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Fatigue crack resistant nickel base superalloys

Assignee: General Electric Co
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Filing: 1990-08-01
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Granted: 1992-07-14
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Expires: 2010-08-01
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Abstract

Abstract The present invention provides an alloy having improved crack growth inhibition and having high strength at high temperatures. The composition of the alloy is essentially as follows: -Concentration in weight % -Ingredient From To -Ni balance -Co 3 13 -Cr 10 16 -Mo 2.5 5.5 -Al 2.5 4.5 -Ti 1.5 3.5 -Ta 2 5 -Nb 2 5 -Zr 0 0.1 -C 0 0.1 -B 0.01 0.05 -W 0 1 -Re 0 3 -Y 0 0.2. -

Inventors

  • 👤 Michael F. Henry

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-09 04:52
CPC Classifications
C; C22; C22C; C22C19/00; C22C19/03; C22C19/05; C22C19/051; C22C19/056

Claims Analysis

Total Claims: 3
Claim 1
Independent Claim 78 words
As a composition of matter an alloy having a high strength and having a substantially lower crack propagation rate, said alloy consisting essentially of the following ingredients in the following proportions: ______________________________________ Concentration in Weight % Claimed Composition Ingredient From To ______________________________________ Ni balance Co 3 13 Cr 10 16 Mo 2.5 5.5 Al 2.5 4.5 Ti 1.5 3.5 Ta 2.0 5.0 Nb 2.0 5.0 Zr 0.00 0.10 C 0.0 0.10 B 0.01 0.05 W 0.0 1.0. ______________________________________
Claim 2
Dependent Claim 87 words
As a composition of matter an alloy having a high strength and having a substantially lower crack propagation rate, said alloy consisting essentially of the following ingredients in the following proportions: ______________________________________ Concentration in Weight % Claimed Composition Ingredient From To ______________________________________ Ni balance Co 3 13 Cr 10 16 Mo 2.5 5.5 Al 2.5 4.5 Ti 1.5 3.5 Ta 2.0 5.0 Nb 2.0 5.0 Re 0.0 3.0 Hf 0.0 0.5 Zr 0.00 0.10 C 0.0 0.10 B 0.01 0.05 W 0.0 1.0 Y 0.0 0.2 ______________________________________
Claim 3
Dependent Claim 63 words
As a composition of matter an alloy having a high strength and having a substantially lower crack propagation rate, said alloy consisting essentially of the following ingredients in the following proportions: ______________________________________ Concentration in Weight % Ingredient Claimed Composition ______________________________________ Ni balance Co 8 Cr 13 Mo 3.5 Al 3.5 Ti 2.5 Ta 3.5 Nb 3.5 Zr 0.06 C 0.05 B 0.03 ______________________________________

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1995-07-14 1996-01-13 1996-07-14 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1999-07-14 2000-01-13 2000-07-14 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2003-07-14 2004-01-13 2004-07-14 $7700.00 Window Closed / Lapsed

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