AIRCRAFT INTAKE DUCT

An aircraft intake duct for channeling a flow of ambient air toward an annular engine compressor inlet of a gas turbine engine having a compressor reference axis and a reference plane that extends from such compressor reference axis. The aircraft intake duct includes an oblong air intake inlet for r...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: CUNNINGHAM, MARK HUZZARD, YAN, GUO RONG
Format: Patent
Sprache:eng ; fre
Schlagworte:
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