Pilot relief to reduce strut effects at pilot interface

A turbine section of an engine that includes a shaft, a plurality of blades extending radially relative to the shaft, a bearing assembly, a flowpath housing, and a shroud is provided. The bearing assembly is mounted to the shaft adjacent to the plurality of blades. The flowpath housing is coupled to...

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Bibliographische Detailangaben

Hauptverfasser:	Barrett, John R, Garcia, Alonso J, Kime, Robert A
Format:	Patent
Sprache:	eng
Online-Zugang:	Volltext bestellen
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