CA1117320A - Article en super-alliage mono-cristallin ayant subi un traitement thermique, et methode connexe - Google Patents

Article en super-alliage mono-cristallin ayant subi un traitement thermique, et methode connexe

Info

Publication number
CA1117320A
CA1117320A CA000301018A CA301018A CA1117320A CA 1117320 A CA1117320 A CA 1117320A CA 000301018 A CA000301018 A CA 000301018A CA 301018 A CA301018 A CA 301018A CA 1117320 A CA1117320 A CA 1117320A
Authority
CA
Canada
Prior art keywords
article
alloy
single crystal
titanium
aluminum
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
CA000301018A
Other languages
English (en)
Inventor
David N. Duhl
Walter E. Olson
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies 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
Application filed by United Technologies Corp filed Critical United Technologies Corp
Application granted granted Critical
Publication of CA1117320A publication Critical patent/CA1117320A/fr
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
    • C30—CRYSTAL GROWTH
    • C30B—SINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
    • C30B11/00—Single-crystal growth by normal freezing or freezing under temperature gradient, e.g. Bridgman-Stockbarger method
    • C—CHEMISTRY; METALLURGY
    • C30—CRYSTAL GROWTH
    • C30B—SINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
    • C30B29/00—Single crystals or homogeneous polycrystalline material with defined structure characterised by the material or by their shape
    • C30B29/10—Inorganic compounds or compositions
    • C30B29/52—Alloys

Landscapes

  • Chemical & Material Sciences (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Inorganic Chemistry (AREA)
  • Mechanical Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Heat Treatment Of Nonferrous Metals Or Alloys (AREA)
  • Inorganic Compounds Of Heavy Metals (AREA)
  • Manufacture And Refinement Of Metals (AREA)
  • Treatments For Attaching Organic Compounds To Fibrous Goods (AREA)
CA000301018A 1977-05-25 1978-04-12 Article en super-alliage mono-cristallin ayant subi un traitement thermique, et methode connexe Expired CA1117320A (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US80050577A 1977-05-25 1977-05-25
US800,505 1977-05-25

Publications (1)

Publication Number Publication Date
CA1117320A true CA1117320A (fr) 1982-02-02

Family

ID=25178568

Family Applications (1)

Application Number Title Priority Date Filing Date
CA000301018A Expired CA1117320A (fr) 1977-05-25 1978-04-12 Article en super-alliage mono-cristallin ayant subi un traitement thermique, et methode connexe

Country Status (12)

Country Link
JP (1) JPS53146223A (fr)
BE (1) BE866609A (fr)
BR (1) BR7803254A (fr)
CA (1) CA1117320A (fr)
CH (1) CH635368A5 (fr)
DE (1) DE2821524C2 (fr)
FR (1) FR2392129A1 (fr)
GB (1) GB1592237A (fr)
IL (1) IL54629A (fr)
IT (1) IT1096317B (fr)
NO (1) NO148523C (fr)
SE (1) SE444324B (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0052911B1 (fr) * 1980-11-24 1985-09-18 Cannon-Muskegon Corporation Alliage monocristallin (à grain unique)
FR2503188A1 (fr) * 1981-04-03 1982-10-08 Onera (Off Nat Aerospatiale) Superalliage monocristallin a matrice a matuice a base de nickel, procede d'amelioration de pieces en ce superalliage et pieces obtenues par ce procede
US5154884A (en) * 1981-10-02 1992-10-13 General Electric Company Single crystal nickel-base superalloy article and method for making
US4583608A (en) * 1983-06-06 1986-04-22 United Technologies Corporation Heat treatment of single crystals
US5100484A (en) * 1985-10-15 1992-03-31 General Electric Company Heat treatment for nickel-base superalloys
US6074602A (en) * 1985-10-15 2000-06-13 General Electric Company Property-balanced nickel-base superalloys for producing single crystal articles
CH675256A5 (fr) * 1988-03-02 1990-09-14 Asea Brown Boveri
US8852500B2 (en) 2006-03-20 2014-10-07 National Institute For Materials Science Ni-base superalloy, method for producing the same, and turbine blade or turbine vane components
US20120070303A1 (en) 2009-08-10 2012-03-22 Yasuhiro Aoki Ni-BASED SINGLE CRYSTAL SUPERALLOY AND TURBINE BLADE
CN115233074A (zh) * 2022-07-12 2022-10-25 北京科技大学 一种燃机动叶片用钴镍基高温合金及其制备方法

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1451347A (fr) * 1964-07-10 1966-01-07 Alliages devant servir à hautes températures
US3567526A (en) * 1968-05-01 1971-03-02 United Aircraft Corp Limitation of carbon in single crystal or columnar-grained nickel base superalloys
GB1260982A (en) * 1970-06-08 1972-01-19 Trw Inc Improvements in or relating to nickel base alloys
US3677835A (en) * 1970-10-16 1972-07-18 United Aircraft Corp Homogeneous nickel-base superalloy castings
GB1397066A (en) * 1971-06-19 1975-06-11 Rolls Royce High temperature corrosion resistant alloys
US3915761A (en) * 1971-09-15 1975-10-28 United Technologies Corp Unidirectionally solidified alloy articles
US3869284A (en) * 1973-04-02 1975-03-04 French Baldwin J High temperature alloys

Also Published As

Publication number Publication date
NO148523B (no) 1983-07-18
NO781787L (no) 1978-11-28
IL54629A0 (en) 1978-07-31
SE7805309L (sv) 1978-11-26
FR2392129A1 (fr) 1978-12-22
GB1592237A (en) 1981-07-01
IT1096317B (it) 1985-08-26
JPS6125773B2 (fr) 1986-06-17
CH635368A5 (en) 1983-03-31
IT7823726A0 (it) 1978-05-24
DE2821524A1 (de) 1978-12-07
SE444324B (sv) 1986-04-07
JPS53146223A (en) 1978-12-20
NO148523C (no) 1983-10-26
BE866609A (fr) 1978-09-01
BR7803254A (pt) 1979-02-06
IL54629A (en) 1981-09-13
FR2392129B1 (fr) 1984-12-28
DE2821524C2 (de) 1981-10-15

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