US3318694A - Nickel chrome alloy - Google Patents

Nickel chrome alloy Download PDF

Info

Publication number
US3318694A
US3318694A US319970A US31997063A US3318694A US 3318694 A US3318694 A US 3318694A US 319970 A US319970 A US 319970A US 31997063 A US31997063 A US 31997063A US 3318694 A US3318694 A US 3318694A
Authority
US
United States
Prior art keywords
alloy
percent
nickel
carbon
manganese
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US319970A
Other languages
English (en)
Inventor
Arthur C Heitmann
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Owens Corning
Original Assignee
Owens Corning Fiberglas Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority to NL126516D priority Critical patent/NL126516C/xx
Application filed by Owens Corning Fiberglas Corp filed Critical Owens Corning Fiberglas Corp
Priority to US319970A priority patent/US3318694A/en
Priority to GB41541/64A priority patent/GB1041930A/en
Priority to FR992194A priority patent/FR1425319A/fr
Priority to BE654656D priority patent/BE654656A/xx
Priority to LU47189D priority patent/LU47189A1/xx
Priority to DK521664AA priority patent/DK116397B/da
Priority to NL6412470A priority patent/NL6412470A/xx
Priority to DE19641758721 priority patent/DE1758721B1/de
Priority to DEO10476A priority patent/DE1295851B/de
Priority to FI2284/64A priority patent/FI43500B/fi
Application granted granted Critical
Publication of US3318694A publication Critical patent/US3318694A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C03GLASS; MINERAL OR SLAG WOOL
    • C03BMANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
    • C03B37/00Manufacture or treatment of flakes, fibres, or filaments from softened glass, minerals, or slags
    • C03B37/01Manufacture of glass fibres or filaments
    • C03B37/04Manufacture of glass fibres or filaments by using centrifugal force, e.g. spinning through radial orifices; Construction of the spinner cups therefor
    • C03B37/047Selection of materials for the spinner cups
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/053Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 30% but less than 40%

Definitions

  • the invention relates to an alloy composed primarily of nickel, but including substantial amounts of chromium, tungsten, iron, molybdenum, a metal from the group consisting of tantalum and columbium, and a controlled amount of carbon, and, in alloys which are to be cast, a controlled amount of silicon and manganese-the alloy being particularly suited for apparatus used in the production of glass fibers by a centrifugal process.
  • Glass fibers can be produced by the so-called rotary or centrifugal process, such as illustrated and disclosed by Slayter Patent No. 2,609,566 and other patents.
  • a rotary fiber forming process involves introducing a molten stream of glass at a temperature above its liquidus into a rotating centrifuge or spinner.
  • the rotating centrifuge has peripheral orifices through which centrifugal force acting upon the rotating mass forces the molten glass to flow in small streams.
  • the streams of glass are usually attenuated into fine fibers.
  • the spinner or centrifuge may have a generally cylindrical peripheral wall in which the orifices or holes are provided. Economical and practical commercial production rates can be achieved only when there are several thousand of such orifices in the spinner and only when the spinner is rotated at least several thousand revolutions per minute. Such a device operates at a temperature at least as high as 2000* F.
  • the alloy of the invention is particularly useful in the form of the aforementioned spinners, and is also useful generally in the glass industry for numerous high temperature service applications which require a high resistance to attack by both molten glass and air, a low creep, and a high load carrying ability at high temperatures.
  • the nickel chrome alloy according to the invention consists essentially of certain balanced amounts of chromium, iron, tungsten, molybdenum, a metal from the group consisting of tantalum and columbium, and carbon, with the balance essentially nickel except for small amounts of certain other elements and minute amounts of impurities.
  • the nickel chrome alloy comprises from 33 to 37 percent of chromium, 3 to 3 /2 *Unless expressly stated otherwise, all parts and percents herein and in the appended claims are expressed as parts and percents by weight.
  • the alloy includes from /2 percent to 1 /2 percent of silicon, and, most desirably, the alloy includes silicon in the indicated proportion and such an amount of manganese that the molal ratio of silicon to manganese is from 3:1 to 6:1. Minute amounts of other elements, such as boron, vanadium, aluminum, titanium may enhance the properties of the alloy.
  • the nickel-base alloy of the invention has a composition upon analysis falling within the broad ranges set forth in the following Table I:
  • the alloy of the invention may be prepared in accordance with recognized present-day melt procedures for nickel-base alloys. Desirably, the constituents used are in a pure state to avoid unwanted constituents and to control carefully the final alloy composition. It is preferred that most constituents be added in the form of relatively pure metals, although compounds or master alloys, such as ferrochromium, ferromanganese, ferrosilicon, and the like, may be used. Preferably, the melting is accomplished in a neutral crucible under an argon atmosphere.
  • the charge when in a molten state, may be protected by a slag of any known type suitable for nickel-base alloys.
  • Other and additional constituents such as additional charges of chomium, manganese, silicon, tungsten, molybdenum, tantalum, and the like, requisite to arrive at the desired alloy composition, then may be added when the melt temperature is about 2700 to 2800" F.
  • these elements may be added with the original charge of chromium and nickel. Heating is continued and, generally, the melt is between about 2.830 and 3000 F. when poured.
  • a suitable scavenger may be added shortly before pouring to impart fluidity to the melt.
  • a desired article usually is made from the nickel-base alloy of the invention by casting.
  • Such articles may be spinners, centrifuge buckets, bushing support frames, or
  • the alloy, as cast, can be welded and machined.
  • Example I A specific example of the alloy of the invention was prepared by the method described above. This alloy, by analysis, consisted essentially of the following weight percentages:
  • the alloy of Example I produced according to the invention has very good resistance to corrosion by molten glass.
  • a cast bar of the alloy when immersed in molten glass at 2200 F. for two hours had a weight loss of 0.3%.
  • a cast bar of Alloy C had a weight loss of 0.7%.
  • Example II Another example of the alloy of the invention was prepared using the following weight percentages of metals prepared in the manner given above:
  • Example 111 Another example of an alloy of the invention was prepared using the following weight percentages of metals This alloy has less weight loss due to corrosion of molten glass than does Alloy C, and, in addition, has a greatly improved rupture life compared to that of Alloy C.
  • the high chromium nickel and molybdenum are required to provide the necessary corrosion resistance. Iron in the matrix appears to add strength. Chromium, tungsten, tantalum and iron form carbides which when precipitated provide strength. Some of each of the tungsten, tantalum and iron must remain in the matrix. At
  • At least about 0.1% carbon is necessary to form carbides. More than about 0.35% carbon causes too great a loss in ductility and results in spinner failures. Tantalum produces a random nonspherical carbide configuration. Columbium has an effect somewhat similar to tantalum, but the carbides formed tend to be spheroidized, so tantalum is preferred.
  • the silicon and manganese are not required for strength or corrosion resistance, but need only be used where the metal is to be cast. For good casting properties the molal ratio of silicon to manganese should be at least 3:1 and not more than about 6:1, preferably about 5: 1.
  • the alloy of the invention provides a unique combination of desirable characteristics and properties. Preparation and evaluation of a number of experimental alloys containing more and less of the various alloying constituents has established that the particular, specified, limited and balanced amounts are necessary to realize the advantages of the invention. The superior service life and excellent corrosion resistance to glass of the alloy of the invention are believed to be provided by a unique balancing effect of the amounts of the various constituents therein. Metallographic studies and microstructural analysis of the alloy support this conclusion.
  • the alloy comprises a dendritic network of complex carbides in an austentic matrix of nickel, chromium, iron and tungsten.
  • the optimum carbon content for the alloy is about 0.25 percent.
  • the alloy microstructure exhibits a random, fine, non-spherical carbide precipitate uniformly dispersed.
  • massive primary carbides and long continuous acicular carbide particles are found in alloys of somewhat higher carbon content. With lower carbon contents the precipitated carbide phase is finerand more randomly dispersed.
  • Percent by weight said alloy being characterized by resistance to attack by molten glass, low creep, and high load carrying ability at elevated temperatures.
  • said alloy being characterized by resistance to attack by molten glass, low creep, and high load carrying ability at elevated temperatures.
  • Percent by weight about said alloy being characterized by resistance to attack by molten glass, low creep, and high load carrying ability at elevated temperatures.
  • said alloy being characterized by resistance to attack by molten glass, low creep, and high load carrying ability at elevated temperatures.
  • said alloy being characterized by resistance to attack by molten glass, low creep, and high load. carrying ability at elevated temperatures.
  • Glass processing apparatus of the type contacted by molten glass said apparatus being formed from an alloy consisting essentially of the following percentages by weight: 33 to 37 percent of chromium, 3 to 3 /2 percent of tungsten, 2 to 10 percent of iron, 1 to 3 percent of a metal from the group consisting of tantalum and columbium, 0.1 to 0.35 percent of carbon, 3 to 3 /2 percent of molybdenum, and the balance essentially nickel.
  • Glass processing apparatus comprising a member having a plurality of openings theret-hrough through which molten glass passes to form tiny filaments of glass, said member being formed from an alloy consisting essentially of:

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Organic Chemistry (AREA)
  • Materials Engineering (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Manufacturing & Machinery (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Manufacture, Treatment Of Glass Fibers (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Laminated Bodies (AREA)
US319970A 1963-10-30 1963-10-30 Nickel chrome alloy Expired - Lifetime US3318694A (en)

Priority Applications (11)

Application Number Priority Date Filing Date Title
NL126516D NL126516C (nl) 1963-10-30
US319970A US3318694A (en) 1963-10-30 1963-10-30 Nickel chrome alloy
GB41541/64A GB1041930A (en) 1963-10-30 1964-10-12 Nickel chrome alloy
BE654656D BE654656A (nl) 1963-10-30 1964-10-21
FR992194A FR1425319A (fr) 1963-10-30 1964-10-21 Alliage nickel-chrome
DK521664AA DK116397B (da) 1963-10-30 1964-10-22 Nikkelchromlegering, der er bestandig mod smeltet glas.
LU47189D LU47189A1 (nl) 1963-10-30 1964-10-22
NL6412470A NL6412470A (nl) 1963-10-30 1964-10-27
DE19641758721 DE1758721B1 (de) 1963-10-30 1964-10-28 Nickel chrom legierung
DEO10476A DE1295851B (de) 1963-10-30 1964-10-28 Verwendung einer Chrom-Nickel-Legierung als Werkstoff fuer Geraete zur Glasfaserherstellung
FI2284/64A FI43500B (nl) 1963-10-30 1964-10-29

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US319970A US3318694A (en) 1963-10-30 1963-10-30 Nickel chrome alloy

Publications (1)

Publication Number Publication Date
US3318694A true US3318694A (en) 1967-05-09

Family

ID=23244323

Family Applications (1)

Application Number Title Priority Date Filing Date
US319970A Expired - Lifetime US3318694A (en) 1963-10-30 1963-10-30 Nickel chrome alloy

Country Status (8)

Country Link
US (1) US3318694A (nl)
BE (1) BE654656A (nl)
DE (2) DE1295851B (nl)
DK (1) DK116397B (nl)
FI (1) FI43500B (nl)
GB (1) GB1041930A (nl)
LU (1) LU47189A1 (nl)
NL (2) NL6412470A (nl)

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3384478A (en) * 1966-01-17 1968-05-21 Miles S. Firnhaber Nickel-chromium alloys
US3536466A (en) * 1968-02-21 1970-10-27 Tokyo Shibaura Electric Co Compression mould assembly for producing glass articles of uneven thickness
US3607210A (en) * 1968-02-23 1971-09-21 Owens Corning Fiberglass Corp Apparatus for conveying glass in a forehearth
US4203746A (en) * 1978-12-08 1980-05-20 Saint-Gobain Industries Method for centrifugal fiberization of hard glass
US4331741A (en) * 1979-05-21 1982-05-25 The International Nickel Co., Inc. Nickel-base hard facing alloy
EP0081091A2 (en) * 1981-12-08 1983-06-15 Nitto Boseki Co., Ltd. Alloy resistant to corrosion and wear at elevated temperature
US4518408A (en) * 1983-07-14 1985-05-21 Owens-Corning Fiberglas Corporation Method for producing glass fiber
US4877435A (en) * 1989-02-08 1989-10-31 Inco Alloys International, Inc. Mechanically alloyed nickel-cobalt-chromium-iron composition of matter and glass fiber method and apparatus for using same
US5914439A (en) * 1997-05-08 1999-06-22 Owens Corning Fiberglas Technology, Inc. Diffusion barrier for bores of glass fiber spinners providing high corrosion and oxidative resistance at high temperatures
US5964915A (en) * 1998-06-02 1999-10-12 Deloro Stellite Company Inc. Mold for forming glassware
US6482275B1 (en) 1998-01-28 2002-11-19 L. E. Jones Company Nickel based alloys for internal combustion engine valve seat inserts, and the like
US6519847B1 (en) 1998-06-12 2003-02-18 L. E. Jones Company Surface treatment of prefinished valve seat inserts
US20100272597A1 (en) * 2009-04-24 2010-10-28 L. E. Jones Company Nickel based alloy useful for valve seat inserts
EP2455504A1 (en) * 2010-11-19 2012-05-23 Schmidt + Clemens GmbH + Co. KG Nickel-chromium-iron-molybdenum alloy
US11261506B2 (en) * 2017-02-28 2022-03-01 Saint-Gobain Seva Alloy for a fibre-forming plate

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4404049A (en) 1978-03-16 1983-09-13 Fukuda Metal Foil & Powder Co., Ltd. Hard facing nickel-base alloy

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2587275A (en) * 1949-09-23 1952-02-26 Driver Harris Co Furnace element
US2607170A (en) * 1950-06-15 1952-08-19 Owens Corning Fiberglass Corp Apparatus for contacting molten glass
CA547402A (en) * 1957-10-08 T. Harris Geoffrey Nickel-chromium base alloys
US2955934A (en) * 1959-06-12 1960-10-11 Simonds Saw & Steel Co High temperature alloy
US3031717A (en) * 1957-03-08 1962-05-01 Saint Gobain Centrifugal fiber forming apparatus

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH284504A (de) * 1949-02-17 1952-07-31 Rolls Royce Verfahren zur Herstellung von Maschinenteilen aus hitzebeständigen Legierungen.
US3010201A (en) * 1958-12-29 1961-11-28 Owens Corning Fiberglass Corp Process for fabricating a centrifuge for handling molten glass

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA547402A (en) * 1957-10-08 T. Harris Geoffrey Nickel-chromium base alloys
US2587275A (en) * 1949-09-23 1952-02-26 Driver Harris Co Furnace element
US2607170A (en) * 1950-06-15 1952-08-19 Owens Corning Fiberglass Corp Apparatus for contacting molten glass
US3031717A (en) * 1957-03-08 1962-05-01 Saint Gobain Centrifugal fiber forming apparatus
US2955934A (en) * 1959-06-12 1960-10-11 Simonds Saw & Steel Co High temperature alloy

Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3384478A (en) * 1966-01-17 1968-05-21 Miles S. Firnhaber Nickel-chromium alloys
US3536466A (en) * 1968-02-21 1970-10-27 Tokyo Shibaura Electric Co Compression mould assembly for producing glass articles of uneven thickness
US3607210A (en) * 1968-02-23 1971-09-21 Owens Corning Fiberglass Corp Apparatus for conveying glass in a forehearth
DE2954306C2 (nl) * 1978-12-08 1987-10-29 Spafi - Societe Anonyme De Participations Financieres Et Industrielles, Courbevoie, Fr
US4203746A (en) * 1978-12-08 1980-05-20 Saint-Gobain Industries Method for centrifugal fiberization of hard glass
US4203747A (en) * 1978-12-08 1980-05-20 Saint-Gobain Industries Glass fiberization spinner alloy and use thereof
US4203748A (en) * 1978-12-08 1980-05-20 Saint-Gobain Industries Glass fiberization spinner
DE2911510A1 (de) 1978-12-08 1980-06-19 Saint Gobain Verfahren, vorrichtung und glaeser zum herstellen von glasfasern und damit hergestellte glasfasern
US4331741A (en) * 1979-05-21 1982-05-25 The International Nickel Co., Inc. Nickel-base hard facing alloy
EP0081091A2 (en) * 1981-12-08 1983-06-15 Nitto Boseki Co., Ltd. Alloy resistant to corrosion and wear at elevated temperature
EP0081091A3 (en) * 1981-12-08 1984-04-25 Nitto Boseki Co., Ltd. Alloy resistant to corrosion and wear at elevated temperature
US4518408A (en) * 1983-07-14 1985-05-21 Owens-Corning Fiberglas Corporation Method for producing glass fiber
US4877435A (en) * 1989-02-08 1989-10-31 Inco Alloys International, Inc. Mechanically alloyed nickel-cobalt-chromium-iron composition of matter and glass fiber method and apparatus for using same
US5914439A (en) * 1997-05-08 1999-06-22 Owens Corning Fiberglas Technology, Inc. Diffusion barrier for bores of glass fiber spinners providing high corrosion and oxidative resistance at high temperatures
US6482275B1 (en) 1998-01-28 2002-11-19 L. E. Jones Company Nickel based alloys for internal combustion engine valve seat inserts, and the like
US5964915A (en) * 1998-06-02 1999-10-12 Deloro Stellite Company Inc. Mold for forming glassware
US6519847B1 (en) 1998-06-12 2003-02-18 L. E. Jones Company Surface treatment of prefinished valve seat inserts
US7216427B2 (en) 1998-06-12 2007-05-15 L. E. Jones Company Surface treatment of prefinished valve seat inserts
US20100272597A1 (en) * 2009-04-24 2010-10-28 L. E. Jones Company Nickel based alloy useful for valve seat inserts
EP2455504A1 (en) * 2010-11-19 2012-05-23 Schmidt + Clemens GmbH + Co. KG Nickel-chromium-iron-molybdenum alloy
WO2012065749A1 (en) * 2010-11-19 2012-05-24 Schmidt + Clemens Gmbh + Co. Kg Nickel-chromium-iron-molybdenum alloy
US11261506B2 (en) * 2017-02-28 2022-03-01 Saint-Gobain Seva Alloy for a fibre-forming plate

Also Published As

Publication number Publication date
LU47189A1 (nl) 1965-04-22
DE1758721B1 (de) 1971-07-29
GB1041930A (en) 1966-09-07
FI43500B (nl) 1970-12-31
BE654656A (nl) 1965-04-21
NL6412470A (nl) 1965-05-03
NL126516C (nl)
DK116397B (da) 1970-01-05
DE1295851B (de) 1969-05-22

Similar Documents

Publication Publication Date Title
US3318694A (en) Nickel chrome alloy
US4140555A (en) Nickel-base casting superalloys
US3933484A (en) Cobalt-base alloy
US3980473A (en) Ultra high strength, carbide-strengthened, cobalt-base superalloy
US3681059A (en) Nickel-chromium alloy for reformer tubes
US3984240A (en) High strength corrosion resistant cobalt-base superalloy
US3806338A (en) Nickel-chromium alloy
UA78681C2 (uk) Спосіб виробництва мінеральної вати (варіанти), сплав на основі кобальту для цього способу (варіанти), виріб із сплаву (варіанти) та спосіб виготовлення виробу
JP4125382B2 (ja) コバルト基合金、この合金から製造された製品及びその製造方法
US4497771A (en) Low tantalum content cobalt-base alloy
US4092183A (en) Directionally solidified castings
US3170789A (en) Nickel-base alloy
US4708848A (en) Nickel/chrome base superalloys
US4119456A (en) High-strength cast heat-resistant alloy
US4456481A (en) Hot workability of age hardenable nickel base alloys
US2783144A (en) Hard facing alloy
JP5461418B2 (ja) 耐火合金、繊維形成板、および鉱物ウールを製造する方法
JPS6254389B2 (nl)
CA1073708A (en) Oxidation resistant iron base alloys
US3902899A (en) Austenitic castable high temperature alloy
US3343949A (en) Nickel-beryllium alloy and method of heat treating same
JPS6330381B2 (nl)
US4367083A (en) Nickel-base spinner alloy
US2955034A (en) Austenitic alloy steel
US4272289A (en) Oxidation resistant iron base alloy articles for welding