Methods of piercing and enlarging elongate metal members such as seamless tubes

• US 4,034,588 A
• Filed: 07/06/1976
• Issued: 07/12/1977
• Est. Priority Date: 05/11/1970
• Status: Expired due to Term

• Current Assignee: Columbiana Foundry Company
• Original Assignee: Columbiana Foundry Company
• Inventors: Williams, Robert C., Way, Lewis A.
• Primary Examiner(s): Combs, E. M.
• Application Number:
  US05/702,686
• Time in Patent Office: 371 Days
• Field of Search: 72/67, 72/97, 72/209, 72/368, 72/370, 75/122, 75/126, 75/128, 75/134, 75/170, 75/171, 148/32
• US Class Current: 72/209
• CPC Class Codes: B21B 19/04 Rolling basic material of solid, i.e. non-hollow, structure; Piercing , e.g. rotary piercing mills
• CPC Class Codes: B21B 25/00 Mandrels for metal tube rolling mills, e.g. mandrels of the types used in the methods covered by group B21B17/00; Accessories or auxiliary means therefor ; Construction of, or alloys for, mandrels or plugs

Abstract

A method is provided for piercing and enlarging metal members at high temperatures, particularly members containing slag inclusion, by the steps of urging said member, over a piercer or enlarger point by rolling whereby said point passes through and forms an axial opening in the ingot, said point being formed of an alloy comprising 0.015% to 2% carbon, about 5% to 65% cobalt, about 15% to 35% chromium and up to about 30% iron and amounts of boron, nickel, silicon molybdenum, vanadium, aluminum, tantalum, tungsten, titanium, copper and columbium for imparting the qualities generally associated therewith without detrimentally affecting the hot hardness and resistance to erosion of said alloy at said elevated temperature.

Claims

1. A method of piercing and enlarging elongated metal members such as seamless tube, particularly such members containing slag inclusions comprising the steps of urging said metal member at an elevated temperature above about 1750°

F. over one of a piercing and enlarging point by rollig whereby said point passes through and forms an axial opening in the metal member, said point being formed of an alloy consisting essentially of 0.015% to 2% carbon, about 5% to 65% cobalt, about 15% to 35% chromium, up to about 30% iron and amounts of boron, nickel, silicon, molybdenum, vanadium aluminum, tantalum, tungsten, titanium, copper and columbium for imparting the qualities generally associated therewith without detrimentally affecting the hot hardness and resistance to erosion of said alloy at said elevated temperature.

2. A method of piercing and enlarging metal members as claimed in claim 1 wherein the alloy consists essentially of about 0.015% to 2% carbon, about 5% to 65% cobalt, about 15% to 35% chromium, up to about 30% iron, about 2% to 20% nickel, about 1.5% to 6% molybdenum, about 0.003% to 0.01% boron, up to about 0.25% titanium, about 15% to 18% tungsten and up to about 1.5% silicon.

3. A method of piercing and enlarging metal members as claimed in claim 1 wherein the alloy consists essentially of about 0.015% to 2% carbon, about 5% to 65% cobalt, about 15% to 35% chromium, up to about 30% iron, about 2% to 20% nickel, about 1.5% to 6% molybdenum, about 0.003% to 0.01% boron, up to about 0.25% titanium and up to about 1.5% silicon.

4. A method of piercing and enlarging metal members as claimed in claim 1 wherein the alloy consists essentially of about 0.02% to 0.71% carbon, about 10.6% to 61.35% cobalt, about 18.8% to 27.5% chromium, up to about 2.8% iron, about 2.3% to about 16.9% nickel, up to about 5.9% molybdenum, up to about 0.01% boron, up to about 0.22% titanium and up to about 17.88% tungsten.

5. A method of piercing and enlarging metal members as claimed in claim 4 wherein the alloy contains about 1.8% to 5.9% molybdenum, about 0.0035% to bout 0.01% boron and about 15.05% to about 17.88% tungsten.