US1718563A - Treatment of metals - Google Patents

Treatment of metals Download PDF

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Publication number
US1718563A
US1718563A US23970A US2397025A US1718563A US 1718563 A US1718563 A US 1718563A US 23970 A US23970 A US 23970A US 2397025 A US2397025 A US 2397025A US 1718563 A US1718563 A US 1718563A
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United States
Prior art keywords
chromium
silicon
treatment
powdered
temperature
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
US23970A
Inventor
Floyd C Kelley
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General Electric Co
Original Assignee
General Electric Co
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Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Priority to US23970A priority Critical patent/US1718563A/en
Application granted granted Critical
Publication of US1718563A publication Critical patent/US1718563A/en
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Expired - Lifetime legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C10/00Solid state diffusion of only metal elements or silicon into metallic material surfaces
    • C23C10/28Solid state diffusion of only metal elements or silicon into metallic material surfaces using solids, e.g. powders, pastes
    • C23C10/34Embedding in a powder mixture, i.e. pack cementation
    • C23C10/52Embedding in a powder mixture, i.e. pack cementation more than one element being diffused in one step
    • C23C10/54Diffusion of at least chromium
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00Stock material or miscellaneous articles
    • Y10S428/922Static electricity metal bleed-off metallic stock
    • Y10S428/9335Product by special process
    • Y10S428/938Vapor deposition or gas diffusion
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771Transition metal-base component
    • Y10T428/12806Refractory [Group IVB, VB, or VIB] metal-base component
    • Y10T428/12826Group VIB metal-base component
    • Y10T428/12847Cr-base component
    • Y10T428/12854Next to Co-, Fe-, or Ni-base component
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771Transition metal-base component
    • Y10T428/12861Group VIII or IB metal-base component
    • Y10T428/12951Fe-base component
    • Y10T428/12958Next to Fe-base component

Definitions

  • My invention relates to the treatment of metals to prevent harmful deterloratlon when heated to high temperatures 1n the presence of oxygen.
  • This surface alloy of chromium and the foundation metal is fundamentally a protection against corrosion, although it also resists oxidation at high temperatures to some extent.
  • a surface alloy is formed with I the metal of the article which has excellent oxidation resisting properties when heated to high temperatures.
  • Various proportions of silicon may be used.
  • the powdered chromium-and silicon are mixed with a powdered iiiert, refractory material, such as aluminum, oxid or magnesium oxid.
  • a powdered iiiert, refractory material such as aluminum, oxid or magnesium oxid. I have found that if 10 per cent by weight of powdered silicon be added to the regular chromium mixture of my aforesaid patentconsisting of equal-parts of powdered chr0- mium and refractory material, either aluminum oxid or magnesium oxid, an excellent heat resisting surface alloy may be formed.
  • the articles to be treated are packed in a receptacle in the chromium silicon treating mixture and then suitably heated, for example, by placing the receptacle with its contents in' a hydrogen furnace.
  • z 1 The duration of the heat treatment or firing to efi'ect'thefldesired penetration of the chromium and silicon with the" foundation metal Varies. with the temperature used; Temperatures offrom 1000 k to 1500 C. are satisfactory. While a te perature of approximately 12OQ C. is required to elfec t penetration of the powdered chromium alone, when thifsismall amount of powdered silicon is addedto' the treating mixture good penepreciably,
  • the surface alloy thus formed gives excellent protection againstgoxidation at surprisingly high temperatures.
  • Another piece of iron after being given a similar treatment was heated in the open air at a temperature of 900 C. for over 400 hpurs without showing any appreciable oxidation. This latter piece showed only an exceedingly small increase in Weight after being thus heated, which is afurther indication of the efficiency of this surface alloy as a protective coating.
  • the firing temperature is reduced apfor example, to approximately 900 C. but little, if any, further penetration of the chromium silicon mixture takes place, and the surface alloy whenv subjected to temperatures of 90OC. or less remains fixed.
  • the method ofprotecting metals against oxidation at high temperatures which consists in heating the metal under non-oxidizing conditions at a temperature of from 1000 C. to 1500 C. in contact with a mixture of powdered chromium and silicon.
  • the methodvof providing iron with a heat protecting surface alloy of iron, chromium and silicon which consists inheating the iron in hydrogen in contact with a mixture of powdered chromium, silicon and alu- 'minum oxid at a temperature of from 1000 10 C. to 1500 0.

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  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Powder Metallurgy (AREA)

Description

Patented June 25 1929.
UNITED STATES PATENT OFFICE.
FLOYD C. KELLEY, OF SCHENECTADY, NEW YORK, ASSIGNOR TO GENERAL ELECTRIC COMPANY, A CORPORATION OF NEW YORK.
TREATMENT OF METALS.
No Drawing.
My invention relates to the treatment of metals to prevent harmful deterloratlon when heated to high temperatures 1n the presence of oxygen.
metal andform therewith a surface alloy' which serves to protect the interior of the foundation metal. This surface alloy of chromium and the foundation metal is fundamentally a protection against corrosion, although it also resists oxidation at high temperatures to some extent.
I have discovered that if the article to be protected be suitably heated in surface con-.
tact With a mixture of powdered chromium and silicon, a surface alloy is formed with I the metal of the article which has excellent oxidation resisting properties when heated to high temperatures. Various proportions of silicon may be used. Preferably the powdered chromium-and silicon are mixed with a powdered iiiert, refractory material, such as aluminum, oxid or magnesium oxid. I have found that if 10 per cent by weight of powdered silicon be added to the regular chromium mixture of my aforesaid patentconsisting of equal-parts of powdered chr0- mium and refractory material, either aluminum oxid or magnesium oxid, an excellent heat resisting surface alloy may be formed. The articles to be treated are packed in a receptacle in the chromium silicon treating mixture and then suitably heated, for example, by placing the receptacle with its contents in' a hydrogen furnace. z 1 The duration of the heat treatment or firing to efi'ect'thefldesired penetration of the chromium and silicon with the" foundation metal Varies. with the temperature used; Temperatures offrom 1000 k to 1500 C. are satisfactory. While a te perature of approximately 12OQ C. is required to elfec t penetration of the powdered chromium alone, when thifsismall amount of powdered silicon is addedto' the treating mixture good penepreciably,
Letters Patent of the Application filed April 17, 1925. Serial No. 23,970.
tration is obtained at approximately 1000 C. Apparently the silicon alloys with the chromium and carries the chromium with it into the foundation metal at this lower temperature. When iron is bein treated, a very satisfactory surface alloy is formed by firing for six hours at a temperature of 1350 C. As with the process described in my aforesaid patent, the firing is carried out under non-oxidizing conditions, preferably in the presence of hydrogen.
The surface alloy thus formed gives excellent protection againstgoxidation at surprisingly high temperatures. A piece of iron after being given the treatment previously described, i. e. fired for six hours at a temperature of 1350 C., was heated at a temperature of 1100 C. in an open furnace for over 200 hours before any signs of breakdown in the protective coating Were perceived. Another piece of iron after being given a similar treatment was heated in the open air at a temperature of 900 C. for over 400 hpurs without showing any appreciable oxidation. This latter piece showed only an exceedingly small increase in Weight after being thus heated, which is afurther indication of the efficiency of this surface alloy as a protective coating. 1 I
f the firing temperature is reduced apfor example, to approximately 900 C. but little, if any, further penetration of the chromium silicon mixture takes place, and the surface alloy whenv subjected to temperatures of 90OC. or less remains fixed.
.In other words, there is little orno tend ency at this or lower temperatures for the chromium and silicon of the surface alloy to gradually diffuse into the interior of the foundation metal and thereby leave the surface unprotected. This is probably one explanation of the extraordinary heatresisting properties obtained by this treatment.
What I claim as new and desire to secure by United States, is, 1. The method of protecting metals against oxidation at: high emperatures which consists in heating the metal at a temperature of from 1000 C. to 150O C. in a hydrogen atmosphere in contact with a mixture of powdered chromium and silicon.
2. The method ofprotecting metals against oxidation at high temperatures which consists in heating the metal under non-oxidizing conditions at a temperature of from 1000 C. to 1500 C. in contact with a mixture of powdered chromium and silicon.
3. The methodvof providing iron with a heat protecting surface alloy of iron, chromium and silicon which consists inheating the iron in hydrogen in contact with a mixture of powdered chromium, silicon and alu- 'minum oxid at a temperature of from 1000 10 C. to 1500 0.
surface alloy which is resistant to oxidation at high temperatures, which consists in heat-' ing the iron in hydrogen in contact with powdered chromium and silicon at a temperature of approximately 1350 C.
In witness whereof, I have hereunto set my hand this 16th day of April, 1925.
FLOYD C. KELLEY.
US23970A 1925-04-17 1925-04-17 Treatment of metals Expired - Lifetime US1718563A (en)

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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2665474A (en) * 1950-03-18 1954-01-12 Fansteel Metallurgical Corp Highly refractory molybdenum alloys
US2665475A (en) * 1950-03-18 1954-01-12 Fansteel Metallurgical Corp Highly refractory body
US2683305A (en) * 1949-07-15 1954-07-13 Sintercast Corp Molybdenum coated article and method of making
US2736670A (en) * 1954-09-17 1956-02-28 Nat Glass Company Inc Method of surface treating and extruding die with chromium
US2763919A (en) * 1950-07-28 1956-09-25 Thompson Prod Inc Coated refractory body
US2763920A (en) * 1951-03-06 1956-09-25 Thompson Prod Inc Corrosion and impact-resistant article
US2771666A (en) * 1950-03-18 1956-11-27 Fansteel Metallurgical Corp Refractory bodies
US2823151A (en) * 1953-10-14 1958-02-11 Fansteel Metallurgical Corp Highly refractive molybdenum bodies
US2857297A (en) * 1951-10-25 1958-10-21 Nat Res Corp Process of coating molybdenum
US3037883A (en) * 1959-02-18 1962-06-05 Chromalloy Corp Diffusion coating of non-ferrous metals
JP2016084502A (en) * 2014-10-24 2016-05-19 新日鐵住金株式会社 Titanium member excellent in oxidation resistance, and production method of titanium member excellent in oxidation resistance

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2683305A (en) * 1949-07-15 1954-07-13 Sintercast Corp Molybdenum coated article and method of making
US2665474A (en) * 1950-03-18 1954-01-12 Fansteel Metallurgical Corp Highly refractory molybdenum alloys
US2665475A (en) * 1950-03-18 1954-01-12 Fansteel Metallurgical Corp Highly refractory body
US2771666A (en) * 1950-03-18 1956-11-27 Fansteel Metallurgical Corp Refractory bodies
US2763919A (en) * 1950-07-28 1956-09-25 Thompson Prod Inc Coated refractory body
US2763920A (en) * 1951-03-06 1956-09-25 Thompson Prod Inc Corrosion and impact-resistant article
US2857297A (en) * 1951-10-25 1958-10-21 Nat Res Corp Process of coating molybdenum
US2823151A (en) * 1953-10-14 1958-02-11 Fansteel Metallurgical Corp Highly refractive molybdenum bodies
US2736670A (en) * 1954-09-17 1956-02-28 Nat Glass Company Inc Method of surface treating and extruding die with chromium
US3037883A (en) * 1959-02-18 1962-06-05 Chromalloy Corp Diffusion coating of non-ferrous metals
JP2016084502A (en) * 2014-10-24 2016-05-19 新日鐵住金株式会社 Titanium member excellent in oxidation resistance, and production method of titanium member excellent in oxidation resistance

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