SINGULAR STATOR VANE CONTROL

Systems and methods for controlling stators of a compressor of a gas turbine engine are provided. The stators and rotatable blades may be included in a stage of the compressor. The rotatable blades may be configured to rotate about an axial axis of the compressor, and each of the stators is rotatabl...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser: Skertic, Richard J
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
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