Titanium Alloy Ignition and Combustion.

Abstract

The objective of this program was to determine the relative ignition and combustibility characteristics of titanium alloys. Nine titanium alloys and two coatings were subjected to a laser ignition source at each of two conditions of temperature, pressure, and airstream velocity typical of gas turbine engine compressor environments. Three of the alloys did not burn and no significant difference could be established in the burning characteristics of six of the alloys. A chromium-molybdenum coating significantly reduced the magnitude of burn and an ion vapor deposited aluminum coating prevented ignition. The higher temperature environment was shown to produce a more severe burn. Comparison of one test run with results predicted by the analytical model currently under development showed good agreement. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Jan 15, 1978
Accession Number
ADA055443

Entities

People

  • B. A. Manty
  • V. G. Anderson

Organizations

  • Pratt & Whitney

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Burning Rate
  • Cameras
  • Combustion
  • Heat Transfer
  • High Temperature
  • Ignition
  • Laser Beams
  • Laser Ignition Systems
  • Low Temperature
  • Photographic Materials
  • Photographs
  • Photography
  • Recording Systems
  • Tape Recording
  • Test Equipment
  • Thermal Conductivity
  • Turbines

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Combustion science or combustion engineering.
  • Surface Engineering/Surface Coating Technology.

Technology Areas

  • Directed Energy