US3658515A - Hard wear-resistant ferrous alloy - Google Patents

Hard wear-resistant ferrous alloy Download PDF

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Publication number
US3658515A
US3658515A US48527A US3658515DA US3658515A US 3658515 A US3658515 A US 3658515A US 48527 A US48527 A US 48527A US 3658515D A US3658515D A US 3658515DA US 3658515 A US3658515 A US 3658515A
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United States
Prior art keywords
weight percent
wear
alloy
hard
ferrous alloy
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Expired - Lifetime
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US48527A
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English (en)
Inventor
Gilbert A Saltzman
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Nordson Xaloy Inc
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Xaloy Inc
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Assigned to IRVING TRUST COMPANY reassignment IRVING TRUST COMPANY SECURITY INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: XALOY, INCORPORATED
Assigned to XALOY INCORPORATED reassignment XALOY INCORPORATED ASSIGNOR DOES NEREBY RELEASE ITS SECURITY INTEREST IN SAID PATENT IN AN ASSIGNMENT RECORDED AT REEL 4175, FRAMES 148-154. (SEE RECORD FOR DETAILS) Assignors: IRVING TRUST COMPANY, ANEW YORK BANKING CORPORATION
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C37/00Cast-iron alloys
    • C22C37/06Cast-iron alloys containing chromium
    • C22C37/08Cast-iron alloys containing chromium with nickel

Definitions

  • the present invention relates to a wear-resistant ferrous alloy having improved hardness characteristics, and more particularly to such an alloy desirable for use as a lining for catalytic crackers, plastic extruders, Banbury mixers or other devices requiring hard, wear-resistant linings.
  • Bimetallic cylinders having centrifugally cast wear-resistant ferrous alloy linings are commonly used for heating, mixing and pressurizing plastic materials in extruders and injection molding equipment. Alloys so useful may principally consist of iron containing carbon in amounts of from 2 to 4 percent by weight, boron in amounts of from 0.2 to 2.5 percent by weight, and nickel in amounts of from about 1.5 to 9 percent by weight, although minor proportions of additional metals such as chromium, tungsten, manganese, vanadium, molybdenum, cobalt, etc. may also be tolerated therein. Such alloys and bimetallic cylinders manufactured by the centrifugal casting thereof are described, for example, in Kormann et al. U.S. Pat. Nos. 2,046,913 and 2,046,914 granted on July 7, 1936 and assigned to the predecessor of the assignee of the present invention.
  • Ferrous alloy linings of the type described in the Kormann et al. patents have typical room temperature hardness characteristics of from 58 to 64 Rockwell C in the as centrifugally cast (as-spun) condition.
  • the surfaces of such alloy linings provide superior resistance to wear during operation of the extruder or injection molder incorporating the same. Such wear may, for example, result from abrasive fillers present in the plastic material to be extruded or molded, or from pressures produced by the feed screw of the device bearing against the cylinder under abnormal operating conditions.
  • Operating temperatures for plastic extrusion and injection molding generally range from about 400 to 650 F., and may be as high as 800 F. for certain materials.
  • Extruder or injection molder cylinder linings must, therefore, possess excellent hot hardness characteristics in addition to other wear-resistant properties. Under abnormal operating conditions, for example when heater controls fail to operate or when, as indicated above, the feed screw bears against the cylinder walls, such a lining material may even be locally exposed to temperatures markedly higher than those specified above which are normally encountered in practice. Such elevated temperature exposure may reduce the subsequent room temperature hardness of the alloy lining, leaving areas of reduced hardness which may be subject to failure.
  • Iron, balance to make up The expression up to" a specified percentage is intended to include 0 percent of the indicated component.
  • centrifugally cast linings of the ferrous alloys of the above compositions possess significantly higher hot hardness characteristics at temperatures up to 700 to 800 F., and significantly lower losses in room temperature hardness after exposure to temperatures of from about 800 to l,300 F., as compared with previously known hard, wear-resistant ferrous alloys.
  • the addition of the specified proportions of chromium and, possibly, molybdenum to the alloy composition provides bimetallic cylinder linings which exhibit these superior characteristics.
  • alloy linings prepared from the composition of Example 3 below have Rockwell hardnesses (Rc) at 500 of 62.3 whereas linings prepared from a composition which has previously been commercially used and which is within the scope of the previously discussed Kormann et al. patents (control A described below, having a composition incorporating 3.67 percent carbon, 1.06 percent boron, 1.42 percent manganese, 0.92 percent silicon, and 4.35 percent nickel) possess a comparable hardness of only 56.4 (see Table III below).
  • the room temperature hardness of linings of the composition of Example 3 is Rc 58.2 after exposure to a l,200 elevated temperature for 4 hours, whereas the comparable hardness exhibited by the above mentioned control composition is only Rc 47.8.
  • the ferrous alloys hereof are, as indicated above, preferably employed in the formation of liners for various devices requiring hard, wear-resistant material contacting surfaces.
  • Such linings may, for example, be formed on either the interior or exterior surfaces of cylindrical ferrous metal shells and the desired devices fabricated therefrom, e.g., asdescribed in the aforesaid Kormann et al. U.S. Pat. No. 2,046,914, as well as in U.S. Pat. Nos. 2,275,503, 2,319,657 and 3,254,381.
  • One mode of manufacturing wear-resistant linings in accordance with the present invention involves charging the alloy composition into the region in which a lining is to be formed, e.g., into the interior of a tubular steel housing.
  • the alloy composition may previously be fused and charged in shot form or in cast and crushed form into the tubular housing.
  • the unit After capping the ends of the tubular steel housing to containthe charged alloy and prevent atmospheric oxidation, the unit is placed in a furnace, frequently'in admixture with a flux to prevent oxidation, and heated at a temperature of from about 2,000 to 2,300 F. to melt the components. After heating the sealed tube to above the melting point of the alloy composition, i.e., from about 2,000 to 2,300 F., for up to 2 hours (depending on the size of the tube), the assembly is removed from the furnace and spun to centrifugally form the alloy lining.
  • the assembly is rapidly cooled during the spinning operation, e.g., within about 10 minutes, to temperature of about 1,700 F.
  • the assembly is thereafter covered with a suitable insulating material, e.g., sand, diatomaceous earth or silica, and permitted to cool over a period of from about 24 to 48 hours to temperatures within the range of from about 300 to 500 F.
  • the alloy melt is thus fused and metallurgically bonded to the steel housing.
  • the caps are thereafter removed from the ends of the housing and the internal and external diameters desired are finished in customary manner.
  • Hard, wear-resistant ferrous alloy compositions within the scope of the present invention were prepared by mixing calculated portions of pig iron and the various alloying ingredients, followed by melting and fusing the same.
  • Various control compositions identified as controls A-E, were similarly prepared, control A corresponding to a composition commercially used for bimetallic tubular linings in accordance with the above mentioned Kormann et al. patents and controls B-E otherwise varying from the composition of the alloys of this invention.
  • the various alloy compositions were air melted in a 20 KW Ajax-Magnethermic induction furnace and cast into waffle plate molds. Each waffle plate was broken up into approximate l-inch squares for loading in steel cylinders, nominally 1% inches I.D. X 3 inches O.D. X 2 feet length, for production of centrifugally cast linings.
  • Table 1 The analyses of the respective alloy compositions of Examples l-3 and controls A-E, as loaded for centrifugal 2 casting, are set forth in Table 1 below.
  • rings were cut from the cylinders incorporating linings of the alloys of Examples 2 and 3 and controls A-E. Waffle plates from which the linings were prepared and the lining ring specimens themselves were examined metallographically and the following hardness measurements made on the respective lining samples.
  • the room temperature hardnesses of the several lining samples, as spun, were determined. The samples were then heated at 1,500 F. for l or 4 hours (the time of heating was found immaterial) and air. cooled, after which the average room temperature hardnesses were again determined.
  • the as-spun and heat treated room temperature hardness characteristics of the various inlay samples are set forth in Table 11 below.
  • the alloys of the present invention have hardnesses of Rc 60 or greater at temperatures up to about 500 F.
  • the composition of control A has a hot hardness of less than Re 58 above about 300 F.
  • control alloys C-E have hardnesses of less than RC 60 above about 300 F.
  • the hardness characteristics of the several alloy compositions drop rapidly above 500; however, it will be noted that the hardnesses of the compositions of Examples 2 and 3 are markedly superior to those of controls A, C, D and E at each of the temperature levels up to l,200 F and superior to control B at temperatures within the range of from 300 to 700.
  • the alloys of Examples 2 and 3 retain hot hardnesses of Re 58 to above 600 F.
  • control A has a room temperature hardness of less than Re 58 tiller exposure in temperatures above 800" F.
  • Controls C, D and E retain room temperature hardnesses of Re 58 or greater after exposure up to 850 to 925.
  • the alloys of Examples 2 and 3 and control B retain hardnesses of Rc 58 or greater after exposure to 950, but the latter material exhibits decreased hardness characteristics relative to the compositions of Examples 2 and 3 after exposure to temperatures of the order of l,300 F.
  • the alloys of the present invention exhibit marked superiority over the previously employed alloy of control A throughout the temperature range of from 800 to 1,300 E, the alloy of Example 3 having room temperature hardnesses of from 2.9 to 10.3 Rockwell-C points greater than those for control A after exposure at temperatures throughout the noted range.
  • a hard, wear-resistant ferrous alloy consisting essentially of the following ingredients fused together in approximately the proportions stated below:
  • a hard, wear-resistant liner for a steel housing constituted of the ferrous alloy of claim 1.
  • a hard, wear-resistant liner for a steel housing constituted of the ferrous alloy of claim 2.
  • a hard, wear-resistant liner for a steel housing constituted of the ferrous alloy of claim 3.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Extrusion Moulding Of Plastics Or The Like (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)
  • Injection Moulding Of Plastics Or The Like (AREA)
US48527A 1970-06-22 1970-06-22 Hard wear-resistant ferrous alloy Expired - Lifetime US3658515A (en)

Applications Claiming Priority (1)

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US4852770A 1970-06-22 1970-06-22

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US3658515A true US3658515A (en) 1972-04-25

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US48527A Expired - Lifetime US3658515A (en) 1970-06-22 1970-06-22 Hard wear-resistant ferrous alloy

Country Status (5)

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US (1) US3658515A (de)
JP (1) JPS5335535B1 (de)
BE (1) BE768691A (de)
DE (1) DE2130714A1 (de)
GB (1) GB1302321A (de)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3909252A (en) * 1973-11-01 1975-09-30 Suzuki Motor Co Wear-resistant cast iron for sliding surfaces
US4089466A (en) * 1977-03-30 1978-05-16 Lomax Donald P Lining alloy for bimetallic cylinders
US4103800A (en) * 1977-04-28 1978-08-01 Lomax Donald P Backing material
DE3227085A1 (de) * 1981-07-20 1983-02-03 Ronald M. 53183 Wales Wis. Boggs Legierung
US4596282A (en) * 1985-05-09 1986-06-24 Xaloy, Inc. Heat treated high strength bimetallic cylinder
US5183636A (en) * 1991-07-01 1993-02-02 Wall Colmonoy Corporation Braze filler metal with enhanced corrosion resistance
US5234510A (en) * 1991-02-15 1993-08-10 Wall Colmonoy Corporation Surfacing nickel alloy with interdendritic phases
US5565277A (en) * 1993-11-04 1996-10-15 Xaloy, Inc. Injection molding and extrusion barrels and alloy compositions thereof
DE3927854C2 (de) * 1986-08-25 1999-05-27 Xaloy Inc Verfahren zur Herstellung einer Innenauskleidung eines Hohlraumes sowie Legierung zur Herstellung dieser Innenauskleidung
US6887322B2 (en) 2001-04-09 2005-05-03 Wexco Corporation High pressure cylinders including backing steel with tool steel lining

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3997370A (en) * 1975-11-17 1976-12-14 Bethlehem Steel Corporation Method of hot reducing ferrous and ferrous alloy products with composite martensitic nodular cast chill iron rolls
DE3390167T1 (de) * 1982-07-19 1984-11-29 GIW Industries, Inc., Grovetown, Ga. Abriebsbeständiger Weißguß
US4638847A (en) * 1984-03-16 1987-01-27 Giw Industries, Inc. Method of forming abrasive resistant white cast iron

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2066848A (en) * 1926-10-21 1937-01-05 Int Nickel Co Chill cast iron alloy roll
US2111278A (en) * 1937-12-24 1938-03-15 Eaton Mfg Co Ferrous alloy
US3370941A (en) * 1966-09-22 1968-02-27 Johnson Products Inc Tungsten-containing alloy cast iron useful for internal combustion engine parts

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2046914A (en) * 1935-05-17 1936-07-07 Ind Res Lab Ltd Hard ferrous-lined tube
FR1453511A (fr) * 1965-08-13 1966-06-03 Promecan Sisson Lehmann Fonte blanche de grande dureté et de grande résilience

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2066848A (en) * 1926-10-21 1937-01-05 Int Nickel Co Chill cast iron alloy roll
US2111278A (en) * 1937-12-24 1938-03-15 Eaton Mfg Co Ferrous alloy
US3370941A (en) * 1966-09-22 1968-02-27 Johnson Products Inc Tungsten-containing alloy cast iron useful for internal combustion engine parts

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3909252A (en) * 1973-11-01 1975-09-30 Suzuki Motor Co Wear-resistant cast iron for sliding surfaces
US4089466A (en) * 1977-03-30 1978-05-16 Lomax Donald P Lining alloy for bimetallic cylinders
US4103800A (en) * 1977-04-28 1978-08-01 Lomax Donald P Backing material
DE3227085A1 (de) * 1981-07-20 1983-02-03 Ronald M. 53183 Wales Wis. Boggs Legierung
US4399198A (en) * 1981-07-20 1983-08-16 Lomax Donald P Lining alloy for bimetallic cylinders
US4596282A (en) * 1985-05-09 1986-06-24 Xaloy, Inc. Heat treated high strength bimetallic cylinder
DE3927854C2 (de) * 1986-08-25 1999-05-27 Xaloy Inc Verfahren zur Herstellung einer Innenauskleidung eines Hohlraumes sowie Legierung zur Herstellung dieser Innenauskleidung
US5234510A (en) * 1991-02-15 1993-08-10 Wall Colmonoy Corporation Surfacing nickel alloy with interdendritic phases
US5183636A (en) * 1991-07-01 1993-02-02 Wall Colmonoy Corporation Braze filler metal with enhanced corrosion resistance
US5565277A (en) * 1993-11-04 1996-10-15 Xaloy, Inc. Injection molding and extrusion barrels and alloy compositions thereof
US6887322B2 (en) 2001-04-09 2005-05-03 Wexco Corporation High pressure cylinders including backing steel with tool steel lining

Also Published As

Publication number Publication date
JPS5335535B1 (de) 1978-09-27
GB1302321A (de) 1973-01-10
DE2130714A1 (de) 1971-12-23
BE768691A (fr) 1971-11-03

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Effective date: 19851002