Method and apparatus to facilitate reducing losses in turbine engines

A method for assembling a compressor for use with a turbine is provided. The method includes coupling at least a first stator ring to a second stator ring via at least one fastener sized to extend through at least one stator ring opening. The method further includes coupling a shield assembly to at...

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Bibliographische Detailangaben

Hauptverfasser:	Ring, Matthew Joseph, Rulli, Samuel, Kirk, Cory, Liu, Hsin-Tuan, Karafillis, Apostolos
Format:	Patent
Sprache:	eng
Online-Zugang:	Volltext bestellen
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