Heat Resisting Metals for Gas Turbine Parts (N-102) - Chromium- Base Alloys

Abstract

Results of a 42-month search for heat resistant metals for gas turbine blades which ended in the development of a new series of alloys of which the principal element of the series is chromium. The chromium rich portions of thirteen binary and nine ternary systems of chromium have been surveyed. Methods of melting, purifying, casting, and machining the alloys have been devised. Stress-rupture properties of certain of the chromium-based alloys are superior to those of all other materials known to have been tested.

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Document Details

Document Type
Technical Report
Publication Date
Nov 28, 1945
Accession Number
ADB808050

Entities

People

  • Alvin J. Herzig
  • Robert M. Parke

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms

DTIC Thesaurus Topics

  • Chemical Analysis
  • Chemistry
  • Chromium
  • Gas Turbines
  • Hardness
  • Manufacturing
  • Materials
  • Materials Laboratories
  • Materials Science
  • Metallurgy
  • Molybdenum
  • Physical Properties
  • Reduction Of Area
  • Solid Solutions
  • Tungsten Alloys
  • Turbine Blades
  • Turbine Components

Fields of Study

  • Materials science

Readers

  • Metallurgy
  • Software Engineering
  • Surface Engineering/Surface Coating Technology.