FENCE FOR DUCT TONE MITIGATION

Aspects of the disclosure are directed to a system (200) associated with an engine (10) of an aircraft comprising a duct (218), an inlet (234) coupled to the duct (218), and a fence (252) coupled to the inlet (234) or located upstream of the inlet (234). In some embodiments, the system further compr...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	DE LA RIVA, Diego H, ZYSMAN, Steven H, POST, Keith A, KOUSHIK, Sudarshan N, ZSURKA, MARK, SHANNON, Daniel W
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	Aspects of the disclosure are directed to a system (200) associated with an engine (10) of an aircraft comprising a duct (218), an inlet (234) coupled to the duct (218), and a fence (252) coupled to the inlet (234) or located upstream of the inlet (234). In some embodiments, the system further comprises a valve body (226) coupled to the duct (218). In some embodiments, the valve body (226) includes at least one valve (230) that is configured to rotate between a closed state and an open state.