Intermediate temperature degradation of a SiC/BN/SiC (MI) composite with holes at 500–900°C in steam

Author:

Ostdiek Gary12ORCID,Jefferson George3,Przybyla Craig3,Pierce Jennifer4,Celli Dino1,Kerans Ronald5ORCID

Affiliation:

1. Air Force Research Laboratory, Aerospace Systems Directorate Wright‐Patterson AFB Dayton Ohio USA

2. University of Dayton Chemical and Materials Engineering Department Dayton Ohio USA

3. Air Force Research Laboratory, Materials and Manufacturing Directorate Wright‐Patterson AFB Dayton Ohio USA

4. University of Dayton Research Institute Advanced Composites Division Dayton Ohio USA

5. Air Force Research Laboratory (retired) Wright‐Patterson AFB Dayton Ohio USA

Abstract

AbstractSpecimens from a Hi‐Nicalon Type S/BN/SiC (MI) ceramic matrix composite with multiple machined holes were subjected to a furnace dwell and then tensile tested. The furnace temperature range was 500–900°C, and the atmosphere was pure steam to approximate the temperature and sea level partial pressure of water vapor in the cooling air going through turbomachinery cooling holes. Exposure of control specimens was done in laboratory air at the same temperatures. Tensile results along with microscopy and spectroscopy showed significant strength degradation in some conditions due primarily to oxidation of the boron nitride fiber coating, with coating volatilization at lower temperatures and probable fiber‐to‐matrix bonding and imposed fiber stresses at higher temperatures. The greatest strength degradation occurred in the 500–600°C steam range. The fiber coating oxidation/volatilization was especially evident near the holes and was exacerbated in the lower temperature tests by porosity networks that were open to the atmosphere at fiber tow ends at the specimen edges and along the inner walls of the holes.

Funder

Air Force Research Laboratory

Publisher

Wiley

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