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NASA NTRS · 20150003215

Reverse Flow Engine Core Having a Ducted Fan with Integrated Secondary Flow Blades

Abstract

Secondary air flow is provided for a ducted fan having a reverse flow turbine engine core driving a fan blisk. The fan blisk incorporates a set of thrust fan blades extending from an outer hub and a set of integral secondary flow blades extending intermediate an inner hub and the outer hub. A nacelle provides an outer flow duct for the thrust fan blades and a secondary flow duct carries flow from the integral secondary flow blades as cooling air for components of the reverse flow turbine engine.

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BibTeXRIS

Kisska, Michael K., Princen, Norman H., Kuehn, Mark S., Cosentino, Gary B.. 2014-03-11. Reverse Flow Engine Core Having a Ducted Fan with Integrated Secondary Flow Blades. https://ntrs.nasa.gov/citations/20150003215

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