DOE OSTI · 1390240
Hot gas path component
Abstract
Various embodiments of the disclosure include a turbomachine component. and methods of forming such a component. Some embodiments include a turbomachine component including: a first portion including at least one of a stainless steel or an alloy steel; and a second portion joined with the first portion, the second portion including a nickel alloy including an arced cooling feature extending therethrough, the second portion having a thermal expansion coefficient substantially similar to a thermal expansion coefficient of the first portion, wherein the arced cooling feature is located within the second portion to direct a portion of a coolant to a leakage area of the turbomachine component.
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Lacy, Benjamin Paul, Kottilingam, Srikanth Chandrudu, Porter, Christopher Donald, Schick, David Edward. 2017-09-12. Hot gas path component. https://www.osti.gov/biblio/1390240
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