Testing of Felt-Ceramic Materials for Combustor Applications.

Abstract

The feasibility of using composite felt-ceramic materials as combustor liners was experimentally studied. The material consists of a porous felt pad sandwiched between a layer of ceramic and one of solid metal. Flat, rectangular test panels, which encompassed several design variations of the basic composite material, were tested, two at a time, in a premixed gas turbine combustor as sections of the combustor wall. Tests were conducted at combustor inlet conditions of 0.5 MPa and 533K with a reference velocity of 25 m/s. The panels were subjected to a hot gas temperature of 2170K with 1% of the total airflow used to film cool the ceramic surface of the test panel. In general, thin ceramic layers yield low ceramic stress levels with high felt-ceramic interface temperatures. On the other hand, thick ceramic layers result in low felt-ceramic interface temperatures but high ceramic stress levels. Extensive thermal cycling appears to cause material degradation, but for a limited number of cycles, the survivability of felt-ceramic materials, even under extremely severe combustor operating conditions, was conclusively demonstrated.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1983
Accession Number
ADA130069

Entities

People

  • Gerald Roffe
  • R. S. Venkat Raman

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Flow
  • Ceramic Materials
  • Ceramic Matrix Composites
  • Combustion
  • Composite Materials
  • Failure Mode And Effect Analysis
  • Film Cooling
  • Films
  • Flow Rate
  • Fluid Flow
  • Heat Transfer
  • Material Degradation Processes
  • Materials
  • Surface Temperature
  • Temperature Gradients
  • Thermal Conductivity
  • Thermal Expansion

Readers

  • Optical Fiber Sensing and Electromagnetic Propagation.
  • Rocket Propulsion.
  • Thin Film Deposition Science.