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FR1451347A - Alliages devant servir à hautes températures - Google Patents

Alliages devant servir à hautes températures

Info

Publication number
FR1451347A
FR1451347A FR22725A FR22725A FR1451347A FR 1451347 A FR1451347 A FR 1451347A FR 22725 A FR22725 A FR 22725A FR 22725 A FR22725 A FR 22725A FR 1451347 A FR1451347 A FR 1451347A
Authority
FR
France
Prior art keywords
alloys
high temperatures
temperatures
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
FR22725A
Other languages
English (en)
Inventor
James French Baldwin
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
Priority claimed from US381932A external-priority patent/US3310399A/en
Application filed filed Critical
Priority to FR22725A priority Critical patent/FR1451347A/fr
Application granted granted Critical
Publication of FR1451347A publication Critical patent/FR1451347A/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
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C19/00—Alloys based on nickel or cobalt

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
FR22725A 1964-07-10 1965-06-29 Alliages devant servir à hautes températures Expired FR1451347A (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR22725A FR1451347A (fr) 1964-07-10 1965-06-29 Alliages devant servir à hautes températures

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US381932A US3310399A (en) 1964-07-10 1964-07-10 Alloys for use at high temperatures
FR22725A FR1451347A (fr) 1964-07-10 1965-06-29 Alliages devant servir à hautes températures

Publications (1)

Publication Number Publication Date
FR1451347A true FR1451347A (fr) 1966-01-07

Family

ID=26164432

Family Applications (1)

Application Number Title Priority Date Filing Date
FR22725A Expired FR1451347A (fr) 1964-07-10 1965-06-29 Alliages devant servir à hautes températures

Country Status (1)

Country Link
FR (1) FR1451347A (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2392129A1 (fr) * 1977-05-25 1978-12-22 United Technologies Corp Articles en superalliage de nickel a structure monocristalline et procede de preparation
FR2444722A1 (fr) * 1978-12-18 1980-07-18 United Technologies Corp Article en superalliage a base de nickel a temperature de fusion superieure a 1 288 oc et procede de fabrication
CN115768911A (zh) * 2020-06-03 2023-03-07 联合发动机制造集团股份公司 耐热锻造镍基合金及其制品

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2392129A1 (fr) * 1977-05-25 1978-12-22 United Technologies Corp Articles en superalliage de nickel a structure monocristalline et procede de preparation
FR2444722A1 (fr) * 1978-12-18 1980-07-18 United Technologies Corp Article en superalliage a base de nickel a temperature de fusion superieure a 1 288 oc et procede de fabrication
CN115768911A (zh) * 2020-06-03 2023-03-07 联合发动机制造集团股份公司 耐热锻造镍基合金及其制品

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