HIGH-TEMPERATURE AGING NICKEL- AND IRON-BASED ALLOYS

Abstract

Alloys of this kind began to be investigated in 1945-1946 in view of their applications to the development of aviation gas-turbine engineering. In this connection, the article surveys the principal results of the pertinent R+D work. Thus research into the effect of treatment with alloy elements on high- temperature alloys of the Kh20N80 and Kh15N35 types has made it possible to elucidate the effect of alloy elements displaying varying and variable solubility. High-temperature strength of these alloys is greatly affected by readily fusible impurities which enhance the adverse properties of grain boundaries. This can be offset and the grain boundaries can be toughened not only by using purer alloys but also by adding small amounts of chemically active alkali-earth, rare-earth metals, boron, etc. The vacuum arc and electroslag melting methods have recently been employed on an increasingly broader scale in the production of high-temperature alloys.

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Document Details

Document Type
Technical Report
Publication Date
Jul 10, 1969
Accession Number
AD0693458

Entities

People

  • M. V. Pridantsev

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • C4I

DTIC Thesaurus Topics

  • Alloys
  • Beyond Visual Range Missiles
  • Boundaries
  • Crystal Structure
  • Elements
  • Engineering
  • Gas Turbines
  • Grain Boundaries
  • Heat Resistant Alloys
  • High Temperature
  • Materials Science
  • Plastic Explosives
  • Rare Earth Elements

Fields of Study

  • Materials science

Readers

  • Metallurgy
  • Surface Engineering/Surface Coating Technology.
  • Systems Analysis and Design