Alloy resistant to seawater and corrosive process fluids

• US 4,818,483 A
• Filed: 12/29/1986
• Issued: 04/04/1989
• Est. Priority Date: 12/29/1986
• Status: Expired due to Fees

• Current Assignee: Carondelet Foundry Co. (Metaltek International Incorporated)
• Original Assignee: Carondelet Foundry Co. (Metaltek International Incorporated)
• Inventors: Culling, John H.
• Primary Examiner(s): Yee, Deborah
• Application Number:
  US06/947,427
• Time in Patent Office: 827 Days
• Field of Search: 420/45, 420/46, 420/47, 420/584, 420/582, 420/585, 420/586
• US Class Current: 420/45
• CPC Class Codes: C22C 38/58 with more than 1.5% by weight of manganese

Abstract

An air-meltable, workable, castable, weldable, machinable, nonmagnetic alloy resistant to seawater and corrosive process fluids of the type that may be circulated in seawater-cooled heat exchangers. The alloy consists essentially of between about 3% and about 8% by weight manganese, between about 12% and about 28% by weight nickel, between about 17.3% and about 19% by weight chromium, between about 0.68% and about 3.51% by weight copper, between about 0.07% and about 0.25% by weight nitrogen, between about 5.9% and about 8% by weight molybdenum, up to about 0.08% by weight carbon, up to about 1.5% by weight silicon, up to about 0.66% by weight niobium, up to about 1.32% by weight tantalum, up to about 1% by weight vanadium, up to about 1% by weight titanium, 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 5% by weight cobalt, and between about 30% and about 56% by weight iron. The titanium equals at least five times any carbon contant in excess of 0.03% by weight. The sum of the cobalt and nickel contents should not be at least about 17% but not exceed about 28% by weight. The sum of the niobium content and one-half the tantalum content should not exceed about 0.66% by weight.

Claims

1. An air meltable, workable, castable, weldable, machinable, nonmagnetic alloy having a single phase austenitic structure and being resistant to seawater and corrosive process fluids, the alloy consisting essentially of between about 3% and 8% by weight manganese, between about 12% and 28% by weight nickel, between about 17.3% and about 19% by weight chromium, between about 0.68% and about 3.51% by weight copper, between about 0.07% and about 0.25% by weight nitrogen, between about 5.9% and about 8% by weight molybdenum, up to about 0.08% by eight carbon, up to about 1.5% by weight silicon, up to about 0.66% by weight niobium, up to about 1.32% by weight tantalum, up to about 1% by weight vanadium, up to about 1% by weight PG,43 titanium, 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 5% by weight cobalt, and between about 30% and about 56% by weight iron, the titanium content being at least about five times any excess of carbon content above 0.03% by weight, the sum of the cobalt content and the nickel content being between about 17% and about 28% by weight, and the sum of the niobium content and one-half the tantalum content not exceeding about 0.66% by eight.

2. An alloy is set forth in claim 1 containing between about 18% and about 22% by weight nickel, between about 17.5% and about 18.5% by weight chromium, between about 7% and about 8% by weight molybdenum, between about 0.7% and about 3.0% by weight copper, between about 3% and about 5% by weight manganese, between about 0.20 and about 0.50% by weight silicon, between about 0.01% and about 0.03% by weight carbon, between about 0.15% and about 0.20% by weight nitrogen, and between about 42% and about 53% by weight iron.

3. An alloy as set forth in claim 2 containing approximately 20% by weight nickel, approximately 18% by weight chromium, approximately 7.3% by weight molybdenum, approximately 0.8% by weight copper, approximately 3.3% by weight manganese, approximately 0.25% by weight silicon, approximately 0.02% by weight carbon, approximately 0.20% by weight nitrogen, and the balance essentially iron.

4. An alloy as set forth in claim 1 wherein the molybdenum and chromium content satisfy the relationship ##EQU3## where [Mo]=weight % molybdenum and

[Cr]=weight % chromium.

5. An air meltable, workable, castable, weldable, machinable, nonmagnetic alloy resistant to sea water and corrosive process fluids, the alloy consisting essentially of between about 3% and about 8% by weight manganese, between about 12% and about 28% by weight nickel, between about 17.3% and about 19% by weight chromium, between about 0.68% and about 3.51% by weight copper, between about 0.07% and about 0.25% by weight nitrogen, between about 5.9% and about 8% by weight molybdenum, up to about 0.08% by weight carbon, up to about 1.5% by weight silicon, up to about 0.66% by weight niobium, up to about 1.32% by weight tantalum, up to about 1% by weight vanadium, up to about 1% by weight titanium, up to about 5% by weight cobalt, and between about 30% and about 56% by weight iron, the alloy being substantially free of lanthanum, the titanium content being at least about five times any excess of carbon content above 0.03% by weight, the sum of the cobalt content and the nickel content being between about 17% and about 28% by weight, and the sum of the niobium content and one half the tantalum content not exceeding about 0.66% by weight.