STATIC HUB TRANSITION DUCT

An engine includes a compressor having a first compressor, a second compressor, and a static hub transition duct. The first compressor includes a rotatable portion and a static portion. The second compressor is disposed downstream of the first compressor and includes an inlet and a rotatable portion...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Acker, Jonathan P, Cooper, Nate J, Whitlock, Mark, Mazur, Steven
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
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