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NASA NTRS · 20010061357

Internally Cooled Monolithic Silicon Nitride Aerospace Components

Abstract

A set of rapid prototyping (RP) processes have been combined with gelcasting to make ceramic aerospace components that contain internal cooling geometry. A mold and core combination is made using a MM6Pro (Sanders Prototyping, Inc.) and SLA-250/40 (3Dsystems, Inc.). The MM6Pro produces cores from ProtoBuild (trademarked) wax that are dissolved in room temperature ethanol following gelcasting. The SLA-250/40 yields epoxy/acrylate reusable molds. Parts produced by this method include two types of specimens containing a high density of thin long cooling channels, thin-walled cylinders and plates, as well as a model hollow airfoil shape that can be used for burner rig evaluation of coatings. Both uncoated and mullite-coated hollow airfoils has been tested in a Mach 0.3 burner rig with cooling air demonstrating internal cooling and confirming the effectiveness of mullite coatings.

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BibTeXRIS

Best, Jonathan E., Cawley, James D., Bhatt, Ramakrishna T., Fox, Dennis S., Lang, Jerry. 2000-01-01. Internally Cooled Monolithic Silicon Nitride Aerospace Components. https://ntrs.nasa.gov/citations/20010061357

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