An Investigation of the Gamma Phase of the Titanium-Aluminum Binary Alloy with Zirconium Additions

Abstract

The titanium-aluminum equiatomic alloy has qualities of excellent corrosion resistance, good strength to weight ratio, and good hot hardness. These qualities would make this alloy a desirable structural material were it not for an inherent brittleness and lack of ductility. The brittleness is attributed to an ordered-face-centered-tetragonal cell with a c/a ratio of 1.020. Several attempts have been made to reduce the c/a ratio to unity through ternary additions. A reduction of this ratio to 1.006 has been reported with zirconium as the ternary addition; however, this value was attained outside of the gamma phase. During this investigation the limit of solubility of zirconium in the gamma phase at 2325F was determined to be slightly less than 10a/o at 55a/o aluminum and slightly more than 10a/o at 60a/o aluminum. The c/a ratio varied with composition from 1.016 to 1.030.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1962
Accession Number
AD0610235

Entities

People

  • Duane H. Troup

Organizations

  • Air Force Institute of Technology

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Active Duty
  • Air Force
  • Atmospheres
  • Binary Alloys
  • Chemical Analysis
  • Corrosion Resistance
  • Crystal Structure
  • Diffraction
  • Elements
  • Flight Training
  • Heat Treatment
  • Materials
  • Measurement
  • Oxidation Resistance
  • Resistance
  • X Rays
  • X-Ray Diffraction

Readers

  • Powder metallurgy of Titanium alloys.