FR2230747A1 - Heat resistant nickel alloy - contg. lanthanum for jet engine components - Google Patents
Heat resistant nickel alloy - contg. lanthanum for jet engine componentsInfo
- 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
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%
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.
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)
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)
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 |
-
1973
- 1973-05-25 FR FR7319141A patent/FR2230747A1/en active Granted
Patent Citations (2)
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)
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 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |