IP Library Granted Patent US 8,551,265
Granted Patent B2
US 8,551,265 · App. 12/036,880 · Granted Oct 8, 2013

Cobalt-base alloy with high heat resistance and high strength and process for producing the same

Inventors: Kiyohito Ishida (Sendai, JP); Ryosuke Kainuma (Natori, JP); Katunari Oikawa (Sendai, JP); Ikuo Ohnuma (Sendai, JP); Jun Sato (Sendai, JP)
Assignee: Japan Science and Technology Agency
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Quick Facts
Patent No.
US 8,551,265
App. No.
12/036,880
Granted
Oct 8, 2013
Kind
B2
Abstract

A Co-base alloy which has a basic composition including, in terms of mass proportion, 0.1%-10% Al, 3.0-45% W, and Co as the remainder and has an intermetallic compound of the Ll 2 type [Co 3 (Al,W)] dispersed and precipitated therein. Part of the Co may be replaced with Ni, Ir, Fe, Cr, Re, or Ru, while part of the Al and W may be replaced with Ni, Ti, Nb, Zr, V, Ta or Hf. The intermetallic compound [Co 3 (Al, W)] has a high melting point, and this compound and the matrix are mismatched little with respect to lattice constant. Thus, the cobalt-base alloy can have high-temperature strength equal to that of nickel-base alloys and excellent structure stability.

Claims (28)

1. A cobalt-base alloy with high heat resistance and high strength comprising: in a cobalt-base alloy comprising a composition of, in terms of mass proportion, 0.1 to 10% of Al, 3.0 to 45% of W, and Co as a remainder containing indispensable impurities, a metal texture in which a Ll 2 -type intermetallic compound (γ′ phase) of Co 3 (Al, W) by atom ratio is precipitated, the Ll 2 -type intermetallic compound is precipitated under conditions where the particle diameter is 10 nm to 1 μm and the precipitation amount is 40 to 85% by volume, and the mismatch of the lattice constant between the γ′ phase and matrix (y phase) is 0.5% or less.

2. A cobalt-base alloy with high heat resistance and high strength, produced by the steps of:

solution-treating the cobalt-base alloy with the composition according to claim 1 in the temperature range of 1100-1400° C. for 1-2 hours; and

performing aging treatment in the temperature range of 500-1100° C. for 1-168 hours.

3. The cobalt-base alloy with high heat resistance and high strength according to claim 1 , further comprising:

one or more components selected from the following

Group (I) in a total of 0.001 to 2.0% by mass, wherein

Group (I): 0.001 to 1% of B, 0.001 to 2.0% of C, 0.01 to 1.0% of Y, and 0.01 to 1.0% of La or misch metal.

4. A cobalt-base alloy with high heat resistance and high strength produced by the steps of:

solution-treating the cobalt-base alloy with the composition according to claim 3 in the temperature range of 1100-1400° C. for 1-2 hours; and

performing aging treatment in the temperature range of 500-1100° C. for 1-168 hours.

5. The cobalt-base alloy with high heat resistance and high strength according to claim 1 , further comprising:

one or more components selected from the following Group (II) in a total of 0.1 to 50%;

wherein an Ll 2 -type intermetallic compound precipitated is (Co,X) 3 (Al,W,Z) by atom ratio;

wherein, X is Ir, Fe, Cr, Re, and/or Ru, Z is Mo, Ti, Nb, Zr, V, Ta, and/or Hf, and nickel can be comprised in both X and Z; and

Group (II): 50% or less of Ni, 50% or less of Ir, 10% or less of Fe, 20% or less of Cr, 15% or less of Mo, 10% or less of Re, 10% or less of Ru, 10% or less of Ti, 20% or less of Nb, 10% or less of Zr, 10% or less of V, 20% or less of Ta, and 10% or less of Hf.

6. A cobalt-base alloy produced by the steps of:

solution-treating the cobalt-base alloy according to claim 5 in the temperature range of 1100 to 1400° C. for 1 to 2 hours; and

performing aging treatment in the temperature range of 800 to 1000° C. for 1 to 168 hours.

7. The cobalt-base alloy with high heat resistance and high strength according to claim 1 , further comprising:

one or more components selected from the following Group (I) in a total of 0.001 to 2.0%; and

one or more components selected from the following Group (II) in a total of 0.1 to 50%;

wherein the Ll 2 -type intermetallic compound precipitated is (Co,X) 3 (Al,W,Z) by atom ratio; wherein, X is Ir, Fe, Cr, Re, and/or Ru, Z is Mo, Ti, Nb, Zr, V, Ta, and/or Hf, and nickel can be comprised in both X and Z;

Group (I): 0.001 to 1% of B, 0.001 to 2.0% of C, 0.01 to 1.0% of Y, and 0.01 to 1.0% of La or misch metal; and

Group (II): 50% or less of Ni, 50% or less of Ir, 10% or less of Fe, 20% or less of Cr, 15% or less of Mo, 10% or less of Re, 10% or less of Ru, 10% or less of Ti, 20% or less of Nb, 10% or less of Zr, 10% or less of V, 20% or less of Ta, and 10% or less of Hf.

8. A cobalt-base alloy with high heat resistance and high strength produced by the steps of:

solution-treating the cobalt-base alloy according to claim 7 in the temperature range of 1100 to 1400° C. for 1 to 2 hours; and

performing aging treatment in the temperature range of 800 to 1000° C. for 1 to 168 hours.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 17, 2008
From: ISHIDA, KIYOHITO; KAINUMA, RYOSUKE; OIKAWA, KATUNARI; OHNUMA, IKUO; SATO, JUN
To: JAPAN SCIENCE AND TECHNOLOGY AGENCY
Reel/Frame 020819/0677 →
Priority Claims (1)
JP 2005-267964 · Sep 15, 2005 · national
Continuity (2)
Continuation PCTJP2006317939 · Sep 5, 2006
Related Publication 20080185078A1 · Aug 7, 2008