Engine bypass valve

Aspects of the disclosure are directed to an engine of an aircraft. The engine may include a first fan configured to output a first air flow, a second fan configured to receive a first portion of the first air flow and output a second air flow, a core configured to receive a first portion of the sec...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Hanlon, Christopher J, Kupratis, Daniel B, Ledwith, Jr., Walter A
Format: Patent
Sprache:eng
Schlagworte:
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