The Versatility of HVOF Burner Rig Testing for Ceramic Matrix Composite Evaluation

Author:

Morscher Gregory N.,Panakarajupally Ragav P.,Hoffman Leland

Abstract

Effective testing of ceramic matrix composites (CMCs) and CMC/coating systems for high temperature, high stress, high velocity and/or severe oxidation/corrosion environments is a critical need in materials/coatings evaluation for extreme environments of hot section parts in jet engine and hypersonic applications. Most current technology can evaluate two or three of the extreme conditions for a given application; however, incorporating as many of the extreme thermo-mechanical-environmental factors is highly advantageous to understand combinatorial effects. A high velocity oxygen fuel (HVOF) burner rig offers an excellent platform to evaluate many of these extreme conditions. In this work, the following three different thermo-mechanical-environmental test conditions using an HVOF rig on SiC-based CMCs are highlighted: (1) fatigue at temperature for >Mach 1 velocity and high temperature compared to typical stagnant air test environment, (2) high temperature hard particle erosion at temperature for ≤Mach 1 conditions and (3) ~Mach 5 near-hypersonic velocity conditions at very high temperature exposure.

Funder

Office of Naval Research Global

Naval Air Systems Command

Publisher

MDPI AG

Subject

General Medicine

Reference38 articles.

1. Ceramic Matrix Composites Taking Flight at GE Aviation;Steibel;Am. Ceram. Soc. Bull.,2019

2. Simultaneous Fatigue and Combustion Exposure of a SiC/SiC Ceramic Matrix Composite

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