Application of Rapidly Solidified Superalloys.

Abstract

This program is being conducted for the purpose of applying the principle of fast solidification to superalloy powders and subsequent development of stronger compositions for jet engine turbine airfoils. Centrifugal atomization and forced convective cooling of the material are bineg used for producing the fast cooled material. During this report period, high speed operation of the atomizer was achieved with resultant high yields of superalloy powder. Metallographic evaluation continued to show cooling rates in excess of 100,000 C/sec and also showed that the existence of a 'microcrystalline' structure in the rapidly quenched powder, as opposed t the classically dendritic form. This crystallite form appears as a more homogeneous structure with almost complete, if not total, secondary phase suppression within the crystallites. Four experimental lots of material were compacted and extruded for initiation of the heat treat and mechanical test program. The working operations proceeded without difficulty. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1976
Accession Number
ADA139198

Entities

People

  • A. R. Cox

Organizations

  • Pratt & Whitney

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Alloys
  • Chemistry
  • Cross Flow
  • Dendritic Structure
  • Equations
  • Flow
  • Heat Energy
  • Mass Flow
  • Materials
  • Materials Processing
  • Mechanical Properties
  • Metallurgy
  • Particle Size
  • Particles
  • Powder Metallurgy
  • Test And Evaluation

Fields of Study

  • Materials science

Readers

  • Internal Combustion Engine (ICE) Technology.
  • Powder metallurgy of Titanium alloys.
  • Systems Analysis and Design