The Manufacturing of Aircraft-Quality Hydraulic Tubing with the Ti-3Al-8V-6Cr-4Mo-4Zr Alloy.

Abstract

Manufacturing procedures were developed for producing high-quality tubing of the metastable beta titanium alloy Ti-3Al-8V-6Cr-4Mo-4Zr. In excess of 500 feet of tubing was produced and evaluated in each of the three sizes at 0.75-, 0.54- and 0.375-inch diameter. The Ti-3Al-8V-6Cr-4Mo-4Zr alloy was found to be a highly producible tubing material with mechanical properties better than those of other titanium tubing alloys. The producibility of Ti-38-6-44 is enhanced most significantly by proper thermal treatments at initial and intermediate tube sizes, proper reduction sequences and precise tooling arrangements. Ti-38-6-44 was found to offer a wide range of strength levels, as tubing, with excellent ductility. Yield strengths were measured from 120 to more than 200 ksi. Aged to 180 ksi yield strength, Ti-38-6-44 has about 14 percent elongation and a strength-to-weight ratio of 1,035,000 inches which is considerably greater than that of other hydraulic tubing alloys. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1971
Accession Number
AD0727779

Entities

People

  • Howard B. Bomberger
  • John M. Olexa
  • Louis J. Bartlo

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Alloys
  • Diameters
  • Ductility
  • Elongation
  • Manufacturing
  • Materials
  • Mechanical Properties
  • Physical Properties
  • Sequences
  • Titanium
  • Titanium Alloys
  • Yield Strength

Fields of Study

  • Materials science

Readers

  • Metallurgy