Fatigue of Two Oxide/Oxide Ceramic Matrix Composites at 1200 deg C in Air and in Steam. Effect of Diamond Drilled Effusion Holes

Abstract

The tension-tension fatigue behavior of two oxide-oxide ceramic matrix composites (CMCs) was investigated at 1200 deg C in laboratory air and steam. Both composites consist of a porous oxide matrix reinforced with laminated, woven mullite/alumina (NextelTM720) xC;fibers. The fixC;rst composite had an alumina matrix, while the second had an alumina-mullite matrix. First, we assessed the effects of incorporating mullite into the matrix material on fatigue performance by studying the tension-tension fatigue behavior of alumina-mullite matrix CMC. Second, we evaluated the effects of effusion holes on the alumina matrix CMC's fatigue performance. Specimens containing an array of 17 effusion holes of 0.5-mm diameter were tested in tension-tension fatigue. The fatigue run-out was set to 100,000 cycles. All specimens that achieved fatigue run-out were subjected to tension tests to failure in order to measure the retained tensile properties. Fracture surfaces of the tested specimens were examined, damage and failure mechanisms are discussed.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Mar 25, 2021
Accession Number
AD1139773

Entities

People

  • Anthony R Cabri

Organizations

  • Air Force Institute of Technology

Tags

Communities of Interest

  • Advanced Electronics

DTIC Thesaurus Topics

  • Advanced Materials
  • Air Force
  • Ceramic Matrix Composites
  • Composite Materials
  • Engineering
  • High Temperature
  • Materials
  • Materials Laboratories
  • Materials Processing
  • Materials Science
  • Materials Testing
  • Mechanical Properties
  • Mechanics
  • Tensile Properties
  • Tensile Strength
  • Turbines
  • United States

Fields of Study

  • Materials science

Readers

  • Materials Science (Mechanical Engineering).
  • Reinforced Composite Materials