Cobalt-base alloy having high strength and high toughness, production process of the same, and gas turbine nozzle

• US 4,789,412 A
• Filed: 03/19/1987
• Issued: 12/06/1988
• Est. Priority Date: 03/20/1986
• Status: Expired due to Term

• Current Assignee: Hitachi, Ltd.
• Original Assignee: Hitachi, Ltd.
• Inventors: Morikawa, Minoru, Nakamura, Shigeyoshi, Fukui, Yutaka, Kurosawa, Soichi, Iizuka, Nobuyuki, Kashimura, Tetsuo
• Primary Examiner(s): Dean, R.
• Application Number:
  US07/028,085
• Time in Patent Office: 628 Days
• Field of Search: 420/439, 148/408, 148/425, 148/158, 148/3
• US Class Current: 148/408
• CPC Class Codes: C22C 19/07 based on cobalt

Abstract

A cobalt-base alloy comprises 0.2-1 wt % C 0.4-2 wt % Si, 0.2-1.5 wt % Mn, 5-15 wt % Ni, 20-35 wt % Cr, 3-15 wt % W, 0.003-0.1 wt % Ni, 20-35 wt % Cr, 3-15 wt % W, 0.003-0.1 wt % B, 0.05-1 wt % Nb, 0.01-1 wt % Ta, 2 wt % or less Fe, 30 ppm or less oxygen, 100 ppm or less nitrogen, and the balance of 45 wt % or more Co, wherein the content of Si is larger than that of Mn. The alloy is in a form of casting and has a structure containing a eutectic carbide and a secondary carbide dispersed therein. The cast alloy is produced through solution treatment at 1,100°-1.200° C., and aging treatment at 950°-1,050° C., and cooling rate after the solution treatment and after the aging treatment is 150° to 300° C./h. A gas turbine nozzle is made of a casting of the above-mentioned alloy.

Claims

1. A cobalt-base alloy having a high strength and a high toughness in the form of a casting, said alloy consisting essentially of 0.2 to 1% by weight of carboxy 0.4 to 2% by weight of silicon, 0.2 to 1.5% by weight of manganese, 5 to 15% by weight of nickel, 20 to 35% by weight of chromium, 3 to 15% by weight of tungsten, 0.003 to 0.1% by weight of boron, 0.05 to 1% by weight of niobium, 0.01 to 1% by weight of titanium, 2% by weight or lower of iron, 30 ppm or lower of oxygen and 100 ppm or lower of nitrogen with the balance being 45% by weight or higher of cobalt, wherein the content of the silicon is larger than a value of a silicon content (Si) obained from a manganese content (Mn) by the following equation:

Si (wt %)=0.7×

Mn (wt %)+0.48, and said alloy has a structure containing a eutectic carbide and a secondary carbide dispersed therein.

2. A cobalt-base alloy having a high strength and a high toughness according to claim 1, wherein said alloy consists essentially of 0.35 to 0.45% by weight of carbon, 0.4 to 1.00% weight of silicon, 0.2 to 0.6% by weight of manganese, 9.5 to 11.5% by weight of nickel, 28.5 to 30.5% by weight of chromium, 6.5 to 7.5% by weight of tungsten, 0.005 to 0.015% by weight of boron, 0.1 to 0.3% by weight of titanium, 0.15 to 0.35% by weight of niobium, 1.5% by weight or lower of iron, 25 ppm or lower of oxygen and 30 ppm or lower of nitrogen with the balance being cobalt.

3. A cobalt-base alloy having a high strength and a high toughness in the form of a casting, said alloy consisting essentially of 0.2 to 1% by weight of carbon, 0.4 to 2% weight of silicon, 0.2 to 1.5% by weight of manganese, 5 to 15% by weight of nickel, 20 to 35 % by weight of chromium, 3 to 15% by weight of tungsten, 0.003 to 0.1% by weight of boron, 0.05 to 1% by weight of niobium, 0.01 to 1% by weight of titanium, 0.02 to 0.5% by weight of zirconium, 2% by weight or lower of iron, 30 ppm or lower of oxygen and 100 ppm or lower of nitrogen with the balance being 45% by weight or higher of cobalt, wherein the content of silicon is larger than a value of a silicon content (Si) obtained from a manganese content (Mn) by the following equation:

Si (wt %)=0.7×

Mn (wt %)+0.48 and said alloy has a structure containing a eutectic carbide and a secondary carbide dispersed therein.

4. A cobalt-base alloy having a high strength and a high toughness according to claim 3, wherein said alloy consists essentially of 0.35 to 0.45% by weight of carbon, 0.4 to 1.00% by weight of silicon, 0.2 to 0.6% by weight of manganese, 9.5 to 11.5% by weight of nickel, 28.5 to 30.5% by weight of chromium, 6.5 to 7.5% by weight of tungsten, 0.005 to 0.015% by weight of boron, 0.1 to 0.3% by weight of titanium, 0.15 to 0.35% by weight of niobium, 0.1 to 0.3% by weight of zirconium, 0.5% by weight or lower of iron, 25 ppm or lower of oxygen and 30 ppm or lower of nitrogen with the balance being cobalt.

5. A cobalt-base alloy having a high strength and a high toughness in the form of a casting, said alloy consisting esentially of 0.2 to 1% by weight of carbon, 0.4 to 2% by weight of silicon, 0.2 to 1.5% by weight of manganese, 5 to 15% by weight of nickel, 20 to 35 % by weight of chromium, 3 to 15% by weight of tungsten, 0.003 to 0.1% by weight of boron, 0.05 to 1% by weight of niobium, 0.01 to 1% by weight of titanium, 2% by weight or lower of iron, at least one member selected from the group consisting of 0.01 to 0.5% by weight of rare earth elements and 0.01 to 0.5% by weight of yttrium, 30 ppm or lower of oxygen and 100 ppm or lower of nitrogen with the balance being 45% by weight or higher of cobalt, wherein the content of silicon is larger than a vlaue of a silicon content (Si) obtained from a manganese content (Mn) by the following equation:

Si (wt %)=0.7×

Mn (wt %)+0.48, and said alloy has a structure containing a eutectic carbide and a secondary carbide dispersed therein.

6. A cobalt-base alloy having a high strength and a high toughness according to claim 5, wherein said alloy consists essentially of 0.35 to 0.45% by weight of carbon, 0.4 to 1.00% by weight of silicon, 0.2 to 0.6% by weight of manganese, 9.5 to 11.5% by weight of nickel, 28.5 to 30.5% by weight of chromium, 6.5 to 7.5% by weight of tungsten, 0.005 to 0.0I5% by weight of boron, 0.1 to 0.3% by weight of titanium, 0.15 to 0.35% by weight of niobium, 0.1 to 0.3% by weight of zirconium, 0.5% by weight or lower of iron, at least one member selected from the group consisting of 0.03 to 0.15% by weight of rare earth elements and 0.003 to 0.15% by weight of yttrium, 25 ppm or lower of oxygen and 30 ppm or lower of nitrogen with the balance being cobalt.

7. A cobalt-base alloy having a high strength and a high toughness in the form of a casting, said alloy consisting essentially of 0.2 to 1% by weight of carbon, 0.4 to 2% by weight of silicon, 0.2 to 1.5% by weight of manganese, 5 to 15% by weight of nickel, 20 to 35 % by weight of chromium, 3 to 15% by weight of tungsten, 0.003 to 0.1% by weight of boron, 0.05 to 1% by weight of niobium, 0.01 to 1% by weight of titanium, 0.02 to 0.5% by weight of zirconium, 2% by weight or lower of iron, at least one member selected from the group consisting of 0.01 to 0.5% by weight of rare earth elements and 0.01 to 0.5% by weight of yttrium, 30 ppm or lower of oxygen and 100 ppm or lower of nitrogen with the balance being 45% by weight or higher of cobalt, wherein the content of the silicon is larger than a value of a silicon content (Si) obtained from a manganese content (Mn) by the following equation:

(Si (wt %)=0.7×

Mn (wt %)+0.48, and said alloy has a structure containing a eutectic carbide and a secondary carbide dispersed therein.

8. A cobalt-base alloy having a high strength and a high toughness according to claim 7, wherein said alloy consists essentially of 0.35 to 0.45% by weight of carbon, 0.4 to 1.00% by weight of silicon, 0.2 to 0.6% by weight of manganese. 9.5 to 11.5% by weight of nickel, 28.5 to 30.5% by weight of chromium, 6.5 to 7.5% by weight of tungsten, 0.005 to 0.015% by weight of boron, 0.1 to 0.3% by weight of titanium, 0.15 to 0.35% by weight of niobium, 0.1 to 0.3% by weight of ziroonium, 0.5% by weight or lower of iron, at least one member selected from the group consisting of 0.03 to 0.15% by weight of rare earth elements and 0.003 to 0.15% by weight of yttrium, 25 ppm or lower of oxygen and 30 ppm or lower of nitrogen with the balance being cobalt.

9. A process for producing a cobalt-base alloy having a high strength and a high toughness in the form of a casting, said alloy consisting esentially of 0.2 to 1% by weight of carbon, 0.4 to 2% by weight of silicon, 0.2 to 1.5% by weight of manganese, 5 to 15% by weight of nickel, 20 to 35% by weight of chromium, 3 to 15% by weight of tungsten, 0.003 to 0.1% by weight of boron, 0.05 to 1% by weight of niobium, 0.01 to 1% by weight of titanium, 0.02 to 0.5% by weight of zirconium, 2% by weight or less of iron, 30 ppm or lower of oxygen and 100 ppm or less of nitrogen with the balance being 45% by weight or higher of cobalt, wherein the content of the silicon is larger than a value of a silicon content (Si) obtained from a manganese content (Mn) by the following equation:

Si (wt %)=0.7×

Mn (wt %)+0.48, and said alloy has a structure containing a eutectic carbide and a secondary carbide dispersed therein, said process comprising the steps of;

producing a casting through vacuum melting of said alloy;

heating said casting to a temperature of 1,100°

to 1,200°

C. and keeping said casting at said temeperature thereby efecting solution treatment;

cooling said casting from said temperature of solution treatment to an aging temperature of 950°

to 1,050°

C. through furnace cooling or air cooling; and

keeping said casting at said aging temperature thereby effecting aging treatment;

wherein said casting is cooled at a cooling rate of 150°

to 300°

C./h both after said solution treatment and after said aging treatment.

10. A nozzle for a gas turbine, which nozzle comprises nozzle segments each having thin wall portions forming a hollow portion therein, and upper and lower shrouds provided at both ends of said nozzle segments so as to arrange said nozzle segments in a direction and at a distance therebetween, said nozzle segments each having cooling air holes passing through said thin wall portions from said hollow portion into the outside thereof, and which nozzle is made of a casting, said alloy consisting esentially of:

0.2 to 1% by weight of carbon, 0.4 to 2% by weight of silicon, 0.2 to 1.5% by weight of manganese, 5 to 15% by weight of nickel, 20 to 35% by weight of chromium, 3 to 15% by weight of tungsten, 0.003 to 0.1% by weight of boron, 0.05 to 1% by weight of niobium, 0.01 to 1% by weight of titanium, 2% by weight or less of iron, 30 ppm or less of oxygen and 100 ppm or less of nitrogen with the balance being 45% by weight or more of cobalt, wherein the content of silicon is larger than a value of a silicon content (Si) obtained from a manganese content (Mn) by the following equation;

Si (wt %)=0.7×

Mn (wt %)+0.48, said casting having a structure containing a eutectic carbide and a secondary carbide dispersed therein.

11. A nozzle for a gas turbine, which nozzle comprises nozzle segments each having thin wall portions forming a hollow portion therein, and upper and lower shrouds provided at both ends of said nozzle segments so as to arrange said nozzle segments in a direction and at a distance therebetween, said nozzle segments each having cooling air holes passing through said thin wall portions from said hollow portion into the outside thereof, and which nozzle is made of a casting, said alloy consisting essentially of:

0.2 to 1% by weight of cargbon, 0.4 to 2% by weight of silicon, 0.2 to 1.5% by weight of manganese, 5 to 15% by weight of nickel, 20 to 35% by weight of chromium, 3 to 15% by weight of tungsten, 0.003 to 0.1% by weight of boron, 0.05 to 1% by weight of niobium, 0.01 to 1% by weight of titanium, 2% by weight or less of iron, 30 ppm or less of oxygen and 100 ppm or less of nitrogen with the balance being 45% by weight or more of cobalt, at least one element selected from the group consisting of 0.02 to 0.5 wt % of Zr, 0.01 to 0.5 wt % of rare earth metal and 0.01 to 0.5 wt % of Y, wherein the content of silicon is larger than a value of a silicon content (Si) obtained from a manganese content (Mn) by the following equation;

Si (wt %)=0.7×

Mn (wt %)+0.48, said casting having a structure containing a eutectic carbide and a secondary carbide dispersed therein.