Method for producing defect-free threads for large diameter beta solution treated and overaged titanium-alloy bolts

Patent metadata

Field	Value
Publication number	US-2016017470-A1
Application number	US-201514711291-A
Country	US
Kind code	A1
Filing date	May 13, 2015
Priority date	Jul 16, 2014
Publication date	Jan 21, 2016
Grant date	—

Abstract

A method for producing a Ti—6Al—4V article, includes providing a work piece of a Ti-6Al-4V alloy having a beta-transus temperature; subjecting the work piece to a beta solution heat treatment process in a furnace with a vacuum at a temperature above the beta transus; quenching the work piece in the furnace using high pressure inert gas following the subjecting of the work piece in the beta solution heat treatment process; and subjecting the work piece to an overage heat treatment process in the furnace with a vacuum to overage the work piece following the quenching of the work piece. The work piece can be a bolt blank that is further manufactured into a titanium bolt with pre-machined wave form threads and wave form rolling process utilized to manufacture threads into the bolt blank.

First claim

What is claimed is:

1 . A method for producing an alpha-beta titanium alloy article, comprising:
providing a work piece of an alpha-beta titanium alloy having a beta-transus temperature; subjecting the work piece to a beta solution heat treatment process in a furnace with a vacuum at a temperature above the beta transus; quenching the work piece in the furnace using high pressure inert gas following the subjecting of the work piece in the beta solution heat treatment process; and subjecting the work piece to an overage heat treatment process in the furnace with a vacuum to overage the work piece following the quenching of the work piece.

2 . The method of claim 2 , further comprising surface cleaning the work piece using one of abrasive media blasting, acid etching, or solvent emulsion cleaning prior to the beta solution heat treatment process.

3 . The method of any of the preceding claims, further comprising beta solution heat treating the work piece at a temperature in a range of about 50 degrees Fahrenheit to about 100 degrees Fahrenheit above the beta transus generally greater than 1875 degrees Fahrenheit for a time period between 30 and 60 minutes.

4 . The method of any of the preceding claims, further comprising quenching the work piece in one of a pressurized helium or argon inert gas that is configured to maintain a cooling rate of at least 280 degrees Fahrenheit per minute.

5 . The method of any of the preceding claims, further comprising quenching the work piece using the high pressure inert gas at a pressure in a range of about 200 kilopascals to about 400 kilopascals that is configured to lower a temperature of the work piece to below 600 degrees Fahrenheit.

6 . The method of any of the preceding claims, further comprising cooling the work piece in a high pressure inert gas following the subjecting of the overage heat treatment process.

7 . The method of claim 6 , further comprising cooling the work piece in one of a high pressure helium or argon inert gas that is configured to lower a temperature of the work piece to below 175 degrees Fahrenheit.

8 . The method of claim 6 or 7 , further comprising pressurizing the furnace at a pressure in a range of about 200 kilopascals to about 400 kilopascals during the cooling of the work piece.

9 . The method of any of the preceding claims, further comprising subjecting the work piece to a temperature in a range of about 1100 degrees Fahrenheit to about 1400 degrees Fahrenheit in a vacuum for about 2.5 hours to about 3 hours.

10 . The method of any of the preceding claims, wherein the work piece is configured to be processed during each of the beta solution heat treatment process, overage heat treatment process, and high pressure inert gas quenching without removal from the furnace.

11 . The method of any of the preceding claims, further comprising manufacturing threads into the work piece using a pre-machined wave formed thread pattern prior to thread rolling.

12 . The method of claim 11 , wherein the manufacturing of the threads further comprises creating the threads using one of a conventional thread rolling process or a wave form thread rolling process.

13 . The method of any of the preceding claims, where the alpha-beta titanium alloy is a Ti—6Al—4V alloy.

Assignees

• Sikorsky Aircraft Corp

Inventors

• Walker Todd David
• Lundeen Gregory William

Classifications

• C22F1/002

  by rapid cooling or quenching; cooling agents used therefor · CPC title

• C22F1/183 Primary

  of titanium or alloys based thereon · CPC title

• C22C14/00

  Alloys based on titanium · CPC title

• C22F1/02

  in inert or controlled atmosphere or vacuum (adjusting the composition of the atmosphere C21D1/76) · CPC title