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US2987805A - Process for surface protection of parts subject to high thermal stress - Google Patents

Process for surface protection of parts subject to high thermal stress Download PDF

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Publication number
US2987805A
US2987805A US661276A US66127657A US2987805A US 2987805 A US2987805 A US 2987805A US 661276 A US661276 A US 661276A US 66127657 A US66127657 A US 66127657A US 2987805 A US2987805 A US 2987805A
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US
United States
Prior art keywords
thermal stress
aluminum
high thermal
surface protection
parts subject
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
US661276A
Inventor
Kubera Gerhard
Prasse Gisela
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.)
Continental Teves AG and Co oHG
Original Assignee
Alfred Teves GmbH
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
Application filed by Alfred Teves GmbH filed Critical Alfred Teves GmbH
Application granted granted Critical
Publication of US2987805A publication Critical patent/US2987805A/en
Anticipated expiration legal-status Critical
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
    • C23C26/00Coating not provided for in groups C23C2/00 - C23C24/00
    • 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
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49229Prime mover or fluid pump making
    • Y10T29/49298Poppet or I.C. engine valve or valve seat making
    • Y10T29/49307Composite or hollow valve stem or head making
    • 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
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/4998Combined manufacture including applying or shaping of fluent material
    • Y10T29/49982Coating

Definitions

  • the present invention relates to the surface protection of parts subject to high thermal stress and corrosion, such as valve cones of intake and exhaust valves of combustion engines, turbine blades of jet units, and similar parts exposed to high temperatures and the incidence of corrosion.
  • Aluminum coating is effected by dipping the parts into an aluminum melt or by spraying them with aluminum. Subsequent heat treatment in salt baths results in a diffusion of the aluminum to the marginal zone of the base material. An iron-aluminum alloy is formed thereby at the surface which has high corrosion resistance.
  • high thermal stress e.g. intake and exhaust valves of combustion engines, combustion chambers. turbine blades, and the like.
  • Patented June 13, 1961 Articles treated in this manner will have a much higher heat and corrosion resistance than those produced by conventional methods due to the contents in ceramic components forming part of the surface.
  • valve cone In the next operation the valve cone is heated to a temperature of 960 C. in an atmosphere of oxygen. This will cause a diffusion of the aluminum into the base metal to take place, while simultaneously oxidation at the surface will set in. This treatment is carried out over a period of 3 hours and results in the formation of A1 0 i.e. a highly heat resistant ceramic material. In a final step the articles are forged into final shape. This operation results in the secure union of the ceramic material with the alloy metal and in the formation of an ex cellent protective coating.
  • a process for eifecting surface protection of valve cones made of ferrous metals and subject to high thermal stress by applying to the surface of said valve cones a ceramic material, resistant to high temperatures, which comprises coating said cones with molten metallic aluminum, heating the cones thus coated at approximately 960 C. in an atmosphere of oxygen for approximately 3 hours to allow diffusion of the aluminum into the ferrous metal to occur, while oxidation takes place at the surface of the aluminum-coated cones with formation of highly heat-resistant aluminum oxide, then heating said cones to forging temperature and forging them into the final shape.

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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)
  • Coating By Spraying Or Casting (AREA)

Description

United States Patent 2,987,805 PROCESS FOR SURFACE PROTECTION OF PARTS SUBJECT TO HIGH THERMAL STRESS Gerhard Kubera and Gisela Prasse, Blnmberg, Baden,
Germany, assignors to Alfred Teves Maschinen- Armaturenfahrik KG., Frankfurt am Main, Germany No Drawing. Filed May 24, 1957, Ser. No. 661,276 Claims priority, application Germany May 26, 1956 1 Claim. (Cl. 29-156.7)
The present invention relates to the surface protection of parts subject to high thermal stress and corrosion, such as valve cones of intake and exhaust valves of combustion engines, turbine blades of jet units, and similar parts exposed to high temperatures and the incidence of corrosion.
It has been found that aluminum coatings are an effective protection against corrosion and scale formation. Thus, it became widely known to coat the exposed surfaces of intake and exhaust valve cones with aluminum in order to extend their useful life.
Aluminum coating is effected by dipping the parts into an aluminum melt or by spraying them with aluminum. Subsequent heat treatment in salt baths results in a diffusion of the aluminum to the marginal zone of the base material. An iron-aluminum alloy is formed thereby at the surface which has high corrosion resistance.
However, the known methods have certain disadvantages. Thus, during the diffusion-heating the accurately finished parts are somewhat distorted, and since in most cases an after-machining is not possible, a large amount of Waste products will result. The applicability of this method is restricted thereby to few cases only.
It is the object of the present invention to overcome the above mentioned shortcomings of known coating methods and to provide a process for surface treatment of parts subject to high thermal stress which is simple, dependable and permits to obtain the desired coated parts with a minimum quantity of waste to be discarded.
According to the invention this is accomplished by the following operational steps: Parts subject to high thermal stress, e.g. intake and exhaust valves of combustion engines, combustion chambers. turbine blades, and the like. are first preformed to a part somewhat thicker than the final shape and coated with aluminum in a manner known per se. Subsequently the parts are heated in an oxygen atmosphere to forging temperature or higher temperature so that a diffusion of aluminum will occur into the base metal as well as oxidation of aluminum at the surface, according to the equation 4Al+3O =2Al,O,. Thus, ceramic material is formed on the surface which, as generally known, is resistant to highest temperatures. After this procedure the parts are forged or pressed to final shape. By that operation, the highly heat-resistant oxides are forged into the base metal consisting of aluminumiron so that they cannot become detached later.
Patented June 13, 1961 Articles treated in this manner will have a much higher heat and corrosion resistance than those produced by conventional methods due to the contents in ceramic components forming part of the surface.
In the following, the method according to the invention will be described by way of example with reference to a valve cone, but it should be understood, that this is only given by way of illustration and not of limitation and that many changes in the details can be made without departing from the spirit of the invention.
Example A valve cone of an exhaust valve of a combustion engine made of known valve steel f.i. silcrom 1, is first extruded. Then the aluminum is sprayed on the head of the valve cone in a known method.
In the next operation the valve cone is heated to a temperature of 960 C. in an atmosphere of oxygen. This will cause a diffusion of the aluminum into the base metal to take place, while simultaneously oxidation at the surface will set in. This treatment is carried out over a period of 3 hours and results in the formation of A1 0 i.e. a highly heat resistant ceramic material. In a final step the articles are forged into final shape. This operation results in the secure union of the ceramic material with the alloy metal and in the formation of an ex cellent protective coating.
What we claim is:
A process for eifecting surface protection of valve cones made of ferrous metals and subject to high thermal stress, by applying to the surface of said valve cones a ceramic material, resistant to high temperatures, which comprises coating said cones with molten metallic aluminum, heating the cones thus coated at approximately 960 C. in an atmosphere of oxygen for approximately 3 hours to allow diffusion of the aluminum into the ferrous metal to occur, while oxidation takes place at the surface of the aluminum-coated cones with formation of highly heat-resistant aluminum oxide, then heating said cones to forging temperature and forging them into the final shape.
References Cited in the file of this patent UNITED STATES PATENTS 1,335,024 Peschko Mar. 30, 1920 1,409,017 Ortiz Mar. 7, 1922 1,823,869 Baur Sept. 15, 1931 1,866,145 Wilson July 5, 1932 2,167,701 Whitfield Aug. 1, 1939 2,303,869 Quinlan et al. Dec. 1, 1942 2,573,229 Stern Oct. 30, 1951 2,845,365 Harris July 29, 1958 FOREIGN PATENTS 731,281 Great Britain June 8, 1955
US661276A 1956-05-26 1957-05-24 Process for surface protection of parts subject to high thermal stress Expired - Lifetime US2987805A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2987805X 1956-05-26

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US2987805A true US2987805A (en) 1961-06-13

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3362057A (en) * 1964-06-13 1968-01-09 Teves Thompson & Co G M B H Method of making valve bodies
US3476614A (en) * 1965-06-29 1969-11-04 Euratom Ductility of dispersed phase alloys,particularly al-al2o3

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1335024A (en) * 1918-11-29 1920-03-30 Dentist S Supply Company Process for preventing distortion of precious metals at temperatures higher than their fusing-points and article produced thereby
US1409017A (en) * 1914-12-23 1922-03-07 Gen Electric Compound metal body and method of making the same
US1823869A (en) * 1926-09-11 1931-09-15 Baur Walter Coating of bodies with metal
US1866145A (en) * 1930-02-27 1932-07-05 Wilson Alfred Edgar Method of making composite tubular members
US2167701A (en) * 1936-09-21 1939-08-01 Reynolds Metals Co Method of producing aluminum treated articles of iron
US2303869A (en) * 1938-12-07 1942-12-01 Gen Electric Treatment of metals
US2573229A (en) * 1948-04-22 1951-10-30 American Electro Metal Corp Producing aluminum coated metal articles
GB731281A (en) * 1952-07-21 1955-06-08 Bristol Aeroplane Co Ltd Improvements in or relating to the hot working of ferrous metal articles
US2845365A (en) * 1953-09-15 1958-07-29 Harris Transducer Corp Aluminum iron alloy

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1409017A (en) * 1914-12-23 1922-03-07 Gen Electric Compound metal body and method of making the same
US1335024A (en) * 1918-11-29 1920-03-30 Dentist S Supply Company Process for preventing distortion of precious metals at temperatures higher than their fusing-points and article produced thereby
US1823869A (en) * 1926-09-11 1931-09-15 Baur Walter Coating of bodies with metal
US1866145A (en) * 1930-02-27 1932-07-05 Wilson Alfred Edgar Method of making composite tubular members
US2167701A (en) * 1936-09-21 1939-08-01 Reynolds Metals Co Method of producing aluminum treated articles of iron
US2303869A (en) * 1938-12-07 1942-12-01 Gen Electric Treatment of metals
US2573229A (en) * 1948-04-22 1951-10-30 American Electro Metal Corp Producing aluminum coated metal articles
GB731281A (en) * 1952-07-21 1955-06-08 Bristol Aeroplane Co Ltd Improvements in or relating to the hot working of ferrous metal articles
US2845365A (en) * 1953-09-15 1958-07-29 Harris Transducer Corp Aluminum iron alloy

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3362057A (en) * 1964-06-13 1968-01-09 Teves Thompson & Co G M B H Method of making valve bodies
US3476614A (en) * 1965-06-29 1969-11-04 Euratom Ductility of dispersed phase alloys,particularly al-al2o3

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