Study of the Creep Resistance in Ti-62222S Alloy

Abstract

Primary creep behavior was studied in Ti-6Al-2Sn-2Zr-2Cr-2Mo-0. 16Si (Ti-6-22-22S) alloy. Creep tests were performed at 480 degrees C under various stresses in the range of 150 to 500 MPa. The creep behavior was analyzed in terms of Larson-Miller time to reach 0.1 % creep strain. The results were compared with those in other Ti alloys as well as in Ti-6-22-22S reported by others. It was found that the a+B processed Ti-6-22-22S showed better creep resistance than the B processed alloy. It was also found that the a+B processed alloy showed much better creep resistance than Ti-6Al-4V (Ti-64) and is in general agreement with that of Ti-6Al-2Sn-4Zr-6Mo (Ti-6246). Therefore, the Ti-6-22-22S alloy is an attractive alloy not only for room-temperature applications but also for long term load-carrying applications near 400 degrees C and lower. The alloy may replace the existing Ti-6246 alloy and can be used for turbine engine parts at intermediate temperature in addition to conventional applications to air frame parts.

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Document Details

Document Type
Technical Report
Publication Date
Nov 30, 1998
Accession Number
ADA360744

Entities

People

  • Jun-ichi Koike

Organizations

  • Tohoku University

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Chemistry
  • Creep
  • Creep Tests
  • Electron Microscopes
  • Experimental Data
  • Fighter Aircraft
  • Heat Treatment
  • Materials
  • Materials Science
  • Mechanical Properties
  • Microstructure
  • Phase Diagrams
  • Resistance
  • Strain Rate
  • Tensile Properties
  • Tensile Strength
  • Turbines

Fields of Study

  • Materials science

Readers

  • Materials Science and Engineering.
  • Mechanical Engineering/Mechanics of Materials.
  • Surface Engineering/Surface Coating Technology.