DE1783138B2 - - Google Patents

Info

Publication number
DE1783138B2
DE1783138B2 DE19651783138 DE1783138A DE1783138B2 DE 1783138 B2 DE1783138 B2 DE 1783138B2 DE 19651783138 DE19651783138 DE 19651783138 DE 1783138 A DE1783138 A DE 1783138A DE 1783138 B2 DE1783138 B2 DE 1783138B2
Authority
DE
Germany
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.)
Granted
Application number
DE19651783138
Other languages
German (de)
Other versions
DE1783138A1 (de
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 filed Critical
Publication of DE1783138A1 publication Critical patent/DE1783138A1/de
Publication of DE1783138B2 publication Critical patent/DE1783138B2/de
Granted legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/056Alloys 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%

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Heat Treatment Of Steel (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Powder Metallurgy (AREA)
DE19651783138 1964-07-10 1965-07-07 Nickellegierungen Granted DE1783138A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US381932A US3310399A (en) 1964-07-10 1964-07-10 Alloys for use at high temperatures

Publications (2)

Publication Number Publication Date
DE1783138A1 DE1783138A1 (de) 1972-06-08
DE1783138B2 true DE1783138B2 (US07223432-20070529-C00017.png) 1972-11-16

Family

ID=23506908

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19651783138 Granted DE1783138A1 (de) 1964-07-10 1965-07-07 Nickellegierungen

Country Status (8)

Country Link
US (1) US3310399A (US07223432-20070529-C00017.png)
BE (1) BE666656A (US07223432-20070529-C00017.png)
CH (1) CH452903A (US07223432-20070529-C00017.png)
DE (1) DE1783138A1 (US07223432-20070529-C00017.png)
ES (1) ES315234A1 (US07223432-20070529-C00017.png)
GB (1) GB1052561A (US07223432-20070529-C00017.png)
NL (1) NL6508887A (US07223432-20070529-C00017.png)
SE (2) SE373161B (US07223432-20070529-C00017.png)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3526499A (en) * 1967-08-22 1970-09-01 Trw Inc Nickel base alloy having improved stress rupture properties
US3617685A (en) * 1970-08-19 1971-11-02 Chromalloy American Corp Method of producing crack-free electron beam welds of jet engine components
US3869284A (en) * 1973-04-02 1975-03-04 French Baldwin J High temperature alloys
USRE28681E (en) * 1973-04-02 1976-01-13 High temperature alloys
US4082581A (en) * 1973-08-09 1978-04-04 Chrysler Corporation Nickel-base superalloy
USRE29920E (en) * 1975-07-29 1979-02-27 High temperature alloys
DE3109293C2 (de) * 1980-03-13 1985-08-01 Rolls-Royce Ltd., London Verwendung einer Nickellegierung für einkristalline Gußstücke
US4492672A (en) * 1982-04-19 1985-01-08 The United States Of America As Represented By The Secretary Of The Navy Enhanced microstructural stability of nickel alloys
US4814023A (en) * 1987-05-21 1989-03-21 General Electric Company High strength superalloy for high temperature applications
US5338379A (en) * 1989-04-10 1994-08-16 General Electric Company Tantalum-containing superalloys
AU624463B2 (en) * 1989-04-10 1992-06-11 General Electric Company Tantalum-containing superalloys
US5207846A (en) * 1989-04-10 1993-05-04 General Electric Company Tantalum-containing superalloys
US6632299B1 (en) 2000-09-15 2003-10-14 Cannon-Muskegon Corporation Nickel-base superalloy for high temperature, high strain application

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2920956A (en) * 1956-10-08 1960-01-12 Universal Cyclops Steel Corp Method of preparing high temperature alloys
US3085005A (en) * 1958-01-16 1963-04-09 Fansteel Metallurgical Corp Alloys
US3107167A (en) * 1961-04-07 1963-10-15 Special Metals Inc Hot workable nickel base alloy
GB979411A (en) * 1961-06-30 1965-01-01 Wiggin & Co Ltd Henry Improvements relating to the production of turbine blades and other hollow articles

Also Published As

Publication number Publication date
CH452903A (fr) 1968-03-15
NL6508887A (US07223432-20070529-C00017.png) 1966-01-11
GB1052561A (US07223432-20070529-C00017.png)
DE1483184A1 (de) 1969-02-13
DE1783138A1 (de) 1972-06-08
US3310399A (en) 1967-03-21
BE666656A (US07223432-20070529-C00017.png) 1965-11-03
ES315234A1 (es) 1965-10-16
DE1483184B2 (de) 1972-06-22
SE338868B (US07223432-20070529-C00017.png) 1971-09-20
SE373161B (US07223432-20070529-C00017.png) 1975-01-27

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Legal Events

Date Code Title Description
C3 Grant after two publication steps (3rd publication)
E77 Valid patent as to the heymanns-index 1977