, trace amounts, typically less than 0.001% each of calcium and zirconium may also be present in the alloy.
• An ingot of the alloy according to the present invention is preferably hot worked from a furnace temperature of about 2000-2300° F. (1093-1260° C.), preferably about 2100-2250° F. (1149-1232° C.), with reheating as necessary after intermediate reductions.
• the alloy is hot worked to size in which it can be hot rolled to a cross-sectional dimension in which it can be cold drawn.
• Intermediate anneals are carried out at about 1650-1700° F. (900-927° C.) for about 4 hours followed by a furnace cool preferably at about 30F.° per hour to 1200° F. (649° C.). The alloy is then cooled in air to room temperature.
• the alloy is preferably hot rolled to a cross-sectional dimension that is suitable for cold drawing. Hot rolling is preferably conducted from a starting temperature of about 2150-2250° F. (1177-1232° C.). After hot rolling, the alloy is annealed at about 1450-1550° F. (788-843° C.) for about 2 hours. Preferably, the alloy is furnace cooled at about 20F.° per hour from the annealing temperature down to about 1200° F. (649° C.) and then air cooled to room temperature.
• the alloy is cold drawn to final dimension in one or more passes depending on the amount of reduction needed. Prior to cold drawing, the alloy can be shaved, polished, and precoated. After cold drawing to the desired size, the wire is cleaned to remove residual drawing compound and any other surface contamination. The alloy wire is then annealed with the same or similar cycle described above.
• the alloy wire can be coated with a surface layer of copper or other coating to prevent galling during cold forming operations.
• the alloy is cold formed, as by cold heading, into a desired shape and dimension.
• Cold formed products include fasteners such as screws, bolts, and nuts.
• the final product form is hardened by austenitizing it at about 1750-2000° F. (954-1093° C.), preferably at least about 1900° F. (1038° C.) for about 1 hour, followed by quenching.
• the alloy is preferably heated at the austenitizing temperature in vacuum for about 1 hour and quenched by rapid gas cooling to protect against thermal scaling (oxidation).
• the alloy can be tempered at about 300-900° F. (149-482° C.) for about 2 hours and then cooled in air.
• the alloy of the present invention can be formed into a variety of shapes for a variety of uses. However, the alloy is preferably formed into rod or wire which can be cold formed into useful articles as described above.

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• Chemical & Material Sciences (AREA)
• Engineering & Computer Science (AREA)
• Materials Engineering (AREA)
• Mechanical Engineering (AREA)
• Metallurgy (AREA)
• Organic Chemistry (AREA)
• Heat Treatment Of Steel (AREA)

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• 2005
  • 2005-07-29 US US11/192,246 patent/US20070025873A1/en not_active Abandoned
• 2006
  • 2006-07-21 CN CNA2006800277959A patent/CN101233254A/zh active Pending
  • 2006-07-21 WO PCT/US2006/028567 patent/WO2007016004A1/fr not_active Ceased
  • 2006-07-21 CA CA2615682A patent/CA2615682C/fr active Active
  • 2006-07-21 KR KR1020087003778A patent/KR20080034939A/ko not_active Ceased
  • 2006-07-21 EP EP06788241A patent/EP1910583A1/fr not_active Withdrawn
  • 2006-07-21 JP JP2008524010A patent/JP2009503257A/ja active Pending
  • 2006-07-28 TW TW095127823A patent/TWI332031B/zh not_active IP Right Cessation
• 2009
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