Alloy resistant to corrosion

• US 4,329,173 A
• Filed: 03/31/1980
• Issued: 05/11/1982
• Est. Priority Date: 03/31/1980
• Status: Expired due to Term

• Current Assignee: Carondelet Foundry Co. (Metaltek International Incorporated)
• Original Assignee: Carondelet Foundry Co. (Metaltek International Incorporated)
• Inventors: Culling, John H.
• Primary Examiner(s): Sheehan, John P.
• Application Number:
  US06/135,525
• Time in Patent Office: 771 Days
• Field of Search: 75/125, 75/128 A, 75/128 G, 75/128 W
• US Class Current: 420/38
• CPC Class Codes: C22C 38/58 with more than 1.5% by weight of manganese

Abstract

An air-meltable, castable, weldable, nonmagnetic alloy resistant to corrosion in sulfuric acid over a wide range of acid strengths. The alloy consists essentially of between about 18 and about 22% by weight nickel, between about 16.8 and 19.2% by weight chromium, between about 0.35 and about 1.95% by weight molybdenum, between about 2.5 and about 3.9% by weight copper, between about 3.2 and about 4.7% by weight manganese, between about 0.35% and 0.80% by weight niobium, up to about 0.7% by weight titanium, up to about 0.4% by weight tantalum, up to about 0.01% by weight boron, up to about 0.5% by weight cobalt, up to about 0.7% by weight silicon, up to about 0.08% by weight carbon, up to about 0.6% by weight of a rare earth component selected from the group consisting of cerium, lanthanum, and misch metal, up to about 0.15% by weight nitrogen, and between about 51% and about 58% by weight iron. The nickel content exceeds the chromium content by about 0.85% to about 5.2% by weight.

Claims

1. An air-meltable, castable, weldable, nonmagnetic alloy resistant to corrosion in sulfuric acid over a wide range of acid strengths, consisting essentially of between about 18 and about 22% by weight nickel, between about 16.8 and about 19.2% by weight chromium, between about 0.35 and about 1.95% by weight molybdenum, between about 2.5 and about 3.9% by weight copper, between about 3.2 and about 4.7% by weight manganese, between about 0.35 and about 0.80% by weight niobium, up to about 0.7% by weight titanium, up to about 0.4% by weight tantalum, up to about 0.01% by weight boron, up to about 0.5% by weight cobalt, up to about 0.7% by weight silicon, up to about 0.08% by weight carbon, up to about 0.6% by weight of a rare earth component selected from the group consisting of cerium, lanthanum and misch metal, up to about 0.15% by weight nitrogen, and between about 51 and about 58% by weight iron, and wherein the nickel content exceeds the chromium content by between about 0.85 and about 5.2% by weight (basis, the entire alloy).

2. An alloy as set forth in claim 1 wherein the nickel content exceeds the chromium content by between about 0.87 and about 4.74% by weight (basis, the entire alloy).

3. An alloy as set forth in claim 2 wherein the nickel content is between about 18.66% and about 21.58% by weight, the chromium contact is between about 16.84 and about 19.01% by weight, the molybdenum content is between about 0.52 and about 1.93% by weight, the copper content is between about 2.51 and about 3.24% by weight, the manganese content is between about 3.29 and about 4.54% by weight, the niobium content is between about 0.45 and about 0.68% by weight and the iron content is between about 51.05 and about 55.14% by weight.

4. An alloy as set forth in claim 1 wherein the nickel content is between about 18.66 and about 21.58% by weight, the chromium content is between about 16.84 and about 18.76% by weight, the molybdenum content is between about 0.52 and about 1.93% by weight, the copper content is between about 2.82 and about 3.18% by weight, the manganese content is between about 3.30 and about 3.70% by weight, the niobium content is between about 0.56 and about 0.68% by weight, the iron content is between about 51.05 and 55.13% by weight and the nickel content exceeds the chromium content by between about 1.82 and about 4.11% by weight (basis, the entire alloy).

5. An alloy as set forth in claim 1 wherein the nickel content is between about 18.6 and about 21.6% by weight, the chromium content is between about 17.20 and about 18.76% by weight, the molydenum content is between about 0.52 and about 1.93% by weight, the copper content is between about 2.82 and about 3.17% by weight, the manganese content is between about 3.30 and about 3.51% by weight, the niobium content is between about 0.56 and about 0.68% by weight, the silicon content is between about 0.3 and about 0.5% by weight, the carbon content is between about 0.03 and about 0.05% by weight, the iron content is between about 51.05 and about 55.13% by weight, and the nickel content exceeds the chromium content by between about 2.18 and about 4.11% by weight (basis, the entire alloy).

6. An alloy as set forth in claim 1 wherein the carbon content does not exceed approximately one-eighth of the niobium content.

7. An air-meltable, castable, weldable, nonmagnetic alloy resistant to corrosion in sulfuric acid over a wide range of acid strengths, comprising approximately 21.0% by weight nickel, approximately 17.5% by weight chromium, approximately 1.2% by weight molybdenum, approximately 3.1% by weight copper, approximately 3.7% by weight manganese, approximately 0.6% by weight niobium, approximately 0.3% by weight silicon, approximately 0.03% by weight carbon, and the balance essentially iron.