US3357826A - Powder metallurgical production of chromium-containing alloys - Google Patents

Powder metallurgical production of chromium-containing alloys Download PDF

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Publication number
US3357826A
US3357826A US594012A US59401266A US3357826A US 3357826 A US3357826 A US 3357826A US 594012 A US594012 A US 594012A US 59401266 A US59401266 A US 59401266A US 3357826 A US3357826 A US 3357826A
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Prior art keywords
chromium
billet
powder
carbon
chromium oxide
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US594012A
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English (en)
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Honaker Harold
James C Judd
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Huntington Alloys Corp
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International Nickel Co Inc
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Priority to US594012A priority Critical patent/US3357826A/en
Priority to GB50140/67A priority patent/GB1141576A/en
Priority to DE19671558719 priority patent/DE1558719A1/de
Priority to AT1018567A priority patent/AT279191B/de
Priority to FR127967A priority patent/FR1544390A/fr
Priority to CH1587467A priority patent/CH504534A/fr
Priority to SE15590/67A priority patent/SE324062B/xx
Priority to BE706484D priority patent/BE706484A/xx
Application granted granted Critical
Publication of US3357826A publication Critical patent/US3357826A/en
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    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C1/00—Making non-ferrous alloys
    • C22C1/04—Making non-ferrous alloys by powder metallurgy
    • C22C1/0433—Nickel- or cobalt-based alloys
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/001—Starting from powder comprising reducible metal compounds
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F9/00—Making metallic powder or suspensions thereof
    • B22F9/16—Making metallic powder or suspensions thereof using chemical processes
    • B22F9/18—Making metallic powder or suspensions thereof using chemical processes with reduction of metal compounds
    • B22F9/20—Making metallic powder or suspensions thereof using chemical processes with reduction of metal compounds starting from solid metal compounds
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C1/00—Making non-ferrous alloys
    • C22C1/04—Making non-ferrous alloys by powder metallurgy
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C33/00—Making ferrous alloys
    • C22C33/02—Making ferrous alloys by powder metallurgy
    • C22C33/0257—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements
    • C22C33/0278—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5%
    • C22C33/0285—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5% with Cr, Co, or Ni having a minimum content higher than 5%

Definitions

  • the present invention is directed to the production of chromium-containihg alloy products by powder metal- I lurgy and, more particularly, -to kthe production of wrought chromium-containing alloy products using powders as the starting materials.
  • metals such as nickel and iron, v nickel-iron alloys, etc.
  • metals such as nickel and iron, v nickel-iron alloys, etc.
  • metal powders of controlled composition are readily available.
  • nickel and iron powders may readilybe obtained commercially.
  • chromium-containing alloys by the aforementioned method also since alloys such as nickelchromium alloys and nickel-chromium-iron alloys have properties which are in industrial demand.
  • chromium powders are invariably contaminated with chromium oxide on the surface thereof and attempts to produce chromium-containing alloys from pressed and sintered blends of such oxide-contaminated chromium powders with other metal powders such as nickel powder have vresulted in the production of' final compacted metal articles which were still contami- ICC useful products which would have properties superior to those obtainable in wrought products of the same nominal composition made by conventional procedures from an ingot of solidified molten metal.
  • FIGURE 1 depicts the time-temperature-sensitization relation determined from corrosion rates in boiling nitric acid of a wrought nickel-chromium-iron alloy produced according to the invention
  • FIGURE 2 is a -photomicrograph taken at 100 diameters depicting the unetched microstructure of a wrought nickelchromium-iron alloy produced in accordance with the invention from an initial metal powder mixture containing oxide-contaminated chromium powder;
  • FIGURES 3 and 4 are photomicrographs taken at' 100 diameters depicting the unetched microstructures of wrought nickel-chromium-iron alloys produced from initial metal powder mixtures containing oxide-contaminated chromiumppowder but in which ingredients required in accordance with the invention to be vpresent in the initial powder mixture were omitted.
  • the invention is directed to a method for producing wrought metal products made of a chromiumcontaining alloy having improved metallurgical properum oxide, which comprises providing such a mixture of chromium powder with an iron-group metal powder having a controlled carbon content and containing a small amount of a volatile spacing agent, pressing'the resulting mixture, heating the powder pressing to a temperature exceeding the volatilization temperature of the said spacing agent in a protective atmosphere, sintering the powder pressing at a temperature exceeding'the reduction tem- A perature of chromium oxide with carbon in a gas reducing atmosphere reducing to chromium oxide, andv working, e.g., hot working, the sin-tered powder mixture to fo'rrnv a consolidated alloy shape substantially 'devoid' of chromium oxide contamination.
  • an initial powder mixture which contains in weight percent about l5% to about 60% of chromium powder, e.g., about 10% to about 30% or 50% chromium, up to about 90% nickel mixture also contains carbon inscontrolled amounts of at least about.0.1% .up to about' 0.8%.
  • the carbon. content Patented Dec.' 12, 1967 ties and characteristics from an initial powder mixture containing chromium powder contaminated with chromipowder, and up to about 90% iron powder.
  • the initial 3 of the mixture is controlled within the required range by additions of carbon thereto.
  • Carbon may be introduced into the mixture as carbonv or graphite powder or as a heat decomposable carbon compound such as a liquid or solid hydrocarbon, carbohydrate, etc.
  • the initial mixture also contains at least about 0.01% up to about 0.5%, by weight, of a heat volatilizable spacing agent having a volatilization temperature between room temperature and about 1200u F.
  • the spacing agent advantageously is a salt such as an ammonium halide, eg., ammonium chloture below about 1200" F., such as ammonium carbonate, may be employed in the place of the ammonium halide.
  • the ammonium halides are particularly advantageous spacing agents for purposes of the present invention, since they volatilize at temperatures below about 1200 F. to yield gaseous products which are not'found in the sintered metal.
  • the amount of heat volatilizable spacing agent is v at least' about 0.01% by weight of the initial powder mixture to obtain the minimum required pore formation during sintering but does not exceed about 0.5% by weight because cracking of the billet may then be encountered during sintering.
  • the amount of spacing agent is about 0.05% to about 0.2% by weight of the initial mixture.
  • Chromium powders including ferrochromium powders, employed in accordance with the invention have a particle size of about 1 to about 60 microns, although from the standpoint of diffusion, the particle size desirably does not exceed about 40 microns, and generally contain about 0.4% to about 0.8% oxygen as a chromium oxide contaminant which is generally present on the surface of the powders.
  • the chromium powder should not contain more than about 0.025% sulfur, more than about 0.05% mag- Y nesium, more than about 0.3% silicon or more than about 0.1% aluminum.
  • Magnesium, silicon and aluminum should Ibe as low as possible since the oxides of these elements form difiicultly-reducible spinels with chromium oxide.
  • electrolytic chromium powder which is very low in silicon, aluminum and magnesium, is very satisfactory for purposes of the invention.
  • other ingredients may be included in the initial powder mixture.
  • the initial powder mixtures may contain up to about 5% columbiurn, up to about 4% copper, up to about 20% molybdenum, up to about 10% tungsten, and up to about 20% cobalt.
  • Powdered materials such as aluminum, titanium,- silicon and manganese desirably are not present in the initial mixtures since these metals and/ or their oxides interfere with the reduction of chromium oxide as contemplated in accordance with the invention.
  • the powders thereof can be initially coated with nickel, iron or cobalt as, for example, by decomposition of a corresponding metal carbonyl Ito reduce the interfering effect of the metals during sintering.
  • any oxides present on the metal powder surface prior tocoating will not be reduced and will remain in the final product with detrimental results inregard to corrosion resistance, etc.
  • carbonyl nickel powders and carbonyl iron powders generally having particle sizes in the range of about 3 to about l0 microns, although other commercial types of iron and nickel powders may be used.
  • Certain powders eg., carbonyl iron powder and carbonyl nickel powder, containing carbon in amounts up to about 1% maybe employed and the carbon content of the powders is effective in contributing the required carbon content in the initial powder mixture.
  • Chromium-containing alloy powders eg., stainless steep powders, and other allow powders may be employed in the initial mixture.
  • the initial powder mixture contains at leas-t about 0.1% or about 0.15% by weight of carbon to effect reduction of chromium oxide but does not contain more-than about 0.8% by weight or carbon because residual carbon in the ride, although other salts which decompose at a temperawrought products would then be excessive in many instances.
  • the initial powder mixture con'- tains about 0.15% to about 0.25% by weight of carbon because such amounts are normally sufficient to reduce the chromium oxide and provide the desired final carbon content.
  • Carbon is included in the initial powder mixture in an amount sufficient to combine stoichiometrically with the oxygen present in the mixture as chromium oxide. Necessary carbon additions are most advantageously made by means of fine carbon powder, c g., carbon black, or graphite powder having a particle size of about 0.5 to about microns.
  • the amount of carbon in the initial mixture is generally about- 20% to about or 100% or more in excess of the aforesaid stoichiometric amount.
  • the other metal powders employed in the initial powder mixture have particle sizes of about 2 to about 50 microns. More advantageously, the particle size of the powders does not exceed about 40 microns in order to facilitate diffusion during sintering so as to yield the homogeneous consolidated metal article.
  • the initial powder mixture After the initial powder mixture has been thoroughly blended, it is pressed at ambient temperatures into a form such as a billet. Hydrostatic pressing is advantageously employed for this operation. Sufficient pressure is employed to provide a green strength rin-the pressed powder article of an order such as to permit handling of the pressed powder billet. Pressures rin the range of about 10,000 to about 50,000 pounds per square inch (p.s.i.), e.g., about 30,000 p.s.i., are sufficient. The green billet has a porosity of about 45% to about 25%. The green billet is then transferred to an atmosphere-controlled furnace.
  • the pressed powder billet is heated to the sintering temperature at a rapid rate while maintaining thereabout a dew point not exceeding about minus F.) atmosphere, temperatures of at least about 1900 F. are required. Heating in the temperature range about 2000 F. is conducted at a slow rate, e.g., approximately 50 F. per hour. At the completion of sin'tering, the sintered shape has a porosity of about 25% to about 15%.
  • the hot sintered billet may be taken directly to a hot working operation such as a hot rolling mill or may be hot extruded in a conventional extrusion press for the formation of fully dense mill forms, including rod, bar, plate, tube, etc.
  • Hot extrusion is the preferred method for consolidating sintered billets made of high chromium alloys such as an alloy containing 50% chromium, balance nickel.
  • the sintered shape may be cooled to a temperature below about 300 F. in a protective atmosphere.
  • heating of the billet up tothe sintering temperature e.g., up to temperatures in the range of about 1000 F. to about 1900 F., may be conducted in an essentially oxygen-free atmosphere such as 90% nitrogen- 10% hydrogen, argon, dry hydrogen, etc.
  • Sintering at temperatures of 1900 F. and above is conducted in dry hydrogen, dry'dissooiated ammonia or other atmosphere reducing to chromium oxide at the .sintering temperature.
  • Example l A billet containing about 76% nickel, about 16% chromium and about 7% iron was prepared by mixing carbonyl nickel powder having a particle size of about 5 microns, carbonyl iron powder having a particle size of about 5 microns, and electrolytic chromium powder containing about 0.7% oxygen and having a minus 325 mesh particle size together with about 0.1% ammonium chloride and suiiieient carbon powder to provide in the mixture about 0.18% carbon.
  • the billet was hydrostatically pressed at about 30,000 p.s.i. pressure.
  • a similar billet was prepared with the exception that no carbon addition was made thereto.
  • the second billet contained about 0.05% carbon. Each billet was 21/2 inches square and weighed 40 pounds.
  • the sintered products produced from the initial mixture containing 0.18% carbon were essentially free from oxide inclusions after the sintering treatment at 2000 F. and 2200" F. as reflected by the materially lower oxygen contents obtained therein.
  • Example II A 21/2 inch by 21/2 inch billet weighing 20 pounds and containing about 77% nickel, 16% chromium, 7% iron, 0.18% total carbon, and 0.05 ammonium chloride was pressed, sintered at 2300 F. for about 9 hours, with total time at temperature above 2000 F. being 14 hours, and hot worked to full density using the procedure and starting materials set forth lin Example I. The microsection of the hot worked material at the center of the wrought product showed no oxide inclusions and the oxygen content was about 0.016%. The procedure was repeated using similar initial mixtures containing 0.1% and 0.2% ammonium chloride, respectively, and identical results were obtained.
  • a 4 inch by 5 inch billet was prepared from an initial powder mixture containing about 0.1% ammonium chloride, about 0.18% carbon, about 76% nickel, about 16% chromium, and about 7% iron.
  • the mixture was hydrostatically pressed to size at about 10,000 p.s.i. and was rapidly heated to 2000 F. and sintered at 2250 F. for about l2 hours.
  • An atmosphere comprising 90% nitrogen and 10% hydrogen was employed during heating to 1150 F. at which point dry iiowing hydrogen was introduced and maintained as the atmosphere up to 2200 F.
  • About the last six hours of sinter-ing was conducted in a owing atmosphere generated from the dissociation of ammonia.
  • a sintered billet was hot worked to flat bar about 1/2 inch yby 3 inches.
  • the worked material contained about 0.001% oxygen and about 0.05% carbon.
  • the material was subjected to room temperatu-re and elevated temperature short-time tensile tests and to corrosion tests comprising immersion for 24 hours in a boiling solution of 65% nitric acid. The results of these tests are shown in the following Tables II and III. In Table III, comparison results obtained upon wrought metal of similar composition produced from au ingot prepared from molten metal are also given.
  • the corrosion rate upon the specimens was determined in terms of inches per month and the diagram shown in the accompanying FIGURE 1 was constructed on the basis of the data.
  • the data demonstrated that the breadth of the sensitization range for the wrought powder metallurgy product is substantially less than that' of a melted alloy product having the same nominal composition tested in wrought form and that the peak corrosion rate is substantially lower t-han that of the melted alloy product.
  • the wrought powder metallurgy product is of the order of 5 times to 500 times more resistant to corrosion in the severe boiling nitric acid test than is the corresponding melted product.
  • compositions which may be produced as consolidated wrought products in accordance with the method of the present invention include alloys containing 50% nickel and 50% chromium; 40% nickel and 601% chromium; 32% nickel, 20% chromium, balance iron; 80% nickel and 20% chromium; 42% nickel, 6% chromium, balance iron; 74% nickel, 16% chromium, 2% columbium, balance iron; ⁇ austenitic stainless steels such as the 18% chromium, 8% nickel grade; martensitic and ferritic stainless steels represented by the AISI Type 403 and Type 430 designations, respectively, etc.
  • Example II Another material prepared in accordance with the procedure of Example II except that neither .ammonium chloride nor carbon was added in the initial powder mixture was prepared in wrought form.
  • the microstructure of this material is shown in the accompanying FIGURE 4 and again undesirable oxide inclusions are clearly evident therein.
  • simultaneously processed material produced with both carbon and ammonium chloride in accordance with Example I had a yield strength (0.2% otset) of 49.7 k.s.i., a tensile strength of 97.6 k.s.i., an elongation of 47% and a reduction in area ot 67.7%.
  • FIGURE 2 The microstructure of this material is shown in the accompanying FIGURE 2 and it is signiicantly cleaner than those of FIGURES 3 and 4.
  • the traces of inclusion material in FIGURE 2 are well distributed and are not harmful.
  • billets having a cross-section of about four inches by live inches were prepared by the procedure of Example II with one of the billets being made from Ian initial mixture containing 0.10% by weight of ammonium chloride spacing agent and the other from a mixture containing no such spacing agent. In each case, the initial mixture contained about 0.18% carbon.
  • the billet made without the initial 'ammonium chloride addition contained about 0.03% oxygen and displayed many oxide inclusions in the microstructure while the forged billet made with the initial spacing -agent addition contained only about 0.005% oxygen and had a clean microstructure.
  • the forged material produced using the spacing agent had an elongation of 41% and a reduction in area of 66% whereas the forged material produced without the spacing .agent had an elongation of 33% and a reduction in area of 47%.
  • the spacing agent in the initial powder mixture which preferably is an ammonium halide, i.e., ammonium iiuoride, ammonium chloride, ammonium bromide or ammonium iodide, or ammonium carfbonate, is essential for purposes of the invention.
  • an ammonium halide i.e., ammonium iiuoride, ammonium chloride, ammonium bromide or ammonium iodide, or ammonium carfbonate
  • the process of the invention provides metallurgically clean chromium-containing alloy products from starting materials including oxide-contaminated chromium powder.
  • control ditliculties apparently have been experienced in insuring that each of the pressed compacts in the retort receives the same dosage of halide. Furthermore, carbon in the pressed compacts has been identied as a poison with respect to the achievement ofthe desired effects.
  • the process provided in accordance with the present invention is free of the serious commercial diiculties which have lbeen encountered with the so-called activated sintering process and may be carried out in conjunction with the treatment of large, heavy billets from powder compacts which may be converted to 4usual mill forms such as tubing, bar, rod, strip, wire, etc., with high metal recovery and with the potential of providing unusual properties in the products, particularly from the viewpoints of close control of composition, improved corrosion resistance, etc.
  • the process for producing wrought chromium-containing metal articles essentially devoid of chromium oxide inclusions which consists essentially of preparing an initial powder mixture contaminated with chromium oxide and consists essentially of, by weight, about 5% to about 60% of chromium, up to about 20% molybdenum, up to about 10% tungsten, up to Aabout 5% columbium, up to about 4% copper, at least 0.1% up to about 0.8% carbon, at least -about 0.01% to about 0.5% of a spacing agent, and the balance substantially an iron-group metal, pressing said mixture into a billet, heating said billet to sintering temperature under nonoxidizing conditions, sintering said billet at a temperature of at least about l900 F. in a flowing gas atmosphere reducing to chromium oxide to provide a sintered billet substantially devoid of chromium oxide inclusions and thereafter working said sintered billet to a consolidated alloy shape substantially devoid of chromium oxide inclusions.
  • the initial powder mixture consists essentially of, by weight, about 5% to about 60% chromium, and at least one metal powder from the group consisting of up to about nickel, up to ⁇ about 90% iron, and up to about 20% cobalt.
  • the spacing agent is lselected from the group consisting of ammonium halides and ammonium carbonate.
  • the initial 5 2,657,127 10/1953 Sindeband 75-224 X powder mixture consists essentially of, on the basis of 2,806,786 9/ 1957 Kelley 75-2215r X metal powder ingredients, about 6% to about 60% chroni- 2,827,407 3/ 1958 Carlson 75-224 X ium, at least about 8% and upto about 80% nickel, and 2,872,725 2/ 1961 Goliber 75-206 the balance essentially iron.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacturing & Machinery (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Powder Metallurgy (AREA)
US594012A 1966-11-14 1966-11-14 Powder metallurgical production of chromium-containing alloys Expired - Lifetime US3357826A (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
US594012A US3357826A (en) 1966-11-14 1966-11-14 Powder metallurgical production of chromium-containing alloys
GB50140/67A GB1141576A (en) 1966-11-14 1967-11-03 Production of chromium alloys
DE19671558719 DE1558719A1 (de) 1966-11-14 1967-11-11 Verfahren zum pulvermetallurgischen Herstellen chromhaltiger Legierungen
FR127967A FR1544390A (fr) 1966-11-14 1967-11-13 élaboration d'alliages de chrome
AT1018567A AT279191B (de) 1966-11-14 1967-11-13 Verfahren zum pulvermetallurgischen Herstellen chromhaltiger Legierungen
CH1587467A CH504534A (fr) 1966-11-14 1967-11-14 Procédé de fabrication d'alliages contenant du chrome
SE15590/67A SE324062B (fr) 1966-11-14 1967-11-14
BE706484D BE706484A (fr) 1966-11-14 1967-11-14

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AT (1) AT279191B (fr)
BE (1) BE706484A (fr)
CH (1) CH504534A (fr)
DE (1) DE1558719A1 (fr)
GB (1) GB1141576A (fr)
SE (1) SE324062B (fr)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3460940A (en) * 1967-03-09 1969-08-12 Charles Robert Talmage Method of producing wrought high purity steels by powder metallurgy
US3463679A (en) * 1967-07-24 1969-08-26 Nasa Process for producing dispersion strengthened nickel with aluminum
US3495958A (en) * 1969-03-06 1970-02-17 Charles Robert Talmage High purity steel by powder metallurgy
US4239557A (en) * 1978-01-11 1980-12-16 Gould Inc. Thermally stable sintered porous metal articles
US4372783A (en) * 1979-07-27 1983-02-08 Mitsubishi Denki Kabushiki Kaisha Electrical contact composition for a vacuum type circuit interrupter
US4419551A (en) * 1977-05-27 1983-12-06 Mitsubishi Denki Kabushiki Kaisha Vacuum circuit interrupter and method of producing the same
US4693863A (en) * 1986-04-09 1987-09-15 Carpenter Technology Corporation Process and apparatus to simultaneously consolidate and reduce metal powders
US4722826A (en) * 1986-09-15 1988-02-02 Inco Alloys International, Inc. Production of water atomized powder metallurgy products

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DK58196A (da) * 1996-05-15 1997-11-16 Man B & W Diesel Gmbh Ophæng i et forbrændingskammer i et forbrændingsanlæg

Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1988861A (en) * 1929-02-23 1935-01-22 Ig Farbenindustrie Ag Production of metallic plates suitable for use as accumulator electrodes
GB468518A (en) * 1935-01-22 1937-07-07 Accumulatoren Fabri Ag Method of producing porous metal bodies
US2122053A (en) * 1935-01-22 1938-06-28 Accumulatoren Fabrik Ag Process of manufacturing porous metallic bodies
US2397831A (en) * 1944-05-15 1946-04-02 Harry T Bellamy Production of molded metallic articles
US2441126A (en) * 1944-01-13 1948-05-11 Callite Tungsten Corp Oxidation resistant alloys
US2470790A (en) * 1945-04-24 1949-05-24 Westinghouse Electric Corp Manufacture of alloys
US2471630A (en) * 1944-01-13 1949-05-31 Callite Tungsten Corp Pressed and sintered oxidation resistant nickel alloys
US2656595A (en) * 1953-10-27 Chromium-alloyed corrosion-resist
US2657127A (en) * 1950-03-31 1953-10-27 American Electro Metal Corp Production of chromium-alloyed corrosion-resistant metal powders and related products
US2806786A (en) * 1954-05-14 1957-09-17 Gen Electric Method of making sintered electrical contact material
US2827407A (en) * 1954-06-15 1958-03-18 Federal Mogul Corp Method of producing powdered steel products
US2872725A (en) * 1954-05-27 1959-02-10 Gen Electric Chromium base refractory compositions
GB972686A (en) * 1960-04-08 1964-10-14 Commissariat Energie Atomique A process for producing a sintered metallic article

Patent Citations (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2656595A (en) * 1953-10-27 Chromium-alloyed corrosion-resist
US1988861A (en) * 1929-02-23 1935-01-22 Ig Farbenindustrie Ag Production of metallic plates suitable for use as accumulator electrodes
GB468518A (en) * 1935-01-22 1937-07-07 Accumulatoren Fabri Ag Method of producing porous metal bodies
US2122053A (en) * 1935-01-22 1938-06-28 Accumulatoren Fabrik Ag Process of manufacturing porous metallic bodies
US2471630A (en) * 1944-01-13 1949-05-31 Callite Tungsten Corp Pressed and sintered oxidation resistant nickel alloys
US2441126A (en) * 1944-01-13 1948-05-11 Callite Tungsten Corp Oxidation resistant alloys
US2397831A (en) * 1944-05-15 1946-04-02 Harry T Bellamy Production of molded metallic articles
US2470790A (en) * 1945-04-24 1949-05-24 Westinghouse Electric Corp Manufacture of alloys
US2657127A (en) * 1950-03-31 1953-10-27 American Electro Metal Corp Production of chromium-alloyed corrosion-resistant metal powders and related products
US2806786A (en) * 1954-05-14 1957-09-17 Gen Electric Method of making sintered electrical contact material
US2872725A (en) * 1954-05-27 1959-02-10 Gen Electric Chromium base refractory compositions
US2827407A (en) * 1954-06-15 1958-03-18 Federal Mogul Corp Method of producing powdered steel products
GB972686A (en) * 1960-04-08 1964-10-14 Commissariat Energie Atomique A process for producing a sintered metallic article

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3460940A (en) * 1967-03-09 1969-08-12 Charles Robert Talmage Method of producing wrought high purity steels by powder metallurgy
US3463679A (en) * 1967-07-24 1969-08-26 Nasa Process for producing dispersion strengthened nickel with aluminum
US3495958A (en) * 1969-03-06 1970-02-17 Charles Robert Talmage High purity steel by powder metallurgy
US4419551A (en) * 1977-05-27 1983-12-06 Mitsubishi Denki Kabushiki Kaisha Vacuum circuit interrupter and method of producing the same
US4239557A (en) * 1978-01-11 1980-12-16 Gould Inc. Thermally stable sintered porous metal articles
US4372783A (en) * 1979-07-27 1983-02-08 Mitsubishi Denki Kabushiki Kaisha Electrical contact composition for a vacuum type circuit interrupter
US4693863A (en) * 1986-04-09 1987-09-15 Carpenter Technology Corporation Process and apparatus to simultaneously consolidate and reduce metal powders
US4722826A (en) * 1986-09-15 1988-02-02 Inco Alloys International, Inc. Production of water atomized powder metallurgy products

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AT279191B (de) 1970-02-25
GB1141576A (en) 1969-01-29
BE706484A (fr) 1968-05-14
DE1558719A1 (de) 1970-04-23
SE324062B (fr) 1970-05-19
CH504534A (fr) 1971-03-15

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