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GB1397066A - High temperature corrosion resistant alloys - Google Patents

High temperature corrosion resistant alloys

Info

Publication number
GB1397066A
GB1397066A GB2889371A GB2889371A GB1397066A GB 1397066 A GB1397066 A GB 1397066A GB 2889371 A GB2889371 A GB 2889371A GB 2889371 A GB2889371 A GB 2889371A GB 1397066 A GB1397066 A GB 1397066A
Authority
GB
United Kingdom
Prior art keywords
alloy
high temperature
corrosion resistant
temperature corrosion
coating
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
Application number
GB2889371A
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB2889371A priority Critical patent/GB1397066A/en
Priority to SE797372A priority patent/SE393401B/en
Priority to IT5098172A priority patent/IT958430B/en
Priority to FR7222006A priority patent/FR2143065B1/fr
Priority to DE19722229785 priority patent/DE2229785C2/en
Priority to US05/532,248 priority patent/US4013424A/en
Publication of GB1397066A publication Critical patent/GB1397066A/en
Expired legal-status Critical Current

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C19/00—Alloys based on nickel or cobalt
    • C22C19/03—Alloys based on nickel or cobalt based on nickel
    • C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/056—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 10% but less than 20%
    • C—CHEMISTRY; METALLURGY
    • C23—COATING 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
    • C23C—COATING 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
    • C23C30/00—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)

Abstract

1397066 Nickel alloys ROLLS-ROYCE (1971) Ltd 15 June 1972 [19 June 1971 6 July 1971] 28893/71 and 31517/71 Heading C7A A high temperature alloy has the following composition in per cent by weight Cr 3 - 15 Al 5 -30 Co 1 - 20 W 3 - 15 Ta 1À5 - 12 Yt 0.001-0À5 Ni the remainder In a modification the alloy contains 5-7% of Al, 3À5-13À5% W and also contains C À02-À2%, B 0À005-0À1% and one or more of Mo, Nb, Zr, Ti each up to 5%. For high temperature uses the alloy may have a diffused Al coating e.g. À001 to À005 in. thick. Alternatively a nickel-base alloy may be provided with a coating of an alloy within the above range and have Al diffused thereinto. The Al diffusion step can be omitted if the alloy coating itself is enriched in Al. Such an alloy may have the composition Ta 1À5-12, Yt À001-À5, Al 10-30, Cr 3-15, Ni remainder.
GB2889371A 1971-06-19 1971-06-19 High temperature corrosion resistant alloys Expired GB1397066A (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
GB2889371A GB1397066A (en) 1971-06-19 1971-06-19 High temperature corrosion resistant alloys
SE797372A SE393401B (en) 1971-06-19 1972-06-16 STORAGE RESISTANT TO OXIDATION AT HOGA TEMPERATURES FOR USE AS A PROTECTIVE LAYER
IT5098172A IT958430B (en) 1971-06-19 1972-06-17 IMPROVEMENT IN CORROSION RESISTANT ALLOYS
FR7222006A FR2143065B1 (en) 1971-06-19 1972-06-19
DE19722229785 DE2229785C2 (en) 1971-06-19 1972-06-19 Machine component made from a nickel-based alloy
US05/532,248 US4013424A (en) 1971-06-19 1974-12-12 Composite articles

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB2889371A GB1397066A (en) 1971-06-19 1971-06-19 High temperature corrosion resistant alloys
GB3151771 1971-07-06

Publications (1)

Publication Number Publication Date
GB1397066A true GB1397066A (en) 1975-06-11

Family

ID=26259621

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2889371A Expired GB1397066A (en) 1971-06-19 1971-06-19 High temperature corrosion resistant alloys

Country Status (5)

Country Link
DE (1) DE2229785C2 (en)
FR (1) FR2143065B1 (en)
GB (1) GB1397066A (en)
IT (1) IT958430B (en)
SE (1) SE393401B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4162918A (en) * 1977-11-02 1979-07-31 General Electric Company Rare earth metal doped directionally solidified eutectic alloy and superalloy materials
US4312682A (en) 1979-12-21 1982-01-26 Cabot Corporation Method of heat treating nickel-base alloys for use as ceramic kiln hardware and product
RU2153020C1 (en) * 1999-05-27 2000-07-20 Всероссийский научно-исследовательский институт авиационных материалов Heat-resistant nickel-based cast alloy
EP1365044A1 (en) * 2002-05-24 2003-11-26 Siemens Aktiengesellschaft MCrAl-coating

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA1117320A (en) * 1977-05-25 1982-02-02 David N. Duhl Heat treated superalloy single crystal article and process
BE880399A (en) * 1978-12-18 1980-04-01 United Technologies Corp NICKEL-BASED SUPERALLOY ARTICLE AND MANUFACTURING METHOD
US4313760A (en) * 1979-05-29 1982-02-02 Howmet Turbine Components Corporation Superalloy coating composition
US4764225A (en) * 1979-05-29 1988-08-16 Howmet Corporation Alloys for high temperature applications
US4447503A (en) * 1980-05-01 1984-05-08 Howmet Turbine Components Corporation Superalloy coating composition with high temperature oxidation resistance
DE3172291D1 (en) * 1980-11-24 1985-10-24 Cannon Muskegon Corp Single crystal (single grain) alloy
JPS57155338A (en) * 1981-03-23 1982-09-25 Hitachi Ltd Metallic body with alloy coating resistant to corrosion and thermal shock
US4451431A (en) * 1982-10-25 1984-05-29 Avco Corporation Molybdenum-containing high temperature coatings for nickel- and cobalt-based superalloys
EP0194391B1 (en) * 1985-03-13 1989-06-21 General Electric Company Yttrium and yttrium-silicon bearing nickel-base superalloys especially useful as compatible coatings for advanced superalloys
US5316866A (en) * 1991-09-09 1994-05-31 General Electric Company Strengthened protective coatings for superalloys

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1621224B1 (en) * 1967-01-31 1971-02-04 Deutsche Edelstahlwerke Ag Process for the diffusion of aluminum into the surfaces of objects made of high-temperature steels and alloys based on nickel or cobalt
US3542530A (en) * 1968-05-23 1970-11-24 United Aircraft Corp Nickel or cobalt base with a coating containing iron chromium and aluminum
US3528861A (en) * 1968-05-23 1970-09-15 United Aircraft Corp Method for coating the superalloys

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4162918A (en) * 1977-11-02 1979-07-31 General Electric Company Rare earth metal doped directionally solidified eutectic alloy and superalloy materials
US4312682A (en) 1979-12-21 1982-01-26 Cabot Corporation Method of heat treating nickel-base alloys for use as ceramic kiln hardware and product
RU2153020C1 (en) * 1999-05-27 2000-07-20 Всероссийский научно-исследовательский институт авиационных материалов Heat-resistant nickel-based cast alloy
EP1365044A1 (en) * 2002-05-24 2003-11-26 Siemens Aktiengesellschaft MCrAl-coating
WO2003100133A1 (en) * 2002-05-24 2003-12-04 Siemens Aktiengesellschaft Mcral layer
US7338719B2 (en) 2002-05-24 2008-03-04 Siemens Aktiengesellschaft MCrAl layer

Also Published As

Publication number Publication date
SE393401B (en) 1977-05-09
DE2229785A1 (en) 1972-12-21
IT958430B (en) 1973-10-20
FR2143065A1 (en) 1973-02-02
FR2143065B1 (en) 1973-07-13
DE2229785C2 (en) 1983-04-14

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee