Booster compressor deicer

The present invention relates generally to gas turbine engines, and, more specifically, to deicing therein. A booster compressor includes inlet guide vanes supported from a shroud. A shell surrounds the shroud and defines a manifold. A splitter nose includes a groove receiving a forward tang of the...

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Bibliographische Detailangaben

Hauptverfasser:	Wadia, Aspi Rustom, Seitzer, Kenneth Edward, Hura, Harjit Singh, Worthoff, Frank, Holm, Raymond Gust, Masse, Eric Pierre, Slagle, Jason Corey
Format:	Patent
Sprache:	eng
Online-Zugang:	Volltext bestellen
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