Research and Development for Improved Toughness Aluminides

Abstract

The objective of this program was to study and identify the basic mechanisms which can improve the toughness of alloys based on the intermetallic compound Ti3A1. The improved properties offered by these alloys will increase their potential for application in rotating components and critical static parts in advanced aircraft engines. The program was conducted in two separate phases which addressed iterative alloy/processing studies as well as alloy scale up concerns. In the first phase of the program, the effects of solid solution alloying, tough second phase, and dispersoid additions were evaluated in parallel tasks. Subsequently, alloys were designed to make use of additive and/ or synergistic effects by combining the various alloying and processing concepts. In the second phase of the program, three of the more promising compositions were selected for scale up and further microstructural and property evaluations. Keywords: Titanium alloys, Alpha-2, Fracture toughness, Microstructure, processing properties.

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Document Details

Document Type
Technical Report
Publication Date
Jun 11, 1990
Accession Number
ADA226627

Entities

People

  • B. J. Marquardt
  • C. G. Rhodes
  • G. K. Scarr
  • H.L. Fraser
  • J. C. Chesnutt

Organizations

  • GE Aerospace

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Aircraft Engines
  • Aircrafts
  • Creep Tests
  • Crystal Structure
  • Electron Microscopes
  • Electron Microscopy
  • Fatigue Life
  • Materials
  • Materials Laboratories
  • Mechanical Properties
  • Mechanical Working
  • Solid Solutions
  • Tensile Properties
  • Tensile Strength
  • Tensile Testing
  • Test And Evaluation

Fields of Study

  • Materials science

Readers

  • Powder metallurgy of Titanium alloys.
  • Systems Analysis and Design