FR2230747A1 - Heat resistant nickel alloy - contg. lanthanum for jet engine components - Google Patents

Heat resistant nickel alloy - contg. lanthanum for jet engine components

Info

Publication number
FR2230747A1
FR2230747A1 FR7319141A FR7319141A FR2230747A1 FR 2230747 A1 FR2230747 A1 FR 2230747A1 FR 7319141 A FR7319141 A FR 7319141A FR 7319141 A FR7319141 A FR 7319141A FR 2230747 A1 FR2230747 A1 FR 2230747A1
Authority
FR
France
Prior art keywords
contg
lanthanum
heat resistant
nickel alloy
jet engine
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.)
Granted
Application number
FR7319141A
Other languages
French (fr)
Other versions
FR2230747B1 (en
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.)
TEREKHOV KUZMA
Original Assignee
TEREKHOV KUZMA
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 TEREKHOV KUZMA filed Critical TEREKHOV KUZMA
Priority to FR7319141A priority Critical patent/FR2230747A1/en
Publication of FR2230747A1 publication Critical patent/FR2230747A1/en
Application granted granted Critical
Publication of FR2230747B1 publication Critical patent/FR2230747B1/fr
Granted 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%

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Powder Metallurgy (AREA)

Abstract

The alloy has the compn. (wt%) 0.04-0.08C, 13-16Cr, 2.3-3.0Ti, 1.8-3.0Al, 2.2-6.0Nb, 6-12Co, 4-8Mo, 0.001-0.1La, 0.101-0.01B, 0.001-0.03Ce, balance Ni. The alloy is composed of a solid soln. of the main alloying elements Al, Ti, Nb which are present in greater quantities than in known heat-resisting ni alloys, and which produce a high fatigue strength and good ductility. The thermal stability is increased by higher contents of Mo and Nb. La and Ce give a grain refinement.
FR7319141A 1973-05-25 1973-05-25 Heat resistant nickel alloy - contg. lanthanum for jet engine components Granted FR2230747A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7319141A FR2230747A1 (en) 1973-05-25 1973-05-25 Heat resistant nickel alloy - contg. lanthanum for jet engine components

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7319141A FR2230747A1 (en) 1973-05-25 1973-05-25 Heat resistant nickel alloy - contg. lanthanum for jet engine components

Publications (2)

Publication Number Publication Date
FR2230747A1 true FR2230747A1 (en) 1974-12-20
FR2230747B1 FR2230747B1 (en) 1976-06-11

Family

ID=9120022

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7319141A Granted FR2230747A1 (en) 1973-05-25 1973-05-25 Heat resistant nickel alloy - contg. lanthanum for jet engine components

Country Status (1)

Country Link
FR (1) FR2230747A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2555205A1 (en) * 1983-11-22 1985-05-24 Metalimphy Nickel-based alloys for the metallurgy of powders intended for gas turbine discs

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1036148A (en) * 1963-09-03 1966-07-13 Birmingham Small Arms Co Ltd Improvements in or relating to alloys
FR2153962A5 (en) * 1971-09-13 1973-05-04 Cabot Corp

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1036148A (en) * 1963-09-03 1966-07-13 Birmingham Small Arms Co Ltd Improvements in or relating to alloys
FR2153962A5 (en) * 1971-09-13 1973-05-04 Cabot Corp

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2555205A1 (en) * 1983-11-22 1985-05-24 Metalimphy Nickel-based alloys for the metallurgy of powders intended for gas turbine discs

Also Published As

Publication number Publication date
FR2230747B1 (en) 1976-06-11

Similar Documents

Publication Publication Date Title
GB2134832A (en) Method of etablishing a bond between titanium and an iron-nickel alloy
US3782925A (en) Ferritic heat-resistant steel
US5755897A (en) Forgeable nickel alloy
ES410675A1 (en) Process of producing nickel chromium alloy products
GB1492262A (en) Titanium base alloy
GB1408372A (en) Nickel base alloys
JPS6179742A (en) Heat resistant alloy
FR2230747A1 (en) Heat resistant nickel alloy - contg. lanthanum for jet engine components
JPS6253583B2 (en)
JPS629659B2 (en)
GB1167067A (en) Improvements in and relating to Coated Nickel Base Engine Alloys and Methods of Producing Same.
SE7614132L (en) NICR ALLOY AND MADE OF WELDING ADDITIVES THEREOF
JPS5582738A (en) Nickel alloy
JP3279949B2 (en) Precipitation strengthened superalloy
SU1511288A1 (en) Refractory intermetallide-base alloy
JPS643944B2 (en)
GB1302293A (en)
US3001870A (en) Niobium-titanium refractory alloy
Zimina Niobium in heat-resistant steels and alloys(Weldability, corrosion resistance and heat resistance increase in Nb alloyed steels, noting aging temperature effects and microstructure)
US2822265A (en) Forgeable high strength austenitic alloy with molybdenum, tantalum, columbium-tantalum, and nitrogen additions
Burova et al. Structural Features of Nickel Alloys, Alloyed with Tantalum
US2698786A (en) Oxidation resistant refractory alloy
JPS62156095A (en) Ni-base high toughness heat resisting alloy for hard facing
GB1344858A (en) Heat resistant alloys
SU274924A1 (en) Nickel-base alloy

Legal Events

Date Code Title Description
ST Notification of lapse